Home
Flight Management System
Contents
1. 2011 Captain Sim www captainsim com 25 DO NOT USE FOR FLIGHT 1 Cruise Before the top of descent FMC is in cruise mode and uses VNAV PTH and ECON cruise speed 2 Level Descent Phase After top of descent FMC is in descent mode VNAV decreases airspeed to ECON descent speed maintains altitude in VNAV PTH 3 Descent Upon reaching descent speed VNAV descends in VNAV PTH at ECON descent speed 4 Speed Limit Protection If a tailwind causes the airplane to accelerate the DRAG REQUIRED scratchpad message will be displayed If the speedbrakes are not deployed the pitch mode will change to VNAV SPD and depart the path before the speed reaches the limit 5 Speed Restriction Deceleration Before the speed restriction altitude VNAV decelerates to commanded speed using VNAV PTH 6 Descent and Approach When at restricted speed VNAV descends and starts approach in VNAV PTH at commanded speed 7 Minimum Descent Altitude When the MDA is reached with VNAV engaged the airplane will maintain the MDA altitude in VNAV PTH If the missed approach point is crossed without selecting GA VNAV will maintain the missed approach point altitude until GA is selected 8 Go Around GA The missed approach go around is commenced by pushing a Go Around switch Pushing a Go Around switch sets go around thrust IT MANUAL Part V Flight Mar rent System 26 DO NOT USE FOR FLIGHT DATA ENTRY RULES ALTITUDE ENTRY
2. 757 Cap 1 G N J art V FIC Aanagement system 87 DO NOT USE FOR FLIGHT 8 FORECAST Push shows the DESCENT FORECAST page 7 Descend Direct DES DIR Push deletes all waypoint altitude constraints between the airplane altitude and the MOP altitude Shown in descent phase with altitude constraint between airplane and E D 9 Descend Now DES NOW Shown when the descent phase is not active Push e starts a 1250 feet per minute descent schedule until intercepting the planned descent path e activates the FMC descent phase DESCENT FORECAST PAGE The descent forecast page is used to enter wind data for descent and the altitude at which anti ice use is anticipated for more accurate descent path calculation The primary entries are wind direction and speed for up to four descent altitudes and the altitude that anti ice is turned on ACT ECON DES FORECAST gt FORECA TAI 1 3 WIND DIR SPD 2 090 105KT 4 078 69KT 130 29KT 5 5 1 Transition Level TRANS LVL Shows the transition level 757 Captain FLIGHT MANUAL Part V Flight Management System 88 DO NOT USE FOR FLIGHT The transition level can be specified by the arrival procedure The default transition level is FL 180 Above transition level altitudes are in flight levels Below transition level altitudes are in thousands of feet Valid entry is an altitude or flight level 2 Altitude ALT Enter altitude of
3. 3 Execute EXEC Key Push e makes data modifications active e extinguishes execute light 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 8 DO NOT USE FOR FLIGHT ALPHA NUMERIC AND MISCELLANIOUS KEYS j lt le Efe IB DHe E OOG DANBA A 1 Alpha Numeric Keys Push e puts selected character in scratchpad e Slash key puts in scratchpad e Plus Minus key first push puts in scratchpad Subsequent pushes alternate between and 2 Clear CLR Key Push e clears last scratchpad character e clears scratchpad message Push and hold clears all scratchpad data 3 Delete DEL Key Push puts DELETE in scratchpad 4 Space SP Key Push puts space in scratchpad 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 9 DO NOT USE FOR FLIGHT CDU PAGE COMPONENTS 1 5 2 3 6 5 9 ACTIVATE gt j i Subject or name of data displayed on page ACT active or MOD modified shows whether page contains active or modified data 2 Line Title Title of data on line below 3 Line Data Displays e data e entry field prompts 4 Prompts Caret lt or gt indicates a prompt Push selects indicated information mode or page 5 Page Number Left number is page number R
4. Section 7 FMC CRUISE INTRODUCTION The cruise phase starts at the top of climb During cruise the primary FMC pages are e RTEXLEGS e CRZ e PROGRESS The RTE LEGS pages are used to modify the route The CRZ pages display VNAV related data The PROGRESS pages display flight progress data During cruise the specific page listed below is used to e POS REF page verify the FMC position e RTE DATA page display progress data for each waypoint on the RTE LEGS page e REF NAV DATA page display data about waypoints navaids airports or runways and can be used to inhibit navaids e RTE page select a route offset e FIX INFO page display position data about waypoints Position data can be transferred to other pages to create new waypoints and fixes e SELECT DESIRED WAYPOINT page shows a list of duplicate waypoints from the navigation database The flight crew selects the correct waypoint from the list e POS REPORT page display data for a position report The CLB page changes to CRZ at the top of climb The CRZ CLB and CRZ DES pages change to CRZ when a new cruise altitude is reached The CRZ page changes to DES at top of descent LNAV MODIFICATIONS This section shows typical techniques to modify the route The modifications include e add and delete waypoints e change waypoint s sequence e connect discontinuities RTE LEGS PAGE MODIFICATIONS Modifications to the LNAV route are usually made on the RTE LEGS page When the
5. Altitudes can be entered into the FMC as three digit XXX four digit XXXX five digit XXXXX or flight level FLXXX numbers The FMC displays altitude or flight level entries in the proper form based on the transition altitude Some data lines further restrict the valid entry forms Three digit entries represent altitude or flight levels in increments of 100 feet Leading zeros are required Examples of three digit XXX FLXXX entries with transition altitude 10 000 feet e 800 feet is entered as 008 or FLO08 displays as 800 e 1 500 feet is entered as 015 or FLO15 displays as 1500 e 11 500 feet is entered as 115 or FL115 displays as FL115 e 25 000 feet is entered as 250 or FL250 displays as FL250 Four digit entries represent feet rounded to the nearest ten feet Leading zeros are required This form is used when the altitude does not exceed 9 994 feet Examples of four digit XXXX entries with transition altitude 18 000 feet e 50 feet is entered as 0050 displays as 50 835 feet is entered as 0835 displays as 840 1 500 feet is entered as 1500 displays as 1500 8 500 feet is entered as 8500 displays as 8500 9 994 feet is entered as 9994 displays as 9990 Five digit entries represent feet rounded to the nearest ten feet This form is used when the altitude exceeds 9 994 feet Examples of five XXXXX digit entries with transition altitude 4 000 feet e 50 feet is entered as 00050 displays as 50 e 835 feet is ente
6. DO NOT USE FOR FLIGHT 757 Captain FLIGHT MANUAL PART V Flight Management System 757 Captain FLIGHT MANUAL Part V Flight Management System 2 DO NOT USE FOR FLIGHT ABOUT THIS MANUAL VERSION 11 OCTOBER 2011 WARNING THIS MANUAL IS DESIGNED FOR MICROSOFT FS9 amp FSX USE ONLY DO NOT USE FOR FLIGHT The 757 Captain FLIGHT MANUAL is organized into five Parts Each Part is provided as a separate Acrobat PDF document Click START gt Programs gt Captain Sim gt 757 Captain gt e Part I User s Manual o The User s Manual describes the 757 Captain product as a software title e Part II Aircraft Systems e Part III Normal Procedures e Part IV Flight Characteristics and Performance Data e Part V Flight Management System this document Adobe Acrobat Reader Required FOR GENERAL INFORMATION ON THE 757 CAPTAIN PRODUCT PLEASE USE WWW CAPTAINSIM COM THIS MANUAL PROVIDES ADDITIONAL INFORMATION ONLY WHICH IS NOT AVAILABLE ON THE WEB SITE DO NOT USE FOR FLIGHT CONTENTS Page 2 ABOUT THIS MANUAL 6 Section 1 FLIGHT MANAGEMENT NAVIGATION CONTROLS AND INDICATORS 6 FLIGHT MANAGEMENT SYSTEM CONTROL DISPLAY UNIT CDU 7 FUNCTION AND EXECUTE KEYS 8 ALPHA NUMERIC AND MISCELLANIOUS KEYS 9 CDU PAGE COMPONENTS 10 FMC ANNUNCIATOR LIGHT 11 Section 2 FLIGHT MANAGEMENT SYSTEM DESCRIPTION 11 INTRODUCTION 11 FLIGHT MANAGEMENT CO
7. Held in Navaids db file File format Altitude Frequecny ID Latitude Longitude Type UsageCode Type VOR VORTAC TACAN VORDME NDB NDBDME DME ONUA WNE Runways Held in Runways db file File format AirportICAO GS_Angle ILS_Frequency Latitude LengthFeet Longitude Name TrueHeading Aircraft type referencing Is fulfilled via productcode cfg file For example AircraftModel 757 200 NavDataID BA19410001 COData BA1001 OPProgram PS4052970 953 OPCNumber 3173BCG00025 Version 0 3 757 Captain FLIGHT MANUAL Part V Flight Management System 101 DO NOT USE FOR FLIGHT CUSTOM TERMINAL PROCEDURES Terms Original database aeronautical data database included into the original product pack Custom terminal procedures terminal procedures db files SIDs STARs or IAPs of any airport created and or modified by user HOW TO ADD CUSTOM TERMINAL PROCEDURES Any advanced user can add custom terminal procedures without a risk of damaging the original database DO NOT modify remove edit files loacated in FSX Root Folder Captain_Sim navigation folder 1 Create airport _stars db and or airport _sids db and or airport _iaps db files In order to do this right click at any folder of your computer create txt file and change the file extension to db airport is the airport ICAO four letters code e g KSEA For example KSEA_stars db KSEA_sids db KSEA_iaps db 2 Paste SID and or
8. INDEX Push shows the INT REF INDEX page 757 Captain FLIGHT MANUAL Part V Flight Management System 92 DO NOT USE FOR FLIGHT 5 FLAPS VREF Shows the calculated reference speed for flaps 20 25 and 30 A gross weight is necessary for VREF speed calculation The display is blank until a gross weight is shown 6 FRONT Course CRS Displays the front course for the ILS and runway shown to the left The FMC computes holding patterns with constant radius turns based on current wind and FMC commanded airspeed The pattern size is limited to FAA or ICAO protected airspace In LNAV the AFDS tracks the holding pattern using up to a 30 degree bank angle Strong winds or airspeed in excess of FAA or ICAO entry speeds may result in the airplane flying outside the protected airspace With LNAV active before sequencing the holding fix holding pattern entries are determined by the following The entry method used parallel teardrop or direct is determined by e airplane track not heading or direction from which the active route approaches the holding pattern e the airplane flies the initial outbound leg a computed distance from the holding fix rather than a specific time The computed distance is a function of the command airspeed and computed wind at the time the holding pattern becomes active e teardrop entries use a 40 degree offset angle e parallel and teardrop entries may cause the airplane to fly beyond the displaye
9. This page is available only for the active route The ETA and calculated fuel remaining are displayed for each waypoint Manual entry is not possible One page shows data for five waypoints ACT RTE 1 LEGS RTE DATA gt i ACT RTE 1 DATA 3 ET WPT FUEL 2 LACRE 30 N47wW122 30 VAMPS 26 BANDR 26 000000 1 Waypoint WPT Displays identifier for waypoint 2 ETA Displays ETA for waypoint 3 FUEL Displays the FMC calculated fuel remaining at the waypoint Note ETA and estimated fuel calculations assume a direct flight across route discontinuities 4 WIND Page Prompts Push selects WIND page for the selected waypoint A W next to the prompt indicates that wind data has been entered on the wind page for that waypoint 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 76 DO NOT USE FOR FLIGHT 5 LEGS Push displays RTE LEGS page WIND DATA The FMC uses wind data to improve performance calculation accuracy The FMC applies the first entered wind to all waypoints in the flight plan Wind data includes altitude and direction speed Wind data entered at another waypoint changes the wind only for the waypoints down track from that waypoint either to the end of the track or to the next entered wind Therefore enter winds for waypoints closest to the airplane first then enter winds for waypoints further down track For example at
10. 2 4 35 POSITION REFERENCE PAGE 3 4 36 POSITION REFERENCE PAGE 4 4 37 ROUTE PAGE 37 ROUTE PAGE 1 X 39 MORE ROUTE PAGE PROMPTS FOR AN ACTIVE ROUTE 40 ROUTE PAGE 2 X 42 PREFLIGHT PAGES PART 2 42 DEPARTURE ARRIVAL INDEX PAGE 43 DEPARTURES PAGE 45 NAVIGATION RADIO PAGE 46 PERFORMANCE INITIALIZATION PAGE 48 TAKEOFF REFERENCE PAGE 50 Section 6 FMC TAKEOFF AND CLIMB 50 INTRODUCTION 50 TAKEOFF PHASE 50 CLIMB PHASE 51 CLIMB PAGE 53 ROUTE LEGS PAGE 55 AIR TURN BACK 55 ARRIVALS PAGE 56 Section 7 FMC CRUISE 56 INTRODUCTION 56 LNAV MODIFICATIONS 56 RTE LEGS PAGE MODIFICATIONS 57 ADD WAYPOINTS 58 DELETE WAYPOINTS DO NOT USE FOR FLIGHT 59 CHANGE WAYPOINT SEQUENCE 60 REMOVE DISCONTINUITIES 61 DIRECT TO 61 MODIFICATION OF THE ACTIVE WAYPOINT 62 SELECT DESIRED WAYPOINT WPT PAGE 64 CRUISE PAGE 64 VNAV MODIFICATIONS 64 CRUISE CLIMB 65 CALCULATED STEP CLIMB 66 CRUISE DESCENT 67 EARLY DESCENT 68 NAVIGATION DATA 68 REFERENCE NAVIGATION DATA PAGE 69 FIX INFORMATION PAGE 71 IN FLIGHT POSITION UPDATE 72 ROUTE AND WAYPOINT DATA 72 ROUTE DATA PAGE 73 WIND DATA 73 WIND PAGE 75 PROGRESS PAGES 75 PROGRESS PAGE 1 77 PROGRESS PAGE 2 79 POSITION REPORT PAGE 81 Section 8 FMC DESCENT AND APPROACH 81 INTRODUCTION 81 EARLY DESCENT 82 DESCENT 82 DESCENT PAGE 84 DESCENT FORECAST PAGE 85 APPROACH 86 ARRIVALS PAGE IFR APPROACHES 88 APPROACH REFERENCE PAGE 89 HOLDING 90 HOLD PAGE FIRST HOLD 92 HOLD PAGE EXISTI
11. 2011 Captain Sim www captainsim com 39 DO NOT USE FOR FLIGHT 2 ORIGIN Entry must be a valid ICAO identifier in the navigation database made automatically when a company route is entered enables direct selection of departure and arrival procedures required for route activation inhibited in flight for active route Entry on the ground deletes existing route 3 RUNWAY Enter the applicable runway for the origin airport Runway must be in the navigation database Entry e is optional e causes MOD to display in the title if route is active e can be selected on the DEPARTURES page 4 Route RTE 2 Push displays the RTE 2 page 1 x Allows access to an inactive route for entry modification or activation Inactive route modifications e do not alter the active route e do not change the inactive RTE page title Prompt changes to RTE 1 when RTE 2 is displayed 5 Destination DEST Entry must be a valid ICAO identifier in the navigation database made automatically when a company route is entered required for route activation displays MOD in page title if entered in an active route 6 Flight Number FLT NO Enter the company flight number Entry e optional for activation of the route limited to 10 characters included in the PROGRESS page title propagated to RTE 2 page deleted at flight completion 7 Company Route CO ROUTE A previously saved route can be loaded from file by entering the company route id
12. 94 DO NOT USE FOR FLIGHT 4 Quadrant Radial QUAD RADIAL The holding quadrant and radial are entered Valid entry is X XXX XX XXX or XXX example NE 040 Automatically changes INBD CRS DIR to agree 5 Inbound Course Direction INBD CRS DIR Displays the holding inbound course and turn direction Valid entry is XXX inbound course XXX X inbound course turn direction X or X turn direction Automatically changes QUAD RADIAL to agree 6 LEG TIME Default display is 1 0 MIN minute at or below 14 000 feet or 1 5 MIN above 14 000 feet Displays if a LEG DIST is entered Valid entry is X X X or X in minutes from 0 1 to 9 9 When climbing descending through 14 000 feet with VNAV engaged and the SPD TGT ALT on line 1R displayed in large font the FMC adjusts leg time 1 0 MIN at or below 14 000 feet 1 5 MIN above 14 000 feet 7 Leg Distance LEG DIST Default display is NM if no leg distance has been entered or if a LEG TIME is entered 8 ERASE Erases all FMC modifications 9 Speed Target Altitude SPD TGT ALT Waypoint holding fix speed altitude constraint from the RTE LEGS page Manual entries are in large font During cruise an altitude entry below cruise altitude activates the descent page unless a new cruise altitude is entered Altitude entry must be at or below cruise altitude A speed entry requires an altitude constraint 10 FIX ETA Displays the ETA to the next passing of the hol
13. CAS and altitude example 240 8000 6 Economy ECON Push changes climb speed to ECON Must be executed Prompt is shown on line 5L when the climb mode is not ECON 7 Waypoint Constraint AT XXXXX Displays next airspeed and or altitude constraint at waypoint XXXXX FMC commands the slower of constraint speed or performance speed Constraints are entered on RTE LEGS page or are inserted as part of a SID Delete here or on RTE LEGS page Blank if no constraint exists 8 Transition Altitude TRANS ALT Transition altitude for origin airport contained in navigation database FMC uses 18 000 feet if transition altitude is not available Manually change transition altitude here or on DESCENT FORECAST page Valid entries are XXX XXXX XXXXX or FLXXX Altitude information displayed on the CDU changes from altitudes to flight levels above the transition altitude 9 Climb Direct CLB DIR Push deletes all waypoint altitude constraints between the airplane altitude and the MCP altitude FMC cruise altitude is not affected Blank if no constraints exist MANUAL Part V Flight Management System 55 DO NOT USE FOR FLIGHT ROUTE LEGS PAGE The RTE LEGS page is used to evaluate and modify the planned route of flight during the climb and to add or delete waypoint constraints to comply with the ATC clearance The data on the RTE LEGS page comes from preflight entries made on the route and departure pages and from
14. Captain Sim www captainsim com 12 DO NOT USE FOR FLIGHT Section 3 FLIGHT MANAGEMENT SYSTEM OPERATION When first powered the FMS is in the preflight phase As a phase is completed the FMS changes to the next phase in this order preflight takeoff climb cruise descent approach flight complete PREFLIGHT During preflight flight plan and load sheet data are manually entered into the CDU The flight plan defines the route of flight from the origin to the destination and initializes LNAV Flight plan and load sheet data provide performance data to initialize VNAV Required preflight data consists of e initial position e route of flight e performance data e takeoff data Optional preflight data includes e navigation database selection e route 2 e SID e STAR Each required or optional data item is entered on specific preflight pages Preflight starts with the IDENT page If the IDENT page is not displayed it can be selected with the IDENT prompt on the INIT REF INDEX page Visual prompts help the flight crew select necessary CDU preflight pages Preflight pages can be manually selected in any order After the necessary data on each preflight page is entered and checked push the lower right line select key to select the next preflight page When ACTIVATE is selected on the ROUTE page the execute EXEC light illuminates Push the EXEC key to make the route active Use the departure arrival DEP ARR page to sel
15. DO NOT USE FOR FLIGHT ARRIVALS PAGE IFR APPROACHES The arrivals page allows selection of an approach standard terminal arrival route STAR and an arrival transition to the destination airport This page can also be used to view data about a selected airport that is not the destination Route 1 and route 2 have separate arrival pages The approaches STARS and transitions are shown and selected on this page Selecting Options Selecting an approach STAR or descent transition option shows lt SEL gt inboard of the selection and makes a route modification The other options within the same category are removed from the list When the modification is executed lt SEL gt changes to lt ACT gt Select another page and return to ARRIVALS to show all options the applicable lt SEL gt or lt ACT gt prompts are shown Less than half way to destination and less than 400 miles from origin displays departure airport KBFI 172 STARS PROACHES CHINS2 ILS 31L EPH4 ILS13R 00 More than half way to destination or more than 400 miles from origin displays 2 3 4 1 Page Title destination airport KMWH ARRIVALS STARS RTE IMP PROACHES POTHS1 lt SEL gt lt SEL gt ILS 32R TRANS TRANS EAT BATUM ELN The airport identifier is shown in the title Airports with more than 5 runways or STARs produce multiple arrivals pages 2 Standard Terminal Arrivals STARS Lists the STARS for the ai
16. FL 350 100 085 is entered at waypoint OED All waypoints in the route have the OED wind data Then additional wind data entered at OAK changes the wind data at OAK and through the end of the route 100 085 100 085 100 085 100 085 100 085 100 085 100 085 BTG OED RBL OAK AVE CRM PJM First Waypoint COED at FL350 100 085 wind entered at OED 100 7085 100 85 100 85 150 120 150 7120 150 120 150 120 BTG OED RBL OAK AVE CRM PJM Second Waypoint OAK at FL350 150 120 wind entered at OAK Entered winds are mixed with sensed winds for performance calculations The FMC uses entered winds for predictions far ahead of the airplane and sensed winds close to the airplane The FMC mixes these winds for predictions in between Sensed winds are displayed on the HSI and on progress page 2 WIND PAGE The wind page is used to enter forecast winds and temperatures at specific altitudes for specific waypoints to enhance VNAV performance The FMC calculates step climb points based on the wind effect The wind page displays waypoint wind data for one to four altitudes per waypoint This data can be uplinked or manually entered The altitudes are entered first The altitudes can be entered in any order and are sorted and displayed in ascending order Wind speed and direction are entered for the specific altitudes OAT can be entered for any one altitude The FMC calculates the temperature for the entered alti
17. FLIGHT ROUTE PAGE 2 X The subsequent route pages 2 X through X X display route segments in air traffic control format Route segments are defined as direct routing airways or procedures with start and end points such as waypoints fixes navaids airports or runways More waypoints for each route segment are shown on the RTE LEGS page 1 2 EPH amp CINTC amp ACTIVATE gt The VIA column displays the route segment to the waypoint or termination in the TO column Enter the path which describes the route segment between the previous waypoint and the segment termination Enter an airway in the VIA column and boxes display in the TO column DIRECT is entered as a result of entering a TO waypoint first Valid airways must e contain the previous TO waypoint or e intersect the previous VIA route segment Dashes change to DIRECT if the TO waypoint is entered first Dashes are displayed for the first VIA beyond the end of the route Invalid VIA entries result in the scratchpad message INVALID ENTRY Invalid VIA entries are e airways routes which do not contain the TO waypoint of the previous line or e airways that do not intersect the previous airway e airways or company routes that are not in the navigation database The start and end waypoints determine whether the entered airway is valid The route segment must contain the waypoint entered in the TO position The TO waypoint of the previous r
18. FLT Status Displays COMPLETE if all required pre flight entries have been made Displays a prompt to access a pre flight page where further entries are required if pre flight is not complete 757 Captain FLIGHT MANUAL Part V Flight Management System 52 DO NOT USE FOR FLIGHT Section 6 FMC TAKEOFF AND CLIMB INTRODUCTION The takeoff phase of flight starts with the selection of takeoff thrust at the start of the takeoff roll The takeoff mode of the autoflight system provides flight director guidance until LNAV and VNAV are engaged after takeoff Preparation for this phase starts in the preflight phase and includes entry of the TAKEOFF REF page data The takeoff phase changes to the climb phase when climb thrust and VNAV are engaged The climb phase continues to the top of climb point where the cruise phase starts AKEOFF PHASE When changes are made to the departure runway and SID the DEPARTURES and TAKEOFF REF pages must be modified to agree The modified data are entered the same as during preflight During takeoff the autothrottle commands the selected thrust and the autoflight system provides pitch and roll commands through the flight director FMC roll commands are provided when LNAV is engaged CLIMB PHASE When climb thrust and VNAV are engaged the FMC provides pitch commands to maintain the climb speed until the acceleration height is reached At the acceleration height the FMC commands acceleration to
19. OFFPATH DES 1 Descend Now DES NOW The DES NOW prompt is shown on the descent page when the cruise phase is active Reset the MCP altitude and select the DES NOW prompt and execute to start an early descent The descent page becomes active and the airplane starts a VNAV ECON descent at ECON descent speed Upon reaching the planned descent path VNAV commands pitch to maintain the planned descent path and ECON speed 757 Captain FLIGHT MANUAL Part V Flight Management System 71 DO NOT USE FOR FLIGHT NAVIGATION DATA REFERENCE NAVIGATION DATA PAGE The reference navigation data page displays data about waypoints navaids airports and runways Use this page to inhibit FMC position updates from radio navaids INIT REF INDEX NAV DATA gt REF NAV DATA F 113 T E 3 LATITUDE LONGI D U N50 36 4 w082 16 MAG VAR ELEVATIO E15 1600F NAVAID INHIBIT VOR ONLY INHIBIT VOR DME NAV OFF e gt 0N gt 1 Identifier IDENT Valid entries are any waypoint navaid airport or runway from the navigation database Only runways at the destination airport can be entered Entry changes to dashes when page is exited and then reselected 2 LATITUDE Displays latitude of entered identifier When the identifier is a runway the latitude displayed is for the threshold of the runway 3 Magnetic Variation MAG VAR LENGTH MAG VAR displays magnetic variation when entered identifier is a navaid LENGTH
20. The approach reference page shows approach planning data and approach reference speed VREF selection INIT co Cruise or Descent mode APPROACH REF GROSS WT FLAPS VREF 182 0 20 133KT 25 127KT 30 124kT KBFI13R 10001FT3048 ILS 13R FRONT CRS 110 9018F I 1 Gross Weight GROSS WT FMC calculated airplane gross weight is usually shown Manual entry is allowed in case the FMC calculated gross weight is unavailable or invalid or to allow previewing recommended approach speeds at other than the calculated FMC gross weight The manually entered gross weight is for reference only and is deleted when a different page is selected Permanent changes to gross weight may only be made on the PERF ESTIT page Shows boxes when gross weight is not available from the FMC Valid entry is XXX X 2 Runway Length The shown runway reference changes based on route progress The destination runway is the reference when the present position is more that halfway to the destination or more than 400 NM from the origin airport The origin airport runway is the reference when less than halfway or less than 400 NM from the origin airport Shows the length in feet and meters of the referenced runway 3 ILS Display is blank prior to entering a destination runway in the active route Displays the runway corresponding ILS frequency and facility identifier from the navigation database for the runway shown 4
21. and enter it into the discontinuity ACT RTE 1 LEGS I4 165 38NM BTG 810 FL350 THEN 1 ROUTE DISCONTINUITY OAK 810 FL350 121 165NM AVE 809 FL350 129 29NM 809 FL350 lt RTE 2 LEGS RTE DATA gt amp OAK MOD RTE 1 LEGS 1 4 165 3ENM BTG 810 FL350 158 47INM 2 OAK _810 FL350 121 165NM ave 809 FL350 B 1 Discontinuity The active route has a discontinuity after BTG The example shows how to fly direct from BTG to OAK Copy OAK to the scratchpad Any subsequent waypoint in the route can be selected to the scratchpad to remove the discontinuity 2 Continuous Route Select OAK to the boxes to remove the discontinuity If a waypoint which does not already exist on the route is entered into the boxes the discontinuity moves one waypoint further down the route 757 Captain FLIGHT MANUAL Part V Flight Management System 63 DO NOT USE FOR FLIGHT DIRECT TO If the airplane is not on the active leg segment LNAV may deactivate or it may not activate when armed This happens after the airplane crosses a discontinuity or is not on an intercept heading to the active leg segment Here are three ways to arm or activate LNAV e When the airplane is within 2 5 miles of the active leg push the LNAV switch LNAV activates and intercepts the active route leg e When more than 2 5 miles from the active leg push the LNAV switch when the airplane i
22. descent speed ECON SPD e economy speed based on cost index e shows CAS or Mach SEL SPD e shows when intermediate level off required below an existing speed constraint e shows when flight crew enters speed CAS or Mach value may be entered page title changes to ACT XXXKT DES or ACT M XXX DES lt ECON prompt appears at line 5L to allow selection of economy descent speed 4 Speed Transition SPD TRANS The transition speed is usually 10 knots less than the destination airport limiting speed from the navigation database When no airport limit speed exists the default speed of 240 knots is shown The transition altitude is the point that the transition speed is active for the destination airport When no altitude exists in the navigation database the default of 10 000 feet is shown Blanks when the transition has occurred Can be deleted 5 Speed Restriction SPD RESTR Speed restrictions not associated with specific waypoints are manually entered on this line Dashes before entry by flight crew Valid entry is a CAS and altitude example 240 8000 An entry creates a modification 6 ATXXXXX Shows the next waypoint constraint from the RTE LEGS page Line title shows e AT XXXXX the waypoint identifier e HOLD AT XXXXX e AT VECTORS e AT INTC The constraint is speed altitude Blank when no constraint exists Can be deleted on this page VNAV commands the lesser of constraint speed or present performance speed
23. flap setting Entry of a value after takeoff speeds are entered removes the speeds and displays the scratchpad message TAKEOFF SPEEDS DELETED ACCEL HT displays the acceleration height in feet above the origin airport VNAV commands acceleration at this altitude or at first flap retraction 2011 Captain Sim www captainsim com 51 DO NOT USE FOR FLIGHT Default value is from the AMI Valid flight crew entries are from 400 to 9999 feet above the origin airport elevation 2 THRUST Initially displays dashes and the thrust reference mode If an assumed temperature value is entered on the thrust management control panel the entered temperature is displayed here Valid flight crew entries are from 0 to 99 C or 32F to 21 OF F The entered value is displayed on EICAS Entry of a value after takeoff speeds are entered removes the speeds and displays the scratchpad message TAKEOFF SPEEDS DELETED 3 INDEX Push displays the INIT REF INDEX page 4 V Speeds Dashes are displayed before speeds are entered and when speeds have been deleted If performance data is changed after speeds are entered the speeds are deleted dashes are displayed and the scratchpad message TAKEOFF SPEEDS DELETED is displayed 5 TRIM Center of Gravity CG Valid entry is CG within the valid range After the CG is entered the FMC calculates and displays the stabilizer takeoff trim setting to the left of the CG entry 6 Pre Flight PRE
24. navigation database May be line selected to the scratchpad and inserted to the ACTVE line while on the ground 9 Company CO DATA Displays the last eight characters of the Airline Modifiable Information AMI part number 10 DRAG Fuel Flow FT Factors Displays the airplane drag and fuel flow correction factors 11 Position Initialization POS INIT Push displays the POS INIT page 757 Captain FLIGHT MANUAL Part V Flight Management System 32 DO NOT USE FOR FLIGHT POSITION INITIALIZATION PAGE The position initialization page allows entry of airplane present position for IRS alignment This page is also used to enter the heading when an IRS is in the ATT mode Inertial position not entered INIT REF INDEX lt POS POS INIT gt POS INIT N47 32 5 5 REF AIRPORT 2 GPS POS 3 1530Z N47 32 5 w122 18 7 6 4 8 lt INDEX 1 Reference Airport REF AIRPORT Entry of the reference airport displays the airport latitude longitude Optional entry Valid entries are ICAO four letter airport identifiers Removes previous GATE entry Entry blanks when airborne 2 GATE The gate entry allows further refinement of the latitude longitude position 2011 Captain Sim www captainsim com 33 DO NOT USE FOR FLIGHT Optional entry after reference airport entered 3 Coordinated Universal Time UTC UTC e displays time from captain s clock when operative otherw
25. route is modified MOD is displayed in the title and the execute light is illuminated 2011 Captain Sim www captainsim com 59 DO NOT USE FOR FLIGHT ADD WAYPOINTS Waypoints can be added to the route at any point Added waypoints are followed by route discontinuities First enter the waypoint name in the scratchpad Second locate the correct line in the flight plan and push the adjacent line select key The scratchpad waypoint name is put into the selected line The entered waypoint is connected to the waypoint above it via a direct route A route discontinuity follows the waypoint For example OED is typed into the scratchpad Push line select key 2L to put OED into line 2 The FMC assumes BTG direct OED RBL and the rest of the flight plan are kept but are put after the route discontinuity NTINUI pieces 000000 RTE DATA gt 1 Page Title MOD replaces ACT when modification is in progress ACT replaces MOD when ERASE is selected or execute key is pushed 2 Modified Waypoint OED waypoint entered into the route after BTG Modification creates a route discontinuity because OED was not in the active route The FMC now requires routing beyond OED 3 Discontinuity Discontinuity is corrected when applicable waypoint is entered in boxes 4 ERASE Push removes all modifications and shows active data Displayed when the FMC contains modified data Removed when the modifications are exe
26. the present route and displays as VAMO1 e ELN 30 is 30 miles before ELN on the present route and displays as ELNO1 HSI MAP DISPLAYS The route is displayed on the HSI in MAP and PLAN modes The display color and format represent the following status e an inactive route is displayed as a cyan dashed line an activated but not yet executed route is displayed as a white dashed line the active route is displayed in magenta modifications to an active route are shown as dashed white lines modified waypoints are displayed in white The HSI displays the FMC position at the apex of the airplane symbol All HSI map data displays relative to this apex ERTICAL NAVIGATION VNAV VNAV provides vertical profile guidance through the climb cruise and descent phases of flight SPEED ALTITUDE CONSTRAINTS VNAV controls the path and speed to comply with waypoint crossing constraints Waypoint crossing constraints are entered on the LEGS page waypoint line by pushing the applicable key on the right side of the CDU Values entered as part of a procedure and manually entered constraints are shown in large font FMC predicted values do not act as constraints and are displayed in small font Waypoints can have altitude or airspeed altitude constraints Speed constraint entries require an altitude constraint at the same waypoint All speed constraints are considered by the FMC as at or below constraints At or above altitude constraints are entere
27. 250 knots The VNAV commanded speed is limited by the airplane configuration At acceleration height VNAV commands a speed 5 knots below the flap placard speed Passing 10 000 feet VNAV commands an acceleration to the economy climb speed which is maintained until reaching the cruise altitude unless the climb profile contains other constraints During the climb VNAV complies with the LEGS page waypoint altitude and speed constraints A temporary level off for a crossing altitude restriction is accomplished at the commanded speed 2011 Captain Sim www captainsim com 53 DO NOT USE FOR FLIGHT CLIMB PAGE The climb page is selected by pushing the CDU VNAV function key while on the ground during takeoff or in climb The climb page is used to evaluate monitor and modify the climb path The data on the climb page comes from preflight entries made on the route and performance pages and from the FMC data bases When the airplane reaches the top of climb the FMC changes to the cruise mode the cruise page is displayed and the climb page data is blanked The FMC provides speed control in the climb mode to provided the best economy a fixed speed or the engine out speed In each mode the same type of data is shown on the page vay Climb mode 50KT CLB 1 3 AT LACRE 25004A SPD TRANS TRANS ALT 2507 10000 SPD RESTR a Wt WN 1 Page Title ACT is displayed when the climb phase is active The page title d
28. AYPOINTS VHF waypoints located at VHF navaids VOR DME LOC are identified by one two three or four character facility identifier Examples e Los Angeles VORTAC LAX e TyndallTACAN PAM e Riga Engure Latvia AN NDB waypoints located at NDBs are identified by use of the station identifier Example FORT NELSON CAN YE FIX WAYPOINTS Waypoints located at fixes with names containing five or fewer characters are identified by the name Examples e DOT e ACRA e ALPHA 15 DO NOT USE FOR FLIGHT LONG WAYPOINT NAMES Waypoints with more than five characters are abbreviated using the following rules sequentially until five characters remain For double letters one letter is deleted Example e KIMMEL becomes KIMEL Keep the first letter first vowel and last letter Delete other vowels starting from right to left Example e BAILEY becomes BAILY The next rule abbreviates names even further Apply the previous rule then delete consonants from right to left Example e BRIDGEPORT becomes BRIDGPRT then BRIDT Fixes with multiword names use the first letter of the first word and abbreviate the last word using the above rules sequentially until a total of five characters remain Examples e CLEAR LAKE becomes CLAKE e ROUGH ROAD becomes RROAD UNNAMED WAYPOINTS If an unnamed turn point intersection or fix is collocated with a named waypoint or navaid on a different route structure such as low alt
29. E CLIMB When VNAV is engaged resetting the MCP to an altitude higher than the current cruise altitude causes the new altitude to be displayed in the scratchpad of the CDU The altitude can then be entered on the CRZ ALT line on the cruise page When the modification is executed the airplane will climb to the new cruise altitude The CRZ page displays ACT ECON CRZ CLB STEP CLIMB Fuel and ETA predictions assume the airplane climbs at each predicted step climb point as airplane weight decreases FMC predicted step climb increments are based on the step size entered on the CRZ page Entering a step size of zero causes the FMC to assume a constant altitude cruise Flight crew entry of a step altitude on the CRZ page overrides the FMC step climb predictions Predicted step altitudes are displayed on the RTE LEGS page The distance and ETA to the next step point is displayed on the CRZ and progress pages Step points are displayed on the HSI map with a green circle and S C label CRUISE DESCENT The new cruise altitude can be entered on the cruise page When the modification is executed the CRZ page displays ACT ECON CRZ DES sN11 Can 757 Captain FLIGHT MANUAL Part V Flight Management System 21 DO NOT USE FOR FLIGHT Note A cruise descent will not provide speed adjustments to comply with speed restrictions or transition altitude speeds Transition or speed restrictions must be maintained by flight crew action MODE CON
30. E FOR FLIGHT 5 Direction and Speed DIR SPD Displays dashes after altitude flight level entry in the ALT line Enter predicted wind direction and speed for the altitude Values propagate to other waypoint winds Propagated values display in small font Manual entries display in large font 6 Altitude Outside Air Temperature ALT OAT Enter altitude and OAT The altitude for OAT does not have to be one of the wind altitudes The FMC uses standard lapse rate to calculate the temperature at the other altitudes Entries must be executed 7 Route Data RTE DATA Push displays the RTE DATA page PROGRESS PAGES The progress page displays general flight progress data PROGRESS PAGE 1 Page one of the progress pages displays general data about e waypoints active and next e destination e FMC speed e next VNAV profile point The page title displays the company flight number entered on the RTE page BO56 PROGRESS 1 2 6 1 7 2 3292 21 7 3 13522 18 5 8 SEL SPD TO T D 4 13302 45M 9 5 POS REPORT POS REF gt 10 1 TO Active waypoint is displayed Can not be modified 2011 Captain Sim www captainsim com 79 DO NOT USE FOR FLIGHT 2 NEXT Waypoint after TO waypoint is displayed Can not be modified 3 Destination DEST When the page is selected the active route destination is displayed Any waypoint or airport in navigation database can be entered over the destina
31. ECON CRZ CLB 2 3 2 ACT ECON CRZ 2 3 1 During Cruise Climb VNAV page title displays ACT ECON CRZ CLB in a climb to a new cruise altitude ECON is replaced by the selected speed if other than ECON 2 End of Cruise Climb 2011 Captain Sim www captainsim com DO NOT USE FOR FLIGHT VNAV page title returns to ECON CRZ after level off at cruise altitude 67 tain FLIGHT MANUAL Part V Flight Management System 68 DO NOT USE FOR FLIGHT CALCULATED STEP CLIMB When a non zero value is entered into the STEP SIZE line on the PERF INIT or CRZ page the FMC calculates optimum points for step climbs as the airplane performance permits The climb altitude is determined by the value in STEP SIZE Multiple step climbs are possible based on performance and route length VNAV commands the step climbs if the MCP altitude and the FMC CRZ ALT are set to the new altitude AB345 PROGRESS 1 2 TO DTA ETA FUEL ELN 17 13052 35 0 5 NEXT auInt 42 13292 33 8 amp DEST 532 s EE SPD en rae 5 210 130727 12N 1 ACT ECON CRZ CRZ ALT FL350 3 ECON SPD 810 1300z 12Nm 4 EPR KORD ETA FUEL 1 3932 20302 14 5 STEP SIZE OPT MAX FL330 FL390 5 ENG OUT gt OOO000D LRC gt 1 TO STEP CLIMB When the step climb start point is the next VNAV event the line title changes to TO STEP CLIMB Displays the ETA and DTG to the point where the step climb starts If the airplane passes the step clim
32. FMC to compute maximum altitude and maneuver margin to buffet Displays default center of gravity in small font A flight crew entered value displays in large font 9 STEP SIZE Displays the climb altitude increment used for planning the optimum climb profile Default value is ICAO which provides a 2000 foot step below FL290 and a 4000 foot step above FL290 Valid manual entries are 0 to 9000 in 1000 foot increments In flight entries are inhibited In flight step size changes are made on the CRZ page For a non zero entry performance predictions are based on step climbs at optimum points For a zero entry performance predictions are based on a constant CRZ ALT 10 TAKEOFF Push displays the TAKEOFF REF page 757 Captain FLIGHT MANUAL Part V Flight Management System DO NOT USE FOR FLIGHT 49 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 50 DO NOT USE FOR FLIGHT TAKEOFF REFERENCE PAGE The takeoff reference page allows the input of the final performance data required for takeoff Entries on the takeoff reference page complete the normal FMC preflight If any required preflight data has been omitted prompts are displayed to access the page where data is missing PERF INIT INIT REF INDEX TAKEOF F gt AKEOFF REF CCEL HT F EOFF REF EL HT lt INDEX 000000 1 Flap Acceleration Height FLAP ACCEL HT Enter a valid takeoff
33. LIGHT ON GPS position data is available to the FMC ON displays in large letters OFF displays in small letters 5 Latitude Longitude LAT LON or Bearing Distance BRG DIST Push alternately changes the display of position data on POS REF 2 4 3 4 and 4 4 to latitude longitude format or bearing distance format The page illustration is shown in the bearing distance display mode POSITION REFERENCE PAGE 4 4 POS REF 3 4 POS INIT 1 4 POS REF IR L GS 47 33 0 W122 18 2 152kKT IR C 1 47 33 0 W122 18 2 152KT 3 IRS R 47 33 0 w122 18 2 152KT 2 LAT LON gt 4 On position reference page 4 the calculated positions and ground speeds from the left center and right IRS are displayed Positions can be displayed in the bearing distance or latitude longitude format 1 IRS L C and R Displays the position of the Left Center and Right IRS Positions can be displayed in latitude longitude or as bearing and distances from the FMC position 2 INDEX Push displays the INIT REF INDEX page 3 Ground Speed GS Displays the ground speed calculated by each IRS The displayed values are frozen when the engines are shut down after flight until power is removed 757 Captain FLIGHT MANUAL Part V Flight Management System 38 DO NOT USE FOR FLIGHT 4 Latitude Longitude LAT LON or Bearing Distance BRG DIST Push alternately changes the displayed position between latitude longitude fo
34. MPUTER FMC 11 CONTROL DISPLAY UNITS CDUS 12 Section 3 FLIGHT MANAGEMENT SYSTEM OPERATION 12 PREFLIGHT 12 TAKEOFF 12 CLIMB 12 CRUISE 13 DESCENT 13 APPROACH 13 OPERATIONAL NOTES 13 TERMINOLOGY 14 LATERAL NAVIGATION LNAV 14 WAYPOINTS 14 NAVAID WAYPOINTS 14 FIX WAYPOINTS 15 LONG WAYPOINT NAMES 15 UNNAMED WAYPOINTS 15 PROCEDURE ARC FIX WAYPOINT NAMES 16 PROCEDURE FIX WAYPOINTS 16 DUPLICATE WAYPOINTS 17 CONDITIONAL WAYPOINTS 17 MANUALLY ENTERED LATITUDE LONGITUDE WAYPOINTS 17 MANUALLY ENTERED PLACE BEARING DISTANCE OR PLACE BEARING PLACE BEARING WAYPOINTS 17 MANUALLY ENTERED AIRWAY CROSSING WAYPOINTS 18 MANUALLY ENTERED ALONG TRACK WAYPOINTS 18 HSI MAP DISPLAYS 18 VERTICAL NAVIGATION VNAV 18 SPEED ALTITUDE CONSTRAINTS 19 TAKEOFF AND CLIMB 20 CRUISE 20 CRUISE CLIMB 20 STEP CLIMB 20 CRUISE DESCENT 21 DESCENT 22 EARLY DESCENT DO NOT USE FOR FLIGHT 23 APPROACH 23 CRUISE AND DESCENT PROFILE NONPRECISION APPROACH 25 DATA ENTRY RULES 25 ALTITUDE ENTRY 25 AIRSPEED ENTRY 25 DATA PAIRS 26 Section 4 FLIGHT MANAGEMENT COMPUTER 26 FMC DATABASES 26 THRUST MANAGEMENT Section 5 FMC PREFLIGHT 27 INTRODUCTION 27 PREFLIGHT PAGE SEQUENCE 27 MINIMUM PREFLIGHT SEQUENCE 28 SUPPLEMENTARY PAGES 28 PREFLIGHT PAGES PART 1 28 INITIALIZATION REFERENCE INDEX PAGE 29 IDENTIFICATION PAGE 31 POSITION INITIALIZATION PAGE 33 POSITION REFERENCE PAGES 33 POSITION REFERENCE PAGE
35. Management System 61 DO NOT USE FOR FLIGHT CHANGE WAYPOINT SEQUENCE Waypoints moved from one position in the flight plan to another do not cause route discontinuities The waypoint may be manually typed or copied from any of the RTE LEGS pages To copy the waypoint push the line select key adjacent to the waypoint The example below shows the flight plan being modified to fly from BTG direct OAK Push the line select key adjacent to OAK to put OAK in the scratchpad Push the line select key adjacent to RBL RBL is removed from the flight plan and the routing is direct from BTG to OAK to AVE The modification does not cause a route discontinuity Several waypoints can be removed from the flight plan at a time with this method 810 FL 810 FL 810 FL 809 7FL lt RTE 2 LEGS RTE DATA gt OAK 000000 000000 EGS 810 FL3 0 810 FL3 809 FL3 1 Active Route The active route shows RBL followed by OAK and AVE The clearance is to fly from BTG direct OAK The OAK waypoint is selected to the scratchpad 2 Change OAK s Sequence OAK is selected to the waypoint after BTG RBL is removed with no discontinuity MANUAL Part V Flight Management System 62 DO NOT USE FOR FLIGHT REMOVE DISCONTINUITIES A discontinuity exists when two waypoints are not connected by a route segment To remove a discontinuity copy the subsequent waypoint from the route into the scratchpad
36. NG HOLD 93 Section 9 FMC MESSAGES 93 FMC ALERTING MESSAGES 94 FMC ADVISORY MESSAGES 94 CDU ANNUNCIATOR LIGHTS 95 Section 10 NAVIGATION DATABASE 95 CAPTAIN SIM NAVIGATION DATABASE FILES FORMAT 98 CUSTOM TERMINAL PROCEDURES 98 AERONAUTICAL DATA 99 CUSTOMER CARE 757 Captain FLIGHT MANUAL Part V Flight Management System 6 DO NOT USE FOR FLIGHT Section 1 FLIGHT MANAGEMENT NAVIGATION CONTROLS AND INDICATORS FLIGHT MANAGEMENT SYSTEM CONTROL DISPLAY UNIT CDU m r A m e 5 B B B B g B B B mn we EG O 5 Cg Es ro GE Fes e rem E 8 a 2 5 ADM 6 OOS HOWL IOOO RMR 0O00 WWWWW O O B be 1 Control Display Unit CDU Display Displays FMS data pages 2 Line Select Keys moves data from scratchpad to selected line moves data from selected line to scratchpad selects page procedure or performance mode as applicable deletes data from selected line when DELETE is displayed in scratchpad 3 Display DSPY Light Illuminated white e when RTE page 3 or greater RTE LEGS page 2 or greater RTE DATA page 2 or greater is displayed e when airplane is not in holding pattern displayed on HOLD page 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 7 DO NOT USE FOR FLIGHT e when modification is in progress and any RTE RTE LEGS RTE DATA HOLD or VNAV page is displayed 4 FAIL L
37. OR frequencies identifiers tuning status and current radial for both VOR receivers The VORs can be remotely tuned from this page RAD NAV RADIO VOR R 1 ELNP117 90 ILS MLS 109 80 162 PARK PRESELECT 1 VOR Frequency and Tune Status The tuning status is displayed adjacent to left and right VOR frequencies Entry of a frequency or identifier remotely tunes a VOR The FMC autotunes VORs and their related DMEs for procedure flying and radio positions The tuning status displays are e A autotuning FMC selects a navaid for best position orientation e P procedure autotuning FMC selects navaids for approach or departure procedure guidance e R remote tuning VOR frequency or identifier has been entered by the flight crew on the NAV RADIO page e M manual VOR is manual tuned using the VOR control panels on the glareshield Manual tuning takes priority over FMC autotuning Valid entries e VOR or non ILS DME identifier e VOR frequency XXX X or XXX XX The identifier and frequencies are green and tuning status is white 2 RADIAL Displays the current radial from the left and right VOR stations to the airplane 3 4 ADF Frequency 5 ILS Frequency and Course The ILS receivers operate in the automatic or manual tuning mode The FMC commands the frequency and course selection in the automatic mode When the ILS is not necessary the FMC sets the ILS to PARK Airplane position on the route determines the IL
38. R FLIGHT e runways for selected SID remain and others no longer display 2 Transitions TRANS Displays transitions compatible with the selected SID Push e selects transition for entry in the route e other transitions no longer display 3 ERASE or INDEX Erase displays when a route modification is pending INDEX displays when no route modification is pending ERASE push removes selections not executed and displays the entire departure page Other vertical or lateral modifications will be erased also INDEX push displays the DEP ARR INDEX page 4 RUNWAYS Displays a list of runways for the selected airport The runway selected on the RTE 1 X page displays as lt SEL gt or lt ACT gt Push e selects runway for use in the route All other runways no longer display e SIDs associated with selected runway remain all others no longer display e subsequent change of a runway deletes departure procedures previously selected 5 lt SEL gt lt ACT gt Selecting an option displays lt SEL gt inboard of the option and creates a route modification After executing the modification lt SEL gt becomes lt ACT gt Executing a modification or leaving the page and returning displays all options and the lt SEL gt or lt ACT gt prompts 6 ROUTE Push displays the related RTE page 46 DO NOT USE FOR FLIGHT NAVIGATION RADIO PAGE VOR navigation radios are normally autotuned by the FMC The NAV RADIO page displays the tuned V
39. S operating mode The operating mode displays are PARK The ILS is not being used and is not tuned XXX XX YYY PARK The ILS is tuned for the selected approach but is not being used A indicates autotuning under FMC control for approach guidance M indicates the ILS is manually tuned tain FLIGHT MANUAL Part V Flight Management System 47 DO NOT USE FOR FLIGHT ILS manual tuning requires entry of a frequency and course NOTE due to Flight Simulator limitations entering an ILS frequency also tunes the VOR L radio to the same frequency This also happens when the ILS is autotuned The VOR L tune status indicates P procedural autotuning in this case PERFORMANCE INITIALIZATION PAGE The performance initialization page allows the entry of airplane and route data to initialize performance calculations This data is required for VNAV operation On ground IRS position entered INIT REF ACT RTE 1 INIT REF INDEX PERF INIT gt G PERF INIT a minka cost TER 2 30 0LB CALC CT 7 eaves G i 9 5 He lt innex TAKEOFF gt 10 1 Gross Weight GRWT Airplane gross weight can be entered by the flight crew or calculated by the FMC after entry of zero fuel weight Valid entry is thousands of pounds with a decimal hundreds optional Entering the zero fuel weight first displays calculated gross weight Entry of a value after takeoff speeds are selected removes the speeds and
40. STAR and or IAP data of the named airport into corresponding db file in accordance with Section 10 Navigation Database Captain Sim Navigation Database Files Format part of this Manual 3 Copy the new db files into FSX Root Folder Captain_Sim navigation user folder Note Custom procedures has a priority over original procedures so if available FMS use custom procedures from the user folder and ignore procedures from original database You may add the _stars db _sids db _iaps db files in any combination just one two or all three files FMS use whatever it finds in the user folder taking the rest from original database AS soon as you remove custom procedures files from the user folder FMS will automatically switch back using original database 4 Run MS FSX and test the custom procedures If you get any error just delete the corrupted files from user folder We support Original FMS database only Original database aeronautical data database included into the original product pack AERONAUTICAL DATA Aeronautical database AIRAC Cycle 0903 included into the original product pack is provided by NAVIGRAPG amp NAVData Service Updates can be purchased at NAVIGRAPG amp NAVData web site We support Original FMS database only Original database aeronautical data database included into the original product pack 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Manag
41. T HOLD annunciates To reinitiate continue the descent the MCP altitude must be reset and VNAV re engaged When a speed transition altitude is included in the descent path typically 250 kts below 10 000 ft the descent path angle shallows temporarily to slow to the transition altitude airspeed Below the speed transition altitude the descent path angle increases to maintain a target speed 10 kts below the transition speed typically 240 kts to allow for unforcast tailwinds Final deceleration is commanded to arrive at the final approach fix or the outer marker at 170 kts It is the flight crew s responsibility to extend flaps as appropriate when the final deceleration segment to 170 kts is initiated by VNAV Note Adding deleting or revising altitude constraints after VNAV enters the descent mode causes a recalculation of the descent path by the FMC This may cause VNAV to revert to speed reversion mode VNAV SPD if the newly calculated path is above or below the old path far enough so as to prevent the path from remaining captured EARLY DESCENT An early descent is initiated by forcing the FMC into the descent phase before reaching the top of descent point VNAV commands a descent at a reduced descent rate until the idle descent path is intercepted so we e T N D a ain Old CRZ ALT New CRZ ALT 1 DES NOW Use the DES NOW prompt on the DES page VNAV starts an early descent and captures the idl
42. TROL PANEL SPEED INTERVENTION VNAV PTH VNAV PTH Altitude Restriction VNAV PTH amp Altitude 4 Restriction VI Speed Intervention Pitch Modes With VNAV engaged pushing the IAS MACH selector enables speed intervention Speed intervention allows the flight crew to change airplane speed with the IAS MACH selector The above illustration shows VNAV mode for each phase of flight during speed intervention In VNAV PTH mode thrust controls speed in VNAV SPD mode pitch controls speed In a path descent VNAV PTH changes to VNAV SPD during speed intervention In all other phases the pitch mode remains the same In approach phase see Approach topic this section during speed intervention pitch mode remains in VNAV PTH and the vertical path is maintained regardless of IAS MACH selector changes DESCENT The FMC calculates a descent path based on airspeed and altitude constraints and the end of descent E D point An E D point is created by the FMC when an arrival or approach procedure is selected on the ARRIVALS page and incorporated into the flight plan During cruise an E D point is also created when an altitude constraint less than cruise altitude is added to a downstream waypoint on the LEGS page The FMC calculates the top of descent T D point after the E D is entered T D is the point where the cruise phase changes to the descent phase The T D is displayed on the HSI as a green circle with the label T D Th
43. adial RteDist is route RouteType describes which part of the procedure this leg belongs to distance 1 SID runway transition 2 SID common part 3 SID enroute transition 4 STAR runway transition 5 STAR common part 6 STAR enroute transition For example there can exist several versions of a SID for different runways they will have the same lines with RouteType of 2 or 3 and different lines with RouteType of 1 describing paths from different runways Or SID blocks with different lines of RouteType 3 show similar SIDs with different enroute transition waypoints Speed is speed restriction at this leg TransitionAlt is Transition altitude for this procedure TransitionID is the name of transition waypoint this procedure applies to Turn can be L or R for left or right turns as demanded by procedure Airports Held in Airports db file File format Elevation ICAO Latitude Longitude Airways Held in Airways db file File format AirwayName Bidirectional Latitude Longitude Type WaypointName Bidirectional equals to either 1 or 0 Type ATLANTIC BAHAMA CORRIDOR ADVISORY DIRECT MILITARY NORTHAMERICAN OCEANIC RNAV SUBSTITUTE TACAN AIRWAY OANDUNBRWNH 100 DO NOT USE FOR FLIGHT Root points Held in Fixes db file File format ID Latitude Longitude UsageCode UsageCode HL LL BOTH RNAV TERMINAL UBRWNeE Stations VOR and NDB
44. and VNAV must be selected The system must be carefully monitored for errors following e activation of a new data base e power interruption e IRS failure When operating far off the route the FMC may not sequence the active waypoint when the airplane passes abeam the waypoint LNAV can only capture the active leg It cannot capture an inactive leg in the active route The DIRECT TO procedures can be used to create an active leg for capture When a waypoint is in the route more than once certain route modifications such as DIRECT TO and HOLD use the first waypoint in the route When entering airways in a route page the start and end waypoints must be in the data base Otherwise the route segment must be entered as a DIRECT leg ERMINOLOGY The following paragraphs describe FMC and CDU terminology Active flight plan data being used to calculate LNAV or VNAV guidance commands Activate the procedure to change an inactive route to the active route for navigation It is a two step procedure e select the ACTIVATE prompt e push the execute EXEC key Altitude constraint a crossing restriction at a waypoint Delete using the delete DEL key to remove FMC data and revert to default values dash or box prompts or a blank entry Econ a speed schedule calculated to minimize operating cost The economy speed is based on the cost index A low cost index causes a lower cruise speed Maximum range cruise or the minimum fuel sp
45. b point and has not started to climb the ETA and DTG are replaced with the word NOW When the FMC calculates that a step climb is not advised the ETA and DTG are replaced with the word NONE 2 STEP SIZE Displays the default step climb size of ICAO Valid entries are altitudes from 0 to 9000 in 1000 foot increments Used for calculation of optimum step point and step climb predictions Deletion of a manual entry defaults back to ICAO 69 DO NOT USE FOR FLIGHT 3 STEP TO Displays a calculated step climb altitude based on the step size Blank when e there is no active flight plan e less than 200 NM from the T D point e less than 500NM from the destination e step size is zero 4 AT Displays the ETA and DTG to the step climb point Displays NOW when past the calculated step climb point Line title changes to TO T D when within 200 NM of the top of descent point ETA and DTG are relative to the T D point The data is the same as displayed on the PROGRESS page 5 Optimum Altitude and Maximum Altitude OPT MAX OPT displays the most economical altitude to fly based on gross weight and the active cruise speed MAX displays the two engine maximum altitude based on gross weight climb and cruise speeds within the speed envelope and sufficient excess thrust to provide a specified residual rate of climb capability CRUISE DESCENT Cruise descents can be started in the cruise phase when the airplane is more than 50
46. cuted 5 ROUTE DISCONTINUITY Line title separates route segments when there is a discontinuity 757 Captain FLIGHT MANUAL Part V Flight Management System 60 DO NOT USE FOR FLIGHT Note Performance predictions to destination on the PROGRESS page are calculated assuming the route of flight is direct between waypoints on either side of a route discontinuity DELETE WAYPOINTS Use the RTE LEGS page to remove waypoints from the route The active waypoint can not be deleted Two methods to remove a waypoint are e delete the waypoint with the DEL function key e change the sequence of other waypoints The data in the route before the deleted waypoint does not change A discontinuity is put in the route when the DEL function key is used to remove a waypoint 1 _810 FL350 337NM 810 FL350 142N 8 810 FL350 165 NM _809 FL350 29NM 809 FL350 000000 000000 lt RTE 2 LEGS RTE DATA gt 2 DELETE LEGS 1 4 ENM _810 FL350 OD RTE 1 3 o ROUTE DISCONTINUITY OAK 810 FL350 000 1 Active Route The active route shows RBL followed by OAK and AVE 2 DELETE Entry Pushing the DEL function key arms the delete function and selects DELETE to the scratchpad 3 Discontinuity With DELETE in the scratchpad pushing the line select key for RBL deletes the waypoint Boxes replace RBL and a route discontinuity is displayed 757 Captain GHT MANUAL Part V Flight
47. d holding pattern however the airplane remains in protected FAA or ICAO limits 2011 Captain Sim www captainsim com 757 Captain GHT MANUAL Part V Flight Management System 93 DO NOT USE FOR FLIGHT HOLD PAGE FIRST HOLD The hold page is used to enter a holding pattern into the route When the flight plan does not have a holding pattern push the HOLD function key to show the RTE X LEGS page with the HOLD AT line The holding page displays actual or default data about the holding pattern Entries make route modifications which can be erased or executed Active holding patterns are magenta on the HSI First hold in route ACT RTE 1 LEGS 144 ACT RTE 1 HOLD 171 FIX SPD TGT ALT BATUM 220 4000 QUAD RADIAL FIX ETA lt E 1424 52 INBD CRS DIR 231 L TURN LEG TIME 1 0MI1IN LEG DIST 1 HOLD AT When the HOLD function key is pushed and no holding pattern exists in the route the RTE LEGS page displays prompts to enter the holding fix Enter the holding fix to show the RTE X HOLD page Normally a route waypoint is entered as the holding fix If a waypoint that is not part of the active route is entered the scratchpad message HOLD AT XXX appears where XXX is the entered waypoint The holding fix can then be inserted in the route in the proper sequence 2 HOLD AT Present Position PPOS Selects the airplane present position as the holding fix 3 Holding FIX Displays the holding fix
48. d in the Captain_Sim navigation subfolder of FS installation folder The data within the files is organised into blocks each block describing a single SID or STAR procedure Each such block is identified by a header enclosed in braces which has this format BIKF RW02 ALD1A ALDAN Which specifies the Airport the Runway to which the procedure applies this can be ALL meaning this procedure exists for all runways the Procedure name and the Transition waypoint Each block then contains several lines each describing a leg in the procedure Each line contains 19 values separated by semicolon that is If any value in line is not available it is not indicated but its field remains I e any line should contain eighteen semicolons anyway SID and STAR SID are held in SIDs db file STARs are held in STARs db file IAPs are held in IAPs db file The format for the three files is identical Airport applicable runways SID name transition name Alt1 Alt2 AltType ArcRadius Bearing Distance Fix FixLat FixLon MagCourse Path RecNav RteDist RouteType Speed TransitionAlt TransitionID Turn Where Alti is the altitude constraint Alt2 is the second altitude constraint for BETWEEN type constraints AltType describes the type of following altitude constraints and can be for AT OR ABOVE for AT OR BELOW B for BETWEEN or for AT type constraints ArcRadius is radius for RF type legs Bear
49. d with a suffix letter A example 220A At or below altitude constraints are entered with a suffix letter B example 240B Mandatory altitude constraints are entered without any suffix letter example 270 Altitude constraints with two altitudes may be entered in either order The lower altitude constraint followed by a suffix letter A and the upper altitude constraint followed by a suffix letter B example 220A240B or 240B220A 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 19 DO NOT USE FOR FLIGHT AKEOFF AND CLIMB a a A E Ce Ws Jo w T oa HQ b y z a Yv w Fl 2 N g wn 5 N gt V ew sai T Z i zu ai w F a a z 2 2 a o D E 8 a E 7 g T lt _ _ jOox y S a lt w 3 n Q G A A m A 28 D y N 58 7 I A U q 5 3 RAS amp m wv K 9 T K a gt 1 Takeoff The takeoff TO pitch mode is used for the takeoff and initial climb VNAV is normally engaged at 1000 feet and pitch guidance continues to maintain the target airspeed During takeoff the target airspeed is between V2 15 and V2 25 knots When VNAV is engaged the FMC airspeed is set to the target airspeed When VNAV is engaged above 400 feet the thrust reference changes to climb 2011 Captain Sim www captainsim com 20 IT MANUAL Part V Flight Mar rent Sys yst
50. dding a two letter prefix to the runway number Examples CF04 RW18L Unnamed turn points that are part of a procedure are identified as a latitude and longitude waypoint These include waypoints except conditional waypoints defined by flying a course or track from a waypoint except conditional waypoints to a radial or DME distance These waypoints are automatically entered in a route by selection of a procedure using these waypoints from the departures or arrivals page Airport reference points are identified by the ICAO identifier DUPLICATE WAYPOINTS Application of the abbreviation rules may create identical identifiers for different waypoints When a duplicate waypoint identifier is entered the page changes to the SELECT DESIRED WPT page The page lists the latitude longitude and the type of facility or waypoint of all the waypoints with the same identifier Select the latitude longitude of the correct waypoint to enter the correct waypoint on the original page 17 DO NOT USE FOR FLIGHT CONDITIONAL WAYPOINTS Conditional waypoints may be displayed in the route when selecting a DEPARTURES or ARRIVALS page procedure Usually conditional waypoints cannot be manually entered on a route or legs page These waypoints indicate when an event occurs and are not at a geographically fixed position The types of conditions are e climb descent through an altitude e flying a heading to a radial or DME distance e intercepti
51. destination is displayed DO NOT USE FOR FLIGHT 6 Speed SPD Displays the target FMC speed 7 Position Fuel POS FUEL Displays the fuel on board at the POS waypoint 83 757 Captain FLIGHT MANUAL Part V Flight Management System 84 DO NOT USE FOR FLIGHT Section 8 FMC DESCENT AND APPROACH INTRODUCTION The descent phase starts at the top of descent point and continues to the end of descent point Planning for the descent phase starts during cruise The approach phase starts at the end of descent point and continues to touchdown The only automatic page change in the descent approach phases is the VNAV selected page change from cruise to descent at the top of descent EARLY DESCENT Early descent is commenced before reaching the top of descent 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 85 DO NOT USE FOR FLIGHT DESCENT During descent LNAV progress is managed using the RTE LEGS page as in the cruise phase VNAV descent management is accomplished primarily on the DES page DESCENT PAGE The descent page is used to monitor and revise the descent path Descent speed modes are economy ECON and fixed speed SEL The default VNAV descent mode is ECON A fixed speed descent is flown when speed intervention is used or a speed is entered on the DES page The descent page is no longer available after the end of descent The
52. ding fix 757 Captain GHT MANUAL Part V Flight Management System 95 DO NOT USE FOR FLIGHT HOLD PAGE EXISTING HOLD When one or more holding patterns are already in the route push the HOLD key to show the hold page for the first holding pattern Holding parameters can be monitored and changed on this page New holding patterns are added using the NEXT HOLD prompt Hold exists in route ACT RTE 1 HOLD 1414 FIX SPD TGT ALT BATUM 220 4000 QUAD RADIAL FIX ETA 1424 52 INBD CRS DIR 231 L TURN LEG TIME 1 QMIN LEG DIST NDOOUO NOOO lt NEXT HOLD EXIT HOLD gt 1 NEXT HOLD Push displays a new hold page for a new holding pattern entry 2 EXIT HOLD Push e arms a return to the holding fix via the inbound course for holding pattern exit e EXIT ARMED displayed e EXEC light illuminated When the EXEC key is pushed the airplane will cross the holding fix and exit holding If executed when outbound in the holding pattern the airplane will immediately turn inbound and exit holding when the fix is crossed 757 Cap 1 G N U art V Flic Aanagement System 96 DO NOT USE FOR FLIGHT Section 9 FMC MESSAGES FMC messages alert the flight crew to conditions that could degrade the system operation and advise the crew of input errors The messages are categorized as e alerting messages e advisory messages The scratchpad messages display according to their level of importance A l
53. displays runway length when entered identifier is a runway 4 INDEX Push displays the INIT REF INDEX page 5 Frequency FREQ Displays frequency of entered identifier when it is a navaid 2011 Captain Sim www captainsim com g ent System 72 DO NOT USE FOR FLIGHT 6 LONGITUDE Displays longitude of entered identifier When the identifier is a runway the longitude displayed is for the threshold of the runway 7 ELEVATION Displays elevation of entered identifier when it is a navaid airport or runway 8 VOR DME NAV Alternately switches VOR DME NAV updating between OFF and ON FIX INFORMATION PAGE Two identical fix information pages are used to create fixes and waypoints for the HSI Some of the created waypoints can be copied into the route FIX BRG INFO DIS FIX FR BRG DIS ETA PRED ETA A Ho00000 000000 BRG DIS ETA 130 24 20042 180 26 20082 2011 Can 73 DO NOT USE FOR FLIGHT 1 FIX Before entry of a name or identifier boxes displayed and most data lines are blank Valid entries are airports navaids and waypoints from the navigation database The selected fix displays on the HSI and is highlighted by a green circle 2 Bearing Distance BRG DIS ETA DTG ALT Valid entries are XXX YYY Y e decimal values can be omitted e leading zeros can be omitted for distance entries e distance only entries must start with a slash Distances from the fix disp
54. displays the scratchpad message TAKEOFF SPEEDS DELETED 2 FUEL Fuel on board displays when the fuel totalizer calculations are valid The source for the display is included in the line e CALC calculated fuel quantity is from FMC calculations 48 DO NOT USE FOR FLIGHT Valid entry is thousands of pounds with a decimal hundreds optional 3 Zero Fuel Weight ZFW Normally ZFW is entered from the airplane dispatch papers and the FMC calculates the airplane gross weight Valid entry is thousands of pounds with a decimal hundreds optional Calculated zero fuel weight displays when airplane gross weight is entered first and fuel on board is valid Entry of a value after takeoff speeds are selected removes the speeds and displays the scratchpad message TAKEOFF SPEEDS DELETED 4 RESERVES Valid entry is thousands of pounds with a decimal hundreds optional 5 INDEX Push displays the INIT REF INDEX page 6 Cruise Altitude CRZ ALT Cruise altitude can be entered by the flight crew or from a company route Entered value is displayed on the CLB and CRZ pages 7 COST INDEX Cost index is used to calculate ECON climb cruise and descent speeds Larger values increase the ECON cruise speed Entering zero results in maximum range airspeed and minimum trip fuel Cost index can be entered by the flight crew or from a company route Valid entries are 0 to 9999 8 Cruise Center of Gravity CRZ CG Used by
55. e actual position Bearing distance display is relative to the FMC position 757 Captain GHT MANUAL Part V Flight Management System 36 DO NOT USE FOR FLIGHT POSITION REFERENCE PAGE 3 4 On position reference page 3 the flight crew can observe the calculated positions from the left and right GPS receivers and the left and right FMC calculations This page also allows the flight crew to enable or disable GPS position updates This page can display the bearing distance or latitude longitude format The bearing distance format displays the positions relative to the active FMC position on the POS REF 2 4 page In the example both the left and right GPS agree with the left FMC position POS REF 2 4 POS REF 4 amp POS REF GPS L 000 0 0NM GPS R 000 0 0NM FMC L PRI 000 0 0NM GPS NAV LAT LON gt 1 GPS Left L and GPS Right R Displays the left and right GPS positions 2 FMC Left L and FMC Right R Displays the left and right FMC calculated position Primary PRI is displayed in line title of the FMC that is the navigation master 3 INDEX Push displays the INIT REF INDEX page 4 GPS Navigation NAV Push alternately selects GPS NAV ON enabled and OFF disabled OFF GPS position data is not available to the FMC OFF displays in large letters ON displays in small letters 757 Captain GHT MANUAL Part V Flight Management System 37 DO NOT USE FOR F
56. e center point on the HSI map in the PLAN mode 9 Center lt CTR gt 757 Captain FLIGHT MANUAL Part V Flight Management System 57 DO NOT USE FOR FLIGHT Displays when PLAN mode selected Displays adjacent to the waypoint around which HSI plan mode is centered 10 MAP Center CTR STEP Replaces ACTIVATE or RTE DATA when PLAN mode selected Push steps lt CTR gt to next waypoint HSI plan mode recenters AIR TURN BACK ARRIVALS PAGE During a turn back situation the flight crew requires quick access to the arrivals data for the origin airport The arrivals page allows access without changing the destination on the route page During climb if the airplane is less than 400 miles from the origin and less that half way to the destination push the DEP ARR key to show the ARRIVALS page for the origin airport KBFI ARRIVALS 172 STARS RTE APPROACHES 1 CHNS2 ILS13R 3 RUNWAYS GLSR3 4 JWBN5 TRANS 2 EPH lt INDEX ROUTE gt 1 Standard Terminal Arrivals STARS Shows STARS for origin airport 2 Transitions TRANS Shows transitions for origin airport 3 APPROACHES Shows approaches for origin airport 4 RUNWAYS Shows runways for origin airport The arrivals page is discussed in more detail in the Descent and Approach Section 11 43 of this chapter 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 58 DO NOT USE FOR FLIGHT
57. e descent path 2 Within 50 NM of Top of Descent Point Use the MCP altitude selector to start an early descent Within 50 NM of the top of descent point VNAV starts an early descent and captures the idle descent path 3 More than 50 NM from Top of Descent Point Enter a new cruise altitude to start a cruise descent If the distance from the top of descent is more than 50 NM VNAV begins a cruise descent to the new cruise altitude and the new T D is displayed 2011 Captain Sim www captainsim com DO NOT USE FOR FLIGHT Monitor the descent profile to ensure the new cruise altitude is reached before T D 23 757 Captain FLIGHT MANUAL Part V Flight Management System 24 DO NOT USE FOR FLIGHT APPROACH VNAV will fly the computed descent path to the E D point altitude if the MOP altitude is set at or below the E D point altitude However it is the responsibility of the flight crew not to descend below the MDA of the approach being flown until adequate visual contact is achieved CRUISE AND DESCENT PROFILE NONPRECISION APPROACH a 6 fee 2528 a Bz gt Oud 1 aoOon W PEPE S o o Lan be ay gt n _ e ene T 44 08 Z Row A 2 a Z u u ak x 4 a lt x l r ue aad Sue gt 0 Site z gt Lo ue nn WwW 253 z2 E D ew Z A J z A E hd z _ Ke a7 F E g y a oF gt S 25 T S 30 g T 2 S A e fa ET Es T v E a i EA Z gt
58. e descent path starts at the T D and includes any waypoint altitude airspeed constraints The path to the first altitude constrained waypoint is based on e idle thrust e speedbrakes retracted e predicted use of anti ice e applicable target speed Descent path segments after the first altitude constrained waypoint are constructed as straight line point to point segments from one altitude constraint to the next The airspeed used to determine the descent path is the existing VNAV cruise airspeed normally economy Mach CAS based on Cost Index and any additional descent airspeed constraints Waypoints with an airspeed constraint must also have an altitude constraint Airspeed constraints after the first altitude constrained waypoint are treated as speed limits e g at or below the speed constraint With the MCP altitude set below the current airplane altitude and at the T D point the FMC commands idle thrust and the AFDS pitches down to track the vertical descent path AFDS pitch maintains the vertical descent path while the angle of the descent path is calculated by the FMC to maintain the descent airspeed at idle thrust normally economy descent Mach CAS 2011 Captain Sim w 757 Captain FLIGHT MANUAL Part V Flight Management System 22 DO NOT USE FOR FLIGHT If the airplane passes the T D point and the window altitude has not been set lower or if the airplane levels at an MCP altitude not in the FMC descent profile AL
59. ect a standard instrument departure SID Selection of the SID may cause a route discontinuity in the flight plan The modification must be connected to the existing route and executed This can be accomplished on the ROUTE or LEGS page When all required preflight entries are complete PRE FLT COMPLETE is displayed on the TAKEOFF REF page TAKEOFF The takeoff phase starts with engagement of takeoff trust on the MCP and extends to the thrust reduction altitude where climb thrust is normally selected CLIMB The climb phase starts at the thrust reduction altitude and extends to the top of climb T C point The T C is the position where the airplane reaches the cruise altitude entered on the PERF INIT page CRUISE The cruise phase starts at the T C point and extends to the top of descent T D point Cruise can include step climbs and en route descents 757 Captain FLIGHT MANUAL Part V Flight Management System 13 DO NOT USE FOR FLIGHT DESCENT The descent phase starts at the T D point or when the VNAV descent page becomes active The descent phase extends to the start of the approach phase APPROACH The approach phase starts when intercepting the first leg of a published approach selected from the ARRIVALS page OPERATIONAL NOTES When operating in the LNAV and VNAV modes system operation must be monitored for unwanted pitch roll or thrust commands If unwanted operation is noticed roll and pitch modes other than LNAV
60. eed schedule may be obtained by entering a cost index of zero This speed schedule ignores the cost of time A low cost index may be used when fuel costs are high compared to operating costs A minimum time speed schedule may be obtained by entering a cost index of 9999 This speed schedule calls for maximum flight envelope speeds Enter put data in the CDU scratchpad and line select the data to the applicable location New characters can be typed or existing data can be line selected to the scratchpad for entry Erase remove entered data which has resulted in a modification by selecting the ERASE prompt 2011 Captain Sim www captainsim com MANUAL Part V Flight Management System 14 DO NOT USE FOR FLIGHT Execute push the illuminated EXEC key to make modified data active Inactive data not being used to calculate LNAV or VNAV commands Initialize entering data required to make the system operational Message FMC information displayed in the scratchpad Modify to change active data When a modification is made to the active route or performance mode MOD displays in the page title ERASE displays next to line select key 6 left and the EXEC key illuminates Prompt CDU symbol that aids the flight crew in accomplishing a task Prompts can be boxes dashes or symbols lt or gt to remind the flight crew to enter or select data Select pushing a key to obtain the necessary data or action or to copy
61. eference data and V speeds 5 APPROACH The APPROACH REF page is used for entry of the approach VREF speed 6 Navigation NAV DATA The REF NAV DATA page is used to access data on waypoints navaids airports and runways The REF NAV DATA page is accessible only from this page IDENTIFICATION PAGE Most of the data on this page is for flight crew verification Active date and drag fuel flow can be modified The flight crew verifies FMC data selects the current navigation database and checks or modifies drag and fuel flow factors on the identification page INIT REF INDEX lt IDENT POS INIT gt 1 MODEL Displays the airplane model from the FMC performance database 31 DO NOT USE FOR FLIGHT 2 Navigation NAV DATA Displays the navigation database identifier 3 Operating OP PROGRAM Displays the operating program identifier 4 Operating Program Configuration OPC Part Number Displays the Operational Program Configuration part number 5 INDEX Push displays the INIT REF INDEX page 6 ENGINES Displays the engine model from the FMC performance database 7 ACTIVE Displays the effectivity date range for the active navigation database The active navigation database can be replaced with the inactive database while on the ground Changing the navigation database removes all previously entered route data 8 Inactive Date Range Displays the effectivity date range for the inactive
62. ement System 10 DO NOT USE FOR FLIGHT N USTOMER CARE You are invited to join Captain Sim community forum DAILY NEWS For Captain Sim daily news please follow us at Twitter or Facebook For Captain Sim videos please watch our YouTube channel TECH SUPPORT The 757 Captain is the most advanced complete and accurate digital replica of the B757 ever available for any game platform Our product is not perfect unfortunately nothing is But we are working on improvements If you have some important issue to report please check in to Your Profile then click Product Name gt Customer Support gt and use the Trouble Ticket System We process all tickets and consider the most significant issues for the next service packs 2011 Captain Sim www captainsim com
63. en DO NOT USE FOR FLIGHT 2 Acceleration Height At the acceleration height flap retraction or AFDS altitude capture before acceleration height VNAV commands an airspeed increase to 250 knots or the speed transition associated with the origin airport limited by configuration 3 VNAV Climb The VNAV climb profile uses VNAV SPD or VNAV PTH at the default climb speed or pilot selected climb speed to remain within all airspeed and altitude constraints that are part of the SID entered into the active route Autothrottle uses selected climb thrust limit 4 Climb Constraints VNAV enters the VNAV PTH mode to remain within departure or waypoint constraints Speed maintained during this time can be e procedure based speed restriction e waypoint speed restriction e default VNAV climb speed e manually entered climb speed 5 Top of Climb T C The point where the climb phase meets the cruise altitude is called the top of climb Approaching this point the FMC changes from the climb phase to the cruise phase The T C point is displayed on the map as a green circle with the label T C At cruise altitude the FMC commands economy cruise speed or the pilot entered speed until reaching the top of descent T D point Alternate cruise speed is flight crew entered speed If the cost index is set to zero the FMC commands maximum range cruise speed Cost index modifications are allowed until within ten miles of the top of descent CRUIS
64. entifier An entry is optional for activation of the route Valid entry is any previously saved company route name If the name isn t found among the saved routes the scratchpad message NOT IN DATABASE is displayed Entry of a new company route replaces the previous route 40 DO NOT USE FOR FLIGHT 8 ACTIVATE Push the ACTIVATE key to arm the route and illuminate the execute light When the EXEC key is pushed the route becomes active ACT is displayed in the title and the ACTIVATE prompt is replaced with the next required preflight page prompt Activation of a route is required for completion of the preflight ACTIVATE is always displayed on the inactive route pages After route activation the ACTIVATE prompt is replaced by e PERF INIT when the required performance data is incomplete or e TAKEOFF when the required performance data is complete MORE ROUTE PAGE PROMPTS FOR AN ACTIVE ROUTE ACT RTE 1 ORIGIN KBFI RUNWAY TAKEOFF gt 1 ROUTE SAVE Selecting ROUTE SAVE prompt allows you to save the currently entered route in a file as a company route Such saved route can be recalled at a later time by using CO ROUTE or REQUEST SEND prompts All routes saved to Captain_Sim navigation routes 2 Route Copy RTE COPY Push copies the entire active route into the inactive route Displayed only on the active route page Displays COMPLETE after the route is copied 41 DO NOT USE FOR
65. ess important message replaces another message in the scratchpad when the CLEAR key is pushed or the condition is corrected The FMC light illuminates and the EICAS advisory message FMC MESSAGE displays when there is an FMC alerting message Scratchpad advisory messages appear in the scratchpad without an EICAS message or FMC light All FMC messages illuminate the CDU message MSG light Clear the message or correct the condition to cancel the message The message is temporarily removed from the scratchpad when manually entering data The message returns when the data is removed from the scratchpad FMC ALERTING MESSAGES FMC alerting messages e display in the CDU scratchpad e illuminate the amber FMC light on the instrument panel e cause the EICAS advisory message FMC MESSAGE to display e illuminate the CDU message light MSG Use the CLEAR key or correct the condition responsible for the message to remove the message DISCONTINUITY LNAV active and the airplane has passed the last waypoint prior to a route discontinuity except on a manually terminated leg such as a VECTORS legs DRAG REQUIRED VNAV active and additional drag required or autothrottle off and less thrust required to maintain the VNAV descent path END OF ROUTE LNAV active and end of active route overflown AFDS maintains last heading ENTER IRS POSITION the flight crew entered present position did not pass one of the IRS comparison checks or the IRS is read
66. forecast wind data Altitudes and flight levels can be entered in any order Entries are not sorted Execute not necessary 3 Thermal Anti Ice On Altitude TAI ON ALT Enter the altitude where anti ice is first turned on during the descent The FMC calculates the descent profile based on the higher thrust caused by thermal anti ice operation below this altitude 4 Wind Direction Speed WIND DIR SPD Enter the wind direction speed for the specified altitude Initial entry must have wind direction and speed subsequent entries may have one or the other Execute not necessary 5 Descent DES Push shows the DES page APPROACH During approach roll and pitch modes usually change to the approach guidance supplied by navigation radios The FMC continues to calculate and show present position and can supply LNAV and VNAV approach guidance for certain types of approaches when radio navigation is not used The RTE LEGS and DESCENT pages are used to manage the airplane until other approach guidance becomes active Other pages which support approaches are e APPROACH REF page to access the FMC calculated approach VREF speed e ARRIVALS page to select arrival and approach procedures e HOLD page to manage holding patterns Holding is described in this section but it can be used during any phase of flight 2011 Captain Sim www captainsim com gt 757 Captain FLIGHT MANUAL Part V Flight Management Systen
67. ht Management System 66 DO NOT USE FOR FLIGHT 3 Economy Speed ECON SPD Selected Speed SEL SPD Displays target speed or Mach MOD displays in the page title until the modification is erased or executed A manually entered speed changes the line title to SEL SPD ECON can be replaced with LRC or company CO SPD depending on the VNAV mode 4 EPR Displays EPR necessary for level flight at the target airspeed 5 Economy ECON Blank when ECON is the active speed Displays a prompt when ECON is not the active speed Push selects economy cruise speed 6 Destination ETA FUEL Estimated time of arrival and calculated fuel remaining at the destination Displays the same data for the alternate airport when a DIVERT NOW modification is selected from the ALTN page Calculations are based on optimum step climbs and cruise altitudes NAV MODIFICATIONS During the cruise phase VNAV can calculate two types of climbs cruise climbs and step climbs Cruise climbs can be entered by the flight crew Optimum step climbs are calculated by the FMC In all cases the new climb altitude must be selected in the MCP altitude window before VNAV commands the climb CRUISE CLIMB To initiate a cruise climb set the higher altitude on the MCP then enter the altitude in the CRZ ALT line and execute When the CRZ page is displayed the new MCP altitude is automatically copied to the scratchpad to be line selected to the CRZ ALT line 1 ACT
68. if the longitude is less than 100 and is the third character if the longitude is 100 or greater N is used for north latitude west longitude E is used for north latitude east longitude S is used for south latitude east longitude W is used for south latitude west longitude Examples N50 W040 becomes 5040N N75 W170 becomes 75N70 N50 E020 becomes 5020E NO6 El 10 becomes 06E10 S52 W075 becomes 5275W S07 W120 becomes 07W20 S50 E020 becomes 5020S S06 El 10 becomes 06S10 PROCEDURE ARC FIX WAYPOINT NAMES Unnamed terminal area fixes along a DME arc procedure are identified with the first character D Characters 2 through 4 indicate the radial on which the fix lies The last character indicates the arc radius The radius is expressed by a letter of the alphabet where A 1 mile B 2 miles C 3 miles and so forth Example EPH252 24 D252X An unnamed waypoint along a DME arc with a radius greater than 26 miles is identified by the station identifier and the DME radius Example CPR338 29 CPR29 16 DO NOT USE FOR FLIGHT When there are multiple unnamed waypoints along a DME arc with a radius greater than 26 miles the station identifier is reduced to two characters followed by the radius and then a sequence character Examples e CPR134 29 CP29A e CPR1900 29 CP29B PROCEDURE FIX WAYPOINTS Waypoints located at unnamed runway related fixes are identified by a
69. ight Illuminated amber fault detected in related FMC 5 Brightness Control Rotate controls display brightness 6 Message MSG Light Illuminated white scratchpad message is displayed FUNCTION AND EXECUTE KEYS INIT DEP i Pa AGE E Del n Fix uess Horo FM i 2 COMM i i maai A L N imal Exec e 3 j I I PREV PAGE PAGE I 1 CDU Function Keys Push INIT REF displays page for data initialization or for reference data RTE displays page to input or change origin destination or route DEP ARR displays page to input or change departure and arrival procedures VNAV displays page to view or change vertical navigation path data FIX displays page to create reference points on HSI map LEGS displays page to evaluate or modify lateral and vertical route data displays page to control HSI PLAN mode display e HOLD displays page to create holding patterns and show holding pattern data e PROG displays page to view dynamic flight and navigation data including waypoint and destination ETAs fuel remaining and arrival estimates e MENU displays page to choose subsystems controlled by CDU e NAV RAD displays page to monitor or control VOR tuning e PREV PAGE displays previous page of related pages for example LEGS pages e NEXT PAGE displays next page of related pages 2 Execute Light Illuminated white active data is modified but not executed
70. ight number is total number of related pages Page number is blank when only one page exists 6 Boxes Data input is mandatory 7 Dashes Data input is optional The data is not mandatory 8 Scratchpad Displays messages alphanumeric entries or line selected data 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System DO NOT USE FOR FLIGHT FMC ANNUNCIATOR LIGHT 1 FMC 1 FMC Annunciator Light Illuminated amber e CDU is displaying an operationally significant message in the scratchpad e pushing CDU CLR key extinguishes the light and clears the scratchpad message 10 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 11 DO NOT USE FOR FLIGHT Section 2 FLIGHT MANAGEMENT SYSTEM DESCRIPTION INTRODUCTION The flight management system FMS aids the flight crew with navigation in flight performance optimization automatic fuel monitoring and flight deck displays Automatic flight functions manage the airplane lateral flight path LNAV and vertical flight path VNAV The displays include a map for airplane orientation and command markers on the airspeed altitude and thrust indicators to help in flying efficient profiles The flight crew enters the applicable route and flight data into the CDUs The FMS then uses the navigation database airplane position and supporting systems to calcula
71. imulates displays positions calculated by the FMC IRS GPS and radio navigation receivers The FMC position can be updated to IRS GPS or radio position on this page Positions are displayed as the latitude longitude calculated by the individual systems When BRG DIST is selected the IRS GPS and radio positions are shown as bearing and distance from the FMC position POS INIT 1 POS REF 3 PREV PAGE 0 FMC GPS 1 N47 32 4 W122 18 6 IRS 3 ACTUAL 2 70 2 N47 32 4 W122 18 7 GPS ACTUAL 0 1 7 3 47 32 4 W122 18 6 RADIO ACTUAL 0 34 4 467 32 4 W122 18 6 RNP ACT DME DME 5 0 0 8 6 9 1 FMC Position and Source The source used by the active FMC for position data is displayed next to the FMC line title In the example the FMC uses LGPS for position data Displays the FMC calculated latitude longitude Identifies the source for calculating the FMC position e GPS position calculated from GPS and inertial position data IRS position calculated from inertial position data only RADIO position calculated from navigation radio and inertial position data LOC GPS position is calculated from localizer GPS and inertial data LOC RADIO position is calculated from localizer navigation radio and inertial data LOC position is calculated from localizer and inertial data 2 IRS Displays latitude longitude position or the bearing and distance from the FMC position determined by the IRS If the displayed
72. ing is the radial for CR and VR legs Distance is distance for CD FC FD or VD legs Fix is a fix or waypoint this leg is based on for example Track to Fix type leg this field shows the name of the fix in question FixLat and FixLon are the coordinates of this fix where applicable The current database lists 91 00 181 00 where such coordinates are not defined for example Heading to Altitude leg but exact values are not important MagCourse is course or heading where it is required Path describes the leg path type and can be one of the following standard AIRAC types HA Hold one circle HF Hold until altitude reached HM Hold with manual termination IF Initial fix PI Procedure turn TF Track between fixes CA Course to altitude CD Course to DME distance CI CR CF DF FA FC FD FM RF VA VD VI VM VR DO NOT USE FOR FLIGHT Course to leg Course to radial termination Course to fix Track to fix Course from fix to altitude Course from fix to given distance Course from fix to DME distance Course from fix to manual termination Constant radius to fix Heading to altitude Heading to DME distance Heading to leg Heading to manual termination Heading to radial termination 99 RecNav is Recommended Navaid for this leg This is used for legs such as Course from Fix to DME Distance or Course to Radial Termination and lists the navaid name which is to be tuned to and checked for DME distance or r
73. ise displays time from first officer s clock e hours set by entering desired hour reference e minutes set by resetting appropriate pilot s clock 4 INDEX Push displays the INIT REF INDEX page 5 Last Position LAST POS Displays the last FMC calculated position 6 GPS Position GPS POS Displays the GPS present position During preflight the GPS POS may not display due to satellite availability performance or unfavorable geometry 7 Set IRS Position SET IRS POS The set inertial position entry is required to initialize the IRS Select the most accurate latitude longitude from LAST POS REF AIRPORT GATE GPS POS or a manual entry to initialize the IRS If an entry is not made before the IRS completes the initial alignment the scratchpad message ENTER IRS POSITION is displayed If the manually entered position fails the IRS internal check the scratchpad message ENTER IRS POSITION is displayed The manually entered position is also compared with the FMC origin airport position If the entered position is not within 6 NM of the FMC origin airport position the scratchpad message IRS POS ORIGIN DISAGREE is displayed Blanks when the IRS changes from the alignment to the navigation mode 8 ROUTE Push displays the ROUTE page 757 Captain FLIGHT MANUAL Part V Flight Management System 34 DO NOT USE FOR FLIGHT POSITION REFERENCE PAGES POSITION REFERENCE PAGE 2 4 Position reference page 2 s
74. isplays the type of climb e ECON speed based on the cost index e LIM SPD speed based on airplane configuration limiting speed e MCP SPD MCP speed intervention selected e XXXKT fixed CAS climb speed profile e M XXX fixed Mach climb speed profile Fixed climb speeds are for e climb segment constraints e waypoint speed constraints e an altitude constraint associated with a speed constraint e a speed transition e a flight crew selected speed 2 Cruise Altitude CRZ ALT Displays cruise altitude entered on PERF INIT page Valid entries are XXX XXXX XXXXX or FLXXX Altitude displays in feet or flight level depending on transition altitude 3 Economy Speed ECON SPD Selected Speed SEL SPD ECON SPD e economy speed based on cost index 54 DO NOT USE FOR FLIGHT e shows CAS and Mach values SEL SPD e shows when intermediate level off required below an existing speed constraint e shows when flight crew enters speed e CAS or Mach value may be entered 4 Speed Transition SPD TRANS The speed transition line shows the transition speed altitude from one of these sources e the navigation database value for the origin airport e a default speed of 250 knots and 10 000 feet Not displayed above the transition altitude Can be deleted 5 Speed Restriction SPD RESTR Speed restrictions not associated with specific waypoints are manually entered on this line Dashes before entry by flight crew Valid entry is a
75. itude routes or an approach the name or identifier of the collocated waypoint is used Example e Unnamed turn point on J2 between the Lake Charles LCH and New Orleans MSY VORTACs is coincidental with the Lafayette LFT low altitude VORTAC LFT is used as the identifier for the turn point Identifier codes for unnamed turn points not coincidental with named waypoints are constructed from the identifier of a navaid serving the point and the distance from the navaid to the point If the distance is 99 nautical miles or less the navaid identifier is placed first followed by the distance If the distance is 100 nautical miles or more the last two digits are used and placed ahead of the navaid identifier Examples NAVAID DISTANCE IDENT e INW 18 INW18 e CSN 106 06CSN Waypoint located at unnamed flight information region FIR upper flight information region UIR and controlled airspace reporting points are identified by the three letter airspace type identification followed by a two digit sequence number Example e FRAO1L Unnamed oceanic control area reporting points in the northern hemisphere use the letters N and E while points in the southern hemisphere use the letters S and W Latitude always precedes longitude For longitude only the last two digits of the three digit value are used Placement of the designator in the five character set indicates whether the first longitude digit is 0 or 1 The letter is the last character
76. l FMC power up page is the identification page Preflight flow continues in this sequence e identification IDENT page e position initialization POS INIT page ROUTE page DEPARTURES page no automatic prompt performance initialization PERF INIT page takeoff reference TAKEOFF REF page Some of these pages are also used in flight MINIMUM PREFLIGHT SEQUENCE POS INIT POS INIT gt ROUTE gt ee ACTIVATE gt EXEC LIGHT ILLUMINATES ACT RTE 1 PERF INIT PERF INIT gt SID ENTRY REQUIRED DEP ARR DEPARTURES TAKEOFF REF PREFLIGHT COMPLETE During preflight a prompt in the lower right directs the flight crew through the minimum requirements for preflight completion Selecting the prompt key displays the next page in the flow If a required entry is missed a prompt on the TAKEOFF page leads the flight crew to the preflight page missing data Airplane inertial position is necessary for FMC preflight and flight instrument operation A route must be entered and activated The minimum route data is origin and destination airports and a route leg 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 29 DO NOT USE FOR FLIGHT Performance data requires the airplane weight and cruise altitude Takeoff data requires a flap setting SUPPLEMENTARY PAGES Supplementary pages are sometimes required these pages have no prom
77. lay on the HSI as a circle around the fix When the circle intersects the active route the ETA DTG and predicted altitude at the intersection display for the closest of the two intersections Bearings from the fix display on the HSI as radial lines from the fix When the bearing intersects the active route the ETA DTG and predicted altitude at the intersection display ETA displays the estimated time of arrival to the intersection point DTG displays the distance to go to the intersection point ALT displays the predicted altitude at the intersection point Push copies the fix place bearing distance into the scratchpad This fix can be placed in the route on a LEGS or RTE page as a waypoint 3 Bearing Distance BRG DIS Dashes Enter a bearing distance or both bearing and distance from the fix A bearing and distance from the fix displays on the HSI as a waypoint fix point ETA DTG and predicted do not display 4 ABEAM Displays ABEAM prompt Push displays bearing and distance from the fix perpendicular to the nearest segment of the flight plan path and ETA DTG and altitude at the intersection point Second push copies the fix place bearing distance into the scratchpad This fix can be placed in the route on a LEGS or RTE page as a waypoint 5 ERASE FIX Push removes all fix data from the page and the HSI 6 Route Intersection Point Copied Pushing the line select key for one of the BRG DIS entries c
78. miles from the T D point A cruise descent can be started by selecting a lower altitude on the MCP entering the new altitude in the CRZ ALT line and executing A VNAV cruise descent is commanded at the current cruise speed and approximately 1250 feet per minute rate of descent The autothrottles adjust thrust to maintain the target descent rate pitch maintains the commanded speed Thrust levers can be manually positioned to adjust the descent rate 1 fecr ECON CRZ DES e a ECON CRZ 1 During Cruise Descent VNAV page title shows cruise phase in a descent to a new cruise altitude 2 End of Cruise Descent VNAV page title shows cruise phase after level off at new cruise altitude 70 DO NOT USE FOR FLIGHT EARLY DESCENT An early descent starts when the descent for landing is commenced prior to the FMC calculated top of descent T D point Early descents should not be started when the distance to the T D is greater than 50 nautical miles When further from the top of descent point the cruise descent function should be used Early descents are started on the DES page Once an early descent is started VNAV changes to the descent phase and cruise features are no longer available The autothrottle adjusts thrust to maintain the target descent rate pitch maintains the commanded speed Thrust levers can be manually positioned to adjust the descent rate ECON DES 3 3 FORECAST gt DES NOW gt lt
79. ng a course e heading vectors to a course or fix Altitude and course intercept conditional waypoints display on the CDU inside parenthesis marks The diagram below shows conditional waypoints EXAMPLE MEANING RTE 1 LEGS 180 HDG 1000 CDE 140 HDG Oo ABC180 180 HDG i BCD ame To 1000 vecTons ABC20 To CI 020 HDG ABC CINTC 020 HDG a 10 120R Jea TO BCD BCD ABC180 d 220 090 HDG TO 20 DM sac2p VECTORS 270 _ CDE _ Note All waypoints except BCD and CDE are enn examples of conditional waypoints MANUALLY ENTERED LATITUDE LONGITUDE WAYPOINTS Pilot defined waypoints entered as a latitude and longitude are shown in a seven character format Latitude and longitude waypoints are entered with no space or slash between the latitude and longitude entries Leading zeroes must be entered All digits and decimal points to 1 10 minute must be entered unless the latitude or longitude are full degrees Examples e N47 W008 is entered as N47W008 and displays as N47W008 e N47 15 4 W008 3 4 is entered as N4715 4W00803 4 and displays as N47W008 MANUALLY ENTERED PLACE BEARING DISTANCE OR PLACE BEARING PLACE BEARING WAYPOINTS Waypoints entered as a place bearing distance or place bearing place bearing are identified by the first three characters of the entry followed by a two digit sequence number Examples e SEA330 10 becomes SEA01 e SEA330 OLM020 becomes SEA02 The two digit
80. nt relative to airplane heading 8 Vertical Track Error VTK ERROR Displays vertical path VTK error above or below vertical path 9 Static Air Temperature SAT Displays outside static air temperature 10 RIGHT FUEL USED Displays fuel used by right engine sensed by fuel flow meters 11 FUEL USED Total TOT Displays sum of the LEFT and RIGHT fuel used values 12 FUEL Quantity QTY 757 Cap 1 G N U art V Flic Aanagement System 82 DO NOT USE FOR FLIGHT POSITION REPORT PAGE The position report page displays data for a position report A data linked position report can be initiated from the page The page contains reference data only Manual entries are inhibited XXXX PROGRESS lt POS REPORT AB345 POS REPORT POS ATA ALT BEEZR 13242 FL190 EST ETA ELN 13272 NEXT DEST ETA QUINT 13412 TEMP WIND SPD 330 30KT POS U N m 1 Position POS Waypoint used to report position This is the previous active waypoint The actual time of arrival ATA and altitude ALT at the waypoint follow the waypoint name 2 Estimate EST The active waypoint is displayed with the ETA to that waypoint 3 NEXT The waypoint following the active waypoint 4 Temperature and Wind TEMP WIND TEMP displays the OAT in degrees C WEND displays the wind direction and speed Wind direction is shown in degrees true 5 Destination ETA DEST ETA The FMC calculated ETA for the
81. on the airway Dashes display on the first TO waypoint after the end of the route 757 Captain FLIGHT MANUAL Part V Flight Management System 43 DO NOT USE FOR FLIGHT PREFLIGHT PAGES PART 2 DEPARTURE ARRIVAL INDEX PAGE The departure and arrival index page is used to select the departure or arrival page for the origin and destination airports for each route The index also allows reference to departure or arrival data for any other airport in the navigation database Departure and arrival prompts are available for the origin airport Destination airports have only arrival prompts DEPARTURES P 7 No active route ry lt INDEX DEP ARR INDEX RTE 1 CACT 1 KBFI 4 KMWH 5 2 6 ______ KGEG ARR gt 7 3 8 1 Departure DEP Route 1 Push displays the departure page for route 1 origin airport 2 Departure DEP Route 2 Push displays the departure page for route 2 origin airport 3 Departure DEP Other Displays the departure page for the airport entered into this line through the scratchpad DEP prompt for OTHER allow display of departure data about airports that are not an origin or destination The data can be viewed but cannot be selected because the airport is not on the route 4 Arrival ARR Route 1 Origin Push displays the arrival page for route 1 origin airport Origin airport arrivals selection is used during a turn back situation 2011 Captain Sim w
82. opies the fix place bearing distance definition into the scratchpad This fix can be placed into the route on a LEGS page as a waypoint 7 Bearing Distance From BRG DIS FR Displays the bearing and distance of the airplane from the fix 757 Captain FLIGHT MANUAL Part V Flight Management System 74 DO NOT USE FOR FLIGHT IN FLIGHT POSITION UPDATE FMC position update can be accomplished on the POS REF 2 3 page in flight XXXX PROGRESS POS REF gt POS REF 2 4 FMC GPS UPDATE N47 32 4 wW122 18 6 ARMED 1 IRS 3 ACTUAL amp N47 32 4 w122 18 6 GPS ACTUAL 0 N47 32 4 wW122 18 6 2 RADIO ACTUAL 0 N47 32 4 W122 18 6 RNP ACTUAL DME DME 0 50 0 06N IBFI PAE lt INDEX BRG DIST gt 000000 1 UPDATE ARMED Pushing the ARM prompt arms the position update function ARM changes to ARMED Each of the position update sources have a NOW prompt 2 NOW Push to update the FMC position from the desired source The FMC position is changed to the position of the selected system If a valid source with a more accurate position smaller ACTUAL exists the FMC position will quickly return to the most accurate position source 2011 Captain Sim w captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 75 DO NOT USE FOR FLIGHT ROUTE AND WAYPOINT DATA ROUTE DATA PAGE The route data page displays progress data for each waypoint on the ACT RTE X LEGS page
83. oute segment must be the same as the start point of the next route segment or a route discontinuity is created between the segments 42 DO NOT USE FOR FLIGHT Entering an airway on the first VIA line of page 2 initiates an airway intercept and boxes are displayed in the first TO line When a waypoint is entered in the boxes the airway and waypoint are moved down to the second line The FMC enters a waypoint in the first TO line which is the first waypoint on the airway segment closest to the airplane position Entering two intersecting airways in successive VIA lines without a TO waypoint causes the FMC to create an airway intersection waypoint to change from one airway to the next The FMC created waypoint is displayed as the TO waypoint for the first airway LACRE3 VAMPS is an example of a SID selection made on the DEPARTURES page V2 and V336 are examples of airway entries APP TRANS is an example of a STAR selection made on the APPROACH page ILS32R is an example of an approach selection made on the APPROACH page 2 TO Enter the end point of the route segment specified by the VIA entry Entry of a waypoint in the TO column without first entering a VIA airway displays DIRECT in the VIA column Boxes indicate data input is required to complete the route segment definition Valid waypoint entries for a DIRECT route segment are any valid waypoint fix navaid airport or runway Valid waypoint entries for airways are waypoints or fixes
84. page title includes the VNAV speed mode The ECON mode controls descent speed at the economy speed until reaching a lower speed restriction The fixed speed mode controls descent speed until a lower speed restriction is reached Descent mode ACT ECON DES 3 3 E D AT AT RUBEL 2800 PELLY 2407 6000 ECON SPD 294 SPD TRANS 2407 10000 SPD RESTR UU A W N m FORECAST gt DES DIR gt 1 Page Title The title usually shows ECON during descent Fixed speed descents modify the title The page title shows the type of descent e ECON speed based on a cost index e LIM SPD speed based on airplane configuration limiting speed MCP SPD MCP speed intervention is selected XXXKT fixed CAS descent speed profile M XXX fixed Mach descent speed profile ACT prefix shown when descent phase is active MOD prefix shown when descent phase is active and the flight plan is modified Reasons for fixed descent speeds are e waypoint speed constraints e an altitude constraint associated with a speed constraint e a speed transition e a flight crew entered selected speed SEL SPD 2011 Captain Sim www captainsim com 86 DO NOT USE FOR FLIGHT 2 End of Descent At E D AT Shows the end of descent altitude and waypoint The end of descent point is a waypoint in the descent phase with the lowest altitude constraint Blank if no E D point exists 3 Economy Speed ECON SPD Selected Speed SEL SPD Shows the current target
85. points 8 pages can be listed Waypoints are sorted as follows e when page is accessed as a result of a flight plan entry or modification sort is based on proximity to the waypoint preceding the entered waypoint e when page is accessed as a result of a DIR INTC FIX INFO or REF NAV DATA entry sort is based on proximity to current aircraft position Select the desired waypoint by pushing either the left or right line select key adjacent to the waypoint The CDU page where the waypoint identifier was entered is then displayed with the selected waypoint inserted 2 Frequency Displays frequency of the waypoint if it is a navaid Blank if the waypoint is not a navaid 3 Type Displays the type of waypoint for each duplicate name 4 Latitude Longitude Displays the latitude longitude for each duplicate name 757 Captain FLIGHT MANUAL Part V Flight Management System 65 DO NOT USE FOR FLIGHT The cruise page is used to monitor and change cruise altitude and speed Speed changes can be manually selected or automatically selected with the selection of other VNAV modes Cruise climbs cruise descents and step climbs can be accomplished from the cruise page When using the economy mode page data is based on operating at ECON SPD Economy cruise speed is based on cost index When the flight crew enters a selected speed page data changes When the FMC is in the engine out mode the data changes to include the airplane capabili
86. position is derived from all three IRSs 3 is displayed If the position is from a single IRS then L C or R is displayed to indicate which IRS position is displayed 2011 Captain Sim www captainsim com 35 DO NOT USE FOR FLIGHT 3 GPS Displays latitude longitude position or the bearing and distance from the FMC position determined by the GPS 4 RADIO After airborne displays latitude longitude position or the bearing and distance from the FMC position determined by navigation radios 5 Required Navigation Performance and Actual Navigation Performance RNP ACTUAL Displays the RNP and actual navigational performance ACTUAL of the FMC Note The FMC stops GPS updating if GPS data accuracy degrades due to satellite availability or unfavorable geometry Subsequently the FMC receives updates from another system 6 INDEX Push displays the INIT REF INDEX page 7 ACTUAL Displays actual navigation performance ANP of the IRS GPS and navigation radios 8 Radio Update Station s Mode Displays radio station identifiers Position update mode is indicated in the line title e DME DME e VOR DME Line and title are blank when no radio position is computed 9 Bearing Distance BRG DIST or Latitude Longitude LAT LON Push alternates position data format between bearing distance or latitude longitude The page illustration is shown in the latitude longitude display format Latitude longitude format displays ar
87. pts and interrupt the usual sequence Discussions of each page includes methods to display the page When the route includes SIDs and STARs they can be entered using the DEPARTURES or ARRIVALS pages Route discontinuities are removed and the route is modified on the ROUTE and RTE LEGS pages Speed altitude restrictions are entered and removed on the RTE LEGS page The RTE LEGS page is described in the FMC Cruise section Waypoint navaid airport and runway data is referenced on the REF NAV DATA page The REF NAV DATA page is described in the FMC Cruise section PREFLIGHT PAGES PART 1 The preflight pages are presented in the sequence used during a typical preflight INITIALIZATION REFERENCE INDEX PAGE The initialization reference index page allows manual selection of several FMC pages It gives access to most of the pages used during preflight XXXXXXX INIT REF INDEX NAV lt TAKEOFF U A UU N m lt APPROACH MAINT gt 1 Identification IDENT The IDENT page is the first page in the preflight sequence 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 30 DO NOT USE FOR FLIGHT 2 Position POS The POS INIT page is used for IRS initialization 3 Performance PERF The PERF INIT page is used for initialization of data required for VNAV operations and performance predictions 4 TAKEOFF The TAKEOFF REF page is used to enter takeoff r
88. red as 00835 displays as 840 1 500 feet is entered as 01500 displays as 1500 8 500 feet is entered as 08500 displays as FLO85 9 995 feet is entered as 09995 displays as FL100 11 500 feet is entered as 11500 displays as FL115 25 000 feet is entered as 25000 displays as FL250 Negative altitude entries are allowed to 1000 feet AIRSPEED ENTRY Airspeeds can be entered into the FMC as calibrated airspeed CAS or Mach number M CAS is entered as three digits XXX in knots Mach numbers are entered as one two or three digits following a decimal point DATA PAIRS Many CDU pages display data in pairs separated by a slash Examples of these pairs include wind direction speed and waypoint airspeed altitude constraints When entering both values in a pair the slash is inserted between the values When it is possible to enter only one value of the pair the slash may not be required When entering only the outboard value of a pair the trailing or leading slash may be entered but is not required before transferring to the data line When entering the inboard value of a pair the trailing or leading slash must be entered before transferring to the data line Omission of the required slash normally results in an INVALID ENTRY message 511 Can 757 Captain FLIGHT MANUAL Part V Flight Management System 27 DO NOT USE FOR FLIGHT Section 4 FLIGHT MANAGEMENT COMPUTER FMC DATABASES The FMC contains two database
89. rmat and bearing distance format When the display is in the bearing distance format the prompt displays LAT LON gt ROUTE PAGE Two routes RTE 1 and RTE 2 can be stored and displayed in air traffic control format The first route page displays origin and destination data Subsequent route pages display route segments between waypoints or fixes Having two routes allows management of alternate or future routes while leaving the active route unmodified RTE 2 has an identical page structure as RTE 1 ROUTE PAGE 1 X On ground RTE 2 not active ARRIVALS DEPARTURES POS INIT 4 ACTIVATE gt 8 On the real aircraft selecting this prompt sends a datalink route request In the simulated FMC this prompt opens the SELECT CO RTE page listing all previously saved routes You can navigate the list pages using the NEXT PAGE and PREV PAGE keys Selecting any route from the list loads this route into the FMC The FLTSIM FPLS on the bottom of SELECT CO RTE page opens IMPORT FS FPL page This page lists all flight plans FPL files created and saved by the Flight Simulator built in flight planner Selecting any entry imports the corresponding flight plan waypoints into the FMC 1 Page Title Preceded by ACT when the route is active and by MOD when the route is modified and the change is not executed Multiple route pages are indicated by the page sequence number to the right of the title The minimum number of route pages is 2
90. rport tainsim com 90 DO NOT USE FOR FLIGHT STARS are shown first in a list under the STAR line title When a selection is made the procedures not selected are removed from the page The selected procedure is listed with lt SEL gt and a list of compatible transitions is shown 3 Standard Terminal Arrivals Transitions STARS TRANS Lists all the transitions for the selected STAR When a selection is made the transitions not selected are removed from the page The selected transition is listed and marked lt SEL gt 4 INDEX Push shows the DEP ARR INDEX page 5 Route 1 RTE 1 Shows the selected route number RTE 1 or RTE 2 6 APPROACHES Lists available approaches and runways for the destination airport When a selection is made other approaches and runways are removed from the page and compatible transitions are listed The list of STARS is reduced to those compatible with the selected approach 7 Approach Transitions TRANS Transitions are listed when an approach is selected Shows a list of available transitions to the selected approach Approach transitions include e IAF e feeder fix e fixes which define routing to the FAR Selecting an approach without a transition makes a straight in approach which starts at e a charted fix or CFXXX where XXX is the runway number e a waypoint 4 8 miles outside the final approach fix 91 DO NOT USE FOR FLIGHT APPROACH REFERENCE PAGE
91. s e performance database e navigation database The performance database supplies all the necessary performance data to the flight crew It supplies the FMC with the necessary data to calculate pitch and thrust commands All necessary data can be shown on the CDU The database includes e airplane drag and engine characteristics e maximum and optimum altitudes e maximum and minimum speeds The navigation database includes most data usually found on navigation charts This data can be shown on the CDU or HSI The database contains e the location of VHF navigation aids airports runways other airline selected data such as SIDs STARs approaches and company routes transition altitudes HRUST MANAGEMENT The autothrottle is controlled by the thrust management computer When VNAV is engaged the FMC controls the autothrottle by setting the command speeds and thrust reference modes on the thrust management computer When VNAV is not engaged the thrust management is controlled by the flight crew as part of the AFDS system 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flight Management System 28 DO NOT USE FOR FLIGHT Section 5 FMC PREFLIGHT INTRODUCTION FMC preflight is required before flight Completion of the FMC preflight requires data entry in all minimum required data locations Additional entry of optional preflight data optimizes FMC accuracy PREFLIGHT PAGE SEQUENCE The usua
92. s on an intercept heading to the active route leg Initially LNAV arms and then activates as the airplane approaches the active leg An intercept heading must intersect the active leg inbound before the active waypoint MODIFICATION OF THE ACTIVE WAYPOINT The example below depicts the airplane being off course to the right followed by a modification to fly direct to BTG MOD RTE 1 LEGS f amp 9INM _810 FL350 197NM 810 FL350 146NM 809 FL350 lt ERASE 000000 1 Course to Active Waypoint Displays current required track to fly inbound course to waypoint 2 Active Waypoint Displays crew entered direct intercept waypoint If entered waypoint is not part of the active route it will be followed by a discontinuity 2011 Captain Sim www captainsim com 64 DO NOT USE FOR FLIGHT SELECT DESIRED WAYPOINT WPT PAGE The SELECT DESIRED WPT page is displayed when a waypoint identifier or name is entered and the navigation database contains more than one location for the same waypoint name Selection of a waypoint returns the display to the previous page LECT DESIRED WPT 1 1 0 VOR 3 8 N40 38 0W064 31 5 4 0 DME 1 O N44 27 0W101 15 0 sues N46 15 3W062 52 9 ENO VORDME 116 60 N50 45 2wW070 12 2 KS Na aaa SE EN 114 EN 12 EN 000000 00 0000 1 Identifier Displays a list of the waypoints in the navigation database that have the same identifier as entered Up to 48 way
93. selected data to the scratchpad Speed restriction an airspeed limit associated with a specified altitude entered by the flight crew Speed transition an airspeed limit associated with a specified altitude entered by the FMC Waypoint a point on the route or in the navigation database It can be a fixed point such as a latitude and longitude VOR or ADF station or an airway intersection A conditional waypoint is not associated with a land reference it is based on a time or altitude requirement An example of a conditional waypoint is when reaching 1000 feet LATERAL NAVIGATION LNAV LNAV provides steering commands to the next waypoint or the selected route intercept point When selected after takeoff LNAV engages when laterally within 2 5 nautical miles of the active route leg FMC LNAV guidance normally provides great circle courses between waypoints However when an arrival or approach from the FMC data base is entered into the active route the FMC commands a heading track to comply with the procedure WAYPOINTS Waypoint navigation fix identifiers display on the CDU and HSI The CDU message NOT IN DATABASE is displayed if a manually entered waypoint identifier is not in the data base The waypoint can still be entered as a latitude longitude place bearing distance or a place bearing place bearing waypoint FMC generated waypoints contain a maximum of five characters assigned according to the following rules NAVAID W
94. sequence numbers reserved for RTE1 are 01 through 49 The two digit sequence numbers reserved for RTE2 are 51 through 99 MANUALLY ENTERED AIRWAY CROSSING WAYPOINTS Airway crossing fixes are entered as a five character waypoint name or by entering consecutive airways on the ROUTE page In the latter case the display is an X followed by the second airway name Example 757 Captain FLIGHT MANUAL Part V Flight Management System 18 DO NOT USE FOR FLIGHT entering J70 on the VIA line of the ROUTE page causes box prompts to display opposite on the same line Leaving the box prompts empty and entering J52 on the next VIA line directly below J70 causes the FMC to calculate the intersection of the two airways and replace the boxes with the waypoint identifier XJ52 MANUALLY ENTERED ALONG TRACK WAYPOINTS Along track waypoints are created on the active route and do not cause route discontinuities when they are created Along track waypoints are entered using the waypoint name the place followed by a slash and minus sign for points before the waypoint or no sign for points after the waypoint followed by the mileage offset for the newly defined waypoint The distance offset must be less than the distance between the originating waypoint and next positive value or preceding negative value waypoint Latitude and longitude waypoints cannot be used to create along track waypoints Examples e VAMPS 25 is 25 miles after VAMPS on
95. ta e LEVEL AT time and distance to level off in engine out mode 3 Captain FLIGH MANUAL Part V Flignt Management system DO NOT USE FOR FLIGHT 10 Position Reference POS REF Push displays the position reference page PROGRESS PAGE 2 Progress page two contains e wind data e true airspeed e fuel data e track error data e static air temperature XXXX PROGRESS 1 2 NEXT PAGE BO56 PROGRESS 2 2 H WIND WIND X WIND 1 32KT 080 57 L 23kT XTK ERROR VTK ERROR 2 LO INM 10FT TAS SAT 3 420KT 25 LEFT FUEL USED RIGHT 4 4 3 TOT 8 5 4 2 FUEL QTY TOTALIZER CALCULATED 5 20 7 20 6 1 Headwind HAVIND Tailwind TAVIND Displays headwind HAVIND or tailwind TAVIND component relative to the airplane heading 2 Crosstrack Error XTK ERROR Displays crosstrack XTK error in nautical miles left or right of the active route 3 TAS Displays airplane true airspeed 4 LEFT FUEL USED Displays fuel used by left engine sensed by fuel flow meters 80 81 DO NOT USE FOR FLIGHT 5 Fuel Quantity QTY TOTALIZER Displays total fuel quantity from the fuel system quantity processor The fuel remaining line displays two independent fuel remaining values TOTALIZER and CALCULATED They can be compared to validate FMC calculations 6 WIND Displays current wind direction and speed referenced to true north 7 Crosswind X WIND Displays left L or right R crosswind compone
96. te commands for manual and automatic flight path control The FMS tunes the navigation radios for position updating The FMS navigation database supplies the necessary data to fly routes SIDs STARs holding patterns and procedure turns Cruise altitudes and crossing altitude restrictions are used to calculate VNAV commands FLIGHT MANAGEMENT COMPUTER FMC The heart of the flight management system is the flight management computer The FMC uses flight crew entered flight plan data airplane systems data and data from the navigation database to calculate airplane present position and generate the pitch roll and thrust commands necessary to fly an optimum flight profile The FMC sends these commands to the autothrottle autopilot and flight director Map and route data are sent to the HSIs The EFIS control panels are used to select the data to be displayed on the HSIs The mode control panel selects the autothrottle autopilot and flight director operating modes The FMC is certified for area navigation when used with navigation radio and or GPS updating The FMC and CDU are used for enroute and terminal area navigation RNAV approaches and as a supplement to primary navigation means when conducting other types of nonprecision approaches Note To use FSX flight plans with 757 Captain they need to be saved at Documents Flight Simulator X Files folder ICONTROL DISPLAY UNITS CDUS CDU is used to control the FMC 2011
97. the FMC data bases LEGS ACT RTE 1 LEGS 174 130 HDG bnm 1000 200 10004 5 131 SNM LACRE 250 2500A 128 2NM 6 N47W122 252 10406 070 7NM VAMPS 320 80004 087 21NM 637 FL190 7 lt RTE 2 LEGS RTE DATA a 9 BANDR lt CTR gt 637 FL190 MAP CTR lt RTE 2 LEGS STEP gt 10 1 Page Title Title format shows route status e RTE X LEGS inactive route e ACT RTE X LEGS active route e MOD RTE X LEGS modified active route 2 Leg Direction Leg segment data in line title courses magnetic xxx or true xxx T arcs distance in miles ARC turn direction example 24 ARC L heading leg segments xxx HDG track leg segments xxx TRK special procedural instructions from database HOLD AT PROC TURN Calculated great circle route leg directions may be different than chart values Dashes are shown for an undefined course 3 Waypoint Identifier Shows waypoints by name or condition Active leg is always the first line of the first active RTE X LEGS page 56 DO NOT USE FOR FLIGHT All route waypoints are shown in flight sequence Waypoints on an airway are included on the route legs page Waypoints can be modified Examples e add waypoints e delete waypoints e change waypoint sequence e connect route discontinuities Boxes are shown for route discontinuities Dashes are diplayed on the line following the last waypoint on
98. the route 4 Route 2 Legs RTE 2 LEGS Push e shows the RTE 2 LEGS e when RTE 2 LEGS page is shown prompt changes to RTE 1 LEGS 5 Waypoint Speed Altitude Constraints Waypoint speed or altitude constraint in large font Manual entry allowed in climb or descent phase Entered by FMC when constraints are part of a procedure Speed constraint is assumed to be at or below the displayed speed Valid entries are e speed airspeed or Mach requires an altitude constraint at the same e waypoint e altitude in thousands of feet or flight level 19000 190 XXX XXXXX airspeed altitude entered simultaneously XXX airspeed only XXXXX or XXXXX altitude only Altitude constraint suffixes e blank cross at altitude e A cross at or above altitude e B cross at or below altitude e both altitude block Example 220A240B 6 Distance to Waypoint Distance between the waypoints displayed in nautical miles The first line displays the distance from the airplane to the active waypoint 7 Waypoint Speed Altitude Predictions Waypoint speed and altitude predictions are displayed in small font Dashes are displayed in the descent region prior to descent path calculation Descent path calculation requires altitude constraint below cruise altitude 8 ACTIVATE Route Data RTE DATA Push three possible prompts e ACTIVATE activates inactive flight plan shows RTE DATA prompt e RTE DATA shows route data page e STEP changes th
99. ties with one engine inoperative The long range cruise LRC mode calculates speeds to maximize airplane range VNAV Cruise mode 1 ACT ECON CRZ 2 3 CRZ ALT STEP TO 2 FL350 FL390 ECON SPD AT 3 810 1300z 1200Nm EPR KORD ETA FUEL 4 1 352 2030z2 14 5 6 STEP SIZE OPT MAX FL330 FL390 5 1 Page Title The page title displays active ACT or modified MOD cruise Usually the title contains ECON for economy cruise Fixed speed engine out and long range cruise modify the title Page titles include e CRZ CLB or CRZ DES cruise climb or descent e ECON speed based on cost index e LIM SPD based on an airplane configuration limiting speed LRC long range cruise selected MCP SPD speed intervention applied from the MCP M XXX fixed Mach cruise speed XXXKT fixed CAS cruise speed Fixed cruise speeds are for e waypoint speed constraints e an altitude constraint associated with a speed constraint e a flight crew selected speed SEL SPD 2 Cruise Altitude CRZ ALT Displays cruise altitude entered on PERF INIT page Valid entries are XXX XXXX XXXXX OR FLXXX Altitude displays in feet or flight level depending on the transition altitude Changing the MCP altitude enters the new altitude in the scratchpad for entry Entry creates a modification When the modification is executed the page title changes to CRZ CLB or CRZ DES 2011 Captain Sim www captainsim com 757 Captain FLIGHT MANUAL Part V Flig
100. tion The line titles are e DEST performance predictions to destination Default display e DIR TO FIX when entered waypoint is not in flight plan Data is based on flying present position direct to the waypoint e EN ROUTE WPT when entered waypoint is in flight plan Line data are based on flying the flight plan route to the waypoint e MOD a modification has been made on another page Performance predictions include modification Entries do not modify the active route and are deleted when CDU is changed to a different page 4 Selected Speed SEL SPD Displays the FMC active command speed The active speed mode is the same as on the performance page unless changed by the MCP or a limit The speed modes are e LRC SPD long range cruise speed ECON SPD economy speed SEL SPD selected speed manually entered on the CDU LIM SPD speed is limited by VMO MMO flap limit or buffet limit MCP SPD MCP speed IAS MACH indicator 5 Position Report POS REPORT Push displays the POS REPORT page 6 ETA Estimated time of arrival at waypoint or destination 7 Distance To Go DTG Distance to go to waypoint or destination 8 FUEL Estimated fuel remaining at waypoint or destination 9 TO Top Of Descent T D ETA and DTG to next VNAV profile point The line title and data change for other phases of flight Other line titles e TO T C top of climb data e TO STEP CLIMB step climb data e TO E D end of descent da
101. tudes using the standard lapse rate 757 Captain FLIGHT MANUAL Part V Flight Management System 77 DO NOT USE FOR FLIGHT ACT RTE 1 DATA BANDR BANDR WIND 3 15 OAT DIR SPD 21 KT 9 C 315 40KT 5 C 317 23KT ALT OAT 10000 5 RTE DATA gt 1 Page Title Displays ACT XXXXX where XXXXxX is the waypoint for which the wind page was selected When a route is being modified MOD in is shown in the page title If ACT is displayed when the wind page is first accessed entry of wind data caused MOD to be displayed Wind entries must be executed 2 Altitude ALT Enter altitude or flight level for wind entries Altitude data entry is possible only on line 1L After altitude entry data is sorted in ascending order in lines 1 through 4 Dashes display on right side of line for wind direction and speed entry When all four lines have data one must be deleted before new data can be entered Entered altitudes are propagated to all wind pages 3 Altitude Flight Level Data Displays the altitude or flight level for wind entries Data entered on 1L is displayed on lines 1 through 4 in ascending order Altitude entry is not possible in lines 2L through 4L Calculated OAT based on standard lapse rate from the entry made on the ALT OAT line are display in small font 4 ERASE Push removes modified data 757 Captain FLIGHT MANUAL Part V Flight Management System 78 DO NOT US
102. waypoint INVALID DELETE deletion of selected data is not allowed INVALID ENTRY entry format or range is incorrect for the selected field or the entered airway or TO waypoint does not coincide with the navigation database MANUALLY TUNED attempt to remotely tune a VOR that is manually tuned NOT IN DATABASE data is not in the route or the navigation database NOT ON INTERCEPT HEADING LNAV selected and the airplane is outside active capture criteria and the present heading will not intercept the active leg UNABLE CRZ ALT performance predicts a zero cruise time at the entered cruise altitude XXXXX altitude set in the MCP window when VNAV is engaged the CLB or CRZ page is displayed and the altitude is above within 4000 feet below and not equal to the CRZ ALT CDU ANNUNCTIATOR LIGHTS These annunciator lights illuminate when certain conditions exists DSPY a flight plan modification is pending and the RTE RTE LEGS RTE DATA or RTE HOLD page not containing the active leg or route segment is displayed or a VNAV page CLB CRZ or DES not corresponding to the active VNAV mode is displayed FAIL the associated FMC has failed MSG an FMC message is waiting to display or is displayed 2011 Captain Sim www captainsim com 757 Captain GHT MANU Part V Flight Management System 98 DO NOT USE FOR FLIGHT Section 10 NAVIGATION DATABASE ICAPTAIN SIM NAVIGATION DATABASE FILES FORMAT The files are hel
103. ww captainsim com lanagement System 44 DO NOT USE FOR FLIGHT 5 Arrival ARR Route 1 Destination Push displays the arrival page for route 1 destination airport 6 Arrival ARR Route 2 Origin Push displays the arrival page for route 2 origin airport Origin airport arrivals selection is used during a turn back situation 7 Arrival ARR Route 2 Destination Push displays the arrival page for route 2 destination airport 8 Arrival ARR Other Displays the arrival page for the airport entered in this line through the scratchpad ARR prompt for OTHER allow display of arrival data about airports that are not an origin or destination The data can be viewed but cannot be selected because the airport is not on the route DEPARTURES PAGE The departures page is used to select the departure runway SID and transition for the route origin airport The departures page for the inactive route displays when the DEP ARR function key is pushed with an inactive RTE or RTE LEGS page is displayed DEP ARR INDEX lt DEP KBFI DEP On ground active route KBFI DEPARTURES 1 1 SIDS RTE 1 RUNWAYS LACRE3 lt SEL gt lt SEL gt 13R TRANS HUMPP ORTIN lt ERASE 1 Standard Instrument Departures SIDS Displays a list of SIDS for the airport Push e selects SID for use in the route e other SIDs no longer display and transitions for the selected SID display 45 DO NOT USE FO
104. y to change to navigate mode and has not received a present position entry Use the CLEAR key to remove this message INSUFFICIENT FUEL estimated fuel at destination less than entered RESERVES value NO ACTIVE ROUTE LNAV selected and no active route activated PERF VNAV UNAVAILABLE VNAV selected and gross weight cost index or cruise altitude are not entered RESET MCP ALT 2 minutes prior to the top of descent point with VNAV active and MCP not set to altitude below cruise altitude TAKEOFF SPEEDS DELETED selected V speeds have been deleted due to changes in takeoff performance or configuration data THRUST REQUIRED VNAV active autothrottle disconnected and additional thrust required to track VNAV descent path and maintain speed 757 Captain FLIGHT MANUAL Part V Flight Management System 97 DO NOT USE FOR FLIGHT FMC ADVISORY MESSAGES FMC advisory messages are displayed on the CDU scratchpad and illuminate the CDU message light MSG There are no EICAS messages associated with these messages and they do not cause the FMC light to illuminate Those messages which are caused by an entry error must be cleared before the entry can continue DELETE DEL key pushed HOLD AT XXXX a waypoint not contained in the active route is entered into the HOLD AT box on the RTE LEGS page after selection of the HOLD function key Selection of HOLD AT XXXX into a RTE LEGS page waypoint line makes a holding fix at the XXXX
Download Pdf Manuals
Related Search
Related Contents
®axel MTS-6000 Module Bedienungsanleitung DE Zonet ZFM5621-MT modems MANUEL D’ENTRETIEN GE PP9830DJBB Use and Care Manual programme_saison_13_14 Untitled - strong>strong> TCS Tuner Software User`s Manual for Dodge 1 Introduction_PC.indd Copyright © All rights reserved.
Failed to retrieve file