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airborne equipment of satellite navigation user`s manual

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1. Flight from TP2 Figure J 1 10 Scheme of the flight in DIRECT TO mode with TP2 being in turn 034 50 00 Appendix J page 15 Dec 17 2009 CH 4312 02 USER S MANUAL Diagrammatic representation of the flight in OFFSET mode is shown in figures J 1 11 J 1 13 Way gt Lisp ALPHA Ice ent P ES 37 7 7 OFFSET ON BRAVO x a E Turn 45 z aralle gt Le N yer a 7 Sie Sblace gt DELTA p gt Mens Le N 7 lt lt VY AT N S SET ae SN 7 i EGNOS Flight plan Flight with displacement Flight with displacement after overflight of final WPT Figure J 1 11 Scheme of flight on a displaced flight plan OFFSET OFF N Turn 45 BRAVO N DELTA Flight plan Flight and cancellation of the flight with displacement EGHOS Figure J 1 12 Scheme of cancellation of the flight according to displaced flight plan 034 50 00 Appendix J page 16 Dec 17 2009 CH 4312 02 USER S MANUAL gt AIr Se Me dis le ALPHA Fi gt S y Sht plan gt Flight plan Flight and cancellation of flight with displacement ALPHA gt Flight plan Flight and cancellation of flight with displacement Figure J 1 13 Scheme of cancellation of flight according to displaced flight plan when executing a turn for angle more than 130 034 50 00 Appendix J page 17 Dec 17 2009 CH 4312 02
2. Creation of user WP is accomplished by input of identifier of a new user WP and by setting coordinates of user WP being created bearing and distance from basic NP bearings from two basic NP Notes 1 Input identifier of forming user point should not contain spaces on the first character cell and in the middle of identifier 2 If after input of identifier of user WP being created right lower angle of WPT10 page displays the message Modify then user WP with such identifier exists and it can be edited used then user WP with such identifier is the waypoint created in pages of FPL form and it cannot be edited Creation of user WP by setting coordinates To create user WP by setting coordinates a set highlight in the field of display of NP identifier b input identifier of user WP being created c press ENT button to confirm input of identifier Highlight will move to the field of identifier of basic NP Request about creation of user WP Create will appear in right lower angle figure J 6 40 9005 0995 Create Figure J 6 40 d set highlight to the coordinates field by pressing ENT or by rotating external knob clockwise 034 50 00 Appendix J page 134 Dec 17 2009 CH 4312 02 USER S MANUAL e set the required value of coordinates f press ENT to confirm input of coordinates Highlight will move to the field of NP name g input name of NP and region if necessary h set highlight to Crea
3. NAV3 page NAV3 page is used for graphic display of a flight plan View of NAV3 page is shown in figure J 2 10 1 Pointer of direction to north 2 Graphic display of a flight plan oriented by direction to north 3 Scale of flight plan display 4 Graphic display of a flight plan oriented by course angle Figure J 2 10 034 50 00 Appendix J page 50 Dec 17 2009 CH 4312 02 USER S MANUAL Activation deactivation of display of navigation references and or air zones Activation deactivation of display of navigation references and or air zones is effected by analogy with those stated in NAVI page Operations being accomplished on the page NAV3 by the button MENU On NAV3 page by pressing MENU button PAGE MENU pop up window is displayed figure J 2 11 its fields are used to accomplish the following operations setup of route orientation to north True Nord field setup of route orientation by course angle DTK field activation of automatic zoom Autozoom field flight plan overview View Route field Figure J 2 11 Setup of route orientation To setup route orientation a set the highlighting in PAGE MENU pop up window figure J 2 11 to True Nord if it is required to get graphic display of a flight plan oriented to north on RICU DTK if it is required to get graphic display of a flight plan oriented by course angle on RICU 6 press ENT 034 50 00 Appendix J page 51 Dec 17 2009
4. b press ENT Selection page of WPTS procedure will appear on RICU display Identifier of final WP is displayed in the field of WP identifier if final WP is an airport figure J 3 24 If final WP is not an airport or an arrival airport set arrival airport in the field of airport identifier Figure J 3 24 034 50 00 Appendix J page 77 Dec 17 2009 CH 4312 02 USER S MANUAL c set highlight to the field of ARRIVAL procedure name d turn internal knob one position further ARRIVAL pop up window is displayed on the WPTS page Set highlight to name of required procedure figure J 3 25 Figure J 3 25 e press ENT Name of selected procedure is displayed in ARRIVAL field If selected procedure has only one transit point and one RW then highlight will at once move to the field Load after selection of procedure figure J 3 26 If selected procedure has several transit points then highlight will move to TRANS field Select a required transit point and press ENT If there are several RW for selected procedure then highlight will move to RUNWAY field Select a required RW and press ENT button Selection of a transit point and RW is accomplished by analogy with selection procedure name Highlight will move to the field Load figure J 3 26 Figure J 3 26 034 50 00 Appendix J page 78 Dec 17 2009 CH 4312 02 USER S MANUAL f press ENT FPL1 page in which points of selected ARRIVAL procedure are included in a
5. Figure J 3 1 shows factory setting of parameters displayed interchangeable fields List of parameters which can be displayed n interchangeable fields 8 10 is shown in table J 3 1 List of possible reference designations of WP is shown in table J 3 2 Table J 3 1 Designation in the form Parameter Interchangeable field Total distance to flight destination point pos 8 10 CUM on desired track DIS Length of flight plan leg along DT pos 8 10 DTK Desired track angle pos 8 10 ETA Time of arrival to WP pos 8 10 ETE Flight time left to reach WP pos 8 10 ESA Safe flight altitude in a flight plan pos 8 ARP Airport identification code 1103 8 10 034 50 00 Appendix J page 63 Dec 17 2009 CH 4312 02 USER S MANUAL Table J 3 2 Reference designation of Parameter Description WP a ABSENT Point was not found during check of flight plan points b BAD Error is registered for a point for example point coordinates failed to be loaded D Mode DIRECT TO is set for a point J Target point of a left arc R Turn Target point of a right arc C Target point of step CF CourseFix B Point of report about passing NE Control point of initial stage of approach M Point of moving to a second circle F FAF Control point of final stage of approach O Visited point ale Point of waiting zone start LS Point of exit from waiting zone C Point of course fixation M Last point of a flight pl
6. Note at DME device tuning in CTRL control mode for tuning the beacon shall be selected whose frequency is set in the top line ifin MODE field one beacon of TEST CTRL mode is set for two other beacons the same mode shall be set DATA VOR DME field DATA VOR DME field is used to activate Data VOR DME window intended to display distance to beacon for beacons DME or bearing for beacons VOR received from airborne systems of distance and bearing determination To activate Data VOR DME window set highlight to the field DATA VOR DME figure J 8 5 and press ENT To return to AUX2 page press CLR button View of Data VOR DME window is shown in figure J 8 20 034 50 00 Appendix J page 165 Dec 17 2009 CH 4312 02 USER S MANUAL 1 Information about the first beacon DME line DME 1 reference designation identifier frequency MHz distance to the beacon VOR 2 Information about the second beacon DME 2 line similar to pos 1 3 Information about the beacon VOR VOR DME line reference designation identifier frequency MHz bearing to the beacon 4 Coordinates received using DME beacons DME DME line 5 Coordinates received using VOR beacons VOR DME line 6 8 Positional accuracy 7 9 Time after navigation decision receiving seconds Figure J 8 20 DATA GNSS field DATA GNSS field is used to activate DATA GNSS window intended for display of main operation parameters of GNSS receiver
7. To activate DATA GNSS window set highlight to DATA GNSS field figure J 8 5 and press ENT To return to AUX2 page press CLR button View of DATA GNSS window is shown in figure J 8 21 034 50 00 Appendix J page 166 Dec 17 2009 CH 4312 02 USER S MANUAL 1 Current coordinates 2 Time 3 Date 4 7 Interchangeable fields 8 Sign of receipt of initial coordinates of NP coordinates received from the receiver GNSS Restore restored coordinates received before the last shutdown of RICU ID identifier of WP coordinates selected from NDB Manual manual input of coordinates CROSS BPIU coordinates received from other RICU coordinates are not defined 9 Graphic display of visible SV situated above the horizon almanac red SNS GLONASS blue SNS GPS green Satellite Based Augmentation System SBAS 10 Signal noise ratio on each channel Note 24 column pos 10 correspond to 24 channel of the receiver GNSS Each column shows S N ratio in graphic and digital view of SV which number is stated under the column figures of red colour SNS GLONASS blue SNS GPS Signal noise correlation is shown only for those satellites which are involved into NT solution Figure J 8 21 The figure J 8 21 shows factory setting of parameters displayed in interchangeable fields List of parameters which can be displayed in interchangeable fields pos 4 7 is shown in table J 8 1 034 50 00 Appendi
8. window of selection of type of control voltage figure J 8 64 Figure J 8 64 034 50 00 Appendix J page 205 Dec 17 2009 CH 4312 02 USER S MANUAL d set highlight to the field with required type of control voltage Note Type of control voltage is defined by scheme of equipment connection on a definite AC e press ENT to confirm a selected type of control voltage Setting of highlight brightness of keyboard To set highlight brightness of keyboard a set highlight to the field of setting mode of highlight brightness of keyboard figure J 8 57 b turn internal knob one position further BRIGHTNESS window displays pop up window of selection of setting mode of highlight brightness MODE figure J 8 58 Factory setting of highlight brightness of keyboard For factory setting of highlight brightness of keyboard a set highlight to Default field figure J 8 58 b press ENT to confirm factory setting of highlight brightness of keyboard Manual setting of highlight brightness of keyboard For manual setting of highlight brightness of keyboard a set highlight to Manual field figure J 8 58 b press ENT RICU display shows information in accordance with figure J 8 65 034 50 00 Appendix J page 206 Dec 17 2009 CH 4312 02 USER S MANUAL DISPLAY KEYBOARD 1 Manual setting of highlight brightness of keyboard 2 Background light 3 Signal light Figure J 8 65 c set highlight to SIGNAL field d by
9. 5 Setting of map parameters 6 Transfer of user database user NP routes to other RICU field is accessible for work only if there is connection with other RICU Figure J 8 40 034 50 00 Appendix J page 188 Dec 17 2009 CH 4312 02 USER S MANUAL SETTINGS field SETTINGS field is used to activate SETTING window intended to set system parameters To activate SETTING window set highlight to SETTINGS field and press ENT To return to AUX3 page press CLR button View of SETTING page is shown in figure J 8 41 1 System of units 2 Operation mode of equipment 3 System of coordinates 4 Scale of deviation from DT CDD sign of automatic or manual setting of scale 5 Threshold of integrity signalling sign of automatic or manual setting of limit of integrity signalling 6 Activation deactivation of magnetic declination registration 7 Activation deactivation of satellites GPS from navigation parameters calculation 8 Activation deactivation of satellites GLON from navigation parameters calculation 9 Language of messages Figure J 8 41 034 50 00 Appendix J page 189 Dec 17 2009 CH 4312 02 USER S MANUAL Setting of system of units To set system of units a set highlight to the field of display of units field UNITS figure J 8 41 b turn internal knob one position further SETTING window displays pop up window of selection of system of units SETTING UNIT figure J 8 42 Figure J 8 42 c set highlight to the
10. DTK flight plan orientation by course angle Graphics View SATs graphic display of satellites position Invert Flight Plan flight plan inversion Reference WP selection of original coordinates from NDB Remove Approach removal of procedure Approach from flight plan Remove Arrival removal of procedure STAR from flight plan Remove Departure removal of procedure SID from flight plan Restore Defaults setup of interchangeable fields according to factory default Retarget To Point retarget to WP SCALE activation of scale mode Select Approach selection and insertion of procedure Approach to flight plan Select Arrival selection and insertion of procedure STAR to flight plan Select Departure selection and insertion of procedure SID to flight plan Select Navaid navaid selection Sort List By Number flight plan sorting by numbers Sort List By Comment or by alphabet Set Info for Navaid beacon selection the distance to which should be displayed in DME indicator 034 50 00 Abbreviation list page 3 Dec 17 2009 CH 4312 02 USER S MANUAL Text View SATs text view of satellites position True North setting of flight orientation to north View Route route view View User Waypoint List user waypoints list view Parameters displayed on interchangeable fields Along Track Distance ATD distance to TP on DT Socr Altitude ALT altitude Bearing BRG bearing to target point Cro
11. Remove Departure Closest Point of FPL Change Fields Restore Defaults Flight setting in DIRECT TO mode G Figure J 1 15 page 1 of 2 034 50 00 Appendix J page 21 Dec 17 2009 CH 4312 02 USER S MANUAL FPL 2 Flight Plan Catalog page Display of flight plan directory numbers and names of flight plans Flight plan removal from flight plan directory Activate Flight Plan Invert Flight Plan Create New Flight Plan Copy Flight Plan Delete Flight Plan Delete All Flight Plan Sort List By Number Sort List By Comment WPT selection Inclusion of a new WPT to flight plan 5 WPT removal from an TE active flight plan Activate Flight Plan ae Invert Flight Plan Delete Flight Plan Change Fields Restore Defaults Flight setting in DIRECT TO mode Figure J 1 15 page 2 of 2 034 50 00 Appendix J page 22 Dec 17 2009 CH 4312 02 USER S MANUAL Logical tree of gt form form Display Target point information Target point transit angle CRS TP selection Input of set transit angle Flight setting in Flight setting in DIRECT TO mode DIRECT TO mode Second target point enqueing Cancellation of the flight in DIRECT TO mode to set TP and flight setting in DIRECT TO mode to another TP Cancellation of the flight in DIRECT TO mode Figure J 1 16 034 50 00 Appendix J page 23 Dec 17 2
12. USER S MANUAL Logical tree of apparatus forms Logical tree of access to pages and windows of each form and functions being accomplished on pages and windows of a form are shown in figures J 1 14 J 1 21 Note Active handle is marked in black Logical tree of NAV form NAV form NAVI page Display navigation parameters in interchangeable fields ATD BRG DIS DTK CUM ETA ETE GS TKE TRK XTK scale of deviation from DT graphic representation of flight plan active flight plan leg Autozoom Change Fields Restore Defaults on off display of navigation references and or air zone Flight in DIRECT TO mode NAV2 page e Display flight stage and flight plan name scale of deviation from DT active flight plan leg main navigation parameters in interchangeable fields current coordinates date and time Change Fields Restore Defaults gt Flight setting in DIRECT TO ee Figure J 1 14 page 1 of 3 034 50 00 Appendix J page 18 Dec 17 2009 CH 4312 02 USER S MANUAL NAV3 page Display of graph based flight plan oriented by direction to north or by track angle on off display of navigation references and or air zone True Nord DTK Autozoom View Route NAV4 page Display flight stage airport identifier information about airport radiocommunication equipment Airport identifier selection to overview information
13. f press ENT TRANS field displays the name of selected transit point highlight will remain in TRANS field Graphic representation of selected procedure APPROACH is displayed on WPT6 page in the field of graphic representation of procedure g press CRSR button Highlight will disappear from the fields of WPT6 page figure J 6 34 034 50 00 Appendix J page 126 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 34 Zoom of graphic display of APPROACH procedure Zoom of graphic display of STAR procedure is accomplished by analogy with zoom graphic display of SID procedure see description of WPT4 page WPT7 page WPT7 page is used for oveview of information about NP of flight plan intersection point category Intersection View of WPT7 page is shown in figure J 6 35 034 50 00 Appendix J page 127 Dec 17 2009 CH 4312 02 USER S MANUAL 1 Identifier of flight plan intersection point Intersection 2 Reference designation of flight plan intersection point 3 Name of flight plan intersection point 4 Region of the country where flight plan intersection point is located 5 Region of earth where flight plan intersection point is located 6 Latitude longitude of flight plan intersection point 7 Symbol of current position of AC 8 Bearing to flight plan intersection point from current position 9 Distance to flight plan intersection point from current position Figure J 6 35 Overview of information about flight plan
14. flight plan identifiers of four nearest airports are displayed 034 50 00 Appendix J page 56 Dec 17 2009 Figure J 2 13 CH 4312 02 USER S MANUAL c set highlight to identifier of airport which information about radiocommunication equipment it is necessary to overview d press ENT e information about radiocommunication equipment of selected airport is displayed on NAV4 page NAVS page NAVS page is intended for selection of landing airport and RW of landing airport to review values of deviation from RW center line distance to RW threshold bearing to RW threshold and distance to RW threshold from the current position of aircraft and also for display of information about selected RW of landing airport View of NAVS page is shown in figure J 2 14 1 Landing airport 2 RW of landing 3 Pointer of direction to north 4 Graphic display of selected RW of landing airport 5 Scale 6 Command of landing airport and RW selection 7 Deviation orthodromic of AC from RW center line to the right to the left 8 Distance orthodromic to RW threshold flight to RW flight from RW 9 Bearing to RW threshold from the current position of aircraft 10 Distance to RW threshold from the current position of aircraft Note If parameter value pos 7 8 is less than I km parameter value is indicated in meters irrespective of required measurement system metric or English Resolution of parameter i
15. page 82 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 3 34 c press ENT to confirm the deletion of the procedure to refuse deletion press CLR button or set highlight to the field NO and press ENT If approach procedure was included in the flight plan then it will be deleted from the flight plan Identifier of WP which has ARRIVAL procedure deleted is displayed in the field of flight plan name in the place of identifier of final WP Deletion of DEPARTURE procedure from a flight plan To delete departure procedure from a flight plan a set highlight to Remove Departure field in PAGE MENU pop up window figure J 3 11 b press ENT Pop up window with the request to delete departure procedure is displayed on RICU display figure J 3 35 Figure J 3 35 034 50 00 Appendix J page 83 Dec 17 2009 CH 4312 02 USER S MANUAL c press ENT to confirm the deletion of the procedure to refuse deletion press CLR button or set highlight to the field NO and press ENT Identifier of WP which has DEPARTURE procedure deleted is displayed in the field of flight plan name in the place of identifier of initial WP Setup of interchangeable fields To setup interchangeable fields a set highlight to field Change Fields in PAGE MENU pop up window figure J 3 11 b press ENT PAGE MENU window will stop being displayed on FPL1 page and mnemonic symbol of one of the interchangeable fields will be highlighted c set highli
16. 034 50 00 Abbreviation list page 5 6 Dec 17 2009 CH 4312 02 USER S MANUAL AIRBORNE EQUIPMENT OF SATELLITE NAVIGATION APPENDIX J mandatory Operator guide Part 2 of user s manual TJJIK 461513 077 02 P91 for satellite navigation airborne equipment TJHK 461513 077 02 code CH 4312 02 hereinafter referred to as equipment defines work order with equipment and is intended for the aircraft crew members Only persons who studied user s manual TAUK 461513 077 02 P93 THWK 461513 077 02 P91 and equipment operating rules are admitted to operate the equipment 034 50 00 Appendix J page Dec 17 2009 CH 4312 02 USER S MANUAL J 1 General information Control elements External view of front panel and equipment controls layout are shown in figure J 1 1 1 3 a J Ny RS Is Oy WITT 1 Navigation database storage removable unit 2 On Off button 3 Display 4 6 Control buttons 5 Photo resistor adjusting display brightness 7 External rotary knob of handle 8 Internal rotary knob of handle When pressing internal knob end the function CRSR is being accomplished Figure J 1 1 RICU ON OFF button ON OFF button identification ON OFF for RICU before serial Ne 03908020 inclusive D for RICU since serial Ne 03910021 Note Hereinafter in the text ON OFF button is indicated for RICU turning on off All ON OFF button operations refer also to button NRST Button Button NRST is
17. 1 Date of determination of function RAIM accessibility forecast 2 Latitude of WP for which function RAIM accessibility forecast was calculated 3 Longitude of WP for which function RAIM accessibility forecast was calculated 4 5 Period of time range from to in which RAIM forecast is not available Figure J 8 38 034 50 00 Appendix J page 185 Dec 17 2009 CH 4312 02 USER S MANUAL SUNRISE field SUNRISE field is used to activate SUNRISE window intended for sunrise and sunset time calculation To activate SUNRISE window set highlight to the SUNRISE field and press ENT To return to AUX2 page press CLR button View of SUNRISE window is shown in figure J 8 39 1 Coordinates of NP 2 Identifier of NP 3 Date 4 Adjustment of zone time in case of zero correction time according to Greenwich 5 Command of sunrise and sunset time calculation execution 6 Sunrise time taking into account input adjustment of zone time 7 Sunset time taking into account input adjustment of zone time Figure J 8 39 034 50 00 Appendix J page 186 Dec 17 2009 CH 4312 02 USER S MANUAL Sunrise and sunset time calculation Coordinates of current NP are displayed in opened window SUNRISE in POSITION field and current data in the field DATE To accomplish sunrise and sunset time calculation for given NP a select NP for which calculation must be accomplished b set required calculation date c set zone time adjustmen
18. 17 2009 CH 4312 02 USER S MANUAL Check external knob by rotating it clockwise counter clockwise In the field of Encoder A parameter RICU display shows values from 0 to 63 from 63 to 0 in turn starting from the value which was displayed before rotating When rotating external knob the field of gt lt symbol over CR field will be highlighted on RICU display Accomplish check of internal knob Check is accomplished by analogy with external knob check SOFTWARE VERSION field SOFTWARE VERSION field is used to activate the window SOFTWARE VERSION window intended to control software versions To activate the SOFTWARE VERSION window set highlight to SOFTWARE VERSION field figure J 8 79 and press ENT button To return to AUX4 page press CLR button View of SOFTWARE VERSION window is shown in figure J 8 86 1 Version of SW of RICU central calculator 2 Version of SW of peripheral control unit 2 Version of SW of GNSS receiver Figure J 8 86 034 50 00 Appendix J page 227 Dec 17 2009 CH 4312 02 USER S MANUAL J 9 Operation description in PROC form The PROC form is used to select and involve APPROACH ARRIVAL DEPARTURE standard procedures in a flight plan Entry in PROC form is accomplished by pressing PROC button on the front panel of RICU By repeated pressing PROC button RICU display shows the form which was displayed on RICU prior to activation of PROC form View of PROC form is shown in figure
19. 3 Field of airport RW name 4 Request for detailed airport overview Figure J 6 2 034 50 00 Appendix J page 108 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 3 Overview of RW airport information For RW airport information overview perform the following operations a set highlight to the field of airport identifier input identifier of airport which RW information it is required to overview b press ENT Highlight will move to the field of RW name figure J 6 4 Detailed Figure J 6 4 c turn internal knob one position further RUNWAY pop up window is displayed on WPT2 page figure J 6 5 034 50 00 Appendix J page 109 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 5 d set highlight to name of RW which information it is necessary to overview e press ENT Highlight will move to the field of enquiry for detailed overview of information about selected RW of airport Detailed f press ENT RICU display shows RUNWAY DETAILED window which represent information about selected RW figure J 6 6 g press CLR button to return from RUNWAY DETAILED window to WPT2 page 034 50 00 Appendix J page 110 Dec 17 2009 CH 4312 02 USER S MANUAL Description of RUNWAY DETAILED window RUNWAY DETAILED window is used for overview of detailed information about selected RW of an airport 1 Airport identifier 2 Identifier of selected RW 3 Latitude longitude of RW end degrees minut
20. 34 034 50 00 Appendix J page 181 Dec 17 2009 CH 4312 02 USER S MANUAL c set highlight to the field with number of satellite which must be included excluded from calculation By rotating internal knob set USE to include OFF to exclude satellite from calculation d press ENT to confirm inclusion exclusion of satellites from calculation Setup of command of function RAIM accessibility forecast calculation accomplishment for a selected NP HT To setup a command of function RAIM accessibility forecast calculation accomplishment for a selected NP a set highlight to the field CALC opposite the field WP b press ENT display will show results of function RAIM accessibility forecast calculation in graphic view figure J 8 35 CALC CALC TEXT gt 0h 3h 6h 49h 12h SETS gt Figure J 8 35 Forecast results Red colour on diagram means that RAIM forecast is not available blue colour RAIM forecast is available Appearance of the message about error CALC ERROR 2 on RICU display means that GNSS sensor doesn t respond to requests repeat the forecast calculation of RAIM function availability 034 50 00 Appendix J page 182 Dec 17 2009 CH 4312 02 USER S MANUAL Function RAIM accessibility forecast calculation for active flight plan Function RAIM accessibility determination for active flight plan is provided within length of the flight plan from specified start time of movement according
21. 5 1 SELECT OBS COURSE 1 Angle of flyover of a target point 2 Identifier of a target point 3 Desired track angle Figure J 5 1 Setting a flight in OBS mode For efficient movement to WP with set angle of flyover a input value of an angle of flyover of target point b press ENT After pressing ENT flight under the flight plan is cancelled new DT is formed which passes a target point with set angle of flyover of target point RICU display shows NAV1 page View of NAVI page after setting OBS mode is shown in figure J 5 2 034 50 00 Appendix J page 104 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 5 2 When accomplishing a flight in OBS mode highlight of OBS button blinks After passing of a target point AC continues a flight along DT which passes through WP with desired track angle Immovable symbol of AC A located in the middle of DT scale after passing a target point looks like Cancellation of a flight in OBS mode To cancel a flight of AC along desired track angle press OBS button After pressing OBS button OBS button highlight goes down and equipment provides moving of AC along LLT to nearest flight plan leg if OBS mode was set for flight plan leg flight in DIRECT TO mode to a target point if OBS mode was set during flight execution in DIRECT TO mode Cancellation of a flight of AC OBS mode also occurs when anew flight plan is activated a flight plan leg is
22. CH 4312 02 USER S MANUAL Activation of automatic zoom Activation of automatic zoom is effected by analogy with activation of automatic zoom described in NAVI page Flight plan overview To view a flight plan a set the highlighting to View Route field in PAGE MENU pop up window figure J 2 11 b press ENT Symbol will appear in the centre of display this symbol indicates flight plan overview c flight plan overview is accomplished by rotating internal and external knob of the handle Graphic display of a flight plan is moved vertically by rotating internal knob Graphic display of a flight plan is moved horizontally by rotating external knob To zoom image use RNG RNG buttons 034 50 00 Appendix J page 52 Dec 17 2009 CH 4312 02 USER S MANUAL NAV4 page NAV4 page is intended to display information about operating frequences of airport communication equipment Overview of NAV4 page is shown in figure J 2 12 DEPARTURE JA 1 Flight stage symbols DEPARTURE departure ENROUTE route ARRIVAL arrival 2 Identifier of airport concerned with communication equipment 3 List of radio communication equipment of an airport 4 Service indicator 5 Operating mode of radiocommunication equipment rx receiver tx transmitter not defined in database 6 Frequency Figure J 2 12 List of radiocommunication equipment which an airport can have is stated in table J 2 2 Val
23. J 6 51 d If user NP with selected for deletion is used at least in one of the flight plans created on the pages of FPL form DELETE WAYPOINT window containing the message stating that selected navigation point can not be deleted will appear in UDB_list window figure J 6 52 Press ENT to refuse deletion Selected NP will not be deleted from user NP list 034 50 00 Appendix J page 143 Dec 17 2009 CH 4312 02 USER S MANUAL Figure 6 52 Renaming of user NP To rename user NP a set highlight to identifier of NP which must be renamed figure 6 49 b input a new identifier of NP Press ENT c if there is no user point with identifier which was input as new one in user NP list RENAME WAYPOINT pop up window with identifier of NP which must be renamed will appear in UDB_list window figure J 6 53 Press ENT when YES field is highlighted User NP will be renamed and will take its place in the list according to alphabet Figure J 6 53 034 50 00 Appendix J page 144 Dec 17 2009 CH 4312 02 USER S MANUAL d if user NP with identifier which was input as new one already exists in user NP list renaming will not be accomplished UDB_list window will display Waypoint exists FIND pop up window figure J 6 54 offering to find existing user NP with identifier which was input as new one By pressing ENT when the field YES is highlighted Yes identifier of NP already existing will be highlighted No identifie
24. J 6 Operation description in WP form soesssesssesssocssoossooessoesssesssoossoossoosssosssoesssocssoossoossssssssee 106 MP ACS anne ns nn a a A ne Nr aa 106 WPT2 page inner int laicee 108 WPT3 page es an nn en ro cts E di menant us Ne 112 NP PARENTS en en BC a a Ne ne 114 WPIS page cee AN EC AR RE Re RS SR ARR EA 120 WW PUG ASS an Re ER EE a an es Sn an Rte tasSee 124 WPTV pas ain anis MGR RG NN IR 127 PES PARENT ss 129 MAP AO DABE et LS en E a GR hah nr Saal a thes lace thle Stent 131 WPTIO DAS arsenal as dre ten Te desea doce 133 J 7 Operation description in NRST form sseeesooesooessossssesssesssoossoossoossssesssesssoossoosssssssossssesesosse 147 NRSTI ae ES En a acca Sata eet ne an ek ea ah de Ne Msn nn 148 NRS TAPANT Ne Te nn te On LR nn ce 149 NRST3 pafen te en ne ce 150 NRS TA page sen EN Re Ne aap ed A nade 151 034 50 00 Contents page 1 Dec 17 2009 CH 4312 02 USER S MANUAL J 8 Operation description in AUX form ssseeeeesssssessssssssssosee 152 AUXI Pa Pe initio acess unin can a a a a an aa a e a a iaa 152 PTD chica csc a E rec E en cna EE EE 155 AUXI eh ts es AS Fala es Set a Sa nl lat ed St Pale asta Sala tla Dd Sa A 188 PUA DAS en rase be deta at awe sl ar arrete 219 J 9 Operation description in PROC form sesssesssesssesssoossoossoosssoesssesesoossoossoossssesssesssosssoossosssose 228 J 10 Messages generated by equipment sseeesooesoossssesssesssecssooesoosessesssesssoessoossoosss
25. J 9 1 1 Selection of standard procedure of approach APPROACH 2 Selection of standard procedure of arrival ARRIVAL 3 Selection of standard procedure of departure DEPARTURE 4 Information about selected APPROACH procedure 5 Information about selected ARRIVAL procedure 6 Information about selected DEPARTURE procedure Figure J 9 1 034 50 00 Appendix J page 228 Dec 17 2009 CH 4312 02 USER S MANUAL Selection of standard procedure of approach APPROACH Selection of standard procedure of approach APPROACH is accomplished by analogy with given one in description of FPL1 page After selection of APPROACH procedure information about selected procedure name of transit point and name of APPROACH procedure is displayed in APR field procedure is involved in active flight plan and RICU displays the page of active flight plan of FPJ form Selection of standard procedure of arrival ARRIVAL Selection of standard procedure of arrival ARRIVAL is accomplished by analogy with given one in description of FPL1 page After selection of ARRIVAL procedure information about selected procedure name of transit point and name of ARRIVAL procedure name of RW is displayed in ARVL field procedure is involved in active flight plan and RICU displays the page of active flight plan of FPJ form Selection of standard procedure of departure DEPARTURE Selection of DEPARTURE standard procedure is accomplished by analogy with given one in desc
26. PREDICTIVE RAIM field is used to activate PRAIM window intended for calculation of forecast RAIM in planned WP or for active flight plan and display of forecast results of function RAIM accessibility in graphic and text view To activate PRAIM window set highlight to the field PREDICTIVE RAIM and press ENT To return to AUX2 page press the CLR button 034 50 00 Appendix J page 176 Dec 17 2009 CH 4312 02 USER S MANUAL View of the window PRAIM is shown in figure J 8 30 1 Coordinates of NP for which forecast of function RAIM accessibility is being accomplished 2 Identifier of NP for which forecast of function RAIM accessibility is being accomplished 3 Name of an active flight plan 4 Field for display of forecast results of function RAIM accessibility in graphic view 5 Start time of function RAIM accessibility forecast calculation accomplishment 6 Data of function RAIM accessibility forecast calculation accomplishment 7 Command of function RAIM accessibility forecast calculation accomplishment for a selected NP 8 Command of function RAIM accessibility forecast calculation accomplishment for active flight plan 9 Output of function RAIM accessibility forecast results in text view 10 Setting of parameters for function RAIM accessibility forecast calculation Figure J 8 30 034 50 00 Appendix J page 177 Dec 17 2009 CH 4312 02 USER S MANUAL Function RAIM accessibility forecast calculation for NP Function RAIM acce
27. RANDOM 0006 0994 Create 1 Page or window display of the form 2 Display of status line Figure J 1 2 Form may contain one or several pages View of form pages is accomplished by rotating internal knob of the handle clockwise or counterclockwise with highlight of parameters or functions display fields switched off Form pages can contain one or several windows Access to windows is stated in equipment forms description Status line is displayed in lower part of RICU display figure J 1 2 034 50 00 Appendix J page 6 Dec 17 2009 CH 4312 02 USER S MANUAL Status line Status line is intended for operation modes and equipment status display External view of the status line is shown in the figure J 1 3 1 Coordinate determination mode GPS GNSS GLON SBAS according to data of GNSS sensor GNS2 according to data of GNSS sensor of the second RICU D D according to data of aircraft distance meter DME DME D D2 according to data of aircraft distance meters DME DME from the second RICU W D according to data of aircraft distance meter bearing measurer to beacon VOR DME V D2 according to data of aircraft distance meter bearing measurer to beacon VOR DME from the second RICU SVS according to data of course and air systems SVS2 according to data of course and air systems from the second RICU fill in the blank field Search mode SIM according to data of
28. Selection of a target point by identifier or name setting a flight in DIRECT TO mode To select a target point by identifier or name a in D form set highlight to the certain identifier name field Input identifier name of TP to which the flight will be accomplished in DIRECT TO mode b press ENT If there are several points in NDB with set identifier name RICU display will show DUPLICATE WAYPOINTS pop up window with the list of regions where waypoints with selected identifier name are located figure J 4 2 Set highlight to the field with required region UK UU Russia Figure J 4 2 034 50 00 Appendix J page 97 Dec 17 2009 CH 4312 02 USER S MANUAL c press ENT DUPLICATE WAYPOINTS pop up window will stop being displayed on RICU display the field ACTIVATE will be highlighted d press ENT to confirm accomplishment of a flight in DIRECT TO mode to the set TP Display RICU will show NAVI page with information about flight in DIRECT TO mode to selected point figure J 4 3 Information about flight in DIRECT TO mode to selected target point is displayed in the field of flight plan name on FPL1 page figure J 3 2 Figure J 4 3 Selection of a target point by identifier from the list of WP of an active flight plan and setting a flight in DIRECT TO mode To select a target point by identifier from the list of WP of an active flight plan and setting a flight in DIRECT TO mode a in D fe set highlight to F
29. VOR DME field TUNE VOR DME field is used to activate the window Tune VOR DME intended for selection of beacons VOR DME To activate Tune VOR DME window set highlight to TUNE VOR DME field and press ENT To return to AUX2 page press CLR button View of Tune VOR DME window is shown in figure J 8 6 034 50 00 Appendix J page 155 Dec 17 2009 CH 4312 02 USER S MANUAL 1 Type of beacons 2 Mode of beacon type 3 List of beacons for adjustment of AE selected in automatic mode reference designation of the beacon identifier frequency MHz T received data from beacon distance and azimuth C received text from airborne equipment VOR DME W beacon is involved into navigation solution distance to the beacon is indicated on the airplane distance indicator set by operator 4 List of beacons for adjustment of AE selected manually information in the list is similar to pos 3 Figure J 8 6 Review of beacons involved in NT solution of selected type For review of beacons a set highlight to the field of beacons type b turn internal knob one position further TYPE NAVAID pop up window is displayed in Tune VOR DME window figure J 8 7 Figure J 8 7 034 50 00 Appendix J page 156 Dec 17 2009 CH 4312 02 USER S MANUAL c set highlight to the indication field of the required type beacon Press ENT On RICU display in the beacon type field the beacons selected type shall be indicated
30. View of WPT9 page is shown in figure J 6 38 1 Identifier of omnidirectional USW beacon VOR 2 Reference designation of omnidirectional USW beacon 4 VOR EJ VOR DME t gt VORTAC 7 TACAN C DME 3 Class of NAVAID means 4 Name of omnidirectional USW beacon 5 Region of the country where omnidirectional USW beacon is located 6 Region of earth where omnidirectional USW beacon is located 7 Latitude longitude of nondirectional beacon 8 Symbol of current position of AC 9 Bearing to omnidirectional USW beacon from current position 10 Frequency of omnidirectional USW beacon 11 Distance to omnidirectional USW beacon from current position Figure J 6 38 034 50 00 Appendix J page 131 Dec 17 2009 CH 4312 02 USER S MANUAL Class of VHF NAVAID means is shown in figure J 6 2 J 6 3 Table J 6 2 Decade in the field of display of class of VHF NAVAID NAVAID means 1 2 3 4 5 VOR V TACAN channels 17 59 x 70 126 TACAN channels 1 16 1 60 69 DME olz Table J 6 3 VHF NAVAID Decade in the field of display of class of NAVAID means 1 2 3 4 5 ILS DME ILS TACAN p MLS DME N MLS DME P a Airfield Small altitude Big altitude Unlimited TACAN part from ILS TACAN ika fani iiie Displaced ILS DME or ILS TACAN Automatic weather forecast Planned weather forecast Speech is not available on
31. accomplishment for active flight plan set highlight to the CALC field opposite the field FPL press ENT display will show results of function RAIM accessibility forecast calculation in graphic view figure J 8 36 034 50 00 Appendix J page 183 Dec 17 2009 CH 4312 02 USER S MANUAL CALC CALC TEXT gt SETS gt Figure J 8 36 Forecast results Red colour on diagram means that RAIM forecast is not available blue colour RAIM forecast is available Appearance of the message about error CALC ERROR n figure J 8 37 where n number of error means n 2 sensor GNSS doesn t respond to requests n 3 speed parameters for calculation are set incorrect n 4 error of flight plan length part calculation n 5 number of calculation points equals zero In the case if message of error CALC ERROR n appears on RICU display repeat the forecast calculation of RAIM function availability CALC CALC TEXT gt SETS gt Figure J 8 37 034 50 00 Appendix J page 184 Dec 17 2009 CH 4312 02 USER S MANUAL Output of results of function RAIM accessibility forecast for NP and for active flight plan in text view To output results of function RAIM accessibility forecast in text form a set highlight to TEXT field in PRAIM window b press ENT button RICU display shows the window of function RAIM accessibility forecast results in the form of a table figure J 8 38 el D z
32. built in simulator Notes 1 With no adequate coordinates and time it is impossible to switch on D D u V D coordinate determination modes 2 To increase determination accuracy of navigation solution in SVS mode it is required to input wind parameters 2 Special manoeuvres execution display field fill in the blank field no special manoeuvres SUSP request to cut off automatic changeover to the next flight plan leg Changeover is fulfilled after pressing button OBS OBS outlet to WP with desired transit angle OFST flight execution on parallel route 3 Messages indication field fill in the blank field no messages MSG blinking inscription of yellow colour there are messages 4 Information field form name and active page number number of form pages window name warning messages output Figure J 1 3 034 50 00 Appendix J page 7 Dec 17 2009 CH 4312 02 USER S MANUAL Parameter input To input edit parameter fix highlight in display field of parameter which value it is necessary to input to edit Note Jf there is no parameter highlighted on display press the button CRSR turn internal knob of the handle one position further First symbol of parameter being input edited will be highlighed by rotating internal knob of the handle adjust set the necessary value of the first parameter symbol moving highlight by rotating external knob of the handle t
33. deviation from DT is changed automatically depending on flight stage It is possible to set scale of deviation from DT manually page AUX3 field SETTINGS Range of desired track deviation is set automatically depending on the flight stage from 10 to 10 km from 5 to 5 NM en route from 2 to 2 km from 1 to 1 NM when flight at airport area from 0 5 to 0 5 km from 0 3 to 0 3 NM 2 miles before aircraft FAWP fly over in APPROACH procedure Five divisions of scale of deviation from DT to the right from the centre and five divisions to the left from mark the corridor Width of the corridor displayed is defined by measure of scale of deviation from DT When AC goes out of the limits of the corridor equipment generates warning message Switching on off display of navigation references and or air zones in field of graphic representation of a flight plan To switch on off display of navigation parameters and or air zones in field of graphic representation of a flight plan press CLR button Only those navigation references and air zones are displayed in field of graphic representation of a flight plan which are selected in MAP SETTUP window figure J 8 72 of AUX3 page With serial pressing CLR button RICU display sequentially in a circle indicates in field of graphic representation of a flight plan together with a flight plan nearest navigation references figure J 2 2 nearest navigation references and air zones figure J
34. executed by pressing the button RNG or RNG button Note Scale means ratio of the ground distance to pictorial route field altitude pos 7 Figure J 2 1 Scale 120 on figure J 2 1 means that pictorial route field altitude corresponds to 120 km on the ground Interchangeable fields change To set interchangeable fields a set highlight to Change Fields field in PAGE MENU pop up window figure J 2 5 b press ENT PAGE MENU pop up window will stop being displayed on NAVI page Mnemonic symbol of one of interchangeable fields will highlight figure J 2 6 Figure J 2 6 c set the highlighting to mnemonic symbol of the parameter which must be changed d rotate internal knob for one position SELECT FIELD TYPE window is displayed on NAVI page figure J 2 7 034 50 00 Appendix J page 46 Dec 17 2009 CH 4312 02 USER S MANUAL BRG Bearing DIS Distance CUM Distance cumulation DTK Desired Track ETA Est Time Arvl Est Time Enrte Ground Speed Track Ang Err Track Figure J 2 7 e set the highlighting in SELECT FIELD TYPE window to the required parameter f press ENT to confirm the change by necessary parameter SELECT FIELD TYPE window will stop being displayed on NAVI page The required parameter is displayed in a selected interchangeable field mnemonic symbol of the parameter of one of interchangeable fields is highlighted g do all necessary changes of interchangeable fields
35. field of display of required system of units d press ENT to confirm setting of selected system of units Selection of operation mode of equipment To select operation mode of equipment a set highlight to the field of display of operation mode of equipment MODE field figure J 8 41 b turn internal knob one position further SETTING window displays pop up window of selection of operation modes of equipment SETTING MODE figure J 8 43 034 50 00 Appendix J page 190 Dec 17 2009 CH 4312 02 USER S MANUAL PS GLON SBAS ON OFF GBAS ON OFF Figure J 8 43 c set highlight to the field of display of required operation mode of equipment GPS GPS GLON or GLON d press ENT to confirm input of required operation mode of equipment e if it is necessary to activate deactivate the use of Satellite Based Augmentation System SBAS GBAS set highlight in SETTING MODE pop up window to SBAS ON OFF GBAS ON OFF field and press ENT figure J 8 44 Note System of functional addition SBAS GBAS must not be used Instruction about possibility of the use of this system will be input to UM by notice Figure J 8 44 034 50 00 Appendix J page 191 Dec 17 2009 CH 4312 02 USER S MANUAL Selection of system of coordinates To select system of coordinates a set highlight to the field of display of system of coordinates DATUM field figure J 8 41 b turn internal knob one position further SETTING window dis
36. flight plan is displayed on RICU Identifier of final point of input ARRIVAL procedure is displayed in the field of flight plan name on the place of identifier of final WP figure J 3 27 In case of successive input of APPROACH procedure into a flight plan identifier of final point of input APPROACH procedure is displayed in the field of flight plan name on the place of identifier of final WP If procedure of arrival and approach were earlier included in a flight plan then they will be deleted from a flight plan when including a new ARRIVAL procedure into a flight plan ACTIVE FLIGHT PLAN 608 136 1 Flight plan points 2 Title of ARRIVAL procedure 3 Points of ARRIVAL procedure 4 Name of the airport on which ARRIVAL procedure is set Figure J 3 27 Selection of standard DEPARTURE procedure To select departure procedure a set highlight to field Select Departure in PAGE MENU pop up window figure J 3 11 b press ENT Page of selection departure procedure WPT4 will appear on RICU display figure J 3 28 Identifier of initial WP is displayed in the field of WP identifier if an initial WP is an airport If initial WP is not departure airport set identifier of departure airport in the field of airport identifier 034 50 00 Appendix J page 79 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 3 28 c press ENT Highlight will move to the field of DEPARTURE procedure name d turn internal knob one position furt
37. flight to a new target point should be activated after finishing the flight to current target point accomplish the following actions a being in the form B gt press the button B gt once more Additional message QUEUE about queuing of a new target point will appear in the form gt figure J 4 6 DIRECT TO WAYPOINT CQUEUE Activate Figure J 4 6 b select a target point and set DIRECT TO mode according to methods described above 034 50 00 Appendix J page 101 Dec 17 2009 CH 4312 02 USER S MANUAL c press ENT to confirm queuing of a new target point RICU display shows the page NAVI which represent a flight DIRECT TO target point set earlier A new target point is put in the queue Information about flight in DIRECT TO mode to current target point and about queuing of a new target point is displayed on the page FPL1 in flight plan name field figure J 3 3 Cancellation of a flight in DIRECT TO mode to set target point and setting a flight in DIRECT TO mode to another target point To cancel a flight to target point set earlier and to set a flight to another TP a select another target point and set a flight in DIRECT TO mode according to methods described above b after confirmation of a flight in DIRECT TO mode to another target point RICU display will show NAVI page with information about a flight in DIRECT TO mode to newly selected target point Setting of an angle of flyover of a target point If i
38. graphic display of SID procedure figure J 6 18 034 50 00 Appendix J page 118 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 18 c rotating graphic display of SID procedure horizontally by means of external knob and vertically by means of internal knob set graphic display of the procedure to symbol in a place which after zooming must be in the centre of the field of graphic display of the procedure d press RNG button if it is necessary decrease the scale of display To increase the scale of display press RNG button figure J 6 19 Figure J 6 19 e press CRSR button to exit from zoom mode figure J 6 20 034 50 00 Appendix J page 119 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 20 WPTS page WPTS page is used for oveview of STAR procedure View of WPTS page is shown in figure J 6 21 1 Airport identifier 2 Field of graphic display of STAR procedure 3 Scale 4 Name of STAR current procedure 5 Name of transit point 6 RW name Figure J 6 21 034 50 00 Appendix J page 120 Dec 17 2009 CH 4312 02 USER S MANUAL Overview of STAR procedure To overview STAR procedure of an airport perform the following operations a set highlight to the field of airport identifier Input identifier of airport which STAR procedure information it is required to overview b press ENT Highlight will move to ARRIVAL field figure J 6 22 Figure J 6 22 c turn
39. in figure J 8 28 034 50 00 Appendix J page 174 Dec 17 2009 CH 4312 02 USER S MANUAL 1 Connection with the other RICU available YES or not available NO 2 Synchronization with NDB of the other RICU available YES or not available NO 3 Synchronization with user DB of the other RICU available YES or not available NO 4 Field of display of navigation data received by RICU2 coordinates altitude accuracy of coordinates determination time required to receive coordinates date 5 Navigation data discrepancy received by two RICUs indication field as to latitude as to longitude as to altitude as to accuracy of coordinates determination as to time required to receive coordinates Figure J 8 28 The input of coordinates received by other RICU as reference ones To input of coordinates received by other RICU as reference ones a Press MENU button PAGE MENU pop up window is indicated in DATA CROSS RICU window figure J 8 29 When there are navigation data from other RICU and navigation data from GNSS sensor are not available Set Nav Data from C RICU field is highlighted 034 50 00 Appendix J page 175 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 8 29 b Press ENT button PAGE MENU pop up window ends to be displayed in DATA CROSS RICU box The flag of reference coordinate receiving from other RICU CROSS BPIU is displayed in DATA GNSS window PREDICTIVE RAIM field
40. internal knob one position further WPTS page displays ARRIVAL pop up window Set highlight to the name of required STAR procedure figure J 6 23 Figure J 6 23 d press ENT ARRIVAL field displays the name of selected STAR procedure Highlight will move to the field of transit point name TRANS figure J 6 24 034 50 00 Appendix J page 121 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 24 e turn internal knob one position further WPTS page displays TRANS pop up window figure J 6 25 Figure J 6 25 e set highlight to the name of required of transit point f press ENT TRANS field displays the name of selected transit point Highlight will move to the field of RW name RUNWAY figure J 6 26 034 50 00 Appendix J page 122 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 26 g turn internal knob one position further WPTS page displays RUNWAY pop up window figure J 6 27 Figure J 6 27 h set highlight to the name of required of RW i press ENT RUNWAY field displays the name of selected RW highlight will remain in RUNWAY field Graphic representation of selected procedure STAR is displayed on WPTS page in the filed of graphic representation of procedure j press CRSR button Highlight will disappear from the fields of WPTS page figure J 6 28 034 50 00 Appendix J page 123 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 28 Zoom of graphic display of STAR
41. intersection point Selection of flight plan intersection point for overview of information about it is accomplished as follows a input identifier of flight plan intersection point which information it is necessary to overview If there are several flight plan intersection points then RICU will display DUPLICATE WAYPOINTS pop up window for selection of region where the point with input identifier is located b press ENT WPT7 page displays information about flight plan intersection point with input identifier 034 50 00 Appendix J page 128 Dec 17 2009 CH 4312 02 USER S MANUAL WPTS page WP TS page overview of information of NP of nondirectional beacons category NDB View of WPTS page is shown in figure J 6 36 1 Identifier of nondirectional beacon NDB 2 Reference designation of nondirectional beacon 3 Class of NAVAID means 4 Name of nondirectional beacon 5 Region of the country where nondirectional beacon is located 6 Region of earth where nondirectional beacon is located 7 Latitude longitude of nondirectional beacon 8 Symbol of current position of AC 9 Bearing to nondirectional beacon from current position 10 Frequency of nondirectional beacon 11 Magnetic declination 12 Distance to nondirectional beacon from current position Figure J 6 36 Class of L MF NAVAID means is shown in table J 6 1 034 50 00 Appendix J page 129 Dec 17 2009 Table J 6 1 CH 4312 02 USER S MANUAL Mean
42. mode display keyboard Highlight brightness setup display keyboard Figure J 1 20 page 5 of 8 CH 4312 02 USER S MANUAL LIMIT DATA field Setup parameters for computation of procedures SID STAR APPROACH average speed in terminal zones of takeoff arrival and on a flight plan limit angle of list on a flight plan MAP SETTUP field on off possibility of detailed representation in forms NAV1 and NAV3 air zones reference designation of nearest navigation references SEND USER DB TO BPIU2 field ENT Transmitted information volume in percents Setting of user database copy to other RICU Received information volume in percents Figure J 1 20 page 6 of 8 034 50 00 Appendix J page 37 Dec 17 2009 CH 4312 02 USER S MANUAL AUX4 page displays option selection fields INNER SIMULATION GNSS TEST DEVICE S TEST BACKGROUND TEST IO TEST KEYBOARD TEST SOFTWARE VERSION INNER SIMULATION field SIMULATOR window Setup speed initial coordinates initial WPT identifier on off built in simulator Performance GNSS TEST field ENT Extended test of GNSS receiver GNSS receiver restarts with RAM clearance Figure J 1 20 page 7 of 8 034 50 00 Appendix J page 38 Dec 17 2009 CH 4312 02 USER S MANUAL Review of information of DEVICE S TEST field EVICE S TEST window H ex
43. of FPL1 page Active Flight Plan with active flight plan is shown in figure 3 1 ACTIVE FLIGHT PLAN 625 119 1 Sign of an active flight plan 2 Field of flight plan name can be displayed identifier of initial WP identifier of final WP identifier of initial WP identifier of final WP rev when executing a reverse flight plan flight plan name input by operator P gt and target point identifier not included in an active flight plan when executing a flight in DIRECT TO mode figure J 3 2 P gt and current target point identifier Q TP identifier standing in the queue when executing a flight in DIRECT TO mode with setting WP ina queue figure J 3 3 3 Number of WP in a flight plan 4 Number of WP possible for input in a flight plan 5 WP identifier 6 Field before WP identifier field of designation of flight plan active step gt flight in DIRECT TO mode 1 flight with reaching WP with desired track angle 4 flight along the arc with fixed radius of a turn left turn flight along the arc with fixed radius of a turn right turn i gt owes ior flight to a target point in a route way gt te 7 Reference designation of WP 8 9 10 WP parameters in interchangeable fields adjusted by the user Figure J 3 1 034 50 00 Appendix J page 62 Dec 17 2009 CH 4312 02 USER S MANUAL ACTIVE FLIGHT PLAN 607 137 ACTIVE FLIGHT PLAN 007 137 Figure J 3 2 Figure J 3 3
44. possible from highlighted WP in an active flight plan will be brightly highlighted 034 50 00 Appendix J page 68 Dec 17 2009 CH 4312 02 USER S MANUAL BRP v VOR UKBB Figure J 3 10 e set the highlighting on the identifier of required WP press ENT RICU display shows FPL1 window with all WP of standard lane included in a flight plan from highlighted one on the FPL1 to selected WP in pop up window inclusive Operations performed on FPL1 page when pressing MENU button PAGE MENU pop up window figure J 3 11 is displayed on FPL1 page by pressing MENU button its fields are used to accomplish the following operations flight plan activation Activate field flight plan leg activation Activate Leg field retarget to flight plan WP Retarget To Point field flight plan copy to memory Copy Flight Plan field flight plan reverse Invert Flight Plan field flight plan removal Delete Flight Plan field selection and inclusion of Approach procedure to a flight plan Select Approach field selection and inclusion of STAR procedure to a flight plan Select Arrival field selection and inclusion of SID procedure to a flight plan Select Departure field deletion of Approach procedure from a flight plan Remove Approach field deletion of STAR procedure from a flight plan Remove Arrival field deletion of SID procedure from a flight plan Remove Departure field 034 50 00 Appe
45. rotating internal knob set required brightness level of signal light e set highlight to BACKLIGHT field f by rotating internal knob set required brightness level of background light g press ENT to confirm setting of brightness level of background and signal light Setting of brightness of keyboard with the use of photosensor To set brightness of keyboard with the use of photosensor a set highlight to FotoSensor field figure J 8 58 b press ENT RICU display shows information in accordance with figure J 8 66 034 50 00 Appendix J page 207 Dec 17 2009 CH 4312 02 USER S MANUAL DISPLAY 1 LS os 1 Setting of highlight brightness of keyboard with the use of photosensor 2 Graphic chart of highlight brightness of keyboard from photosensor illumination figure J 8 67 Figure J 8 66 Highlight brightness of keyboard 100 10 QWumination 0 10 100 1000 JIk Figure J 8 67 Graphic chart of highlight brightness of keyboard from photosensor illumination 034 50 00 Appendix J page 208 Dec 17 2009 CH 4312 02 USER S MANUAL c turn internal knob one position further BRIGHTNESS window displays pop up window of selection of graphic chart of brightness of keyboard from photosensor illumination figure J 8 68 Figure J 8 68 d set highlight to the field with required line e press ENT to confirm setting of highlight brightness of keyboard with the use of photosensor in accordance with se
46. similarly h press CLR or CRSR button for exit out of the mode of interchangeable fields change Highlight of an interchangeable field will disappear Setup of interchangeable fields in accordance with factor Y required up For setup of interchangeable fields in accordance with factor Y required up a set the highlighting in Restore Defaults field of PAGE MENU pop up window figure J 2 5 b press ENT c PAGE MENU pop up window will stop being displayed on NAVI page Interchangeable fields in accordance with factor Y required up will be displayed on the NAVI page 034 50 00 Appendix J page 47 Dec 17 2009 CH 4312 02 USER S MANUAL NAV2 page NAV page is used to display navigation parameters View of NAV2 page is shown in figure J 2 8 034 50 00 Appendix J page 48 1 Flight stage Possible values ENROUTE route TERMINAL airport area APPROACH approach landing 2 Name of the route 3 Display field of previous WP identifier symbols with flight in modes DIRECT TO and VTF desired flight angle of target point at flight performance in OBS mode 4 Display field of type of maneuver being accomplished flight to target point in a route way gt flight in mode DIRECT TO gt flight with achieving the point with specified course angle VTF flight in mode VTF LZ flight along the arc with fixed radius of a turn left turn MA flight along the arc with fixed radius of a tu
47. to TP not included in active flight plan the overflight of target value is always effected TP ae LCL ELLE EEE TETE PETER RE a 7 Desired flight track ACP Aircraft track line at the turn from flight activation point in DIRECT TO mode ACP to flight transition point on target point straight ae Hi Aircraft track line on TP after AC recovery from the turn ons Flight from target point Figure J 1 8 Scheme of the flight in DIRECT TO mode to TP not included in active flight plan TP WPT3 WPT 1 WPT2 Route WPT1 WPT2 WPT3 WPT4 Aircraft track line at the turn from flight activation point in DIRECT TO mode ACP to flight transition point on TP straight Aircraft track line on TP after AC recovery from the turn orere Switching from LLT to the flight on leg WPT3 WPT4 Figure J 1 9 Scheme of the flight in DIRECT TO mode to TP included in active flight plan 034 50 00 Appendix J page 14 Dec 17 2009 CH 4312 02 USER S MANUAL After flyover of target point WPT2 flight in DIRECT TO mode is cancelled and the flight is executed according to flight plan TP1 DT _ Desired flight track Aircraft track line at the turn from flight activation point in DIRECT TO mode ACP to flight transition point on TP straight Aircraft track line on TP after AC recovery from the turn cennennernnnses Switching from LLT to the flight on leg TP1 TP2
48. to a flight plan By using set averaged speeds of AC in LIMIT DATA window of AUX3 page description of this window and setup of parameters in it are given in description of AUX3 page and period of time in which forecast calculation is accomplished see description of SETTING PRAIM window coordinates of calculating points and time of flying over them are calculated RAIM forecast is calculated for each calculating point and is compared with factory setting of limits Value of limit for terminal areas is set to 550 m 0 3 NM Value of limit for a flight plan is set to 1 8 km 1 mile Change of these limits is not accessible for user To accomplish function RAIM accessibility forecast calculation for active flight plan a set start time and date of forecast calculation accomplishment start of flight according to a flight plan Setup of time and date is shown in description of function RAIM accessibility forecast calculation for NP b if it is necessary to change factory settings set parameters except limit of integrity signalling for function RAIM accessibility forecast calculation see description of SETTING PRAIM window figure J 8 32 c set averaged value of AC speed on the page AUX3 window LIMIT DATA in the field AVERAGE SPEED DEPARTURE for terminal area of departure ENROUTE for averaged flight part ARRIVAL for terminal area of arrival d set command of function RAIM accessibility forecast calculation
49. up window with the enquiry about flight plan leg activation is displayed on RICU display figure J 3 14 Figure J 3 14 034 50 00 Appendix J page 71 Dec 17 2009 CH 4312 02 USER S MANUAL e press ENT After pressing ENT addition to a flight plan leg is accomplished an active leg is stated figure J 3 15 and all calculations under an active flight plan are done if the first WP is a target point then a flight to it is executed in DIRECT TO mode If a target point happened to be passed in accordance with calculations under a flight plan then a successive activation of the next flight plan legs is accomplished until non passed is found ACTIVE FLIGHT PLAN 004 140 Figure J 3 15 Retarget to WP Retarget to WP can be accomplished with an active flight plan leg Retarget can be accomplished both to non passed and to passed WP To retarget accomplish the following actions a set highlight on FPL1 page to identifier of WP which retarget must be done to b press MENU button c set highlight to Retarget To Point field in PAGE MENU pop up window figure J 3 11 d press ENT Pop up window with the enquiry about retarget to a selected WP is displayed on RICU display figure J 3 16 034 50 00 Appendix J page 72 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 3 16 e press ENT After pressing ENT retarget to a selected WP is accomplished figure J 3 17 ACTIVE FLIGHT
50. which are displayed after pressing MSG blinking button is shown in table J 10 1 List of informative messages which are displayed automatically is shown in table J 10 2 Table J 10 1 Messages Messages in English in Russian No Aircraft is found outside legal bounds CaMoJIeT BbIINEJI 3a TPAHHAMEI YCTAHOBJICHHOTO Kopuyopa Integrity threshold has been exceeded I pesbimen nopor HEJOCTHOCTH Non precision PexuM cyncienns C Non precision computing is correspond to a mode COOTBETCTBYET peKHMY computing NHOHHKEeHHO TOYHOCTHIO activated Message about non possibility to RAIM is not RAN aeniei accomplish RAIM function it is available ue necessary to transfer to alternative navigation Scale CDI does not Hikana CDI ne Threshold does not correspond to a mode Ilopor neJI0CTHOCTH He COOTBETCTBYET PEKAMY Select true angle mode Bbi6epu pekuM HCTHHHBIX YIJI10B Coordinates aren t accessible KOOPAAHATEI OTCYTCTBYIOT Message appears when current coordinates are absent or their accuracy more than 5 miles Degradation accuracy to RNP20 Yxyamenne TOUHOCTH ao RNP20 Enter coordinates time and date BBezxuTe KOOPAHHATBI BpeMa H AATY Enter wind _ speed BBeJUTe CKOPOCTE BeTpa 034 50 00 Appendix J page 231 Dec 17 2009 CH 4312 02 USER S MANUAL Table J 10 2 Messages Messages in English in Russian Nose DAT
51. 0 Dec 17 2009 CH 4312 02 USER S MANUAL Activation deactivation of built in simulator To activate deactivate built in simulator a set highlight to SIMULATION field b turn internal knob one position further SIMULATOR window displays a pop up window of built in simulator activation deactivation c set highlight to the field ON to activate a built in simulator OFF to deactivate a built in simulator d press ENT GNSS TEST field GNSS TEST field serves for fetching GNSS TEST pop up window meant for starting enhanced test of GNSS receiver and restarting GNSS receiver with memory clearing To switch on the test of receiver GNSS a set highlight to GNSS TEST field figure J 8 79 b press ENT the page AUX4 displays GNSS TEST pop up window figure J 8 81 Figure J 8 81 c set highlight to FUNCTIONAL TEST field to activate GNSS receiver test d press ENT to confirm selected function Pop up window will stop being displayed Result of testing of receiver GNSS is displayed in FonTest 1 window AUX4 BACKGROUND TEST ENT 034 50 00 Appendix J page 221 Dec 17 2009 CH 4312 02 USER S MANUAL For activation of GNSS receiver restart with RAM clearance a set highlight in GNSS TEST field Fig J 8 79 b press ENT AUX4 page shall indicate GNSS TEST popup window Fig J 8 81 c set highlight in COLD START field d press ENT to restart GNSS receiver with RAM clearance WARNING AFTER RESET OF RECEI
52. 00 Appendix J page 94 Dec 17 2009 CH 4312 02 USER S MANUAL c press ENT to confirm deletion to refuse deletion press CLR button or set highlight to the NO field and press ENT Flight plan catalogue on FPL2 page will be empty figure J 3 49 FLIGHT PLAN CATALOG A 00 900 Figure J 3 49 Flight plans sorting by numbers and alphabet To sort flight plan by numbers or alphabet a set highlight to the Sort List By Number or Sort List By Comment field in PAGE MENU pop up window figure J 3 42 Note Jf flight plans on FPL2 page were sorted by flight plan numbers then PAGE MENU page will display the request to sort by alphabet Sort List By Comment and vice versa b press ENT Sorting of flight plans according to the request will be effected on the FPL2 page 034 50 00 Appendix J page 95 Dec 17 2009 CH 4312 02 USER S MANUAL J 4 Operation description in gt form The D forr is used to set a flight in DIRECT TO mode DIRECT TO mode ensures a quick selection of a target point and a possibility to set an angle of flyover of a target point After flight activation in DIRECT TO mode equipment computes the desired track from ACP to selected target point along the line of great circle orthodromy and accomplishes a flight to the target point Angle of flyover of the target point set in CRS field allows to change DT primary calculation Flight along computed DT is kept until DIRECT TO mode is cancelled or
53. 009 CH 4312 02 USER S MANUAL Logical tree of OBS form 034 50 00 Appendix page 24 OBS form Display Target point transit angle target point identifier set transit angle TP transit angle setting Flight setting in OBS mode Figure J 1 17 J Dec 17 2009 CH 4312 02 USER S MANUAL Logical tree of WPT form Display airport information bearing and distance from current aircraft position to airport WPT1 page is the main page for NP of airport category Airport selection by name or identifier Flight setting in DIRECT TO mode WPT2 page is for NP of airport category Display airport identifier number of airport RW graphic representation of airport RW e RW selection for overview ENT Flight setting in DIRECT TO mode Figure J 1 18 page 1 of 5 034 50 00 Appendix J page 25 Dec 17 2009 CH 4312 02 USER S MANUAL WPT3 page is for NP of airport category Display airport identifier information about radiocommunication equipment Airport selection by identifier Flight setting in DIRECT TO mode WPT4 page is for NP of airport category Display airport identifier parameters of current SID procedure graphic representation of current SID procedure Selection and overview of SID procedures of airport selected Flight setting in DIRECT TO mode Figure J 1 18 page 2 of 5
54. 009 51 10 Dec 17 2009 52 11 Dec 17 2009 53 12 Dec 17 2009 54 13 Dec 17 2009 55 14 Dec 17 2009 56 15 Dec 17 2009 57 16 Dec 17 2009 58 17 Dec 17 2009 59 18 Dec 17 2009 60 19 Dec 17 2009 61 20 Dec 17 2009 62 034 50 00 List of effective pages page 1 Dec 17 2009 CH 4312 02 USER S MANUAL LIST OF EFFECTIVE PAGES Section Sub section Page Date Paden Page Paragraph i Appendix J 63 Dec 17 2009 Appendix J 105 64 Dec 17 2009 106 65 Dec 17 2009 107 66 Dec 17 2009 108 67 Dec 17 2009 109 Dec 17 2009 68 Dec 17 2009 110 69 Dec 17 2009 111 Dec 17 2009 70 Dec 17 2009 112 71 Dec 17 2009 113 72 Dec 17 2009 114 73 Dec 17 2009 115 74 Dec 17 2009 116 75 Dec 17 2009 117 Dec 17 2009 76 Dec 17 2009 118 77 Dec 17 2009 119 78 Dec 17 2009 120 79 Dec 17 2009 121 80 Dec 17 2009 122 81 Dec 17 2009 123 82 Dec 17 2009 124 83 Dec 17 2009 125 84 Dec 17 2009 126 85 Dec 17 2009 127 86 Dec 17 2009 128 87 Dec 17 2009 129 Dec 17 2009 88 Dec 17 2009 130 89 Dec 17 2009 131 90 Dec 17 2009 132 91 Dec 17 2009 133 92 Dec 17 2009 134 93 Dec 17 2009 135 94 Dec 17 2009 136 95 Dec 17 2009 137 96 Dec 17 2009 138 97 Dec 17 2009 139 98 Dec 17 2009 140 99 Dec 17 2009 141 100 Dec 17 2009 142 101 Dec 17 2009 143 102 Dec 17 2009 144 103 Dec 17 2009 145 104 Dec 17 2009 146 Oo 034 50 00 Li
55. 034 50 00 Appendix J page 26 Dec 17 2009 CH 4312 02 USER S MANUAL WPTS page is for NP of airport category Display airport identifier parameters of current STAR procedure graphic representation of current STAR procedure CRSR Airport selection by Selection and overview of STAR identifier procedures of airport selected Zooming of STAR procedure graphic display Flight setting in DIRECT TO mode WPT6 page is for NP of airport category Display airport identifier parameters of current procedure APPROACH graphic representation of current procedure APPROACH Selection and overview of APPROACH procedures of airport selected Zooming of APPROACH procedure graphic display Flight setting in DIRECT TO mode Figure J 1 18 page 3 of 5 034 50 00 Appendix J page 27 Dec 17 2009 CH 4312 02 USER S MANUAL WPT7 page is for NP of flight plans intersection points category Display NP information bearing and distance from current aircraft position to flight plans intersection point NP selection by identifier Flight setting in DIRECT TO mode WPTS page is for NP of nondirectional radiobeacon category Display NP information bearing and distance from current aircraft position to nondirectional radiobeacon NP selection by identifier or by name Flight setting in DIRECT TO mode WPT9 page is for NP of omnidirectional USW beacons Displa
56. 1 133 From UUEE ss Departure ARO7D Enroute lt a 1 Name of airport which Departure procedure is set for 2 Title of Departure procedure 3 Points of Departure procedure 4 Title of a flight plan 5 Waypoints Figure J 3 32 034 50 00 Appendix J page 81 Dec 17 2009 CH 4312 02 USER S MANUAL Deletion of APPROACH procedure from a flight plan To delete approach procedure from a flight plan a set highlight to field Remove Approach in PAGE MENU pop up window figure J 3 11 b press ENT Pop up window with the request to delete approach procedure is displayed on RICU display figure J 3 33 Figure J 3 33 c press ENT to confirm the deletion of the procedure to refuse deletion press the button CLR or set highlight to the field NO and press ENT Identifier of WP which has APPROACH procedure deleted is displayed in the field of flight plan name in the place of identifier of final WP If ARRIVAL procedure was included in the flight plan identifier of final point of ARRIVAL procedure is displayed in the field of flight plan name in the place of identifier of final WP Deletion of the procedure ARRIVAL from a flight plan To delete arrival procedure from a flight plan a set highlight to field Remove Arrival in PAGE MENU pop up window figure J 3 11 b press ENT Pop up window with the request to delete arrival procedure is displayed on RICU display figure J 3 34 034 50 00 Appendix J
57. 1 5 All the flight according set flight plan consists of consistent leaving one WP for another one along DT To avoid going out of aircraft beyond the limits of airway width during a turn and a transition from one flight plan leg to another equipment carries out computation of linear allowance of a turn and beginning of turn prior to aircraft going to WP along the arc of inscribed circle of optimal radius see figure J 1 6 a 034 50 00 Appendix J page 10 Dec 17 2009 CH 4312 02 USER S MANUAL Linear allowance of a turn is computed for maximum angle of list of AC LLT is calculated depending on true airspeed angle of turn direction and speed of the wind While flying over WP an aircraft is moving along the trajectory defined as arc of inscribed circle with a radius R Notes 1 When approaching turn start point or when crossing bisector of angle created by adjacent legs of the flight plan depending on which occurs first equipment stops to trace previous WP and begins to trace the next WP and in connection with this the change of all indicating parameters takes place on the display 2 When angles of turn are more than 130 LLT forms two turn radiuses see figure J 1 6 6 defined by true airspeed of AC maximal angle of list of AC direction and speed of the wind Transition of AC to the next leg of the flight plan is executed along a special trajectory turn with maximum possible aircraft list along the circle with radius R
58. 19 J Ds 1 Flight plan number 2 Flight plan name field can display identifier of initial WP identifier of final WP identifier of initial WP identifier of final WP rev if to accomplish reverse flight plan flight plan name input by operator P gt and identifier of TP not included in active flight plan when accomplishing flight in DIRECT TO mode figure J 3 2 P gt and identifier of current TP Q and identifier of TP being in the queue when accomplishing flight in DIRECT TO mode with putting WP in the queue figure J 3 3 3 Number of WP in a flight plan 4 Number of WP possible to input in a flight plan 5 WP identifier 6 Reference designation of WP 7 9 Interchangeable fields Figure J 3 40 034 50 00 Appendix J page 87 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 3 40 shows factory setting of interchangeable fields List of parameters which can be displayed in interchangeable fields 7 9 is shown in table J 3 3 List of possible reference designations is shown in table J 3 4 Table J 3 3 Designation in the Paramete Interchangeable form field CUM Total distance to final WP in desired track pos 8 9 DIS Length of flight plan leg along DT pos 8 9 DTK Desired track angle pos 8 9 ESA Safe flight altitude of the flight plan pos 7 Table J 3 4 Reference Parameter Description designation of ABSENT Point not found in ND
59. 2 3 air zones figure J 2 4 indication of navigation zones and nearest navigation references is unavailable figure J 2 1 034 50 00 Appendix J page 44 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 2 2 Figure J 2 3 Figure J 2 4 Functions performed on NAVI page by pressing MENU button When pressing MENU button PAGE MENU pop up window is displayed on NAVI page figure J 2 5 its fields are intended for fulfilling the following operations of automatic scale change of flight plan graphic representation Autozoom field interchangeable fields setting Change Fields field interchangeable fields setting in accordance with factory setting Restore Defaults field Autozoom Change Fields Restore Defaults 034 50 00 Appendix J page 45 Dec 17 2009 CH 4312 02 USER S MANUAL Activation of automatic scale change of flight plan graphic representation Change of flight plan graphic representation can be accomplished manually by means of the button RNG and RNG or in automatic mode To activate automatic scale change a set highlight to Autozoom field in PAGE MENU pop up window figure J 2 5 6 press ENT PAGE MENU pop up window will stop being displayed on NAVI page Automatic scale change will switch on A scale with which an active flight plan leg is displayed in the field of flight plan graphic representation should be set automatically Deactivation of automatic scale change is
60. 4 Dec 17 2009 CH 4312 02 USER S MANUAL Check of input one time orders Check availability of one time orders received from respective external devices see 034 50 00 Appendix A connector X4 RICU Availability of symbol 1 in decades of the line RK IN means availability of one time order Rightmost symbol of the field RK IN corresponds to one time order IN_L_1 the eighth symbol from the right corresponds to one time order IN_L_8 the ninth symbol from the right corresponds to one time order IN_N_1 leftmost symbol corresponds to one time order IN_N 8 Check of formation of signal of deviation from DT To check formation of signal of deviation from DT a set highlight to XTK field b set value of deviation from DT c check on HSI deviation of arrow on lateral deviation scale to the value corresponding to the value set in XTK field Check of formation of Selected roll signal To check formation of Selected roll signal a set highlight to GAMMA field b set value of Selected roll signal c press ENT d check direct voltage on external device connected to RICU through Selected roll circuit The voltage must correspond to set value of Selected roll signal in GAMMA field from the calculation of 0 33 V for 1 degree The check of formation of deviation signal from course To check formation of deviation signal from course a set highlight to E_k field b set value of deviation signal
61. 5 Dec 17 2009 CH 4312 02 USER S MANUAL Service indicator Designation Description value 1 2 3 Aeronautical Enroute Information Aeronautical Enroute Information A Service AEIS Service AEIS Enroute Flight Advisory Service Enroute Flight Advisory Service E EFAS EFAS Flight Information Service FIS Flight Information Service FIS F Air Ground Air Ground A Discrete Frequency Discrete Frequency D Air Air Air Air C Mandatory Frequency Mandatory Frequency M Secondary Frequency Secondary Frequency S VHF Direction Finding Service VDF VHF Direction Finding Service D VDF Remote Communications Air to Remote Communications Air to G Ground RCAG Ground RCAG Language other than English Language other than English L Military Use Frequency Military Use Frequency M Remote Communications Outlet Remote Communications Outlet R RCO RCO Overview of radio communication equipment of airport To overview information about radio communication equipment of airport a press the CRSR button identifier of airport will be displayed b rotate internal knob of the handle one position further AIRPORT pop up window will be displayed on NAV4 page in accordance with figure J 2 13 in which identifiers of initial WP final WP and two nearest airports are displayed In case if there is no active
62. 8 40 and press ENT button To return to AUX3 page press CLR button View of MAP SETTUP window is shown in figure J 8 72 CR AIRSPACE a LS NAVAID 1 Field of activation deactivation of possibility of detailed representation of air zones in NAVI and NAV3 pages of districts of FIR UIR flight information of air space of limited use of controlled air spaces 2 Field of activation deactivation of possibility of detailed representation of NAV1 and NAV3 of references designations of nearest navigation references of airports of NDB beacons of VOR DME beacons Figure 8 72 034 50 00 Appendix J page 214 Dec 17 2009 CH 4312 02 USER S MANUAL Selection of air zones and reference designations of navigation reference possible for detailed representation in NAVI and NAV3 pages To select air zones and reference designations of navigation references possible for detailed representation in NAV1 and NAV3 pages a set highlight to the field of activation deactivation of detailed representation of air zone or reference designation of navigation reference detailed representation of which it is possible to activate deactivate in NAVI and NAV3 pages b turn internal knob one position further The window MAP SETTUP displays SELECT pop up window figure J 8 73 Figure J 8 73 c set highlight in SELECT pop up window to the field ON to activate possibility of detailed representation OFF to deactivat
63. ABASE Cpok axe crBus HB EXPIRED 3AKOH4HJICA DATABASE HBJI orcyrcrByer MISSING Cannot activate He Mory aKTHBHPOBATE OFFSET OFFSET Active FPL AKTHBHBIii MAPIUPYT Message is displayed if attemping to is absent OTCYTCTBYET switch on the mode of movement on a parallel fligt plan when a flight plan is not activated Link with GNSS is bad OTcyTcTByeT CBA3b c Mozxyem GNSS Link with KVU is bad OTcyTcTByeT CBA3b c Mozysiem KBY Antenna is bad OTkKa3 aHTeHHBI Receiver s testing is failure OTKa3 KaHaJIOB IPHEMHHKA The NDB with CROSS RICU differ HAB c apyrum DBIIHY pa3JIM4HbI The data with annie c Apyrum CROSS RICU differ BITHY pa3 1IM4HBbI Route off Mapuipyt Integrity threshold ACAKTHBHPOBAH has been exceeded IlpeBbimeH nopor WeecTHOCTH Program error during acccomplishment SYSTEM ERROR n CucTeMHas ommokKa n where n code of error 1 access to non existing memory 2 error of selection of commands data from memory 3 program interruption 4 invalid command Data of error can be followed by additional text information 034 50 00 Appendix J page 232 Dec 17 2009 Warning messages CH 4312 02 USER S MANUAL Warning messages are automatically displayed in the right part of status line of the form List of warning messages is shown in table J 10 3 Table J 10 3 Messages Messages in English in
64. AIRBORNE EQUIPMENT OF SATELLITE NAVIGATION USER S MANUAL OPERATOR S GUIDE PART 2 TJIILK 461513 077 02 P91 CH 4312 02 USER S MANUAL RECORD OF REVISIONS Section Covering Rev Sub ti 7 Page Document document da Dat Nos ER Ref No Ref No LEE a Paragraph Revised Added Deleted and Date 034 50 00 Record of revision page 1 Dec 17 2009 CH 4312 02 USER S MANUAL RECORD OF REVISION Section Covering Rev Sub section Page Document document Sioni Dat No Ref No Ref No and En Paragraph Revised Added Deleted Date 034 50 00 Record of revision page 2 Dec 17 2009 CH 4312 02 USER S MANUAL LIST OF EFFECTIVE PAGES Section Sub section Section Sub Title page 1 Dec 17 2009 Appendix J 21 22 Record of revision 1 Dec 17 2009 23 Dec 17 2009 2 Dec 17 2009 24 25 List of effective 1 Dec 17 2009 26 pages 2 Dec 17 2009 27 Dec 17 2009 3 4 Dec 17 2009 28 Contents 1 Dec 17 2009 29 2 Dec 17 2009 30 31 Abbreviation list 1 Dec 17 2009 32 2 Dec 17 2009 33 Dec 17 2009 3 Dec 17 2009 34 4 Dec 17 2009 35 5 6 Dec 17 2009 36 37 38 39 40 41 42 Appendix J 1 Dec 17 2009 43 2 Dec 17 2009 44 3 Dec 17 2009 45 4 Dec 17 2009 46 5 Dec 17 2009 47 6 Dec 17 2009 48 7 Dec 17 2009 49 8 Dec 17 2009 50 9 Dec 17 2
65. B b BAD Error is registered for a point for example point coordinates failed to be loaded Point of report about passing Note Symbol indicates decade in reference designation of WP Flight plan editing Flight plan editing in FPL_ree window means execution of the following operations deletion of WP form a flight plan input of a new WP into a flight plan input of a leg of standard lane into a flight plan These three operations in FPL_rec window are accomplished by analogy with operations stated in FPL2 page description 034 50 00 Appendix J page 88 Dec 17 2009 CH 4312 02 USER S MANUAL Operations performed in FPL_rec window when pressing MENU button PAGE MENU pop up window figure J 3 41 is displayed in the window FPL rec by pressing MENU button its fields are used to accomplish the following operations flight plan activation Activate Flight Plan field copy of flight plan in memory Copy Flight Plan field flight plan reverse Invert Flight Plan field flight plan deletion Delete Flight Plan field creation of WP on DT in minimum distance from selected WP Closest Point of FPL field setup of interchangeable fields Change Fields field setup of interchangeable fields in accordance with factory setting Restore Defaults field Note Copy Flight Plan and Closest Point of FPL fields are not used Invert ight Plan Delete Flight Plan Chan
66. DIS Highlight will move to the field of bearing from basic NP figure J 6 43 Note To input current position of AC as basic NP set highlight to the field of identifier of basic NP and press CLR button Symbol of current position of AC P_POS is displayed in the field of identifier of basic NP 6005 0995 create Figure J 6 43 e set value of bearing f press ENT Highlight will move to the field of distance to basic NP Values of coordinates being displayed in POSITION field will change figure J 6 44 034 50 00 Appendix J page 136 Dec 17 2009 CH 4312 02 USER S MANUAL 0006 0994 Create Figure J 6 44 g set distance from NP being created to basic NP h press ENT Coordinates of user NP created by setting bearing and distance from basic NP are displayed in POSITION field figure J 6 45 6006 0994 Create Figure J 6 45 i set highlight to the field Create j press ENT to confirm the creation of user NP NP with input identifier and coordinates displayed in the field POSITION is created 034 50 00 Appendix J page 137 Dec 17 2009 CH 4312 02 USER S MANUAL Creation of user WP by setting bearing from two basic NP To create user NP by setting bearing from two basic NP a set highlight to the field of display of NP identifier b input identifier of user NP being created c press ENT to confirm input of identifier Highlight will move to the field of identifier of basic N
67. F SATELLITE NAVIGATION 034 50 00 Appendix J Operators Guide san sidesevsicsivesancavceks niesssdecelsccpasoakesansecsBoaesinisssuseseissseascousdoucdAveecs 1 J 1 General information sesssesseseessoesoesseseossoossessoesoossessossoosseesoseooesossoeseossossoeseoesossseseossoessessossoossessose 2 RO KI ea TA E E EA AE EE AA TEE NE TE 2 Information presentation on RICU display 3 Antenne nn nn RM eis 6 Parameter npt aos ee MR nd at ri ren etat er ie udwas eed A R a a ais 8 Ways OP PONG CX COUT Sos Re ae SN nes Lin 10 Logical tree of apparatus OMS En ae tt ne ET ee fat et A nt ua 18 J 2 Operation description in NAV form ssessseesseessoossoosssoessoesssocssooesoossooessseessosssoossosssssesssesesoses 41 NAVI Dash needed rat leds nel a dit 42 NA V2 page nl Ainsi 48 NAN STAR nd tut it wade scala aac 50 NAN D oe B e Pe DRO Ree Ree E ee Pua eRe Ae eee PE EERE Reet ere ete eR ne 53 NANS ASS sata nine A re ere AT Maas Naan E age At aa 57 J 3 Operation description in FPL fOrnn ccccccccsscccssscccssccscssccscssccecscsccsscsesssssosssssoessssossseoes 61 BER Ta aes ess ns Te diese ana tae neuen ne ce nn A vas 62 LES A SE OT cube cae ch gc cosas E aes ance c ce ee cacas ecm aeanee 85 J 4 Operation description im D fOr IM scscssccscscsccccisesesscsesssnssesassescsssoonescodesdscncssscesssoeesssecsecsesuccsaus 96 J 5 Operation description in OBS fora ciccicccecssecsesssonsssesorsoecnessovesesooeessvssaovoacssenssssbsavsveesecnansse 104
68. J 3 38 1 O PLAN CATALOG A 03 87 1 Flight plan number 2 Flight plan name field can display identifier of initial WP identifier of final WP identifier of initial WP identifier of final WP rev if reverse flight plan name input by operator Figure J 3 38 034 50 00 Appendix J page 85 Dec 17 2009 CH 4312 02 USER S MANUAL Deletion of a flight plan from flight plan catalogue To delete a flight plan from flight plan catalogue a set highlight on FPL2 page to the field of flight plan which must be deleted from flight plan catalogue b press CLR button Pop up window with the enquiry to delete highlighted flight plan is displayed on RICU display figure J 3 39 Figure J 3 39 c press ENT to confirm the deletion of the flight plan to refuse deletion press CLR button or set highlight to NO field and press ENT Detailed overview of a flight plan For detailed overview of a flight plan a set highlight on FPL2 page to the field of flight plan which should be overviewed b press ENT FPL_ree window figure J 3 40 which contains detailed information about selected flight plan is displayed on RICU display c press CRSR button to return from FPL_rec window to FPL2 page 034 50 00 Appendix J page 86 Dec 17 2009 CH 4312 02 USER S MANUAL Description of FPL_rec window Detailed information about selected flight plan is displayed in FPL_ree window FLIIGHT PLAN 625 1
69. LR button View of DATA SVS IRS WIND window is shown in figure J 8 25 1 Altitude of AC and sign of value accuracy FAULT not reliable OK reliable 2 Speed of AC and sign of value accuracy 3 Gyromagnetic course of and sign of value accuracy 4 Wind direction metro wind 5 Wind speed Figure J 8 25 034 50 00 Appendix J page 172 Dec 17 2009 CH 4312 02 USER S MANUAL Input of wind parameters Automatic calculation of wind parameters occurs failing Strut compression one time command or if aircraft speed is no less than 70 m s in the presence of navigation solving using GNSS sensor VOR DME or DME DME devices If input of wind parameters is required a press CRSR button Wind direction field will be highlighted Insert the required value of wind direction Press ENT button for inserted value confirmation b Wind speed field will be highlighted Insert the required value of wind speed Press ENT button for inserted value confirmation NAVIGATION MODE field NAVIGATION MODE field is designed for NAVIGATION MODE call necessary for the navigation data source selection used for the complex NT solution For NAVIGATION MODE window call install highlight in NAVIGATION MODE field Fig J 8 5 and press ENT To return on AUX2 page press CLR View of NAVIGATION MODE window is shown in fig J 8 26 ie NAVIGATION DATA Fes NAY DATA C BPIU 1 Use control of navigation data source in the complex NT sol
70. LR button Pop up window with the enquiry about confirmation or refusal of deletion of selected WP is displayed on RICU display figure J 3 5 034 50 00 Appendix J page 65 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 3 5 c press ENT to delete selected WP to refuse deletion press the button CLR or set the highlighting to NO field and press ENT Input of a new WP to an active flight plan To input anew WP to an active flight plan a set the highlighting on FPL1 page to identifier of WP before which a new WP should be input if it is required to input WP in a flight plan after final WP set the highlighting on the field located below identifier of final WP of a flight b turn internal knob one position to the right or left c if standard lanes do not pass through WP which is highlighted or there is no information about standard lanes window fpl_add is displayed on RICU display figure J 3 6 WAYPOINT INFORMATION CENT ACCEPT Figure J 3 6 034 50 00 Appendix J page 66 Dec 17 2009 CH 4312 02 USER S MANUAL In this case to input WP input identifier of WP which should be input in a flight plan press ENT If there are several WP with identifier input DUPLICATE WAYPOINTS pop up window for selection of a region where WP with input identifier is located will appear on RICU display figure J 3 7 BG Greenland Denma Figure J 3 7 set the highlighting on the required region of WP and p
71. NAVAID Nonconcentrated VOR and TACAN or DME zlo gt o Overview of information about NP of omnidirectional USW beacons Selection of NP of omnidirectional USW beacons category for overview of information about it is accomplished as follows a input identifier name of NP of omnidirectional USW beacons category which information it is necessary to overview If the are several NP of omnidirectional USW beacons category with input identifier then RICU will display DUPLICATE WAYPOINTS pop up window for selection of region where the point with input identifier is located b press ENT WPT9 page displays information about NP of omnidirectional USW beacons category with input identifier name WPT9 034 50 00 Appendix J page 132 Dec 17 2009 CH 4312 02 USER S MANUAL WPT10 page WPT10 page is used for overview of information editing and creation of NP of User WP category User WP View of WPT10 page is shown in figure J 6 39 1 Identifier of NP of User WP category User WP 2 Number of user WP possible for creating 3 Number of created user WP 4 Identifier of basic NP 5 Distance from basic NP 6 Bearing from basic NP 7 Identifier of the second basic NP 8 Bearing from second basic NP 9 Latitude longitude of user WP 10 Name of user WP 11 Region Figure J 6 39 034 50 00 Appendix J page 133 Dec 17 2009 CH 4312 02 USER S MANUAL Creation of user WP
72. P A request about creation of user WP Create will appear in right lower angle of RICU display d input identifier of basic NP if there are several NP with input identifier then RICU will display DUPLICATE WAYPOINTS pop up window for selection of region where the point with input identifier is located Set highlight to required region of NP Press ENT Bearing and distance from input basic NP to the point with coordinates displayed in POSITION field are displayed on WPT10 page in RAD and DIS fields e press ENT Highlight will move to the field of bearing to basic NP Set bearing value press ENT f move highlight to the field of the second basic NP Input identifier of the second basic NP if there are several NP with input identifier then RICU will display DUPLICATE WAYPOINTS pop up window for selection of region where the point with input identifier is located Set highlight to required region of NP g press ENT Values of coordinates displayed in POSITION field will change Highlight will move to the field of bearing to the second basic NP h set bearing value Press ENT Coordinates of user NP created by setting bearings from two basic NP are displayed in POSITION field i set highlight to the field Create by pressing ENT or by rotating external knob clockwise j press ENT to confirm the creation of user NP User NP with input identifier and coordinates displayed in POSITION field is created 034 50 00 Appendix J pag
73. PL field figure J 4 1 b turn internal knob one position further FPL pop up window with the list of WP of an active flight plan will be displayed on RICU figure J 4 4 034 50 00 Appendix J page 98 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 4 4 c set highlight to required target point from the list of WP d press ENT Fields of D form except the field NRST are filled with information about selected target point Activate field will be highlighted e press ENT to confirm activation of the flight to selected target point RICU display will show NAVI page with information about the flight to selected point in DIRECT TO mode FPL1 page displays the arrow pointing to target point identifier Selection of a target point from the list of the nearest airports and setting a flight in DIRECT TO mode To select a target point from the nearest airports and for the flight task in DIRECT ON mode a in D formset highlight to the NRST field b turn internal knob one position further RICU display will show NEAREST pop up window with the list of the nearest airports figure J 4 5 034 50 00 Appendix J page 99 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 4 5 c set highlight to required target point from the list d press ENT The field of D formte eept FPL field are filled with information about selected target point Activate field will be highlighted e press ENT to confirm activation of the flight t
74. PLAN 0047140 Figure J 3 17 Flight plan copy to memory To copy a flight plan to memory a set the highlighting to Copy Flight Plan field in PAGE MENU pop up window figure J 3 11 b press ENT Pop up window with the enquiry to copy a flight plan to memory stating number of a flight plan is displayed on RICU display figure J 3 18 034 50 00 Appendix J page 73 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 3 18 c press ENT to confirm copying After pressing ENT a flight plan is copied to RICU memory with number stated in copy enquiry window Note Copy of a flight plan to memory is impossible to accomplish if SID STAR APPROACH procedures are available in a flight plan You should delete these procedures before copying Flight plan reverse To reverse a flight plan accomplish the following actions a set the highlighting on Invert Flight Plan field in PAGE MENU pop up window figure J 3 11 b press ENT A reverse flight plan is displayed on FPL1 page Identifiers of initial and final waypoint will swap in the field of flight plan name and the sign of a reverse flight plan rev will appear if flight plan name is automatic figure J 3 19 If input of a flight plan name is manual no changes in the field of flight plan name will occur ACTIVE FLIGHT PLAN 0047140 Figure J 3 19 034 50 00 Appendix J page 74 Dec 17 2009 CH 4312 02 USER S MANUAL Note 1 Reverse of a flight pla
75. RST4 page NEAREST VOR is used to overview nearest NP of omnidirectional USW beacons category Entry to NRST form is accomplished by pressing NRST button on RICU In case of repeated pressing NRST button RICU display shows the form which was on RICU prior to activation of NRST form Switching of pages of NRST form is accomplished by rotating internal knob 034 50 00 Appendix J page 147 Dec 17 2009 CH 4312 02 USER S MANUAL NRST1 page NRST1 NEAREST ARP page is used to overview nearest NP of airport category View of NRST1 page is shown in figure J 7 1 NEAREST ARP a 1 Lines of table with parameters Reference designation of parameter Airport identifier Bearing to airport from current position Distance to airport from current position Length of the longest RW of airport Figure J 7 1 Overview of information about nearest NP of airport category To overview information about nearest NP of airport category perform the following operations a press CRSR button first line of the table will become highlighted b by rotating external knob clockwise move highlight through lines of the table until the last line When rotating external knob anticlockwise highlight will move through lines to the upper line of the table 034 50 00 Appendix J page 148 Dec 17 2009 CH 4312 02 USER S MANUAL NRST2 page NRST2 NEAREST INTERSECTION page is used to overview nearest NP of flight plans inte
76. Russian note Arrival to WP with name UKKB in 120 Arriv at UKKB Ipa 8 UKKB seconds message is displayed when in 120s uepes 120 c following the flight plan Time left to start of course change Turn to 123 Kypc 123 procedure transfer to next way leg within 15s uepe3 15 c 155 034 50 00 Appendix J page 233 234 Dec 17 2009
77. SER S MANUAL View User Waypoint List Delete User Waypoint Figure J 6 46 Deletion of user NP To delete user NP a set highlight to the field of display of NP identifier b input identifier of user NP which must be deleted c press MENU button PAGE MENU window will appear on WPT10 page figure J 6 46 d set highlight to Delete User Waypoint field e press ENT f if user NP selected for deletion is used in none of flight plans created on the pages of FPL form DELETE WAYPOINT window with enquiry about deletion of selected NP will appear on WPT10 page figure J 6 47 In this case set highlight to Yes field press ENT to confirm deletion Selected NP will be deleted from user NP list WPT10 page will be displayed on RICU figure J 6 39 034 50 00 Appendix J page 140 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 47 g If user NP with selected for deletion is used at least in one of the flight plans created on the pages of FPL form DELETE WAYPOINT window with the message stating that selected navigation point can not be deleted will appear on WPT10 page figure J 6 48 Press ENT to refuse deletion Selected user NP will not be deleted from user NP list Figure J 6 48 Overview of user NP list To overview user NP list a press MENU button PAGE MENU window will appear on WPT10 page figure J 6 46 b set highlight to View User Waypoint List field c press ENT UDB list windo
78. U display will show FPL_rec window with WP input figure J 3 46 034 50 00 Appendix J page 92 Dec 17 2009 CH 4312 02 USER S MANUAL FLIGHT PLAN A 07 83 Figure J 3 46 f input all necessary WP g input flight plan name if necessary By default set flight plan name automatically identifier of initial WP identifier of final WP h press CRSR button RICU display will show FPL2 page Created flight plan will be added to a flight plan catalogue Flight plan deletion To delete a flight plan perform the following operations a set highlight on FPL2 page to the line with a flight plan which should be deleted b press MENU button c set highlight to Delete Flight Plan field in PAGE MENU pop up window figure J 3 42 034 50 00 Appendix J page 93 Dec 17 2009 CH 4312 02 USER S MANUAL d press ENT Pop up window with the enquiry to confirm highlighted flight plan deletion is displayed on RICU display figure J 3 47 Figure J 3 47 e press ENT to confirm deletion to refuse deletion press CLR button or set highlight to NO field and press ENT Deletion of all flight plans To delete all flight plans perform the following operations a set highlight to Delete All Flight Plans field in PAGE MENU pop up window figure J 3 42 6 press ENT Pop up window with the request to confirm deletion of all flight plans highlighted is displayed on RICU display figure J 3 48 Figure J 3 48 034 50
79. VER GNSS WITH RAM CLEANING IT IS NECESSARY TO SWITCH OFF AND THEN SWITCH ON RICU DEVICE S TEST field DEVICE S TEST field is used for DEVICE S TEST window call which is purposed for review of the information concerning availability unavailability of connection with external devices To call DEVICE S TEST window set highlight in DEVICE S TEST field Fig J 8 79 and press ENT To return on AUX4 page press CLR View of DEVICE S TEST window is given on Fig J 8 82 1 Devices antenna DME device VOR device SVS sensors IRS sensors 2 Availability YES unavailability NO of communication with the device Figure J 8 82 034 50 00 Appendix J page 222 Dec 17 2009 CH 4312 02 USER S MANUAL BACKGROUND TEST field BACKGROUND TEST field is used to FonTest1 and FonTest2 open windows with the results of background testing To activate FonTest1 window set highlight to BACKGROUND TEST field figure J 8 79 and press ENT To display second window of background testing results FonTest2 turn internal knob one position further To return to AUX4 page press CLR button View of FonTest1 and FonTest2 windows is shown in figure J 8 83 1 Functional assemblies of equipment 2 Result of background testing OK functional assembly is correct ERR functional assembly is erroneous WAIT sign of testing accomplishment 3 Serial number of equipment 4 Production date of equipment 5 Operating tim
80. a new point of a flight plan target point is stated Equipment enables to put a point in the queue for execution of a flight in DIRECT TO mode Entry into D form is eeomplished by pressing D button on RICU dtesplay View of D form is skown in figure J 4 1 Activate D PA 1 TP identifier 2 City TP name 3 Field of selection of TP from an active flight plan 4 Latitude longitude TP 5 Field of selection of TP from the list of nearest airports 6 Field of setting an angle of flyover of a target point 7 Field of activation confirmation can take on the following values Activate activate ENT DUPS message about availability of several points with set identifier name Figure J 4 1 034 50 00 Appendix J page 96 Dec 17 2009 CH 4312 02 USER S MANUAL Selection of a target point and setting a flight in DIRECT TO mode Selection of a target point and setting a flight in DIRECT TO mode is accomplished from D form by identifier or name with a possibility to create a new user NP by identifier from the list of WP of an active flight plan by identifier from the list of the nearest airports Target point can be also set from NAV FPL NRST WP forms After selection of a target point if necessary a required angle of flyover of target point can be set in CRS field see figure J 4 1 in this case a new DT is formed and it passes through target point with set angle of flyover of target point
81. about radiocommunication equipment Flight setting in DIRECT TO mode Figure J 1 14 page 2 of 3 034 50 00 Appendix J page 19 Dec 17 2009 CH 4312 02 USER S MANUAL NAVS page Display landing airport identifier identifier of selected TLR of landing airport graphic display of selected TLR of landing airport oriented by direction to north or by track angle deviation orthodromic from RW center line distance orthodromic from RW threshold bearing to airport from the current position distance to airport from the current position field SET ENT Selection of landing airport TLR selection True Nord DTK Figure J 1 14 page 3 of 3 034 50 00 Appendix J page 20 Dec 17 2009 CH 4312 02 USER S MANUAL Logical tree of FPL form FPL form FPL1 Active Flight Plan page Display flight plan name number of flight plans created and possible flight plans WPT identifiers parameters in interchangeable fields CUM DIS DTK ETA ETE ESA Window fpl_add WPT Selection aa ta ie sri Display of information about WPT vere Non Inclusion of standard way leg to flight plan Selection of standard way WPT removal from active flight plan Activate e Activate Leg Retarget To Point Copy Flight Plan Invert Flight Plan Delete Flight Plan Select Approach Select Arrival Select Departure Remove Arrival Remove Approach
82. about nearest NP of airport category NRST1 page 034 50 00 Appendix J page 150 Dec 17 2009 CH 4312 02 USER S MANUAL NRST4 page NRST4 NEAREST VOR page is used to overview nearest NP of omnidirectional USW beacons category View of NRST4 page is shown in figure J 7 4 NEAREST VOR m 1 Lines of table with parameters Reference designation of omnidirectional USW beacon Identifier of omnidirectional USW beacon Bearing to omnidirectional US W beacon from current position Distance to omnidirectional USW beacon from current position Frequency Figure J 7 4 Overview of information about nearest NP of omnidirectional USW beacons category Overview of information about nearest NP of omnidirectional USW beacons category is accomplished by analogy with overview of information about nearest NP of airport category NRST1 page 034 50 00 Appendix J page 151 Dec 17 2009 CH 4312 02 USER S MANUAL J 8 Operation description in AUX form AUX form is used to set parameters and activate manoeuvres to overview the information from navigation beacons to setup values of system parameters and to test equipment The form includes 4 pages a AUX1 page is used to select manoeuvres of the flight b AUX2 page is used to overview information from navigation beacons c AUX3 page is used to setup values of system parameters d AUX4 page is used to test equipment Entry to AUX form is accomplished by pre
83. activated setting a flight in DIRECT TO mode 034 50 00 Appendix J page 105 Dec 17 2009 CH 4312 02 USER S MANUAL J 6 Operation description in WP form WP form is intended to overview NDB information WP form contains 10 pages WPT1 WPT6 pages for overview of NP of airport category APT WPT7 page for overview of NP of flight plan intersection point category Intersection WPTS page for overview of NP of nondirectional beacons category NDB WPT9 page for overview of NP of omnidirectional USW beacons category VOR WPT10 page for work with NP of user WP category User WP Entry into WP form is accomplished by pressing the button WP on the front panel of RICU RICU display shows the form which was on RICU display prior to activation of WP form by repeated pressing WP button When entering WP form RICU display always shows WPT1 page Switching of the form WP pages is accomplished by rotating internal knob Note Jn the case of absence of the navigation database storage removable unit in RICU work with NP of user s category is available only The work with other NP categories is not available WPT1 page WPT1 page is used for overview of information about NP of airport category APT View of WPT1 page is shown in figure J 6 1 034 50 00 Appendix J page 106 Dec 17 2009 CH 4312 02 USER S MANUAL 1 Airport identifier 2 Reference designation of airport no informat
84. an further subroute of interrupted approach Empty field No reference designation Note Symbol indicates decade in reference designation of WP View of FPL1 page in case of absence of an active flight plan is shown in figure J 3 4 ACTIVE FLIGHT PLAN 000 144 Figure J 3 4 034 50 00 Appendix J page 64 Dec 17 2009 CH 4312 02 USER S MANUAL Active flight plan editing Active flight plan editing means execution of the following operations deletion of WP form a flight plan input of anew WP into a flight plan input of a leg of standard lane into a flight plan input and deletion of standard SID STAR APPROACH procedures by pressing MENU button WARNING 1 AFTER EACH ACTIVE ROUTE THE ACTIVE LEG OF ROUTE SHALL BE CONTROLLED AND THE REQUIRED LEG OF ROUTE SHALL BE ACTIVATED IF NECESSARY 2 AT SID PROCEDURE ENTERING REPLACING IN ACTIVE ROUTE THE REQUIRED LEG OF ROUTE SHALL BE ACTIVATED 3 AT APPROACH PROCEDURE ENTERING REPLACING WITH ACTIVE LAST LEG OF ROUTE THE REQUIRED LEG OF ROUTE SHALL BE ACTIVATED 4 IN THE CASE OF NECESSITY OF ARRIVAL AND APPROACH PROCEDURES ENTERING IN ROUTE THESE PROCEDURES SHALL BE ENTERED IN THE SEQUENCE AS FOLLOWS FIRST ENTER ARRIVAL PROCEDURE THEN APPROACH WP deletion from an active flight plan To delete WP from an active flight plan a set highlight to identifier of WP which should be deleted from a flight plan on FPL1 page b press C
85. and in AUTO SELECT and MAN SELECT fields selected type beacons list involved in NT solution Task of beacons selection mode The equipment supports three modes of beacons selection AUTO MANUAL TEST CTRL During activation the equipment is always in the beacons selection automatic mode In AUTO mode the first five beacons are automatically selected from the nearest beacons list corresponding to conditions as follows for beacons with T class Terminal the beacons coverage is given on Fig J 8 8 J 8 9 25 nm 12000 ft lt 1000 ft Se Figure J 8 8 034 50 00 Appendix J page 157 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 8 9 For beacons with L class low altitude beacons the beacons coverage is given on Fig J 8 10 J 8 11 40 nm 18000 ft 1000 ft en 7 ft Figure J 8 10 1000 SS SSS SSS SSeS es eee S28 Se Sees See eee Seer 4a LILLILILLILELTL LL LIL LL LILEL LL aan 500 EEE oO LA L LL EI RER sessi LE LE LL RE LL LL LEA LIL ees ee eee o 5 10 15 20 25 30 35 a Figure J 8 11 034 50 00 Appendix J page 158 Dec 17 2009 CH 4312 02 USER S MANUAL for beacons with H class high altitude beacons the beacons coverage U is given on Fig J 8 11 J 8 12 100 nm 60000 ft 130 nm 45000 gt 18000 gt 14500 1000 ft T N 40nm Figure J 8 12 MANUAL mode is purposed for the manual selection of one or two beacons mee
86. ast absence time CH 4312 02 USER S MANUAL Figure J 1 20 page 3 of 8 SUNRISE field ENT WPT selection for computation of sunrise and sunset time Setup date zone time amendments Computation of sunrise and sunset time for selected WPT NAVIGATION MODE field ENT Navigation data source selection used for complex NT solution GNSS sensor DME DME device VOR DME device Navigation data source selection used for complex NT solution from other RICU Figure J 1 20 page 4 of 8 034 50 00 Appendix J page 35 Dec 17 2009 displays option selection fields SETTINGS NEAREST CRITERIA BRIGHTNESS LIMIT DATA MAP SETTUP SEND USER DB 034 50 00 Appendix J page 36 Dec 17 2009 SETTINGS field NEAREST CRITERIA field BRIGHTNESS field CH 43 12 02 USER S MANUAL AUX3 page Setup measuring units equipment operation modes coordinate system CDI scale integrity signalling threshold magnetic declination consideration inclusion exclusion of GPS satellites from computation inclusion exclusion of GLON satellites from computation message language selection Setup number of nearest WPT displayed on pages of the form NRST type of surface of main TLR of airports displayed on page NRST1 minimum length of main TLR of airports displayed on page NRSTI Selection of highlight brightness setup
87. ation according to figure J 8 60 DISPLAY KEYBOARD 1 Setting of highlight brightness of display with the use of photosensor 2 Graphic chart of highlight brightness of display from photosensor illumination see figure J 8 61 Figure J 8 60 034 50 00 Appendix J page 203 Dec 17 2009 CH 4312 02 USER S MANUAL Display brightness Illumination 0 10 100 1000 JIk Figure J 8 61 Graphic chart of highlight brightness of display from photosensor illumination b turn internal knob one position further BRIGHTNESS window displays pop up window of selection of graphic chart of highlight brightness of display from photosensor illumination figure J 8 62 Figure J 8 62 034 50 00 Appendix J page 204 Dec 17 2009 CH 4312 02 USER S MANUAL d set highlight to the field of required line e press ENT to confirm setting of highlight brightness of display with the use of photosensor in accordance with selected line Setting of highlight brightness of display with the use of external voltage To set highlight brightness of display with the use of external voltage a set highlight to Board Power field figure J 8 58 b press ENT RICU display shows information according to figure J 8 63 KEYBOARD 1 Setting of highlight brightness of display with the use of external voltage 2 Type of control voltage Figure J 8 63 c turn internal knob one position further BRIGHTNESS window displays pop up
88. cision Vert Precision RAIM Available How Vis GNSS Sats How Work GNSS Sats Figure J 8 23 e set highlight in SELECT FIELD TYPE window to the parameter which must be displayed in DATA GNSS window instead of parameter being changed f press ENT to confirm change SELECT FIELD TYPE window will stop being displayed Selected parameter is displayed in DATA GNSS window in selected interchangeable field Mnemonic symbol of one of interchangeable fields is highlighted g perform similarly all required changes of interchangeable fields h press CLR button to exit from the mode of change of interchangeable fields Highlight of interchangeable filed will disappear Setup of interchangeable fields according to factory setting To setup interchangeable fields according to factory setting a set highlight to Restore Defaults field in PAGE MENU pop up window figure J 8 22 b press ENT c PAGE MENU pop up window will stop being displayed in DATA GNSS window DATA GNSS window will display interchangeable fields according to factory setting 034 50 00 Appendix J page 170 Dec 17 2009 CH 4312 02 USER S MANUAL Input of initial coordinates from NDB Input of initial coordinates can be accomplished only if data from GNSS sensor are not available To input initial coordinates from NDB a set highlight to Reference WP field in PAGE MENU pop up window figure J 8 22 b press ENT WPT1 window is displayed on RICU c set th
89. dix J page 198 Dec 17 2009 CH 4312 02 USER S MANUAL NEAREST CRITERIA field NEAREST CRITERIA field is used to activate NRSTCriteria window intended to set criteria of selection of nearest airports displayed in NRST form To activate NRSTCriteria window set highlight to NEAREST CRITERIA field figure J 8 40 and press ENT To return to AUX3 page press CLR button View of NEAREST CRITERIA window is shown in figure J 8 55 NEAREST CRITERIA NEAREST AIRPORT CRITERIA 1 Setting of number of nearest navigation NP displayed in the pages of the form NRST 2 Type of surface of the main RW of airports displayed in the page NRST1 3 Minimum length of the main RW of airports displayed in the page NRST1 Figure J 8 55 Setting of required number of nearest NP displayed in the pages of NRST form To set required number of nearest NP displayed in the pages of NRST form a set highlight to the field AMOUNT OF RECORDS b set the required number of NP c press ENT to confirm setting of required number of NP displayed in the pages of NRST form 034 50 00 Appendix J page 199 Dec 17 2009 CH 4312 02 USER S MANUAL Selection of type of RW surface of airports displayed in NRST form To select type of surface of the main RW of airports displayed in the form NRST a set highlight to RUNWAY SURFACE field figure J 8 55 b turn internal knob one position further NRSTCriteria window displays pop up window of selection of t
90. djustment 034 50 00 Appendix J page 32 Figure J 1 20 page 1 of 8 Dec 17 2009 pag CH 4312 02 USER S MANUAL DATA GNSS field ENT Input of initial coordinates date time MENU Change Fields Restore Defaults Reference WPT Text View SATs Graphics View SATs DATA SVS IRS WIND field Wind parameter input DATA VOR DME field Input of al I coordinates received by as initial G ones Figure J 1 20 page 2 of 8 034 50 00 Appendix J page 33 Dec 17 2009 CH 4312 02 USER S MANUAL PREDICTIVE RAIM field NP selection for RAIM computing Computing start time and date setup SETs field computation step angle of elevation Time and date setup of flight start according to a flight plan pacueta SETs field Setup Overview of In graphic view forecast results 034 50 00 Appendix J page 34 Dec 17 2009 integrity signalling threshold incl excl Into from biometric altitude calculation inc exl NSV from computation computation period angle of elevation inc excl NSV from computation TEXT field ENT Computation of forecast of RAIM function availability for NPT Computation of forecast of RAIM function availability for an active flight plan Display forecast date coordinates of WPT or active flight plan points forec
91. e d press ENT Possibility of detailed representation of selected types of air zones and reference designations of nearest navigation references will be activated deactivated in NAVI and NAV3 pages 034 50 00 Appendix J page 215 Dec 17 2009 CH 4312 02 USER S MANUAL COPY USER DB field COPY USER DB field is used to activate SEND USER DB window intended to copy user database of user NP flight plans to other RICU To activate SEND USER DB window set highlight to the field COPY USER DB TO BPIU2 figure J 8 40 and press ENT To return to AUX3 page press CLR button View of SEND USER DB window is shown in figure J 8 74 T FOR BEGIN ENTER WORD 1 Field of setting of copying of user database to other RICU Figure J 8 74 Copying of user database to other RICU When operating two sets of equipment it is necessary that databases were identical If two sets of equipment are installed in AC after switching on identity of user databases is automatically checked If databases are different than RICU display automatically shows message saying that databases are different In this case it is necessary to copy user data base with one RICU to another User database copying is recommended to make during preflight preparation To copy user database to other RICU a set highlight to the field of setting of copying of user database to other RICU 6 input OK value Copying of user database to other RICU takes place Display of tran
92. e 138 Dec 17 2009 CH 4312 02 USER S MANUAL Overview of information about user NP To overview information about user NP a set highlight to the field of display of NP identifier b input identifier of user NP which information it is necessary to overview Information about NP with input identifier is displayed in the fields of WPT10 page Editing of user NP To edit user NP a set highlight to the field of display of NP identifier b input identifier of user NP which information it is necessary to edit Information about NP with input identifier is displayed in the fields of WPT10 page Note If user NP with input identifier is used at least in one of the flight plans created on the pages of FPL form message used is displayed in right lower angle it is impossible to edit it c press ENT d set highlight to the field of user NP parameter which value it is necessary to change e set a new value of parameter f set highlight to the field of enquiry about change of user NP Modify g press ENT to confirm change of parameter Operations performed on WPT10 page when pressing MENU button PAGE MENU pop up window is displayed on WPT10 page when pressing MENU button figure J 6 46 its fields are used to perform the following operations overview of user NP list View User Waypoint List field deletion of user NP Delete User Waypoint field 034 50 00 Appendix J page 139 Dec 17 2009 CH 4312 02 U
93. e of equipment hours minutes Figure J 8 83 In case of normal background testing OK must be displayed in the fields of display of testing results in FonTest1 and FonTest2 windows Appearance of ERR signals about failure of a definite functional assembly of equipment 034 50 00 Appendix J page 223 Dec 17 2009 CH 4312 02 USER S MANUAL 10 TEST field TEST IO field is used to activate IO TEST window intended to test external devices To activate the window IO TEST set highlight to IO TEST field figure J 8 79 and press ENT To return to AUX4 page press CLR button View of IO TEST window is shown in figure J 8 84 1 Output one time order 2 Input one time order 3 Deviation from DT 4 Selected roll 5 Deviation from course 6 Deviation from glide path Note SETTING window is not used it is reserved for further application Figure J 8 84 Check of output one time orders To check output one time orders a set highlight to RK OUT field b activate output of one time orders in RK OUT field Activation of one time order see 034 50 00 Appendix A X2 connector of RICU is accomplished by setting 1 symbol in respective decade of RK_OUT field Rightmost symbol corresponds to one time order RKO_OUT leftmost symbol corresponds to one time order RK15_OUT c check availability of output of one time order to external devices in accordance with set one time orders in RK OUT field 034 50 00 Appendix J page 22
94. e page of the form WP which provides overview of WP which coordinates must be used as initial d input identifier of WP Press ENT Highlight will move to the DONE field e press ENT RICU displays DATA GNSS window with input coordinates from NDB and the sign of receipt of coordinates from NDB Setup of text view of satellites position To setup text view of satellites position a set highlight to Text View SATs field in PAGE MENU pop up window figure J 8 22 b press ENT DATA GNSS window is displayed on RICU according to figure J 8 24 1 Line of parameters of visible SV symbol of SNS or system of functional addition number of satellite number of character bearing of the place angle of elevation Figure J 8 24 034 50 00 Appendix J page 171 Dec 17 2009 CH 4312 02 USER S MANUAL Setup of graphic view of satellites position To setup graphic view of satellites position a set highlight to Graphics View SATs field in PAGE MENU pop up window figure J 8 22 b press ENT DATA GNSS window is displayed on RICU according to figure J 8 21 DATA SVS IRS WIND field DATA SVS IRS WIND field is used to activate DATA SVS IRS WIND window intended to display information from sensors of air parameters SVS course system IRS and also to indicate and input wind parameters To activate DATA SVS IRS WIND window set highlight on DATA SVS IRS WIND field figure J 8 5 and press ENT To return to AUX2 page press C
95. es minute part 4 Width of RW 5 Length of RW 6 Identifier and frequency of the main RW beacon 7 Identifier and frequency of the second RW beacon 8 Additional information about RW 9 Elevation of RW 10 Slope of RW 11 Bearing of RW 12 Distance from the beginning of RW to touchdown point 13 Altitude above RW threshold at the aircraft normal descent 14 Distance from RW edge to RW threshold Figure J 6 6 034 50 00 Appendix J page 111 Dec 17 2009 CH 4312 02 USER S MANUAL WPT3 page WPT3 page is used for overview of information about radiocommunication equipment of an airport View of WPT3 page is shown in figure J 6 7 ES 1 Airport identifier 2 List of radiocommunication equipment of airport 3 Service indicator 4 Number of radiocommunication equipment quantity of radiocommunication equipment of airport 5 Frequency 6 Mode of operation of radiocommunication equipment tx receiver rx transmitter not defined in database Figure J 6 7 List of radiocommunication equipment which can be available in an airport is shown in table J 2 2 values which service indicator can take on are shown in table J 2 3 034 50 00 Appendix J page 112 Dec 17 2009 CH 4312 02 USER S MANUAL Overview of radiocommunication equipment of airport For overview of information about radiocommunication equipment of airport fulfil the following actions a set highlight to the field of airport ident
96. flight with zero aircraft list at an angle 45 to DT additional turn for a smooth getting to DT 034 50 00 Appendix J page 11 Dec 17 2009 CH 4312 02 USER S MANUAL DTAe 6 change of flight plan legs at an angle of the turn gt 130 A turn start point B point on actual track C turn completion point D intermediate WPT DC new leg of a flight plan b semi width of airway LAT linear allowance of a turn R radius of turn circle AT angle of the turn AT DTAs DTAe N direction to the north DTAs desired track angle of the leg AD DTAe desired track angle of the leg DC Figure J 1 6 034 50 00 Appendix J page 12 Dec 17 2009 CH 4312 02 USER S MANUAL Graphic representation of parameters defined when executing the flight along DT is shown in figure J 1 7 WPT 2 NORTH direction to the north WPT1 WPT2 waypoints DT desired track DTK desired track desired track angle BRG bearing bearing to target point TRK track actual track angle DIS distance distance between current aircraft position and target point GS ground speed speed relative to ground XTK crosstrack error deviation from desired track Figure J 1 7 034 50 00 Appendix J page 13 Dec 17 2009 CH 4312 02 USER S MANUAL Diagrammatic display of the flight in DIRECT TO mode is shown in figures J 1 8 J 1 10 When executing the flight in DIRECT TO mode
97. from course c press ENT d check direct voltage on external device connected to RICU through the circuit of deviation from course Voltage must correspond to set value of the signal of deviation from course in E_k field from the calculation of 15 mV for 1 degree 034 50 00 Appendix J page 225 Dec 17 2009 CH 4312 02 USER S MANUAL Check of formation of deviation signal from glide path To check formation of signal of deviation from glide path a set highlight to E_g field b set value of deviation signal from glide path c press ENT d check direct voltage on external device connected to RICU through the circuit of deviation from glide path The voltage must correspond to set value of the signal of deviation from glide path in the field E_g from the calculation 15 mV for 1 degree KEYBOARD TEST field KEYBOARD TEST field is used to activate Keyboard Test window intended to accomplish keyboard test To activate the window Keyboard Test set highlight to KEYBOARD TEST field figure J 8 79 and press ENT button To return to AUX4 page press CRSR button and then ENT View of Keyboard Test window is shown in figure J 8 85 Exit test lt CRSR gt RN RNY D gt MEN AUX Figure J 8 85 Accomplish check of keyboard by pressing buttons of RICU keyboard in turn When pressing the button the field corresponding to pressed button will be highlighted on RICU display 034 50 00 Appendix J page 226 Dec
98. g Restore Defaults Figure J 3 41 Operations in FPL rec window by pressing MENU button are accomplished by analogy with respective operations described in FPL1 page 034 50 00 Appendix J page 89 Dec 17 2009 CH 4312 02 USER S MANUAL Operations being accomplished on FPL2 page by pressing MENU button PAGE MENU pop up window figure J 3 42 is displayed on FPL1 page by pressing MENU button its fields are used to accomplish the following operations flight plan activation Activate Flight Plan field flight plan reverse Invert Flight Plan field creation of a new flight plan Create New Flight Plan field copy of flight plan in memory Copy Flight Plan field flight plan deletion Delete Flight Plan field deletion of all flight plans Delete All Flight Plan field flight plans sorting by numbers and alphabet Sort List By Number or Sort List By Comment field Invert Flight Plan Create New Flight Plan Copy Flight Plan Delete Flight Plan Delete All Flight Plans Sort List By Comment Figure J 3 42 Flight plan activation To activate a flight plan a set highlight on FPL2 page to the field with a flight plan which should be activated b press MENU button c set highlight to the Activate Flight Plan field in PAGE MENU pop up window figure J 3 42 d press ENT RICU display will show FPL1 page which will contain information about selected flight plan with active f
99. g of CDI scale factor Setting of threshold of integrity signalling To set limit of integrity signalling a set highlight to numerical value of threshold of integrity signalling field THRESHOLD figure J 8 41 b turn internal knob one position further SETTING window displays the pop up window for threshold value selection of integrity signalling SELECT THRESHOLD figure J 8 49 Figure J 8 49 034 50 00 Appendix J page 194 Dec 17 2009 CH 4312 02 USER S MANUAL c set highlight to the field of display of required threshold of integrity signalling d press ENT to confirm input of selected threshold of integrity signalling The field THRESHOLD displays the sign of manual input of threshold of integrity signalling Activation of automatic setting of threshold of integrity signalling To activate automatic setting of threshold of integrity signalling a set highlight to the sign of automatic or manual setting of threshold of integrity signalling field THRESHOLD figure J 8 41 b turn internal knob one position further The window SETTINGS displays pop up window of selection of automatic or manual setting MODE figure J 8 50 Figure J 8 50 c set highlight to the sign AUTO d press ENT THRESHOLD field displays the sign n and numerical value of automatic setting of threshold of integrity signalling Activation deactivation of magnetic declination To activate deactivate magnetic declination registrat
100. geable fields adjusted by user 6 Scale of compass 7 Field of graphic display of a flight plan 8 Display field identifier of previous WP symbols when executing flights in DIRECT TO mode specified transit angle of target point when executing flight in OBS mode 9 Filed of display of maneuver type flight to a target point by route way P gt flight in DIRECT TO mode flight with achieving the point with specified course angle wy flight along the arc with fixed radius of a turn left turn ry flight along the arc with fixed radius of a turn right turn 10 Field of display of target point identifier 11 13 Range of scale of deviation from DT 12 Scale of deviation from DT Figure J 2 1 Figure J 2 1 shows factory setting of parameters displayed in interchangeable fields List of parameters which can be displayed in interchangeable fields 1 5 is stated in table J 2 1 034 50 00 Appendix J page 42 Dec 17 2009 CH 4312 02 USER S MANUAL Table J 2 1 Designation in Parameter form ATD Distance to TPon DT Sleft BRG Bearing to target point DIS Distance to target point CUM Total distance to flight destination point on desired track DTK Desired course angle ETA Target point arrival time ETE Flight time left to target point GS Ground speed TKE Turn angle difference between desired track angle and current track angle TRK Actual co
101. ght to mnemonic symbol of the parameter which must be changed d turn internal knob one position further SELECT FIELD TYPE pop up window is displayed on FPL1 page in accordance with J 3 36 if the interchangeable field position 9 10 is changed or in accordance with figure J 3 37 if the interchangeable field position 8 is changed figure J 3 1 CUM Cumitv Dist CUM Cumitv Dist DIS Leg Distance DIS Leg Distance DTK Desired Track DTK Desired Track ESA Enrte Safe Alt ETA Est Time Arvl ETA Est Time Arvl ETE ESE Time Enrte ETE Est Time Enrte ARP Airport ICAO Id ARP Airport ICAO Id Figure J 3 36 Figure J 3 37 e set highlight to required parameter f press ENT to confirm the change by required parameter SELECT FIELD TYPE window will stop being displayed on the FPL1 page Required parameter is displayed in selected interchangeable field 034 50 00 Appendix J page 84 Dec 17 2009 CH 4312 02 USER S MANUAL Setup of interchangeable fields according to factory setting To setup interchangeable fields in accordance with factory setting a set highlight to Restore Defaults field in PAGE MENU pop up window figure J 3 11 b press ENT c PAGE MENU pop up window will stop being displayed on FPL1 page Interchangeable fields in accordance with factory setting will be displayed on FPL1 page FPL2 page View of FPL2 page Flight Plan Catalog with flight plans available is shown in figure
102. ght to the parameter which value it is necessary to set b set required value of the parameter c press ENT to confirm input of set value of the parameter Note When calculating RAIM accessibility forecast for approaching stage set step of RAIM forecast calculation for 5 minutes Inclusion exclusion of barometric altitude into from calculation To include exclude barometric altitude into from calculation a set highlight on USE BALT field Fig J 8 32 b turn internal knob of shaft encoder one position further SETTINGS PRAIM window shall indicate the popup window for barometric altitude inclusion exclusion into from calculation Fig J 8 33 034 50 00 Appendix J page 180 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 8 33 c set highlight on YES field to include the barometric altitude into calculation NO to exclude d press ENT to confirm inclusion exclusion into from calculation Inclusion or exclusion of NSV from RAIM forecast calculation To include exclude NSV in from RAIM forecast calculation a set highlight to the field of activation of the list NSV GPS GLON figure J 8 32 b turn internal knob one position further The window SETTINGS PRAIM shows pop up window of inclusion exclusion of satellites GPS GLON from RAIM forecast calculation figure J 8 34 SAT SAT SAT SAT SAT SAT SAT SAT SAT SAT 24 USE USE USE USE USE USE USE USE USE USE Figure J 8
103. ghting to display field of airport identifier Select necessary landing airport RW Press ENT Highlighting will move to Done field Note Jf it is required to overview parameters of selected RW set the highlighting to Detailed field and press ENT RUNWAIT DETAILED window is displayed on RICU display To quit RUNWAIT DETAILED window press CLR or CLRS button h press ENT SELECT ARP AND RW window in which information about selected landing airport RW is shown is displayed on RICU display Field of the command of confirmation of landing airport and RW selection 034 50 00 Appendix J page 59 Dec 17 2009 CH 4312 02 USER S MANUAL i press ENT NAVS window in which values of deviation from RW axis and distance to RW end and graphic representation of selected RW of landing airport are displayed is displayed on RICU display Operations performed on NAVS page when pressing MENU button PAGE MENU pop up window figure J 2 18 which fields are used to perform the following operations setup of RW orientation to north True Nord field setup of RW orientation by course angle DTK field scale automatic change activation Autozoom field route view View Route field is displayed on NAVS page by pressing MENU button Note Viet Route fields are not used Figure J 2 18 Setup of RW orientation For setup of RW orientation a in PAGE MENU pop up window figure J 2 18 set the highlighting to the field Tr
104. her DEP pop up window is displayed on WPT4 page Set highlight to name of required procedure figure J 3 29 Figure J 3 29 e press ENT Name of selected procedure is displayed in DEP field If there are several RW for selected procedure then highlight will move to RUNWAY field Turn internal knob one position further RUNWAY pop up window is displayed on the WPT4 page figure J 3 30 Figure J 3 30 034 50 00 Appendix J page 80 Dec 17 2009 CH 4312 02 USER S MANUAL f select a required RW Press ENT If selected procedure has only one transit point then highlight will at once move to the field Load name of a transit point is automatically displayed in TRANS field figure J 3 31 If selected procedure has several transit points then highlight will move to TRANS field Select a required transit point and press ENT Highlight will move to the field Load figure J 3 31 Selection of a transit point is accomplished by analogy with selection procedure name Figure J 3 31 g press ENT FPL1 page in which points of selected departure procedure Departure are included in a flight plan will appear on RICU display Initial point identifier of input procedure Departure figure J 3 32 is displayed in the field of flight plan name in the place of initial WP identifier If departure procedure was earlier input in a flight plan then it will be deleted from the flight plan ACTIVE FLIGHT PLAN 011 133 ACTIVE FLIGHT PLAN 61
105. hrough decades of parameter display field and fixing necessary value of the symbol by rotating internal knob of the handle set necessary value of parameter being input edited to confirm parameter input press ENT or move highlight by rotating external knob of the handle clockwise beyond the range of display field of parameter being input edited NOTE 1 If symbol _ is displeyed in display field of symbol being input edited then when inputing editing parameter when rotating internal knob of the handle clockwise letters from A to Z figures form 0 to 9 symbol if first symbol of parameter is being input edited symbol _ if subsequent symbols of parameter are being input edited are displayed serially 034 50 00 Appendix J page 8 Dec 17 2009 CH 4312 02 USER S MANUAL when rotating internal knob of the handle counterclockwise symbol if first symbol of parameter is being input edited symbol _ if subsequent symbols of parameter are being input edited figures form 9 to 0 letters from Z to A are displayed serially 2 If symbol different from symbol _ is displaeyd in display field of symbol being input edited then when inputing editing parameter display of symbols starts with symbol displayed before beginning of input editing To input parameters with a line of specified values set highlight to display field of parameter which value it is neces
106. ifier Input identifier of airport which radiocommunication equipment information it is necessary to overview b press ENT Highlight will move to the field of display of information about radiocommunication equipment of airport By rotating internal knob clockwise highlight will move through lines until the last line of the field By rotating internal knob anticlockwise highlight will move through lines until the upper line of the field figure J 6 8 Figure J 6 8 034 50 00 Appendix J page 113 Dec 17 2009 CH 4312 02 USER S MANUAL WPT4 page WPT4 page is used for overview of procedures SID View of WPT4 page is shown in figure J 6 9 1 Airport identifier 2 Field of graphic display of SID procedure 3 Scale 4 Name of SID procedure 5 Name of RW 6 Name of transit point Figure J 6 9 Overview of SID procedure To overview SID procedure of an airport perform the following operations a set highlight to the field of airport identifier Input identifier of airport which SID procedure information it is required to overview b press ENT Highlight will move to DEP field figure J 6 10 034 50 00 Appendix J page 114 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 10 c turn internal knob one position further WPT4 page displays DEP pop up window Set highlight to name of the required procedure figure J 6 11 Figure J 6 11 d press ENT DEP field displays name of selected proced
107. intended for transition to nearest WP form from database Repeated pressing of the button NRST returns the form which was before activation of the form NRST 034 50 00 Appendix J page 2 Dec 17 2009 CH 4312 02 USER S MANUAL OBS Button OBS Button is used for setting flight in OBS mode outlet to WP with desired transit angle When accomplishing flight in OBS mode signal highlight of the button OBS is being switched on After flight cancellation in OBS mode background highlight of the button is being switched on By pressing OBS button with indication in status line SUSP interruption of automatic changeover to next leg of flight plan and transition to repeated flight of waiting area for procedure STAR approach to second circle for procedure APPROACH are being accomplished Note SUSP request for interruption of automatic changeover to next leg of flight plan when executing procedures STAR or APPROACH MSG Button MSG Button is intended for display output of system messages and messages about mating equipment operation When a message is output signal highlight of the MSG button is turned on If several messages signal highlight of the MSG button will blink until the last message is read After all messages are read background highlight of the MSG button is switched on NAV Button NAV is Button intended for transition to navigation form This form is main one for equipment therefore repeated pressing of the NAV b
108. ion a set highlight to the field of display of activation deactivation of magnetic declination field MAG figure J 8 41 b turn internal knob one position further SETTING window displays the pop up window of activation deactivation of magnetic declination registration SELECT figure J 8 51 034 50 00 Appendix J page 195 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 8 51 c set highlight to the field ON to activate magnetic declination registration OFF to deactivate magnetic declination registration d press ENT to confirm or cancel magnetic declination registration Inclusion exclusion of satellites GPS from calculation To include exclude satellites GPS from calculation a set highlight to the field of inclusion exclusion of satellites GPS from calculation USE SATs GPS field figure J 8 41 b turn internal knob one position further SETTING window displays pop up window of inclusion exclusion of satellites GPS from calculation of USE SATs GPS figure J 8 52 SAT Ol USE USE USE USE USE USE USE USE USE USE Figure J 8 52 034 50 00 Appendix J page 196 Dec 17 2009 CH 4312 02 USER S MANUAL c set highlight to the field with number of satellite which should be included excluded from calculation Turn internal knob one position further USE to include satellite in calculation OFF to exclude satellite from calculation d press ENT to confirm inclusion exc
109. ion about RW surface R private airport II a airport with soft RW surface 0 airport with hard RW surface water 3 Airport category It can take on the following values CIVIL civil MILITARY military PRIVATE private category is not defined 4 Airport name 5 Country region where airport is located 6 Earth region where airport is located 7 Latitude longitude of airport 8 Symbol of current position of AC 9 Airport altitude 10 Length of the longest RW of airport 11 Bearing to airport from current position 12 Distance to airport from current position Figure J 6 1 034 50 00 Appendix J page 107 Dec 17 2009 CH 4312 02 USER S MANUAL Overview of airport information For overview of airport information a set highlight to the field of airport identifier name b input identifier name of a required airport c press ENT to confirm input Information about airport with selected identifier name is displayed in fields of the pages WPT1 WPT6 WPT2 page WPT2 page is used for overview of information about airport RW View of WPT2 page with information about airport RW is shown in figure J 6 2 View of WPT2 page without information about airport RW is shown in figure J 6 3 Detailed 1 Airport identifier 2 Graphic representation of all RW and reference point of airport RW selected in the field RUNWAY is displayed in green colour others are in grey colour
110. kilohertz Special symbols used m degrees with magnetic declination r true degrees without magnetic declination N northern latitude S southern latitude E eastern longitude W western longitude a NT category airport APT v NT category omnidirectional USW beacons VOR n NT category nondirectional radio beacon NDB i NT category flight plans intersection Intersection u NT category user waypoints User WP _ symbol filling parameter display if parameter to be computed in process of navigation task solving but solution is absent search of NP to be accomplished by identifier or name for indication of identifier decades name and region 034 50 00 Abbreviation list page 2 Dec 17 2009 CH 4312 02 USER S MANUAL Glossary Activate Flight Plan flight plan activation Activate Leg leg activation Activate flight plan activation Autozoom switching on automatic zoom of graphic flight plan image Change Fields change field selection Closest Point of FPL creation of WP on DT at minimum distance from WP chosen Copy Flight Plan copy of flight plan to memory Create New Flight Plan creation of a new flight plan Delete All Flight Plan deletion of all flight plans Delete All User Waypoint deletion of all NP of User WP category Delete Flight Plan deletion of a flight plan Delete Navaid navaid deletion Delete User Waypoint deletion of user WP User WP
111. lected line Setting of brightness of keyboard with the use of external voltage To set highlight brightness of keyboard with the use of external voltage a set highlight to Board Power line figure J 8 58 b press ENT RICU display shows information in accordance with figure J 8 69 034 50 00 Appendix J page 209 Dec 17 2009 CH 4312 02 USER S MANUAL DISPLAY fa KEYBOARD 1 Setting of highlight brightness of keyboard with the use of external voltage 2 Type of control voltage Figure J 8 69 c turn internal knob one position further BRIGHTNESS window displays pop up window of selection of type of control voltage figure J 8 70 Figure J 8 70 d set highlight to the field with required type of control voltage e press ENT to confirm selected type of control voltage 034 50 00 Appendix J page 210 Dec 17 2009 CH 4312 02 USER S MANUAL LIMIT DATA field LIMIT DATA field is used to activate LIMIT DATA window intended to set parameters of standard procedure calculation SID STAR APPROACH and to set limit values of angle of list To activate LIMIT DATA window set highlight to the field LIMIT DATA figure J 8 40 and press ENT To return to AUX3 page press CLR button View of LIMIT DATA window is shown in figure J 8 71 1 2 3 Lines with parameters for SID STAR APPROACH procedures calculation aircraft average speed SPEED field maximum angle of list BANK field gradient of al
112. light brightness of display MODE figure J 8 58 034 50 00 Appendix J page 201 Dec 17 2009 CH 4312 02 USER S MANUAL 1 Factory setting of highlight brightness of display 2 Manual setting of highlight brightness of display 3 Setting of highlight brightness of display with the use of photo sensor 4 Setting of highlight brightness of display with the use of external voltage Figure J 8 58 Factory setting of highlight brightness of display For factory setting of highlight brightness of display a set highlight to Default field figure J 8 58 b press ENT to confirm factory setting of highlight brightness of display Manual setting of highlight brightness of display For manual setting of highlight brightness of display a set highlight to the field Manual figure J 8 58 b press ENT RICU display shows information according to figure J 8 59 034 50 00 Appendix J page 202 Dec 17 2009 CH 4312 02 USER S MANUAL DISPLAY DES agg KEYBOARD 1 Manual mode of setting of highlight brightness of display 2 Brightness level Figure J 8 59 c by rotating internal knob set required brightness level of display light d press ENT to confirm set brightness level of display light Setting of highlight brightness of display with the use of photosensor To set highlight brightness of display with the use of photosensor a set highlight to FotoSensor field figure J 8 58 b press ENT RICU display shows inform
113. light plan leg stated 034 50 00 Appendix J page 90 Dec 17 2009 CH 4312 02 USER S MANUAL Flight plan reverse For flight plan reverse a set highlight on FPL2 page to the field with a flight plan which should be reversed b press MENU button c set highlight to Invert Flight Plan field in PAGE MENU pop up window figure J 3 42 d press ENT Identifiers of initial and final waypoint will swap in the field of selected flight plan on FPL2 page and the sign of a reverse flight plan rev will appear if flight plan name is automatic figure J 3 43 If input of a flight plan name is manual no changes in the field of flight plan name will occur FLIGHT PLAN CATALOG A 03 87 Figure J 3 43 Creation of a new flight plan To create a new flight plan a set highlight to Create New Flight Plan field in PAGE MENU pop up window figure J 3 42 b press ENT RICU display will show FPL_ree window with number of a flight plan being created figure J 3 44 034 50 00 Appendix J page 91 Dec 17 2009 CH 4312 02 USER S MANUAL FLIGHT PLAN A 06 84 Figure J 3 44 c turn internal knob one position further RICU display will show fpl_add window in accordance with figure J 3 45 WAYPOINT INFORMATION Figure J 3 45 d input identifier of WP Input of identifier is accomplished by analogy with described in FPL1 page input of a new WP in a flight plan e after confirmation of the input RIC
114. lusion of satellites GPS from calculation Inclusion exclusion of satellites GLONASS from calculation To include exclude satellites GLONASS from calculation a set highlight to the field of inclusion exclusion of satellites GLONASS from calculation USE SATs GLON field figure J 8 41 b turn internal knob one position further SETTINGS window displays pop up window of inclusion exclusion of GLONASS satellites from calculation of USE SATs GLON figure J 8 53 SAT O1 USE SAT USE SAT USE SAT USE SAT USE SAT USE SAT USE SAT USE SAT USE SAT USE Figure J 8 53 c set highlight to the field with number of satellite which should be included excluded from calculation Turn internal knob one position further USE to include satellite in calculation OFF to exclude satellite from calculation d press ENT to confirm inclusion exclusion of satellites from calculation 034 50 00 Appendix J page 197 Dec 17 2009 CH 4312 02 USER S MANUAL Language of messages To select language of messages a set highlight to the field of display of messages language LANGUAGE field figure J 8 41 b turn internal knob one position further The window SETTING displays pop up window of language selection of SETTING LANGUAGE messages figure J 8 54 Figure 8 54 c set highlight to the field of display of required message language d press ENT to confirm setting of a selected language of messages 034 50 00 Appen
115. me date 034 50 00 Appendix J page 168 Dec 17 2009 CH 4312 02 USER S MANUAL Operations being accomplished in DATA GNSS window by pressing MENU button PAGE MENU pop up menu is displayed in DATA GNSS window by pressing MENU button figure J 8 22 its fields are used to perform the following operations setup of interchangeable fields Change Fields field adjustment of interchangeable fields according to factory setting Restore Defaults field input of initial coordinates from NDB Reference WP field setup of text view of satellites position Text View SATs field setup of graphic view of satellites position Graphics View SATs field 4 Restore Defaults Reference WPT Text View SATS Graphics View SATS Figure J 8 22 Setup of interchangeable fields To setup interchangeable fields perform the following steps a set highlight to Change Fields field in PAGE MENU pop up window figure J 8 22 b press ENT PAGE MENU window will stop being displayed in DATA GNSS window Mnemonic symbol of one of interchangeable fields is highlighted c set highlight to the interchangeable field of the parameter which must be changed d turn internal knob one position further SELECT FIELD TYPE window is displayed in DATA GNSS window figure J 8 23 034 50 00 Appendix J page 169 Dec 17 2009 CH 4312 02 USER S MANUAL HIL Horiz Integr Limit VIL Vert Integr Limit HDOP Horiz DOP VDOP Vert DOP Pre
116. n can not be accomplished if SID STAR APPROACH procedures are available in a flight plan You should delete this procedure before reverse 2 To return to initial direction of a flight plan it is necessary to reverse a flight plan again Flight plan deletion To delete a flight plan a set the highlighting on Delete Flight Plan field in PAGE MENU pop up window figure J 3 11 b press ENT Information about a flight plan will stop being displayed on the page figure J 3 4 Selection of standard APPROACH procedure To select approach procedure a set the highlighting on Select Approach field in PAGE MENU pop up window figure J 3 11 b press ENT Page of selection of WPT6 approach procedure will appear on RICU display Identifier of final WP is displayed in the field of WP identifier figure J 3 20 If final WP is not an airport or an airport of arrival set identifier of arrival airport in the field of airport identifier Load Activate Figure J 3 20 c press ENT Highlight will move to the field of APPROACH procedure d turn internal knob one position further APPROACH pop up window is displayed on WPT6 page Set highlight to the name of required procedure figure J 3 21 034 50 00 Appendix J page 75 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 3 21 e press ENT Name of selected procedure is displayed in APPROACH field If selected procedure has only one transit point then highlight will at
117. ncy 034 50 00 Appendix J page 54 Dec 17 2009 CH 4312 02 USER S MANUAL Continuation of Table J 2 2 Symbol STEN Airport and Connec Both in Symbol in the Radiocommunication Description heliports tion on types of ARINC form equipment the commu 424 connection route nication INF Information Information Information X MUL Multicom Multicom Multicom X OPS Operations Operations Operations X RDO Radio Radio Radio X RDR Radar Radar Radar X RFS RFSS Remote Flight Service Remote Flight X Station RFSS Service Station RMP RampTaxiCntr Ramp Taxi Control Ramp Taxi X Control RSA ARSA Airport Radar Service Airport Radar X Area ARSA Service Area ARSA TCA TCA Terminal Control Area Terminal Control X TCA Area TMA TMA Terminal Control Area Terminal Control X TMA Area TML Terminal Terminal Terminal X TRS TRSA Terminal Radar Service Terminal Radar X Area TRSA Service Area TWE TWEB Transcriber Weather Transcriber X Broadcast TWEB Weather Broadcast TWR TowerATCtrl Tower Air Traffic Tower Air Traffic X Control Control UAC UpAreaCtrl Upper Area Control Upper Area X Control UNI Unicom Unicom Unicom X VOL Volmet Volmet Volmet X Note Availability of respective communication type for radiocommunication equipment of airport is marked by symbol X Table J 2 3 034 50 00 Appendix J page 5
118. ndication at the value to 999 m is 1 m Figure J 2 14 034 50 00 Appendix J page 57 Dec 17 2009 CH 4312 02 USER S MANUAL If scale is not more than 15 miles inclusive RW is displayed in the form of pointer which wide end defines the end of RW If scale is more than 15 miles airport symbol is displayed instead of RW Overview of values of deviation from RW axis distance to RW end For overview of values of deviation from RW axis distance to RW end a set highlight to command of landing airport and RW selection figure J 2 14 b press ENT Window SELECT ARP AND RW is displayed on RICU display figure J 2 15 1 Landing airport identifier 2 RW identifier 3 Landing airport coordinates 4 RW course 5 RW length 6 Command of confirmation of landing airport and RW selection Figure J 2 15 c turn internal knob one position to the right or left Page WPT1 is displayed on RICU display figure 2 16 034 50 00 Appendix J page 58 Dec 17 2009 CH 4312 02 USER S MANUAL Figure 2 16 d set highlight to display field of airport identifier Input landing airport identifier Press ENT Highlight will move to Done field e press ENT SELECT ARP AND RW window in which the field of airport RW identifier is highlighted is displayed on RICU display f turn internal knob one position to the right or left Page WPT2 is displayed on RICU display figure 2 17 Detailed Figure 2 17 g set the highli
119. ndix J page 69 Dec 17 2009 CH 4312 02 USER S MANUAL creation of WP on DT in minimum distance from selected WP Closest Point of FPL field setting of interchangeable fields Change Fields field setting of interchangeable fields in accordance with factory setting Restore Defaults field Activate Activate Leg Copy Flight Plan Invert Flight Plan Delete Flight Plan Select Approach Select Arrival Select Departure Flight plan activation To activate a flight plan Figure J 3 11 Delete Flight Plan Select Approach Select Arrival Select Departure Change Fields Restore Defaults a set the highlighting on Activate field in PAGE MENU pop up window figure J 3 11 b press ENT button Pop up window with the enquiry about flight plan activation is displayed on RICU display figure J 3 12 034 50 00 Appendix J page 70 Dec 17 2009 Figure J 3 12 CH 4312 02 USER S MANUAL c press ENT After pressing ENT flight plan is activated target point is stated and all calculations under a flight plan are done figure J 3 13 ACTIVE FLIGHT PLAN 604 140 Figure J 3 13 Flight plan leg activation To activate a flight plan leg a set the highlighting on FPL1 page to a final WP of a flight plan leg which should be activated b press MENU button c set highlight to field Activate Leg in pop up menu PAGE MENU PAGE MENU figure J 3 11 d press ENT Pop
120. nearest LES flight plans intersection points in DIRECT TO mode a Flight setting Figure J 1 19 page 1 of 2 034 50 00 Appendix J page 30 Dec 17 2009 CH 4312 02 USER S MANUAL NRST 3 page NEAREST NDB Display of information about nearest nondirectional radiobeacons identifier bearing distance frequency Overview of information about nearest nondirectional radiobeacons Flight setting in DIRECT TO mode NRST4 page NEAREST VOR Display of information about nearest omnidirectional radiobeacons identifier bearing distance frequency Overview of information about nearest omnidirectional radiobeacons Flight setting in DIRECT TO mode Figure J 1 19 page 2 of 2 034 50 00 Appendix J page 31 Dec 17 2009 CH 4312 02 USER S MANUAL Logical tree of AUX form AUX form AUXI page Display of option OFFSET selection field OFFSET field ENT Displacement direction and value setting On off mode of flight on parallel flight plan AUX2 page Display of option selection fields TUNE VOR DME DATA GNSS DATA SVS IRS WIND DATA VOR DME DATA BPIU2 PREDICTIVE RAIM SUNRISE NAVIGATION MODE TUNE VOR DME field Beacons involved in selected NT solution review Beacon type selection mode setting Select Navaid Delete Navaid Set Info for Navaid TEST CTRL VOR DME a
121. o MANUAL window Press ENT d set highlight to the manually selected beacons list on identifier of the beacon subject to deletion from the list e press MENU button Tune VOR DME window shall indicate PAGE MENU popup window Fig J 8 14 f set highlight to Delete Navaid field Press ENT and the selected beacon shall be deleted from the manually selected beacons list 034 50 00 Appendix J page 162 Dec 17 2009 CH 4312 02 USER S MANUAL Selection of the beacon the distance to which shall be indicated on DME device indicator a set highlight to the beacons selection mode field b turn internal knob of shaft encoder one position further Tune VOR DME window shall indicate MODE popup window Figure J 8 13 c set highlight to the required mode field AUTO or MANUAL Press ENT d set highlight to the beacons list AUTO SELECT or MAN SELECT on identifier of the beacon the distance to which shall be indicated on DME device indicator e press MENU Tune VOR DME shall indicate PAGE MENU popup window Fig J 8 14 d set highlight to Set Info for Navaid field Press ENT DME device indicator shall indicate the distance to the selected beacon I sign shall be indicated in the selected beacon line on RICU display DME VOR devices tuning in TEST CTRL mode For DME VOR devices tuning in TEST CTRL mode a set highlight to the beacons selection mode field b turn internal knob of shaft encoder one position further T
122. o selected target point RICU display will show the page NAV1 with information about the flight to selected point in DIRECT TO mode Information about flight in DIRECT TO mode to selected target point is displayed in the field of flight plan name on FPL1 page figure J 3 2 Selection of a target point and setting a flight in DIRECT TO mode from NAV FPL NRST WP forms To set a flight in DIRECT TO mode from NAV1 and NAV2 mode a press the button D RICU display will show the form D Data of a target point current WP are displayed in informational fields b activate the flight to target point in DIRECT TO mode set highlight to the field Activate and press ENT RICU display will show NAVI page which represents the flight in DIRECT TO mode Information about flight in DIRECT TO mode to target point is displayed in the field of flight plan name on FPL1 page figure J 3 2 034 50 00 Appendix J page 100 Dec 17 2009 CH 4312 02 USER S MANUAL To select a target point and set a flight in DIRECT TO mode from the forms FPL NRST WP a set highlight to identifier of WP which should be used as TP b press the button D RICU display shows the form gt its informational fields displays data of selected TP c activate flight to selected target point set highlight to the field Activate and press ENT RICU display shows NAV1 window representing flight in DIRECT TO mode to selected TP Queuing of second target point If a
123. once move to Load field name of transit point is automatically displayed in TRANS field figure J 3 22 If selected procedure has several transit points then highlight will move to TRANS field Select necessary transit point and press ENT Selection of transit point is accomplished by analogy with selection of procedure name Activate Figure J 3 22 f press ENT Page FPL1 in which points of selected APPROACH procedure are included in a flight plan is displayed on RICU Identifier of final point of input APPROACH procedure is displayed in the field of flight plan name on the place of identifier of final WP figure J 3 23 If procedures of arrival and approach were earlier included in a flight plan they will be deleted from a flight plan if approach procedure is set for another airport If approach 034 50 00 Appendix J page 76 Dec 17 2009 CH 4312 02 USER S MANUAL procedure is set for the same airport then only approach procedure set earlier will be deleted and arrival procedure set earlier will remain in a flight plan of Approach I10R 1 Flight plan points 2 Title of APPROACH procedure 3 Points of APPROACH procedure 4 Name of the airport on which APPROACH procedure is set ACTIVE FLIGHT PLAN 611 133 ACTIVE FLIGHT PLAN 611 133 Figure J 3 23 Selection of standard ARRIVAL procedure To select arrival procedure a set the highlighting on Select Arrival field in PAGE MENU pop up window figure J 3 11
124. page of respective form closure of pop up window PAGE MENU 034 50 00 Appendix J page 4 Dec 17 2009 CH 4312 02 USER S MANUAL ENT Button Button ENT is intended for confirmation of information input confirmation of action accomplishment or for moving highlight to next editing parameter CRSR button CRS Button is located on the internal knob end of handle and is used for activation deactivation of parameter display field in window or form page refusal to edit return from window to page of respective form closure of pop up window PAGE MENU Function of the CRSR button is accomplished by pressing the internal knob end of handle Background highlight of control buttons is constantly switched on Handle Handle consists of two rotary knobs external and internal External knob is intended for editing element selection moving highlight on pop up windows Internal knob is used for page flipping in the form and for search within editing element Function of the CRSR button is accomplished by pressing the internal knob end of handle 034 50 00 Appendix J page 5 Dec 17 2009 CH 4312 02 USER S MANUAL Information presentation on RICU display All navigation parameters information and function being executed necessary for equipment operation are joined in forms and displayed on pages and windows of the forms on RICU Example of the page displayed is shown in the figure NOTE PARAMETERS VALUES IN FORMS STATED BELOW ARE
125. plays pop up window of selection of SETTING DATUM system of coordinates figure J 8 45 Figure J 8 45 c set highlight to the field of display of required system of coordinates d press ENT to confirm setting of required system of coordinates Setting of CDI scale factor To set CDI scale factor a set highlight to numerical value of CDI scale factor CDI field figure J 8 41 b turn internal knob one position further SETTINGS window displays pop up window of selection of scale CDI factor value SELECT CDI figure J 8 46 034 50 00 Appendix J page 192 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 8 46 c set highlight to the field of display of required CDI scale factor d press ENT to confirm input of selected CDI scale factor The CDI field displays sign of manual input of CDI scale factor MANUAL figure J 8 47 Figure J 8 47 Activation of automatic setting of CDI scale factor To activate automatic setting of CDI scale factor a set highlight to the sign of automatic or manual setting of CDI scale factor CDI field figure J 8 41 b turn internal knob one position further SETTING window displays the pop up window of selection of automatic or manual setting MODE figure J 8 48 034 50 00 Appendix J page 193 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 8 48 c set highlight to the sign AUTO d press ENT CDI field displays the sign and numerical value of automatic settin
126. procedure Zoom of graphic display of STAR procedure is accomplished by analogy with zoom graphic display of SID procedure see description of WPT4 page WPT6 page WPT6 page is used for oveview of APPROACH procedure View of WPT6 page is shown in figure J 6 29 1 Airport identifier 2 Field of graphic display of APPROACH procedure 3 Scale 4 Name of current APPROACH procedure 5 Name of transit point Figure J 6 29 034 50 00 Appendix J page 124 Dec 17 2009 CH 4312 02 USER S MANUAL Overview of APPROACH procedure To overview APPROACH procedures of an airport perform the following operations a set highlight to the field of airport identifier Input identifier of airport which APPROACH procedure information it is necessary to overview b press ENT Highlight will move to the field of current APPROACH procedure figure J 6 30 Figure J 6 30 c turn internal knob one position further WPT6 page displays APPROACH window Set highlight to the name of required procedure figure J 6 31 Figure J 6 31 d press ENT APPROACH field displays the name of selected procedure Highlight will move to the field of transit point name figure J 6 32 034 50 00 Appendix J page 125 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 32 e turn internal knob one position further WPT6 page displays TRANS pop up window Set highlight to the name of required transit point figure J 6 33 Figure J 6 33
127. r of the point standing in user NP list after the point which had to be renamed will be highlighted Figure J 6 54 Deletion of all user NP from UDB list window by pressing MENU window To delete all user NP a press MENU button RICU display will show PAGE MENU pop up window figure J 6 55 Delete ATI User Waypoints Figure J 6 55 b press ENT button RICU display will show DELETE ALL WAYPOINT pop up window containing a request to delete all user NP figure J 6 56 034 50 00 Appendix J page 145 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 56 c set highlight to Yes field and press ENT button to confirm deletion All user NP which are not used at least in one of flight plans created on the pages of FPL form will be deleted from the list RICU display will show WPT10 page 034 50 00 Appendix J page 146 Dec 17 2009 CH 4312 02 USER S MANUAL J 7 Operation description in NRST form NRST form is used to overview information about nearest navigation points Bearing and distance from current position to nearest navigation points are displayed in this form NRST form contains 4 pages NRST1 page NEAREST ARP is used to overview nearest NP of airport category NRST2 page NEAREST INTERSECTION is used to overview nearest NP of flight plans intersection points category NRST3 page NEAREST NDB is used to overview nearest NP of nondirectional radio beacons category N
128. resentation of a flight plan and navigation references airports and beacons The NAV form contains five pages a NAV1 page is used for display of navigation parameters graphic representation of a flight plan b NAV2 page is used for display of navigation parameters current coordinates altitude UTC time and date c NAV3 page is used for display of graphic representation of a flight plan d NAV4 page is used for display of frequency information of radio communication equipment of the nearest airport e NAVS page is used for display deviation orthodromic from RW center line distance orthodromic from RW threshold bearing to RW threshold from the current position of aircraft distance to RW threshold from the current position of aircraft graphic representation of selected RW of landing airport information about selected RW of landing airport Entry in NAV form is accomplished automatically after power up after pressing NAV button on RICU automatically after flight setting in DIRECT ON mode When entering NAV form NAVI page is always displayed on RICU Switching of NAV form pages is executed by rotating an internal knob 034 50 00 Appendix J page 41 Dec 17 2009 CH 4312 02 USER S MANUAL NAVI page NAVI page is used for display of information which is necessary for AC control when moving according to a flight plan NAVI page view is shown in figure J 2 1 1 5 Interchan
129. ress ENT Page according to figure J 3 8 is displayed on RICU display WAYPOINT INFORMATION ACCEPT Figure J 3 8 press ENT to confirm input of a new WP FPL1 page in which a new WP is included in a flight plan is displayed on RICU display d if highlighted WP is included at least in one of standard lanes then FPL correction pop up window is displayed in FPL1 page figure J 3 9 Identifiers of standard lanes which contain WP highlighted are displayed in FPL correction window 034 50 00 Appendix J page 67 Dec 17 2009 CH 4312 02 USER S MANUAL figure J 3 9 In this case to input WP press ENT when Insert WP field is highlighted Window fpl_add is displayed on RICU display figure J 3 6 input anew WP ina flight plan in a way described above Input of a leg of standard lane in an active flight plan To input a leg of standard lane in an active flight plan a set highlight on FPL1 page to identifier of WP after which a leg of standard lane should be input WP must be included in at least one of standard lanes b turn internal knob one position to the right or left FPL correction pop up window is displayed on FPL1 page figure J 3 9 c set the highlighting to identifier of required standard lane d press ENT Page according to figure J 3 10 is displayed on RICU display As standard lanes can have signs of approved movement directions thus all identifiers of WP of standard lane flight to which is
130. ription of FPL1 page After selection of DEPARTURE procedure information about selected procedure name of transit point name of DEPARTURE procedure name of RW is displayed in DEP field procedure is involved in active flight plan and RICU displays the page of active flight plan of FPJ form 034 50 00 Appendix J page 229 Dec 17 2009 CH 4312 02 USER S MANUAL J 10 Messages generated by equipment Messages generated by equipment can be a informative which are displayed after pressing MSG button which are displayed automatically b warning Messages can be generated by equipment in Russian and English Fulfil language setting when setting system parameters on AUX3 page After eliminating the reason causing message generation the message will stop being displayed Informative messages When informative message appears signal light of MSG button is activated When pressing MSG button RICU display shows informative message View of the window of informative message is shown in figure J 10 1 1 Field of message display Figure J 10 1 If there are several informative messages thus signal light of MSG button remains activated until all the messages are read After reading all messages and pressing MSG button RICU display shows the form which was on RICU display prior to appearance of message window 034 50 00 Appendix J page 230 Dec 17 2009 CH 4312 02 USER S MANUAL List of informative messages
131. rn right turn 5 Field of display of target point identifier 6 Scale of deviation from DT described on NAVI page 7 8 Range of DT scale 9 14 Interchangeable fields adjustable by the user 15 Current coordinates 16 Time hours minutes seconds 17 Altitude over geoid 18 Coordinates determination accuracy 19 Date year month date Figure J 2 8 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 2 8 demonstrates factory requiredup of parameters displayed in interchangeable fields List of parameters which can be displayed in interchangeable fields 9 14 is shown in table J 2 1 Operations being accomplished on NAV2 page with MENU button On NAV2 page by pressing MENU PAGE MENU pop up window is displayed figure J 2 9 its fields are used to accomplish the following operations setup of interchangeable fields Change Fields field adjustment of interchangeable fields in accordance with factory setting Restore Defaults field Figure J 2 9 Adjustment of interchangeable fields Adjustment of interchangeable fields on NAV2 page is effected analogically with adjustment of interchangeable fields stated when describing NAVI page Adjustment of interchangeable fields in accordance with factory setting Adjustment of interchangeable fields on NAV2 page is effected analogically with adjustment of interchangeable fields stated when describing NAVI page 034 50 00 Appendix J page 49 Dec 17 2009 CH 4312 02 USER S MANUAL
132. rsection points category View of NRST2 page is shown in figure J 7 2 NEAREST INTERSECTION 1 Lines of table with parameters Reference designation of flight plans intersection point Identifier of flight plans intersection points Bearing to flight plans intersection point from current position Distance to flight plans intersection point from current position Figure J 7 2 Overview of information about nearest NP of flight plans intersection points category Overview of information about nearest NP of flight plans intersection points category is accomplished by analogy with overview of information about nearest NP of airport category NRST 1page 034 50 00 Appendix J page 149 Dec 17 2009 CH 4312 02 USER S MANUAL NRST3 page NRST3 NEAREST NDB page is used to overview nearest NP of nondirectional radio beacons category View of NRST3 page is shown in figure J 7 3 NEAREST NDB 1 7 1 Lines of table with parameters Reference designation of nondirectional radio beacon Identifier of nondirectional radio beacon Bearing to nondirectional radio beacon from current position Distance to nondirectional radio beacon from current position Frequency Figure J 7 3 Overview of information about nearest NP of nondirectional radio beacons category Overview of information about nearest NP of nondirectional radio beacons category is accomplished by analogy with overview of information
133. s L MF NAVAID Decade in the field of display of class of NAVAID means 1 2 3 4 5 NDB H SABH S Sea beacon Internal marker Middle marker External marker Marker of reverse course alolzi Transmitter power 2000 watt or more Transmitter power 25 50 watt Transmitter power less than 25 watt zx Automatic weather forecast Planned weather forecast Speech is not available on NAVAID Required work of BFO lt w gt Overview of information about NP of nondirectional beacons Selection of NP of nondirectional beacons category for overview of information about it is accomplished as follows a input identifier name of NP of nondirectional beacons category which information it is necessary to overview If the are several NP of nondirectional beacons category then RICU will display DUPLICATE WAYPOINTS pop up window for selection of region where the point with input identifier is located figure J 6 37 HE Egypt LR Romania LH Hungary P Poland 034 50 00 Appendix J page 130 Dec 17 2009 Russia Ukraine Russia Finland Russia Figure J 6 37 CH 4312 02 USER S MANUAL b press ENT WPTS8 page displays information about NP of nondirectional beacons category with input identifier name WPT9 page WPT9 page is used to overview information about NP of omnidirectional USW beacons category VOR
134. sary to input turn internal knob of the handle one position further Pop up window with a list of possible values for parameter being input is displayed on RICU figure J 1 4 PS GLON SBAS ON OFF GBAS ON OFF Figure J 1 4 by rotating external knob of the handle fix highlight to parameter value to be input to confirm parameter input press ENT 034 50 00 Appendix J page 9 Dec 17 2009 CH 4312 02 USER S MANUAL Ways of flight execution Equipment ensures execution of the flight on DT on great circle track orthodromy to put AC to WP by route way Route way of flight execution on DT and delivery of AC to WP it is the flight within fixed air route defined by required flight plan When executing route way of the flight along DT equipment makes a continuous computation of deviation from DT linear lateral deviation Z distance left along DT to IWP S left and distance from aircraft position to WP D see figure J 1 5 Values of distance from aircraft position to WP DIS and linear lateral deviation deviation scale from DT and parameter XTK are indicated on NAVI page of display of equipment CH 3301 Equipment generates signal of deviation from DT to control AC manually and signal Selected roll to control AC automatically S left Z linear lateral deviation S left distance on DT left to current WP AP aircraft position D distance from aircraft position to WP Figure J
135. smitting RICU shows SEND USER DB window in which volume of transmitted information is stated in percents figure J 8 75 Display of receiving RICU shows the 034 50 00 Appendix J page 216 Dec 17 2009 CH 4312 02 USER S MANUAL RECEIVE USER DB window in which volume of received information is stated in percents figure J 8 76 Note If user database copying was stopped for more than 2 minutes transmitted and received information volume shown in fig J 8 75 J 8 76 is not changed both RICU should be turned off then turned on and copying should be repeated SEND USER DB Figure J 8 75 RECETVE USER DB Figure J 8 76 c after copying of user database to other RICU display of transmitting RICU displays SEND USER DB window in accordance with figure J 8 77 Display of receiving RICU shows RECEIVE USER DB window in accordance with figure J 8 78 034 50 00 Appendix J page 217 Dec 17 2009 CH 4312 02 USER S MANUAL SEND USER DB Figure J 8 77 RECETVE USER DB Figure J 8 78 d to continue operation of receiving RICU switch off and then switch on receiving RICU 034 50 00 Appendix J page 218 Dec 17 2009 CH 4312 02 USER S MANUAL AUX4 page View ofh AUX4 page is shown in figure J 8 79 1 Activation of built in flight simulator 2 Activation of GNSS test GNSS receiver restart with RAM clearance 3 Availability unavailability of communication with external devices 4 Background te
136. ss Track Err XTK deviation from desired track Cumltv Dist CUM total distance to flight destination point on desired track Desired Track DTK desired track angle Distance DIS distance to target point Empty empty line Enrte Safe Alt ESA safe flight altitude on flight plan Est Time Arvl ETA arrival time to WP Est Time Enrte ETE flight time remained to WP Ground Speed GS ground speed Horiz DOP HDOP horizontal geometric factor Horiz Integr Limit HIL horizontal integrity limit How Vis GLN Sats VGLN number of visible satellites GLONASS How Vis GNSS Sats VGNS number of visible satellites GPS GLONASS How Vis GPS Sats VGPS number of visible satellites GPS How Work GLN Sats WGLN number of operating satellites GLONASS How Work GNSS Sats WGNS number of operating satellites GPS GLONASS How Work GPS Sats WGPS number of operating satellites GPS Leg Distance DIS leg distance on DT Precision RMS standard coordinates deviation RAIM Available RAIM off line test of GNSS signals integrity Track TRK actual course angle 034 50 00 Abbreviation list page 4 Dec 17 2009 CH 4312 02 USER S MANUAL Track And Err TKE additional turn angle difference between desired track angle and current track angle Vert DOP VDOP vertical geometric factor Vert Integr Limit VIL vertical integrity limit Vert Precision RMSH standard altitude deviation
137. ssessessseessossso 230 Ijformative message SAS RS tt E E ce ter 230 Warming messapes SU oc tn ne RS en usm stth 233 034 50 00 Contents page 2 Dec 17 2009 CH 4312 02 USER S MANUAL ABBREVIATION LIST ACP aircraft current position AP aircraft position ATC air traffic control AC aircraft BFO booster frequency oscillation CP central processing DME distance measurement equipment DT desired track GLON Global Navigation AE airborne equipment GLONASS Global Navigation Satellite System GNSS GPS GLONASS joint system GPS US global positioning system HSI horizontal situation indicator LLT linear lead of turn NDB navigation database NP navigation point NSV navigational space vehicle NT navigation task on off switch on off OTC one time command PCU peripheral control unit RAM random access memory RICU operation and acceptance indicator unit RS radar station RW runway SBAS Satellite Based Augmentation System SNS satellite navigation system SV space vehicle SW software TP target point UM user s manual USW ultrashort waves VHF very high frequency WP waypoint 034 50 00 Abbreviation list page 1 Dec 17 2009 CH 4312 02 USER S MANUAL Special symbols displayed on RICU Measuring unit k junctions K a kilometres m metres n miles ten feet K kilometres per hour degrees Mz megahertz az
138. ssibility forecast determination for NP is provided within 12 hours from specified calculation start time To accomplish function RAIM accessibility forecast calculation a select NP for which forecast must be accomplished b set start time and date of function RAIM accessibility forecast calculation c if it is necessary to change factory setting accomplish parameters setting for function RAIM accessibility forecast calculation d set command of function RAIM accessibility forecast calculation accomplishment for a selected NP Selection of NP for function RAIM accessibility forecast calculation Selection of NP for function RAIM accessibility forecast calculation is accomplished by input of NP coordinates in POSITION field NP identifier in WP field To input NP coordinates in POSITION field a set highlight to POSITION field b set NP coordinates for which function RAIM accessibility forecast calculation must be accomplished c press ENT to confirm input of set coordinates To input identifier of NP in the field WP a set highlight to WP field figure J 8 31 Figure J 8 31 034 50 00 Appendix J page 178 Dec 17 2009 CH 4312 02 USER S MANUAL b turn internal knob of shaft encoder one position further RICU display shows WPT1 page c set page of WP form of required category and input identifier of NP d set highlight to Done field and press ENT RICU display shows window of RAIM forecast calc
139. ssing AUX button on RICU By repeated pressing AUX button RICU display will show the form which was displayed prior to activation of AUX form Switching of pages of AUX form is accomplished by rotating internal knob AUXI page AUXI page is used to select maneuvres of the flight View of AUX1 page is shown in figure J 8 1 1 The field of activation of the window of flight maneuvres setting Figure J 8 1 034 50 00 Appendix J page 152 Dec 17 2009 CH 4312 02 USER S MANUAL OFFSET field OFFSET field is used to activate OFFSET window Set highlight to OFFSET field and press ENT To return to AUX1 page press CLR button View of OFFSET page is shown in figure J 8 2 1 Direction of displacement R displacement to the right L displacement to the left 2 Displacement value Maximum displacement value is 99 9 km or 53 9 m m 3 Activation deactivation of the flight on parallel flight plan Figure J 8 2 OFFSET window is used to set parameters and activate the flight on parallel flight plan flight with displacement Setting the flight on parallel flight plan is possible provided the following conditions availability of active flight plan except the flight in DIRECT TO and OBS mode active step is not a part of standard procedure SID STAR and APPROACH Mode of the flight with displacement starts immediately after activation of the flight on parallel flight plan Movement to displaced flight plan is accomplished a
140. st of effective pages page 2 Dec 17 2009 CH 4312 02 USER S MANUAL Section Sub Section Sub section Page Date section Paragraph Page Date Paragraph f Appendix J 147 Dec 17 2009 Appendix J 191 148 Dec 17 2009 192 149 Dec 17 2009 193 150 Dec 17 2009 194 Dec 17 2009 151 Dec 17 2009 195 Dec 17 2009 152 Dec 17 2009 196 153 Dec 17 2009 197 Dec 17 2009 154 Dec 17 2009 198 155 Dec 17 2009 199 156 Dec 17 2009 200 157 Dec 17 2009 201 158 Dec 17 2009 202 159 Dec 17 2009 203 Dec 17 2009 160 Dec 17 2009 204 161 Dec 17 2009 205 162 Dec 17 2009 206 163 Dec 17 2009 207 164 Dec 17 2009 208 165 Dec 17 2009 209 166 Dec 17 2009 210 167 Dec 17 2009 211 168 Dec 17 2009 212 169 Dec 17 2009 213 170 Dec 17 2009 214 171 Dec 17 2009 215 172 Dec 17 2009 216 173 Dec 17 2009 217 Dec 17 2009 174 Dec 17 2009 218 175 Dec 17 2009 219 176 Dec 17 2009 220 177 Dec 17 2009 221 178 Dec 17 2009 222 179 Dec 17 2009 223 180 Dec 17 2009 224 181 Dec 17 2009 225 182 Dec 17 2009 226 183 Dec 17 2009 227 184 Dec 17 2009 228 185 Dec 17 2009 229 186 Dec 17 2009 230 187 Dec 17 2009 231 188 Dec 17 2009 232 189 Dec 17 2009 233 234 190 Dec 17 2009 o 034 50 00 List of effective pages page 3 4 Dec 17 2009 CH 4312 02 USER S MANUAL CONTENTS Part 2 Section Page subsection Name clause AIRBORNE EQUIPMENT O
141. sting 5 External devices test 6 Keyboard test 7 Software versions Figure J 8 79 INNER SIMULATION field INNER SIMULATION field is used to activate SIMULATOR window intended to activate built in simulator To activate SIMULATOR window set highlight to INNER SIMULATION field figure J 8 79 and press ENT To return to AUX4 page press CLR button View of SIMULATOR window is shown in figure J 8 80 034 50 00 Appendix J page 219 Dec 17 2009 CH 4312 02 USER S MANUAL INNER SIMULATION 1 Speed 2 Coordinates of initial WP 3 Identifier of initial WP 4 Activation deactivation of built in simulator Figure J 8 80 Setting of speed To set a speed a set highlight to display field of speed b set required speed c press ENT Setting of coordinates of initial WP It is possible to set coordinates of initial WP either by setting coordinates in the field of coordinates setting or by setting identifier in WP field To set coordinates in the POSITION field a set highlight to display field of coordinates b set initial coordinates To set identifier in WP field a set highlight to WP field b turn internal knob one position further RICU display shows the WPT1 page c input identifier of required WP Press ENT Highlight will move to the field DONE d press ENT RICU display shows SIMULATOR window in which coordinates of selected WP are displayed as initial coordinates 034 50 00 Appendix J page 22
142. t d set command of sunrise and sunset time calculation execution Selection of NP for sunrise and sunset time calculation Selection of NP for sunrise and sunset time calculation is accomplished by analogy with selection of NP for function RAIM accessibility forecast calculation given in description of function RAIM accessibility forecast calculation for NP Setting of date of sunrise and sunset time calculation To set date of sunrise and sunset time calculation a set highlight to DATE field figure J 8 39 b set required calculation date c press ENT to confirm input of set date Setting of zone time adjustment To set zone time adjustment a set highlight to TIME ZONE field figure J 8 39 b set zone time adjustment c press ENT to confirm input of set adjustment Setting of command of sunrise and sunset time calculation accomplishment To set command of sunrise and sunset time calculation execution a set highlight to the field CALC figure J 8 39 b press ENT results of sunrise filed SUNRISE and sunset field SUNISET time calculation will be displayed in the window SUNRISE 034 50 00 Appendix J page 187 Dec 17 2009 CH 4312 02 USER S MANUAL AUX3 page View of AUX3 page is shown in figure J 8 40 1 Setting of system parameters 2 Setting of criteria of nearest airports selection 3 Setting of brightness 4 Setting of parameters for calculation of standard procedures and RAIM calculation
143. t an angle of 45 degrees Flight cessation on parallel flight plan is accomplished by operator instruction if moving to the next step it is necessary to accomplish a turn at an angle of less than 130 degrees automatically if moving to the next step it is necessary to accomplish a turn at an angle of more than 130 degrees 034 50 00 Appendix J page 153 Dec 17 2009 CH 4312 02 USER S MANUAL Setting the flight on parallel flight plan To set flight on parallel flight plan it is necessary to accomplish the following actions a set highlight to the field of direction an value of displacement and input direction an value of displacement b set highlight to the field of activation deactivation of the flight on parallel flight plan c turn internal knob one position further SELECT pop up window is displayed in OFFSET window figure J 8 3 Figure J 8 3 d set highlight to ON field Press ENT message about flight on parallel flight plan OFFSET is displayed on RICU in status line figure J 8 4 Figure J 8 4 034 50 00 Appendix J page 154 Dec 17 2009 CH 4312 02 USER S MANUAL AUX2 page View of AUX2 page is shown in figure J 8 5 1 Adjustment VOR DME 2 Data from VOR DME 3 Data of sensor GNSS 4 Data of sensors SVS IRS wind computation 5 Navigation solution mode selection 6 Data about other RICU 7 Computation of RAIM forecast 8 Computation of sunrise and sunset time Figure J 8 5 TUNE
144. t is necessary to set an angle of flyover of a target point a set highlight to CRS field after selection of a target point by one of methods described above in the form gt b set a necessary value of an angle of flyover of a target point c press ENT to confirm a selected angle of flyover of a target point d activate a flight to a target point with a selected angle of flyover Cancellation of a flight in DIRECT TO mode To cancel a flight in DIRECT TO mode a press the button gt RICU display will show the form Br its fields are filled with data of the target point 6 press the button MENU The window according to figure J 4 7 is displayed in the formB gt 034 50 00 Appendix J page 102 Dec 17 2009 CH 4312 02 USER S MANUAL Cancel Direct To NAV z Figure J 4 7 B press ENT to confirm cancellation of a flight in DIRECT TO mode After cancellation of a flight in DIRECT TO mode and with an active flight plan available accomplish activation of a flight to required flight plan leg 034 50 00 Appendix J page 103 Dec 17 2009 CH 4312 02 USER S MANUAL J 5 Operation description in OBS form The form OBS is intended to set a flight in OBS mode OBS mode provides movement to WP with set angle of flyover when flying according to a flight plan or in DIRECT TO mode Entry to OBS form is accomplished by pressing OBS button if an active flight plan leg is available View of OBS form is shown in figure J
145. te field figure J 6 41 00057 90995 Figure J 6 41 i press ENT to confirm creation of user NP Number of created NP will increase by one unit in the field of created user NP number and number of NP possible for creating will decrease by one unit in the field of number of NP possible for creating figure J 6 42 Highlight will move to the field of identifier of user NP and request about change of user NP Modify will appear 0006 0994 Modify Figure J 6 42 j press CRSR button to exit from user NP creation mode 034 50 00 Appendix J page 135 Dec 17 2009 CH 4312 02 USER S MANUAL Creation of user WP by setting bearing and distance from basic NP To create user NP by setting bearing and distance from basic NP a set highlight to the field of display of NP identifier b input identifier of user NP being created c press ENT to confirm input of identifier A request about creation of user WP Create will appear in right lower angle of RICU display Highlight will move to the field of identifier of basic NP d input identifier of basic NP if there are several NP with input identifier then RICU will display DUPLICATE WAYPOINTS pop up window for selection of region where the point with input identifier is located Set highlight to required region of NP Press ENT Bearing and distance from input basic NP to the point with coordinates displayed in POSITION field are displayed on WPT10 page in the fields RAD and
146. te MODE popup window Figure J 8 13 c set highlight on MANUAL field Press ENT button d set highlight on the field of beacons selected in MAN SELECT manual mode list e press MENU button Tune VOR DME window shall indicate PAGE MENU popup window Figure J 8 14 034 50 00 Appendix J page 160 Dec 17 2009 CH 4312 02 USER S MANUAL Figure 8 14 f set highlight on Select Navaid field Press ENT button RICU display shall indicate NRST4 page Figure J 8 15 NEAREST VOR Figure J 8 15 Note Prohibited for use beacons are shaded If no permitted for use beacons of selected type are available then there will be no highlighted line in NRST4 page Press CLR button to return into Tune VOR DME window g set highlight on the required beacon field Press ENT RICU display shall indicate Tune VOR DME window The information of the selected beacon shall be indicated in the list of selected in manual mode beacons Fig J 8 16 In manual mode one or two beacons involved into NT solution may be set 034 50 00 Appendix J page 161 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 8 16 Deletion of beacons from the manually selected beacons list To delete the beacons from the manually selected beacons list a set highlight on the beacons selection mode field b turn internal knob of shaft encoder one position further Tune VOR DME window shall indicate MODE popup window Fig J 8 13 c set highlight t
147. ternal device communication availability BACKGROUND TEST field FonTest wi Results of functional nodes testing IO TEST field IO TEST window OTC setting and setup of parameters for external devices and functional nodes testing Check output OTC input OTC formation of signal of deviation from DT formation of signal Y set formation of signal of course shift formation of signal of deviation from approach descent KEYBOARD TEST field Keyboard testing SOFTWARE VERSION field SOFTV Versions display SW of central computer of RICU SW of PCU SW of GNSS receiver Figure J 1 20 page 8 of 8 034 50 00 Appendix J page 39 Dec 17 2009 CH 4312 02 USER S MANUAL Logical tree of PROC form PROC form 034 50 00 Appendix J page 40 Dec 17 2009 PROC page Approach procedure activation Selection of Approach standard procedure Information overview transit point name procedure name Information overview transit point name procedure name TLR name Selection of Arrival standard procedure Information overview transit point name procedure name TLR name Selection of Departure standard procedure Figure J 1 21 CH 4312 02 USER S MANUAL J 2 Operation description in NAV form Navigation form is intended for display of main navigation parameters and for graphic rep
148. ting the requirements given at AUTO mode description Note for navigation solution two beacons are required at least selected in auto or manual mode TEST CTRL mode is purposed to tune VOR DME airborne devices on the frequency set by operator At DME tuning it is permissible to tune DME on 1 2 or 3 beacons At one beacon tuning DME device shall be activated for one frequency mode At 2 or 3 beacons tuning DME device shall be activated in directional scanning mode In CTRL mode the beacon with the frequency indicated in the top line shall be selected for tuning At VOR tuning the VOR device shall be always tuned on one beacon 034 50 00 Appendix J page 159 Dec 17 2009 CH 4312 02 USER S MANUAL Beacons selection in AUTO mode For the task of the beacons selection in AUTO mode a set highlight to the beacons selection mode field b turn internal knob of shaft encoder one position further MODE popup window shall be indicated in Tune VOR DME Figure J 8 13 Figure J 8 13 c set highlight on AUTO field Press ENT button the selected mode shall be indicated in SELECT field RICU display and five permitted to use nearest beacons corresponded to the listed requirements shall be indicated in AUTO SELECT field Beacons manual selection To select beacons in manual mode a set highlight on the beacons selection mode field b turn the inner handle of shaft encoder for one position Tune VOR DME window shall indica
149. titude change GRAD field 4 Maximum angle of list en route 5 Roll angle rate of rise 6 Slope of a signal Selected roll 7 Aircraft average speed AVERAGE SPEED DEPARTURE field for terminal area of departure 30 miles ENROUTE field for averaged flight part ARRIVAL field for terminal area of arrival 30 miles Figure J 8 71 034 50 00 Appendix J page 211 Dec 17 2009 CH 4312 02 USER S MANUAL Input of parameters values for calculation of SID STAR APPROACH procedures To input parameters values for calculation of SID STAR APPROACH procedures a set highlight to the line of parameters for calculation of SID STAR APPROACH procedures b set the parameter required values for SID STAR APPROACH procedures calculation aircraft average speed SPEED field maximum angle of list BANK field gradient of altitude change GRAD field c press ENT Input of value maximum roll angle Maximum roll angle limits the value Selected roll at all stages of the aircraft flight To input the value maximum roll angle a set highlight to the field of maximum roll angle en route b turn internal knob of the handle into one position Herewith LIMIT DATA window will display SET BANK MAX pop up window containing the list of possible values of maximum roll angle Set highlight to the field of desired value of maximum roll angle Note The value of maximum roll angle en route should not e
150. ue North if it is required to obtain graphic display of RW oriented to north on RICU display DTK if it is required to obtain graphic display of RW oriented by course angle on RICU display b press ENT 034 50 00 Appendix J page 60 Dec 17 2009 CH 4312 02 USER S MANUAL Scale automatic change activation The scale automatic change is activated in similarly to the scale automatic change activation as described on NAVI page J 3 Operation description in FPL form FPL form is used to work with flight plans created by users The form contains two pages page of detailed overview of active flight plan FPL1 Active Flight Plan page of flight plan catalogue FPL2 Flight Plan Catalog To enter FPL form one should press FPL buttons on RICU In case of repeated pressing the FPL button the form which was on RICU display prior to activation of the form FPL form is displayed on RICU display When entering the form FPL form FPL1 page is always displayed on RICU display Page switching of FPL form is performed by rotating internal knob of the handle Creation and editing of a flight plan is accomplished on FPL1 or FPL2 page Flight plan created on FPL1 page is stored in RICU memory until it is deleted or until activation of another flight plan is done SID STAR APPROACH procedures can be included only in active flight plan 034 50 00 Appendix J page 61 Dec 17 2009 CH 4312 02 USER S MANUAL FPLI1 page View
151. ues which service indicator can take on are shown in table J 2 3 034 50 00 Appendix J page 53 Dec 17 2009 CH 4312 02 USER S MANUAL Table J 2 2 Symbol Ai tana Connec Both in Symbol in the Radiocommunication Descripti nae a tion on types of ARINC form equipment sae a ence the commu 424 connecuon route Mnication ACC ArCntrCenter Area Control Center Regional centre ATC X ACP AliftComPost Airlift Command Post Command Post X APP AppControl Approach Control Approach Control X ARR ArrControl Arrival Control Arrival Control X ATI ATIS Automatic Terminal Automatic Terminal X Info Service ATIS Information Service AWO AWOS Automatic Weather Automatic Weather X Observing Service Observing Service AWOS CLD CleaDelivery Clearance Delivery Air traffic clearance X delivery CPT CleaPre Taxi Clearance Pre Taxi Air traffic clearance X pre taxi CTA ControlArea Control Area Control Area X Terminal Terminal CTL Control Control Control X DEP DeparControl Departure Control Departure Control X DIR Director Director Approach Director Approach X Control Radar Control Radar EMR Emergency Emergency Emergency X FSS FlgServStat Flight Service Station Flight Service X Station GND Ground Ctrl Ground Control Ground Control X GTE Gate Control Gate Control Gate Control X HEL HelicopFreq Helicopter Frequency Helicopter X Freque
152. ulation Identifier of a selected NP is displayed in WP field and coordinates of a selected NP in POSITION field Setup of start time and date of function RAIM accessibility forecast calculation To set start time and date of function RAIM accessibility forecast calculation a set highlight to TIME DATE field b set required time date of forecast start c press ENT to confirm input of set time date Setup of parameters for function RAIM accessibility forecast calculation the window SETTING PRAIM Setup of parameters for function RAIM accessibility forecast calculation is accomplished in SETTING PRAIM window To activate SETTING PRAIM window set highlight to SETs field figure J 8 30 and press ENT button To return to PRAIM window press CLR button View of SETTING PRAIM window is shown in figure J 8 32 034 50 00 Appendix J page 179 Dec 17 2009 CH 4312 02 USER S MANUAL 1 Step of function RAIM accessibility forecast calculation 2 Limit of integrity signalling 3 Angle of elevation of satellites over the horizon 4 Inclusion exclusion of barometric altitude into from calculation 5 Field of activation of the list NSV GPS 6 Field of activation of the list NSV GLONASS Figure J 8 32 Setup of values of step of RAIM forecast calculation limit of integrity signalling angle of elevation To set values of step of RAIM forecast calculation limit of integrity signalling angle of elevation a set highli
153. une VOR DME window shall indicate MODE popup window Figure J 8 13 c set highlight to TEST field Press ENT RICU display shall indicate Test VOR DME window Fig J 8 17 034 50 00 Appendix J page 163 Dec 17 2009 CH 4312 02 USER S MANUAL DHE NAVAID 2 1 Table for DME devices tuning frequency DME device tuning frequency switching on off DME device tuning frequency delivery tuning mode selection TEST mode command word delivery for the airborne distance meter normal operation command word status matrix CTRL mode command word delivery for the airborne distance meter function test command word status matrix 2 Distance to beacon 3 Table for VOR device tuning the information is analogous to that for DME device tuning 4 Azimuth to beacon Figure J 8 17 d set highlight to FREQ field Enter DME VOR device tuning frequency e set highlight to ON OFF field Turn the inner handle of shaft encoder for one position Test VOR DME window shall indicate SELECT popup window Fig J 8 18 Figure J 8 18 034 50 00 Appendix J page 164 Dec 17 2009 CH 4312 02 USER S MANUAL f set highlight to ON OFF field to switch on off the beacon form DME VOR device test g set highlight to MODE field turn the inner handle of shaft encoder for one position Test VOR DME window shall indicate SELECT popup window Fig J 8 19 Figure J 8 19 h select the tuning required mode Press ENT
154. ure Highlight will move to the field of RW name RUNWAY figure J 6 12 034 50 00 Appendix J page 115 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 12 e turn internal knob one position further WPT4 page displays RUNWAY pop up window figure J 6 13 Figure J 6 13 f set highlight to the name of required RW g press ENT RUNWAY field displays name of selected RW and highlight will move to the field of transit point name TRANS figure J 6 14 034 50 00 Appendix J page 116 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 14 h turn internal knob one position further WPT4 page displays TRANS pop up window figure J 6 15 Figure J 6 15 i set highlight to the name of required transit point j press ENT TRANS field displays name of selected transit point highlight will remain in the field of transit point name Graphic representation of selected procedure SID is displayed on the WPT4 page in the filed of graphic representation of procedure k press CRSR button Highlight will disappear from the fields of WPT4 page figure J 6 16 034 50 00 Appendix J page 117 Dec 17 2009 CH 4312 02 USER S MANUAL Figure J 6 16 Zoom of graphic display of SID procedure To zoom graphic display of the procedure SID perform the following operations a press MENU button figure J 6 17 Figure J 6 17 b press ENT Symbol will appear in the centre of the field of
155. urse angle XTK Cross Track Distance Deviation Empty Reserved line Compass scale description Fixed indicator of actual track angle is located in the upper part of compass scale movable indicator of desired track angle is located in the lower part Range of scale displayed 60 degrees Division value of compass scale is 5 degrees Digital values of calibration in 30 degrees without last zero in digital value are stated on compass scale World parts are marked with respective symbols Description of scale of deviation from DT Scale of deviation from DT scale CDI has ten divisions motionless symbol of AC amp when executing flight to the point or WY when executing flight from the point in the middle of DT scale movable symbol of DT ff Scale of deviation from DT is intended for graphic display of AC position and desired track Display principle from aircraft to earth is accepted in equipment that is AC symbol is motionless and displayed in the centre of the scale and symbol of desired track moves relatively to AC symbol 034 50 00 Appendix J page 43 Dec 17 2009 CH 4312 02 USER S MANUAL If AC deviation from DT is to the left symbol of desired track moves in display to the right and vice versa When DT leaves the limits of the scale deviation from DT in digital form and direction necessary to reach DT is displayed Measure of scale of
156. ution GNSS sensor DME DME device VOR DME device SVS IRS sensor 2 Use control of navigation data source in the complex NT solution from other RICU Note Removal of SVS IRS and SVS IRS2 sensors from the list of navigation data sources used in the complex NT solution is impossible Figure J 8 26 034 50 00 Appendix J page 173 Dec 17 2009 CH 4312 02 USER S MANUAL Navigation data source selection used for the complex NT solution For navigation data source selection used for the complex NT solution a set highlight on switching on off navigation database source solution field opposite the required source b turn internal knob of shaft encoder one position further RICU display shall indicate SELECT pop up window Fig J 8 27 Figure J 8 27 c set highlight on ON field to switch on and in OFF to switch off the selected navigation data source use for complex NT solution d press ENT Note Switching off all sources shall disable the complex NT solution DATA CROSS RICU field The DATA CROSS RICU field is used to activate the DATA CROSS RICU window intended to display data from other RICU and to input coordinates received by other RICU as reference coordinates To activate DATA CROSS RICU window set highlight to DATA CROSS RICU field figure J 8 5 and press ENT To return to AUX2 page press CLR button View of DATA CROSS RICU window if there is connection with other RICU is shown
157. utton does not lead to any actions FPL Button FPL Button is intended for transition to flight plans form Repeated pressing of the FPL button returns the form which was before activation of the form FPJ 034 50 00 Appendix J page 3 Dec 17 2009 CH 4312 02 USER S MANUAL PROC Button PROC Button is intended for transition to form of selection and loading of standard takeoff landing and approach procedures Repeated pressing of the PROC button returns the form which was displayed before activation of the form PROC Buttons RNG and RNG Buttons RNG and RNG are used for displayed graphic information zooming P gt Button Button gt is used to ensure flight in DIRECT TO mode to selected target point AUX Button AUX Button is intended for transition to form AUX Repeated pressing of the AUX button returns the form which was before activation of the form AUX MENU Button MENU Button is intended for activation of pop up window PAGE MENU relating to active page or active form window The button is used to ensure selection of additional options of active page or to accomplish settings for this form page Repeated pressing of the MENU button closes pop up window PAGE MENU WP Button WP Button is intended for transition to database form Repeated pressing of the WP button returns the form which existed before activation of the form WP CLR Button CLR Button is intended for refusal to edit return from window to
158. w will appear on RICU display figure J 6 49 034 50 00 Appendix J page 141 Dec 17 2009 CH 4312 02 USER S MANUAL Description of UDB_list window List of user points in alphabetical order of symbols is displayed in UDB_list window USER WAYPOINT LIST 9004 0996 Selection of user NP for overview To select NP for overview a set highlight to identifier of NP information of which is required to overview figure J 6 49 b press ENT WPT10 page with information about selected NP is displayed on RICU Highlighted Done message will appear in right upper angle figure J 6 50 Return to UDB list window is accomplished by pressing ENT with highlighted Done message Note Done message will be displayed on WPT10 page until return from UDB list window by pressing CRSR button is accomplished 00047 0996 Modify Figure J 6 50 034 50 00 Appendix J page 142 Dec 17 2009 CH 4312 02 USER S MANUAL Deletion of user NP To delete user NP a set highlight to identifier of NP which must be deleted figure 6 49 b press CLR button c If user NP with selected for deletion is used in none of the flight plans created on the pages of FPL form DELETE WAYPOINT window containing the request about deletion of selected NP will appear in the window UDB list figure J 6 51 In this case set highlight to Yes field press ENT to confirm deletion Selected NP will not be deleted from user NP list Figure
159. x J page 167 Dec 17 2009 CH 4312 02 USER S MANUAL Table J 8 1 Symbol in the form Parameter name ALT Altitude HIL Horizontal integrity limit VIL Vertical integrity limit HDOP Horizontal geometric factor VDOP Vertical geometric factor RMS Root mean square deviation RMSH Root mean square deviation on altitude RAIM Off line test of integrity of GNSS signals VGNS Number of visible GPS GLONASS satellites WGNS Number of operating GPS GLONASS satellites VGPS Number of visible GPS satellites WGPS Number of operating GPS satellites VGLN Number of visible GLONASS satellites WGLN Number of operating GLONASS satellites Input of initial coordinates Input of initial coordinates can be accomplished only if data from GNSS sensor are not available For initial coordinates manual input a set highlight to the field of coordinates b input initial coordinates c press ENT to confirm input of set coordinates RICU display shall indicate DATA GNSS window with input coordinates and the sign of the coordinates manual input Manual Input of initial coordinates can be performed from NDB after pressing MENU button Input of time and date Input of time and date can be accomplished only if data from GNSS sensor are not available To input time and date a set highlight to the field of time date b enter current time date c press ENT to confirm input of set ti
160. xceed the value of maximum roll angle for aircraft type where the equipment is used c press ENT Rise rate input of roll angle a set highlight to the field of rise rate of roll angle b turn internal knob of the handle into one position Herewith LIMIT DATA window will display SET BANK SPEED pop up window containing the list of possible values of rise rate of roll angle Set highlight to the field of desired value of rise rate of roll angle c press ENT 034 50 00 Appendix J page 212 Dec 17 2009 CH 4312 02 USER S MANUAL Input of averaged speed in terminal areas of departure arrival and en route The input values of averaged speed in terminal areas of departure arrival and en route shall be used for calculation of RAIM function for route forecast To input averaged speed in terminal areas of takeoff arrival and en route a set highlight to the field of averaged speed in terminal area of takeoff b set required value of speed B press ENT Input similarly required values of averaged speed in terminal area of arrival and en route 034 50 00 Appendix J page 213 Dec 17 2009 CH 4312 02 USER S MANUAL MAP SETTUP field MAP SETTUP field is used to activate MAP SETTUP window intended to select air zones and reference designations of navigation references airports beacons possible for detailed representation in NAV1 and NAV3 pages To activate MAP SETTUP window set highlight to MAP SETTUP field figure J
161. y NP information bearing and distance from current aircraft position to omnidirectional USW beacon NP selection by identifier CRSR or by name Flight setting 4 eae in DIRECT TO mode Figure J 1 18 page 4 of 5 034 50 00 Appendix J page 28 Dec 17 2009 CH 4312 02 USER S MANUAL WPT10 page is for NP of user WPT category Display NP information field for inputting two basic points Input of identifier of respective NP and overview of information about NP selected NP parameters editing Creation of a new NP by input of identifier and by setting point coordinates bearing and distance from basic NP bearings from two basic NP Delete User Waypoint User WPT removal View User Waypoint List User WPT removal Delete All User Waypoint oN User WPT Renaming Flight setting in DIRECT TO mode Figure J 1 18 page 5 of 5 034 50 00 Appendix J page 29 Dec 17 2009 CH 4312 02 USER S MANUAL Logical tree of NRST form Form NRST NRST1 page NEAREST ARP Display of information about nearest airports identifier bearing distance length from the longest TLR of an airport Overview of information about nearest airports Flight setting in DIRECT TO mode NRST2 page NEAREST INTERSECTION Display of information about nearest flight plans intersection points identifier bearing distance Overview of information about
162. ype of surface of the main RW figure J 8 56 iard Only Hard Soft 1 Any type of RW surface 2 Only hard surface of RW 3 Hard or soft surface of RW 4 Water Figure J 8 56 c set highlight to the field of required type of RW surface d press ENT to confirm input of a selected type of RW Setting of minimum length of the main RW of airports displayed in NRST form To set minimum length of the main RW of airports displayed in NRST form a set highlight to MINIMUM LENGTH field b set minimum length of RW c press ENT to confirm input of a selected minimum length of RW 034 50 00 Appendix J page 200 Dec 17 2009 CH 4312 02 USER S MANUAL BRIGHTNESS field BRIGHTNESS field is used to activate BRIGHTNESS window intended to set highlight brightness of display and keyboard To activate BRIGHTNESS window set highlight to BRIGHTNESS field figure J 8 40 and press ENT To return to AUX3 page press CLR button View of BRIGHTNESS window is shown in figure J 8 57 UU Lm DRE ES S 1 Setting mode for highlight brightness of display 2 Setting mode for highlight brightness of keyboard Figure J 8 57 Setting of highlight brightness of display To set of highlight brightness of display a set highlight to the field of setting mode for highlight brightness of display figure J 8 57 b turn internal knob one position further BRIGHTNESS window displays pop up window of selection of setting mode for high

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