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Garmin Pilatus PC_6 Cockpit Reference Guide

1. Export a Hight Plan to an SD Card R a d Load and Activate a Departure Procedure Activate A Departure Leg sss Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure 36 Activate An Approach in the Active Flight Plan 37 Activate a Vector to Final Approach Fix sss 38 Activate A Missed Approach in the Active Flight Plan ww lt 38 HAZARD AVOIDANCE 39 Customizing the Hazard Displays on the Navigation 39 STORMSCOPE Optional 39 Traffic Systems oriente aca nid gr tem ata entren 41 Terrain And Obstacle Proximity ssssssseen 43 Terrain Awareness 8 Warning System TAWS B Display Optional 44 Airborne Color Weather Radar Optional sss 45 ADDITIONAL FEATURES TL CD sss KOIDSIUDI ABNORMAL OPERATION 51 Reversionary Mode cccccsccsssscsssssscsssssescesssssceesssssceesssnsceesssssceesssnsceesssnsceesssnsceesnsnseen 51 Abnormal COM Operation 51 Hazard Displays with Loss of GPS Position 51 Unusual Attitudes usa ote Rare 52 Dead Reckoning ssssssseeneeen nnne 53 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN LLL Tabl
2. 72 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B dh GARMIN Appendir APPENDIX sjuauimasu sub PFD SOFTKEY MAP optional mer L 1 Kos mx we Dew ST fe Wer wmm nan ES 59 olpny uqax uo2 AEN CDI NAV2 52 Top Level PFD Softkeys optional pmpmnmnnnunnunnn AEN Sd5 buluueld nubi optional rrarric Toro enra erms L Teac _J aters F ENES HU mnm Press the BACK Softkey to return to 8 the top level softkeys gt Inset Map Softkeys PE INSET Displays Inset Map in PFD lower left corner E OFF Removes Inset Map 83 DCLTR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan SHE unuuy gt 5 o 3 x x pul TRAFFIC Displays traffic information on Inset Map 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 n Flight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index Appendix TOPO TERRAIN STRMSCP INSET A GARMIN Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Inset Map Displays terrain i
3. ssssseeeet nnne 9 FLIGHT PLANNING a 21 Trip Planning e debe b Ail ee d a be de edge 21 Create a New User Waypoint Defined by Latitude amp Longitude 23 Create a New User Waypoint Defined by Radials from Other Waypoints 23 Create a New User Waypoint Defined by a Radial amp Distance from Another Waypolnt eee eed 25 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Table of Contents GARMI N Delete a User WAyPONN w nnn 26 Create a New Flight PIAN ww ma 2 Import a Flight Plan from an SD Card 28 Insert a Waypoint in the Active Flight Plan 29 Enter an Airway in a Flight Plan 29 Invert An Active Flight Plan 30 Remove a Departure Arrival Approach or Airway from a Flight Plan 30 Store a Flight Plan nennen 31 Edit a Stored Flight 66 31 Delete a Waypoint from the Flight Plan sss 31 Invert and Activate a Stored Flight 5 32 Copy a Flight PIAN ww nnn Delete a Flight Plan Graphical Flight Plan 5
4. 2 Elevator Trim Bar ELEV 3 Flap Position Indicator FLAPS Engine Indication System Displays engine torque in foot pounds ft lb Displays Interstage Turbine Temperature ITT in degrees Celsius C When the engine is not running OFF is annunciated above the ITT readout this changes to STRT upon engine start No annunciation is shown when the engine is running normally Displays propeller speed in revolutions per minute rpm Displays gas generator speed as a percentage Displays current fuel flow in gallons per hour gph Displays engine oil pressure in pounds per square inch psi Displays engine oil temperature in C Displays DC current in amperes amps for the generator G Alternate Power A is not used Displays DC bus voltages for bus 1 and bus 2 Displays quantities of fuel in gallons in the main left L and right R tanks Aileron and rudder trim are indicated with pointers along slide bars the green bars indicate takeoff trim positions Elevator trim is indicated with a pointer along a slide bar takeoff trim position is indicated with a green bar and T O label Flap deflection is indicated with a pointer along a slide bar Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN Engine Indication System SYSTEM DISPLAY ELECTRICAL G GEN A ALT A 4 BUS 1 V BUS 2 V System Display Oil Pressure Displays
5. Altitude Reporting Mode transponder replies to identification and altitude interrogations Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations Automatically enters the VFR code 1200 in the U S A only Displays transponder code selection softkeys 0 7 Use numbers to enter code Removes numbers entered one at a time Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN o Appendix IDENT Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen sjuauimasu nubi TMR REF Displays Timer References VVindovv a NRST Displays Nearest Airports Window ALERTS Displays Alerts Window ze on o MFD SOFTKEY MAP mew qp we L L L L L E29 1 1L 8 LA DJ V3 V V V ji a ES Press the BACK softkey on this level to m return to the top softkey level 7 2 ENGINE system Fu C8 z FS rv v3 n EES ipe eum to the top softkey level optional m m T 38 Q RAFFIC ToPo TERRAIN AIRWAYS Ernvserl 1 a v AIRWY ON Y ARAYLO ENGINE SYSTEM FUEL becFurt incruet ssrrurL 1 Back Y EY EY EY Y FN XA EY su SeJnpa20Jd MFD Softkeys q ENGINE Displays
6. 2 Press the NAV1 NAV2 DME or ADF Key on the audio panel to select or deselect the navigation radio audio source All radio keys can be selected individually or together NAV COM TUNING 1 Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 2 Press the appropriate Frequency Transfer Key to place the frequency into the active frequency field Or 1 Press the COM or NAV Key on the PFD MFD Control Unit to select the desired COM or NAV frequency box 2 Turn the FMS XPDR COM NAV Knob to tune the desired frequency large knob for MHz small knob for kHz 3 Press the Frequency Transfer Key to transfer the frequency to the active field DIGITAL CLEARANCE PLAYER NOTE Only the audio for the selected COM MIC Key is recorded Audio is not recorded for COM3 MIC Pressing the PLAY Key once plays the latest recorded memory block then returns to normal operation Pressing the MKR MUTE Key while playing a memory block stops play Pressing the PLAY Key during play begins playing the previously recorded memory block Each subsequent press of the PLAY Key begins playing the next previously recorded block Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COPLT Key on the audio panel to select those isolated from hearing the Nav Com radi
7. WPT ARRIVAL Arriving at waypoint boxx Arriving at waypoint boox where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft will penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and Special use airspace is near and ahead of the ahead aircraft position ARSPC NEAR Airspace near less Special use airspace is within 2 nm of the aircraft than 2 nm position APR INACTV Approach is not active The system notifies the pilot that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver PTK FAIL Parallel track unavailable bad geometry Bad parallel track geometry PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset PTK FAIL Parallel track unavailable past IAF IAF wayp
8. Attempt to reload the aviation database If problem persists the G950 system should be serviced MFD1 DB ERR MFD1 basemap database error exists database error exists PFD1 DB ERR PFD1 basemap The MFD and or PFD detected a failure in the basemap database MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists The G950 system should be serviced The terrain database is present on another LRU but is missing on the specified LRU 60 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists Comments The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists The G950 system should be serviced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing The obstacle database is present on another LRU
9. Press the ENT Key The cursor is displayed in the RAD radial field for the second waypoint Enter the desired radial from the reference waypoint 15 Press the ENT Key 16 Press the FMS Knob to remove the flashing cursor CREATE A NEW USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM ANOTHER WAYPOINT sjuauimasu Yid oipny udax si U105 AeN 52 1 Turn the large FMS Knob on the MFD to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 4 Enterthe desired waypoint name 5 Press the ENT Key 6 The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field 7 With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types 8 Tum the small FMS Knob to select RAD DIS radial distance 9 Press the ENT Key 10 The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints m
10. but is missing on the specified LRU MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists The G950 system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists The G950 system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD and or PFDs detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The G950 system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD and or PFDs detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The G950 system should be serviced DB MISMATCH Aviat
11. window 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 oipny uddx 59 sjuaumasu U105 AEN 16114 52 2 Buluuejd AEN Sd5 nubi uoneiado saunyea4 e uepioAy Junuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com Fight EIS Instruments XPDR Audio AFCS Flight Procedures Planning GPS Nav Hazard Features Avoidance Additional Abnormal Operation Appendix Index Flight Planning GARMI N 4 5 With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Once all changes have been made press the FMS Knob to remove the cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the desired flight plan 5 Press the INVERT Softkey Invert and activate stored flight plan is displayed 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location COPY A FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the larg
12. 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight Map Setup 3 Press the ENT Key 4 Turn the small FMS Knob to highlight Weather 5 Press the ENT Key 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 39 AEN Sd5 S24V oipny uddx sia syuawinyysuy Tuo2 AEN fid Duruue d kija aoueploay s mp oold paezey suelv uoneiedo sainjea4 Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 40 6 Turn the large FMS Knob to place the cursor in the STRMSCP MODE field 7 Turn the small FMS Knob to display the Cell Strike window 8 Turn either FMS Knob to select Cell or Strike Press the ENT Key 9 Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure th
13. AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Flight Instruments A GARMIN ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 2 3 Press the OBS Softkey to select OBS Mode Turn a CRS Knob to select the desired course to from the waypoint Press a CRS Knob to synchronize the Selected Course with the bearing to the next waypoint Press the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 2 3 Press the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted Turn the small FMS Knob to display the UP DOVVN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it starts counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS 1 2 3 4 5 6 Press the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vspeed Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field Turn the small FMS Knob clockwise to ON or counterclockwise to O
14. Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 5 6 7 A GARMIN with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway vvaypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key Repeat step numbers 4 and 5 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list IMPORT A FLIGHT PLAN FROM AN SD CARD 28 1 2 3 4 5 6 1 8 NOTE See the Annunciations amp Alerts section for flight plan import message descriptions Insert the SD card containing the flight plan in the top card slot on the MFD Press the FPL Key on the MFD to display the Active Flight Plan Page Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn either FMS Knob to highlight an empty or existing flight plan Press the IMPORT Softkey If an empty flight plan is selected a list of the available flight plans on the SD card will be displayed Or If an existing flight plan is selected an Overwrite existing flight plan OK or CANCEL prompt is displayed Press the ENT Key to choose to overwrite the selected flight plan and see a list of the av
15. Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN 1 After creating a flight plan on either the PFD or MFD it may be saved by pressing the ME NU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK highlighted press the ENT Key to store the flight plan EDIT A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD then turn the small FMS Knob to display the Flight Plan Catal og Page 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan 4 Press the EDIT Softkey 5 Turn the large FMS Knob to place the cursor in the desired location 6 Enterthe changes then press the ENT Key 7 Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the curs Of Or for a stored flight plan a Press the FP b Turn the small FMS Knob to select the Flight Plan Catalog Page L Key on the MFD Press the FMS Knob to activate the cursor d Turn the large FMS Knob to highlight the desired flight plan e Press the EDIT Softkey 2 Tum the large FMS Knob to highlight the waypoint to be deleted 3 Press the CLR Key to display a REMOVE Wpt Name confirmation
16. airborne press the WEATHER Softkey Or If the aircraft is already airborne press the WEATHER or GROUND Softkey The one minute warm up period is initiated after which the radar begins transmitting The horizontal scan is initially displayed 5 Turn the Joystick to select the desired range 6 If desired press the VERTICAL Softkey for vertical scanning Adjusting Antenna Tilt Move the Joystick up or down to adjust the tilt of the antenna up or down Moni tor the displayed tilt value in the TILT field When scanning vertically a Tilt Line may be displayed to aid in positioning the tilt of the antenna If the Tilt Line is not displayed perform the following steps 1 Press the MENU Key 2 Tum the large FMS Knob to select Show Tilt Line 3 Press the ENT Key Adjusting Antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left Monitor the displayed bearing value in the BEARING feld When scanning horizontally a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan If the Bearing Line is not displayed perform the fol lowing steps 1 Press the MENU Key 2 Tum the large FMS Knob to select Show Bearing Line 3 Press the ENT Key 46 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN Hazard avoidance Vertically Scan a Storm Cell 1 While in the Horizontal Scan view move the Joystick to pla
17. are shown first in the list followed by all altitude airways and then high altitude airways Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted Press the ENT Key The system returns to editing the flight plan with the new airway inserted INVERT AN ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the MENU Key to display the Page Menu Turn the large FMS Knob to highlight Invert Flight Plan Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT 30 1 2 PLAN Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key on the MFD b Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor d Turn the large FMS Knob to highlight the desired flight plan e Press the EDIT Softkey Turn the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedure s waypoints Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN Flight Planning 3
18. be entered manually AM ae AI arce White 22V g m 12400r7 MA 220 SA aaa na a Large Light d Blue Text Approach KDFH RNAV 17LcPs LPY RIVET iaf 259 18 8NM 10007 3 Small Light 1776 33 2000rT 176 3 2NM S a t 1757 39w 176 5 3NM x eon 9 Small VVhite Text 990FT 174 8NM with Altitude POLKE Restriction Bar SIUS Cross AT or ABOVE 5 000 ft PAGO Cross AT 2 300 ft cinsli Cross AT or BELOW 3 000 ft 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Sjueuingjsu nubi 59 oipny uddx U105 AeN suelv uoneiedo sainjea4 2 Duruue d Tunuuy Jeuuouqy Jeuonippy paezey bi xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS AFCS Procedures Appendix Alerts Operation Features Index A GARMIN Altitudes associated with approach procedures are auto designated This means the system automatically uses the altitudes loaded with the approach for giving vertical flight path guidance outside the FAF Note these altitudes are displayed as small light blue text Altitudes associated with arrival procedures are manually designated This means the system does not use the altitudes loaded with the arrival for giving vertical flight path guidance until designated to do so by the pilot Note that these altitudes are initially displayed as
19. installed Install correct obstacle database version in all displays DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrrain databases installed Install correct airport terrain database in all displays GMA 347 MESSAGE ADVISORIES Message Comments GMAT FAIL GMAT is inoperative The audio panel self test has detected a failure The audio panel is unavailable The G950 system should be serviced GMA1 CONFIG GMAT config error Config service req d MANIFEST GMAT software mismatch communication halted The audio panel configuration settings do not match backup configuration memory The G950 system should be serviced The audio panel has incorrect software installed The G950 system should be serviced GMA1 SERVICE GMAT needs Service Return unit for repair The audio panel self test has detected a problem Certain audio functions may still be available and the audio panel may still be usable The G950 system Should be serviced when possible 62 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES Message f Config service req d GIA1 CONFIG GIA1 config error Comments Config service req d GIA2 CONFIG GIA2 config error G950 system should be serviced The GIA1 and or GIA2 configuration setti
20. operation DEAD RECKONING While in Enroute or Oceanic phase of flight if the G950 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G950 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G950 stops navigating in GPS Mode DRModeisindicated on the G950 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure Also the CDI deviation bar is removed from the display Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS WAAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G950 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also l
21. sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV oipny uddx sia sjuaumasu jeuonippy Ju105 AEN jeuuouqy Sue v unuuy iui hi 2 mk d Additional Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts KI Appendix Index M Message advisories 59 62 64 70 Minimums 58 MKR MUTE 12 Mode S 76 Mode selection softkeys 11 Multi Function Display MFD Softkeys 77 N NAV 12 NAV1 1 12 NAV2 1 12 Navigation database 19 20 NEXRAD 78 0 OBS 2 Obstacles 62 63 Oil Pressure 6 7 Temperature 6 7 P Pressure oil 6 7 Propeller speed 6 R Range aircraft 9 10 Reversionary mode 51 ROC 56 57 S SafeTaxi 49 Sector scan 48 STAB 48 Standby 46 Index 2 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 A GARMIN Store Flight Plan 31 Stormscope lightning data 39 40 74 Strike 39 Strike mode 40 T TA 58 59 TAS 42 66 TAWS 44 45 56 Temperature Interstage Turbine 6 Temperature oil 6 7 Terrain 43 44 62 74 78 Terrain SVS 15 Tilt line 46 Timer 68 Topographical data 74 78 Torgue 6 Traffic 39 41 73 78 Traffic advisory 41 Traffic Advisory 58 59 Traffic map page 41 42 43 Transponder 11 76 77 Trim 6 V Vertical speed guidance 20 Vertical track 58 VNV 17 52 70 Voltmeter 6 8 Vspeed 2 W WAAS 63 WATCHG 48 Waypoint Selec
22. select the desired Nav radio Press the ENT Key to complete the selection ENTER A TRANSPONDER CODE 1 2 3 Press the XPDR Softkey to display the transponder mode selection softkeys Press the CODE Softkey to display the transponder code selection softkeys for digit entry Press the digit softkeys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active SELECTING A COM RADIO Transmit Receive Press the COM1 MIC COM2 MIC or COM3 MIC Key optional COM if installed on the audio panel Receive Only Press the COM1 COM2 or COM3 Key optional COM if installed on the audio panel 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 sjuauimasu sub S24V orpnyygqax sia JUI05 AEN xipueddy Suelv uoneiedo sainjea4 e uepioAy 2 Duruue d AEN Sd5 Tunuuy Jeuuouqy Jeuonippy paezey bi x pul Flight Instruments Abnormal Additional Hazard Flight Planning Annun Nav Com XPDR Audio EIS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN SELECTING A NAV RADIO 1 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VORT LOC1 NAV1 or VOR2 LOC2 NAV2
23. the desired waypoint d Press the ENT Key 11 Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint 12 Press the ENT Key 13 The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 26 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN flight Planning 4 Turnthe large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the desired waypoint 6 Press the DELETE Softkey 7 The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key CREATE A NEW FLIGHT PLAN NOTE When creating a new flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan 1 Press the FPL Key 2 Press the FMS Knob to activate the cursor only on MFD 3 Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counte
24. white text These altitudes may be designated by placing the cursor over the desired altitude and pressing the ENT Key After designation the text changes to light blue Altitudes that have been designated for use in vertical navigation may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key The altitude is now displayed only as a reference t is not used to give vertical flight path guidance Other displayed altitudes may change due to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude GPS Navigation White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated bythe Altitude has been entered The system cannot System estimating the by the pilot Altitude is use this altitude in altitude of the aircraft as it designated for use in determining vertical passes over the navigation giving vertical flight path 1 flight path guidance point This altitude is guidance Altitude does provided as a reference not match the published and is not designated to 1 altitude in navigation be used in determining database or no published vertical flight path altitude exists guldance Small Text Altitude is not designated Altitude is designated The system cannot to be used in determining for use in giving vertical use this altitude in vertical flight path flight path guidance determining vert
25. 59 sjuauimasu U105 AEN 346 3 52 AEN 540 Duruue d wold s mp old uoneiado saunyea4 Junuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures GARMIN 4 5 6 1 8 3 10 11 12 Turn the large FMS Knob to highlight the desired arrival Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways may be displayed for the selected arrival Turn the large FMS Knob to highlight the desired runway Press the ENT Key With LOAD highlighted press the ENT Key The arrival becomes part of the active flight plan If an altitude associated with a waypoint in an arrival procedure is to be used to calculate vertical guidance perform the following steps a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight the desired waypoint altitude Press the ENT Key to designate the altitude for use in giving vertical guidance ACTIVATE AN ARRIVAL LEG 1 2 3 4 5 Press the FPL Key on the MFD to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight t
26. 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00851 00 Rev B Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 GARMIN Engine indication System ENGINE INDICATION SYSTEM ENGINE DISPLAY In all cases green indicates normal operation yellow indicates caution and red indicates warning Pressing the ENGINE Softkey makes available the SYSTEM and FUEL Softkeys which in turn provide access to the Lean Page and the System Page respectively FFLOW GPH OIL PSI OIL C AMPS iG cO X UO Engine Display 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Sjueuinijsu UATE MES xipueddy Suelv uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld AEN Sd5 2 olpny uqax unuuy jeuuouqy jeuonippy paezey BITE U105 AEN x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS Procedures GPS Nav Appendix Alerts Operation Features Index Torque Gauge TRQ FT LB Interstage Turbine Temperature Gauge ITT C Propeller Speed Gauge NP RPM Gas Generator Speed Gauge NG G Fuel Flow FFLOW GPH 5 Oil Pressure Indicator OIL PSI Oil Temperature Indicator OIL C VOLTS Fuel Quantity Indicator FUEL QTY 1 Aileron and Rudder Trim Bars AIL RUD
27. 950 Pilot s Guide documentation Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G950 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation WARNING The illustrations in this guide are only examples Never use the G950 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 A Warnings Gintars amp Notes GARMIN WARNING Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between l
28. CTIVE FLIGHT PLAN 38 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH Press the ENT Key A confirmation window is displayed With ACTIVATE highlighted press the ENT Key Or Press the Go around Button Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN Hazara avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page STORMSCOPE OPTIONAL WARNING The Stormscope system is not intended to be used for hazardous thunderstorm penetration Weather information on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 Press the MAP Softkey 2 Press the STRMSCP Softkey Press the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page Lightning Age Symbol Strike is less than 6 seconds old KA Strike is between 6 and 60 seconds old ET Strike is between 1 and 2 minutes old Strike is between
29. DR Reduced Required PULL UP RE Se Terrain Terrain Pull Up Terrain Clearance or Pull Up Warning RTC or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain PULL UP Terrain Ahead Pull Up Impact Warning ITI or Terrain Ahead Pull Up TERRAIN PULL UP M 7 Terrain Terrain Pull Up Pull Up Reduced Required PULL UP HAr Obstade Obstacle Pull Obstacle Clearance or Up Pull 5 i Obstacle Ahead Pull Up Obstade Ahead Pull Up 56 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN Annunciations amp Alerts PFD MFD MFD Alert Type TAWS B Page Aural Message PME Pop Up Alert Annunciation Imminent Obstade Obstacle Ahead Pull Up Impact Warning or Obstacle Ahead Pull Up OBSTACLE PULL UP yi Obstacle Obstacle Pull Up Pull Reduced Required CAUTION TERRAIN Caution Terrain Caution Terrain Clearance or Terrain Caution RTC TERRAIN AHEAD or Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN AHEAD Terrain Ahead Terrain Impact Caution ITI or Ahead CAUTION 1 1 Caution Terrain Caution Terrain Reduced Required CAUTION OBSTACLE Caution Obstacle Obstacle Clearance or Caution Obstacle Caution ROC HB o Obstacle Ahead Obstacle Ahead Imminent Obstacle OBSTACLE AHEAD Obstacle Ahead Obstacle Impact Cautio
30. EXPIRD Timer has expired The system notifies the pilot that the timer has expired DB CHANGE Database changed Verify user modified procedures This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an aviation database update Verify that the user modified procedures in stored flight plans are correct and up to date DB CHANGE Database changed Verify stored airways FPL TRUNC Flight plan has been This occurs when a stored flight plan contains an airway that is no longer consistent with the aviation database This alert is issued only after n aviation database update Verify use of irways in stored flight plans and reload airways as needed ab This occurs when a newly installed aviation truncated database eliminates an obsolete approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach 68 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message LOCKED FPL Cannot navigate locked flight plan Comments This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint
31. FF To remove the window press the CLR Key or the TMR REF Softkey Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN Pightinstruments SET BAROMETRIC MINIMUM DESCENT ALTITUDE mal ED g 2 a 1 Press the TMR REF Softkey 2 Turn the large FMS Knob to highlight the OFF BARO field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to BARO 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 To remove the window press the CLR Key or the TMR REF Softkey 593 olpny uqax 0105 AEN 52 DISPLAYING WIND DATA AEN Sd5 1 Press the PFD Softkey 2 Press the WIND Softkey to display wind data to the left of the HSI 3 Press one of the OPTN softkeys to change how wind data is displayed 4 To remove the Wind Data Window press the OFF Softkey Duruue d yi SeJnpa20Jd CHANGING HSI FORMAT 1 Press the PFD Softkey 2 Press the HSI FRMT Softkey 3 Press the 360 HSI Softkey to display the full size HSI Or Press the ARC HSI Softkey to display the arc style HSI sual uoneiado saunyea4 unuuy jeuuouqy jeuonippy paezey xipueddy x pul 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 A GARMIN Flight Instruments i E oipny uadx U105 AEN S2dV AeN Sd5 Buluuejd Blank Page
32. Fuel pressure is low Generator has failed Oxygen pressure is low Single Chime SAFE OPERATING ANNUNCIATION Annunciation Text Alerts Window Message Audio Alert Auxiliary fuel pump is active Anti ice system on Alternate power source battery in use Aircraft using external power None 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 55 sainjea4 2 buluueld AEN Sd5 S24JV olpny uqax sia sjuaumnasu 2 yi uio AeN Yid jeuonippyv uoneiedo Jeuuouqy 2 Do x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix bres Annunciations amp Alerts A GARMIN Annunciation Text Alerts Window Message Audio Alert Landing light is on Left external fuel transfer pump is active Right external fuel transfer pump is active Prop deice is on i Tow cable attached ALERT MESSAGE Alerts Window Message Audio Alert PFD FAN FAIL The cooling fan for the PFD is inoperative None MFD FAN FAIL The cooling fan for the MFD is inoperative None TAWS B ALERTS PFD MFD MFD Alert Type TAWS B Page Aural Message e Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Rate Warning E
33. G The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G950 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74A Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G950 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G950 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on the G950 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING Use of the Stormscope is not intended for ha
34. G950 Integrated Flight Deck Cockpit Reference Guide for the Pilatus PC 6 A GARMIN Copyright O 2009 2010 Garmin Ltd or its subsidiaries All rights reserved f software versions Garmi Tel 9 Garmi This manual reflects the operation of System Software version 0935 02 or later Some differences in operation may be observed when comparing the information in this manual to earlier or later n International Inc 1200 East 151st Street Olathe Kansas 66062 U S A 13 397 8200 Fax 913 397 8282 n AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmi South n Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park ampton 5040 9RB U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garm in Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 STI or af Web Site Address www garmin com Except ter hours emergency aircraft on ground AOG technical support for Garmin panel mount and integrated avionics systems please contact Garmin s AOG Hotline at 913 397 0836 as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose witho down other or pri notice and provided furthe revision hereto is strictly prohibited ut the expres
35. G950 system should be serviced when possible GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEA1 config error Config service req d The GEA1 configuration settings do not match those of backup configuration memory The G950 system should be serviced MANIFEST GEA1 software mismatch communication halted The 1 GEA 71 has incorrect software installed The G950 system should be serviced 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 65 aoueplony sainpadojd Buluueld AEN 540 S24V oipny uadx si sjueumasu jeuonippy 2 nubi JUI0 NEN nub SoJnjeaJ uoneiedo Jeuuouqy i E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix m Annunciations 8 Alerts GTX 33 MESSAGE ADVISORIES A GARMIN Message XPDR1 CONFIG 1 config error Config service req d Comments The transponder configuration settings do not match those of backup configuration memory The G950 system should be serviced MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The G950 system should be serviced XPDR1 SRVC XPDR1 needs service Return unit for repair The 1 transponder should be serviced when possible XPDR1 FAIL XPDRI is inop
36. Generic TIGE occorre e ac c an cara p cr 2 Configure Vspeed Bugs 2 Set Barometric Minimum Descent Altitude sss 3 Displaying Wind Data 3 Changing HSI FOTMat wwwwwww nnns 3 ENGINE INDICATION 5 9 5 Engine Display een etn eee nae n n 5 System Display entere en rere ttd inerenti RR HR edm 7 Fuel Display ose edebat dede MUME MUME 8 NAV COM TRANSPONDER AUDIO 1 ADF Tuning 1 DME Tuning Optional cc ccccccssscssssssssssccssssssssssesssssssssssesssssssssscessssssssssessssssssnsess 1 Enter a Transponder Code 1 Selecting a COM Radio 1 Selecting a NAV Radio 2 NAV COM Tuninj x oct erm tht rem tht remet tret trm veg eee 2 Digital Clearance Player 2 Intercom System ICS Isolation sss 3 AUTOMATIC FLIGHT CONTROL 5 5 S TEC Fifty Five X Autopilot sese 5 ob b b k 7 Direct to NAVIGAtION 7 Activate a Stored Flight Plan 8 Activate a Flight Plan Leg 8 Stop Navigating a Flight 6755 9 Vertical Navigation VNAV
37. M for the installed autopilot S TEC FIFTY FIVE X AUTOPILOT A NOTE This section covers only the additional FD status annunciations that may appear in the G950 AFCS Status Box These status annunciations are not analogous to both the G950 and the S TEC Fifty Five X Refer to the approved S TEC Fifty Five X Pilot s Operating Handbook POH for comprehensive list of annunciations and operating instructions Inadditiontothe redundant status mode annunciations and or visual representations that are simultaneously displayed on both the G950 AFCS Status Box and or PFD and the S TEC Fifty Five X Autopilot Display and or Remote Annunciator Display the G950 displays the additional status mode annunciation of FD when the Flight Director Mode is engaged 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 sia sjueunasu oipny uddx UI0JNeN ARN Sd5 52 suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d junuuy Jeuuouqy Jeuonippy paezey xipueddy x pul iui bi GARMIN AFCS Sjueuinijsu fila 59 U105 AEN 52 AeN 5492 Buluuejd Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00851 00 Rev B Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 16 A GARMIN GPS Navigation GPS NAVIGATION DIRECT TO NAVIGATION Direct t
38. PS Position 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 eoueproAy Senpa204d Buruue d AEN Sd5 52 oipny uddx 53 5149 11 15 puezey ubi U105 AEN ubiu soJnjeoJ jeuonippy Sue v unuuy xipueddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EIS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index Abnormal Operation UNUSUAL ATTITUDES A GARMIN The PFD declutters when the aircraft enters an unusual attitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes 52 Traffic Annunciations AFCS Annunciations Flight director Com mand Bars Inset Map Temperatures DME Information Window Wind Data Selected Heading Box Selected Course Box Transponder Status Box System Time PFD Setup Menu Windows displayed in the lower right corner of the PFD Timer References Nearest Airports Flight Plan Messages Procedures DME Tuning Barometric Minimum Descent Altitude Box Glideslope Glide path and Vertical Deviation Indicators Altimeter Barometric Setting Selected Altitude VNV Target Altitude Extreme Pitch Indication Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN Abnormal
39. S AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 50 4 5 6 1 8 9 A GARMIN Use the FMS Knob to enter the message text to be displayed in the Alerts Window and press the ENT Key Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to Type Turn the small FMS Knob to select the message alert type Event Message issued at the specified date time One time Message issued when the message timer reaches zero default setting Periodic Message issued each time the message timer reaches zero Press the ENT Key again or use the large FMS Knob to move the cursor to the next field For periodic and one time message use the FMS Knob to enter the timer value HH MM SS from which to countdown and press the ENT Key For event based messages a Use the FMS Knob to enter the desired date DD MM YY and press the ENT Key b Press the ENT Key again or use the large FMS Knob to move the cursor to the next field Use the FMS Knob to enter the desired time HH MM and press the ENT Key 10 Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message Delete a Scheduler Message 1 2 3 4 5 Select the AUX Utility Page Press the FMS Knob momentarily to activate the flashing cursor Turn the large FMS Knob to highlight the name field of the scheduler message to be delet
40. T Key to accept the waypoint Or For flight plan leg planning a Press the FPL Softkey at the bottom of the display b Turn the small FMS Knob to select the desired flight plan already stored in memory by number Turn the large FMS Knob to highlight the LEG field d Turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 21 oipny uddx s q sjuauimasu UI05 AEN 1614 52 2 Buluuejd AEN Sd5 nubi uoneiado saunyea4 Junuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 5 22 6 1 8 9 10 11 12 13 A GARMIN Selecting FPL 00 displays the active flight plan If an active flight plan is selected REM is an available option to display planning data for the remainder of the flight plan NOTE The page mode must be set to MANUAL to perform the following steps Turn the large FMS Knob to highlight the departure time DEP TIME field NOTE The departure time on the Trip Planning Page is used for preflight planning Refer
41. Terrain or Obstacle database unavailable or invalid invalid TAWS System software configuration system TAWS FAIL Failure audio fault TAWS Not D No GPS position TAMS N A Available Excessively degraded GPS TANI Not signal Out of database TAMS N A None Available coverage area Sufficient GPS signal received TAWS None None M after loss Available VOICE ALERTS Voice Alert Description Minimums minimums 1 The aircraft has descended below the preset barometric minimum descent altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Traffic Played when a Traffic Advisory TA is issued TIS TIS Not Available The aircraft is outside the Traffic Information Service TIS coverage area 58 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN Annunciations amp Alerts Voice Alert Description Traffic Traffic Played when a Traffic Advisory TA is issued TAS system TAS System Test OK Played when the TAS system passes a pilot initiated self test TAS System Test Played when the TAS system fails a pilot initiated self test Failed MFD amp PFD MESSAGE ADVISORIES Message Comments DATA LOST Pilot stored data was lost Recheck settings The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure th
42. Traffic Symbol Description e Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA Not available with TIS system intruder is within 5 nm and less than 1200 vertical separation O Traffic Advisory TA dosing rate distance and vertical separation meet TA citeria 9 Traffic Advisory Off Scale Traffic Symbol Description Traffic Information Service TIS A NOTE If the G1000 is configured to use a Traffic Advisory System TAS TIS is not available for use A NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Press the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Press the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 AeN Sd5 S24V oipny uadx si sjueumasuj u102 AEN 10614 Duruue d ELE aoueploay s mp oold paezey saunqea4 Jeuonippy Suelv uoneiedo junuuy Jeuuouqy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Pl
43. access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude Black Enable Disable Aviation Data 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN HaadAvoidante TAWS Inhibit Inhibit TAWS While the TAWS B Page is displayed press the INHIBIT Softkey 1 2 3 Or Press the MENU Key Turn the small FMS Knob to select Inhibit TAWS Press the ENT Key Enable TAWS While the TAWS B Page is displayed press the INHIBIT Softkey 1 2 3 Or While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Enable TAWS Press the ENT Key NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current a
44. activate or deactivate Weather Alert press the WX ALRT Softkey Activating and deactivating also enables or inhibits the alert on the PFD Automatic Standby When the weather radar system is in the Weather or Ground Map Mode upon landing the system automatically switches to Standby Mode 48 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN 0 Additional Features ADDITIONAL FEATURES SAFETAXI SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Pressing the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Pressing the DCLTR Softkey twice removes VOR station ID the VOR symbol and intersection names if within the airport plan view Pressing the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Pressing the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams provide the pilot with situational awareness by displaying the aircraft position in re
45. ailable flight plans on the SD card If overwriting the existing flight plan is not desired select CANCEL using the FMS Knob press the ENT Key select another existing or empty flight plan and again press the IMPORT Softkey Turn the small FMS Knob to highlight the desired flight plan for importing Press the ENT Key Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan If required press the FMS Knob to activate the cursor Flight Planning Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint Turn the small FMS Knob The Waypoint Information Window is now displayed Enter the new flight plan waypoint by one of the following a b a b c d a b d e Enter the user waypoint identifier facility or city Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the NRST airport waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display t
46. anning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 42 5 6 A GARMIN Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Press the TNA MUTE Softkey to mute the Traffic Not Available aural alert Displaying Traffic on the Navigation Map 1 2 Ensure TIS is operating With the Navigation Map displayed press the MAP Softkey Press the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory System TAS Optional Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Select the NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field 5 Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 6 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area System Self Test 1 With the Traffic Map Page displayed set the range to 2 6 nm 2 Select the STANDBY Softkey 3 Selec
47. are installed The G950 system should be serviced 66 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN GMU 44 MESSAGE ADVISORIES Annunciations amp Alerts Message HDG FAULT AHRS1 magnetometer fault has occurred Comments A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G950 system should be serviced MANIFEST GMU1 software mismatch communication halted The GMU 44 has incorrect software installed The G950 system should be serviced GWX 68 ALERT MESSAGES Message Comments GWX CONFIG GWX config error Config service req d GWX FAIL GWX is inoperative GWX 68 configuration settings do not match those of the GDU configuration The system should be serviced The GDU is not recieving status packet from the GWX 68 or the GWX 68 is reporting a fault The GWX 68 radar system should be serviced GWX SERVICE GWX needs service Return unit for repair MANIFEST GWX software mismatch communication halted A failure has been detected in the GWX 68 The GWX 68 may still be usable The GWX 68 has incorrect software installed The system should be serviced WX ALERT Possible severe weather ahead GDC 74A MESSAGE ADVISORIES Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm Messag
48. at the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page 1 Turn the large FMS Knob until the Map Page group is selected 2 Turn the small FMS Knob until the Stormscope Page is selected Change the Stormscope Lightning Mode Between Cell and Strike 1 Select the Stormscope Page 2 Press the MODE Softkey The CELL and STRIKE Softkeys are displayed Press the CELL Softkey to display CELL data or press the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 Select the Stormscope Page 2 Press the VIEW Softkey The 360 and ARC Softkeys are displayed Press the 360 Softkey to display a 360 viewing area or press the ARC Softkey to display a 120 viewing area Press the CLEAR Softkey to remove all Stormscope lightning data from the display Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN Hazardavoidance TRAFFIC SYSTEMS If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE softkeys are displayed Ifa Traffic Advisory System TAS is configured STANDBY NORMAL TEST and ALT MODE softkeys are displayed
49. ay also be selected as follows 2 Buluuejd AEN Sd5 nubi a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint Press the ENT Key 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 25 eouepioAy paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning GARMI N Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select
50. ce the Bearing Line on the desired storm cell or other area to be vertically scanned 2 Press the VERTICAL Softkey A vertical slice of the selected area is now displayed 3 Move the Joystick right or left to move the scanned slice a few degrees right or left 4 Turn the Joystick to adjust the range 5 To select a new area to be vertically scanned press the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps Adjusting Gain A WARNING Changing the gain in Weather Mode causes precipitation intensity to be displayed as a color not representative of the true intensity Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation 1 Press the GAIN Softkey to activate the cursor in the GAIN field 2 Turn the small FMS Knob to adjust the gain for the desirable level The gain setting is visible in the gain field as a movable horizontal bar in a flashing box The line pointer is a reference depicting the calibrated S24V oipny uddx 59 sjueuingsu U10 AEN 4613 AEN 540 buluueld Mb position 3 Press the FMS Knob to remove the cursor 4 Press the GAIN Softkey again to recalibrate the gain CALIBRATED is displayed in the GAIN field Ground Mapping 1 Press the MODE Softkey 2 Press the GROUND Softkey to place the radar in Ground Map Mode 3 Press the BACK Softkey 190 00851 00 Rev B Garmin G950 Coc
51. cedures PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Tum the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure is active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key on the MFD to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired waypoint within the departure 4 Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 35 oipny uddx
52. d 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 63 so1njeoJ 2 AEN Sd 24V oipny uadx sia syu unysu paezey Wfila u102 NEN nubi jeuonippy uoneiedo Jeuuouqy dd EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message MANIFEST GFC software mismatch communication halted Comments Incorrect servo software is installed or gain settings are incorrect COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the G950 system should be serviced COM1 SERVICE COM1 needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair COM1 PTT COM push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The system has detected a failure in COM1 and or COM2 COMI and or COM2 may still be usable The G950 system should be serviced when possible The COM1 and or COM2 external push to talk switch is stuck in the enable or pr
53. e Comments MANIFEST GDC1 software mismatch communication halted The GDC 74A has incorrect software installed The G950 system should be serviced 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 67 sainjea4 2 Duruue d AEN Sd5 24JV olpny uqax sia sjuauimasu 2 nubi Tuo2 NeN Yid jeuonippy uoneiedo Jeuuouqy d E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix z Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES Message FPL WPT LOCK Flight plan waypoint is locked Comments Upon power up the G950 system detects that a stored flight plan waypoint is locked This occurs when an aviation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved The system has detected that a waypoint coordinate has changed due to a new aviation database update Verify that stored flight plans contain correct waypoint locations TIMER
54. e FMS Knob to highlight the flight plan to be copied 5 Press the COPY Softkey A Copy to flight plan confirmation window is displayed 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be deleted 32 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN Flight Planning 5 Press the DELETE Softkey A Delete flight plan confirmation window is displayed 6 With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key on the MFD to display the Active Flight Plan Page 2 Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan 3 The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired inser
55. e MFD amp PFDs with preferred settings if desired XTALK ERROR A flight display crosstalk error has occurred The MFD and PFDs are not communicating with each other The G950 system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair MANIFEST PFD1 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD self test has detected a problem The G950 system should be serviced The PFD and or MFD has incorrect software installed The G950 system should be serviced PFD1 CONFIG PFD1 config error Config service req d The PFD configuration settings do not match backup configuration memory The G950 system should be serviced MFD1 CONFIG MFD1 config error Config service req d The MFD configuration settings do not match backup configuration memory The G950 system should be serviced SW MISMATCH GDU software version mismatch Xtalk is off The MFD and PFDs have different software versions installed The G950 system should be serviced PFD1 COOLING PFD1 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the G950 system should be
56. e of Contents ANNUNCIATIONS amp WARNING Annunciation sss CAUTION Annunciation sss Safe Operating Annunciation Alert Message crore a saa ei aiam tie e RR TAWS B Aleits ee ena ben deba Lade ooi lo adia beste TAWS B System Status ANnUnciations wwww s s s s s s s si s s 58 Voice Alerts eee i R ASL dagen 58 MFD amp PFD Message Advisories ss s ss s s ss s s sss s ssis 59 Database Message AdVISOFIGS ea 60 GMA 347 Message Advisories s s s s s s s s s sss ss s s sss 62 GIA 63W Message AdVISOFI6S aterrar rnrn ar ret 63 GEA 71 Message AdVISOFI6S ia 65 GTX 33 Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories GWX 68 Alert Messages nennen GDC 74A Message Advisories Miscellaneous Message AdVISOrI6S aa 68 Flight Plan Import Export Messages 71 APPENDIX eT ada 73 PFD Softkey Map iia 73 MED Softkey Map s s nnne 77 s fe P e t Index 1 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 a Table of Contents GARMI N Blank Page Garmin G950 Cockpit Reference Guide for the Pilat
57. ed Press the CLR Key to clear the message text If the CLR Key is pressed again the message is restored Press the ENT Key while the message line is cleared to clear the message time Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN X U Abnormal Operation ABNORMAL OPERATION REVERSIONARY MODE Should a system detected failure occur in either display the G950 automatically enters reversionary mode In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display Reversionary display mode can be manually activated by pressing the display backup button installed in the cockpit NOTE The Pilot s Operating Handbook POH and or Airplane Flight Manual AFM always takes precedence over the information found in this section ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected In the event of a failure of both PFDs the emergency frequency 121 500 MHz automatically becomes the active frequency on both COM radios HAZARD DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established Loss of Hazard Functions with Loss of G
58. eference Guide for the Pilatus PC 6 saunqea4 2 AEN 5649 S24V olpny uqax si syu unysu paezey nubi nubi jeuonippy uoneiedo Jeuuouqy EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN FLIGHT PLAN IMPORT EXPORT MESSAGES CONT Flight Plan Import Export Results User waypoint database full Not all loaded Description The flight plan file on the SD card contains user waypoints The quantity of stored user waypoints has exceeded system capacity therefore not all the user waypoints on the SD card have been imported Any flight plan user waypoints that were not imported are locked in the flight plan The flight plan must be edited within the system before it can be activated for use One or more user waypoints renamed One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system Flight plan successfully exported The stored flight plan was successfully exported to the SD card Flight plan export failed The stored flight plan was not successfully exported to the SD card The SD card may not have sufficient available memory or the card may have been removed prematurely
59. engine oil pressure in pounds per square inch PRES PSI psi Oil Temperature Displays engine oil temperature in C TEMP C 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Sjueuinijsu sub MU xipueddy Suelv uoneiado saunyea4 aoueplony 2 AEN 540 2 olpny uqax unuuy jeuuouqy jeuonippy paezey BITE U105 AEN x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS AFCS Procedures GPS Nav Appendix Alerts Operation Features Index Engine Indication System G Ammeter GEN A ALT A Voltmeter BUS 1 V BUS 2 V FUEL DISPLAY o o 5 9 8 Displays DC bus voltages PRES PSI TEMP C FPUEL FFLOW GPH PRES PSI QTYLGAL 48 QTYRGAL 48 FUEL CALC GAL REM 167 GAL USED 3 ENDUR 4 16 RANGE NH 684 Fuel Display Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 A GARMIN Displays DC current in amperes amps for the generator and the alternator ALT A is not used 190 00851 00 Rev B GARMIN Engine Indication System Fuel Flow Displays current fuel flow in gallons per hour gph FFLOW GPH Fuel Pressure Displays current fuel pressure in psi PRES PSI 0 Fuel Quantity Left Displays quantity of fuel in gallons in the left L tank QTY L GAL Fuel Quantity Right Displays quantities o
60. erative There is no communication with the 1 transponder GRS 77 MESSAGE ADVISORIES Message Comments AHRS1 TAS AHRS1 not receiving valid airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G950 system should be serviced AHRS1 GPS AHRS1 using backup GPS source AHRS1 GPS AHRS1 not receiving any GPS information The 1 AHRS is using the backup GPS path Primary GPS path has failed The G950 system should be serviced when possible The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G950 system should be serviced AHRS1 GPS AHRS1 not receiving backup GPS information AHRS1 GPS AHRS1 operating exdusively in no GPS mode The 1 AHRS is not receiving backup GPS nformation The G950 system should be serviced The 1 AHRS is operating exclusively in no GPS mode The G950 system should be serviced AHRS1 SRVC AHRS1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid MANIFEST GRS1 software mismatch communication halted The 1 AHRS has incorrect softw
61. essed position Press the PTT switch again to cycle its operation If the problem persists the G950 system should be serviced COM1 RMT COM1 remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck The COM1 and or COM2 transfer switch is stuck in the enabled or pressed position Press the transfer Switch again to cycle its operation If the problem persists the G950 system should be serviced LOI GPS integrity lost Crosscheck with other NAVS GPS integrity is of flight insufficient for the current phase GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by WAAS is unavailable use LNAV only minimums 64 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT Message TRUE APR True north approach Change HDG reference to TRUE Comments Di
62. f fuel in gallons in the right R QTY R GAL tank G Set Fuel Remaining Displays current fuel remaining in gallons as set by the GAL REM pilot and adjusted for fuel burn since last set 5 Calculated Fuel Displays quantity of fuel used in gallons based on fuel Used flow since last reset GAL USED Calculated Displays flight time remaining in hours minutes Endurance HH MM based on the calculated fuel remaining ENDUR Calculated Range Displays aircraft range in nautical miles nm based on RANGE NM the calculated fuel remaining the aircrafts heading and the wind direction and speed 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 sjuaumasu iui Suelv uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld AEN Sd5 2 olpny uqax unuuy jeuuouqy jeuonippy paezey Wija U105 AEN xipueddy x pul GARMIN Engine Indication System Sjuauinjjsu fila oipny uadx U105 AEN Buluuejd Yi Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy x pul 190 00851 00 Rev B Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 10 A GARMIN Nav Com XPDR Audio Panel NAV COM TRANSPONDER AUDIO PANEL ADF TUNING OPTIONAL Tune the ADF using the remote ADF control head DME TUNING OPTIONAL 1 2 3 4 Press the DME Softkey Turn the large FMS to select the DME source field Turn the small FMS Knob to
63. g the selected vertical deviation to go invalid NO WGS84 WPT waypoint for navigation xxxx Non WGS 84 The position of the selected waypoint boox is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed Do not use GPS to navigate to the selected non WGS84 waypoint failed TRAFFIC FAIL Traffic device has The G950 is no longer receiving data from the traffic system The traffic device should be serviced variance Verify all FAILED PATH A data path has A data path connected to the GDU or the GIA failed 63 W has failed MAG VAR WARN Large magnetic 1 The GDU s internal model cannot determine the course angles exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2 SCHEDULER lt message gt Message criteria entered by the user 70 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN Annunciations amp Alerts FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Results Flight plan successfully imported Description A flight plan file stored on the SD card was successfully imported as a stored flight plan File contained user waypoints only U
64. he RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 1 2 3 Press the FPL Key Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint after the desired airway entry point If this waypoint is not a valid airway entry point a valid entry point should be entered at this time 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 29 oipny uddx s q sjuauimasu U105 AEN 1614 52 2 Buluuejd AEN Sd5 nubi uoneiado saunyea4 Junuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning 4 5 6 7 A GARMIN Turn the small FMS Knob one click dockwise and press the LD AIRWY Softkey or press the MENU Key and select Load Airway The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways
65. he desired waypoint within the arrival Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 1 2 36 NOTE If certain GPS parameters WAAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN LLL Precedures Press the ENT Key A list of available approaches for the destination airport is displayed 4 Turn either FMS Knob to highlight the desired approach 5 Press the ENT Key A list of available transitions for the selected approach procedure is now displayed 6 Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO UJ sjueumasu olpny uqax 59 U105 AeN 52 AEN 540 9 Pres
66. ht the desired flight plan Press the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 1 2 3 4 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint Press the ACT LEG Softkey on the MFD OR Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN GPS Navigation STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This does not delete the stored flight plan only the active flight plan VERTICAL NAVIGATION VNAV The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may
67. ical 20 guidance Altitude has been retrieved from the navigation database and is provided as a reference Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published altitude in the navigation database Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 flight path guidance 190 00851 00 Rev B GARMI N 8 Hil htPlanning FLIGHT PLANNING TRIP PLANNING 1 Turn the large FMS Knob to select the AUX page group 2 If necessary turn the small FMS Knob to select the Trip Planning Page 3 The current page mode is displayed at the top of the page AUTOMATIC or MANUAL To change the PAGE MODE press the AUTO or MANUAL Softkey 4 For Direct to planning a Press the WPTS Softkey and verify that the starting waypoint field indicates P POS present position b If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field d Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint Or For point to point planning a Enter the identifier of the starting waypoint b Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending waypoint d Press the EN
68. ion database version mismatch Xtalk is off The PFDs and MFD have different aviation database versions installed Crossfill is off Install correct aviation database version in all displays 190 00851 00 Rev B Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 so1njeoJ 2 AEN 5649 S24V oipny uadx sia siu umn sul paezey ETSI nubi jeuonippy uoneiedo Jeuuouqy IBN EE x pul Flight Instruments Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Aviation database type mismatch Xtalk is off Comments The PFDs and MFD have different aviation database types installed Americas European etc Crossfill is off Install correct aviation database type in all displays DB MISMATCH Terrain database version mismatch The PFDs and MFD have different terrain database versions installed Install correct terrain database version in all displays DB MISMATCH Terrain database type mismatch The PFDs and MFD have different terrain database types installed Install correct terrain database type in all displays DB MISMATCH Obstacle database version mismatch The PFDs and MFD have different obstacle database versions
69. ircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix AIRBORNE COLOR WEATHER RADAR OPTIONAL WARNING Begin transmitting only when it is safe to do so If it is desired to transmit while the aircraft is on the ground no personnel or objects should be within 11 feet of the antenna CAUTION In Standby Mode the antenna is parked at the center line It is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly 45 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 xipueddy Suelv uoneiedo sainjea4 aueploAY SoJnpa204d Duruue d AEN Sd5 52 olpny uqax 513 sjuauimasu Tunuuy Jeuuouqy jeuonippy 2 Yi U10 AEN fid x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Displaying Weather on the Weather Radar Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Radar Page 3 Press the MODE Softkey 4 If the aircraft is on the ground press the STANDBY Softkey to initiate the one minute warm up period After the warm up is complete the radar enters Standby Mode After the aircraft is
70. isplay to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DTK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD Current Track Indicator All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values The accuracy of all nearest information airports airspaces and waypoints is questionable Also airspace alerts continue to function but with degraded accuracy Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN ANNUNCIATIONS amp ALERTS Annunciations amp Alerts WARNING ANNUNCIATION Annunciation Text Alerts Window Message Audio Alert Low voltage on the battery bus Low voltage on the generator bus Repeating Tone Prop low pitch condition exists Aircraft stall condition exists Stall repeating Trim not in take off configuration Trim repeating CAUTION ANNUNCIATION Annunciation Text Alerts Window Message Audio Alert Battery temp outside normal op limits Battery temp monitor maintenance ectrical load reduction recommended uel filter is blocked E Engine oil contamination detected F L eft external fuel transfer pump inactive Right external fuel transfer pump inactive Left fuel tank is low is low Right fuel tan
71. kpit Reference Guide for the Pilatus PC 6 4 aoueploay s mp oold paezey suelv uoneiedo sainjea4 Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Sector Scan 1 2 3 4 5 6 While in the Horizontal Scan Mode move the Joystick right or left to place the Bearing Line in the desired position The location of the Bearing Line becomes the center point of the Sector Scan Press the FMS Knob to display the cursor Turn the large FMS Knob to place the cursor in the SECTOR SCAN field Turn the small FMS Knob to select FULL 60 40 or 20 scan If desired readjust the Bearing Line with the Joystick to change the center of the Sector Scan Press the FMS Knob to remove the cursor Antenna Stabilization 1 2 To activate or deactivate the antenna stabilization press the MODE Softkey Press the STAB ON Softkey to activate antenna stabilization or press the STAB OFF Softkey to deactivate The current stabilization condition is shown in the upper right of the weather radar display Weather Attenuated Color Highlight WATCH To activate or deactivate the WATCH feature press the WATCH Softkey This feature is only available in the Horizontal Scan Mode Weather Alert To
72. l cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN A Activate a flight plan 18 ADF 11 12 52 AHRS 66 67 Aircraft range 9 10 Airways 78 Alert messages 67 ALT 42 Altitude mode 42 Altitude volume 42 Ammeter 6 8 Antenna stabilization 48 Antenna tilt 46 Audio panel controls NAV1 NAV2 12 Barometric Altitude Minimums 3 Barometric pressure 75 Bearing line 46 47 48 Bus voltage 6 8 C CDI 1 12 69 Cell 39 40 Cell mode 40 Clearance player 12 Clearance Recorder 12 Code selection softkeys 11 COM 11 12 51 D Database Updates 78 DCLTR Softkey 49 Dead Reckoning 53 Declutter 52 73 78 Direct to 17 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 DME 11 12 DR mode 53 54 E Edit a flight plan 31 Electrical indications 6 Endurance 9 F Flaps 6 Index Flight plan import export messages 71 72 Frequency Transfer 12 Fuel Flow 6 9 Quantity 6 9 Remaining 9 Used 9 G Gain 47 Generator speed 6 H HF 11 Horizontal scan 47 Inhibit 45 Inhibit TAWS 45 Inset Map 73 74 Intercom isolation 13 Interstage Turbine Temperature ITT 6 IOI 57 ITT 6 L Lightning 39 40 74 Index 1 uoneiedo
73. lation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground This database is updated on a 56 day cycle SCHEDULER Scheduler messages appear in the Alerts Window on the PFD When a scheduler message is waiting the ALERTS Softkey label changes to ADVISORY Pressing the ADVISORY Softkey opens the Alerts Window and acknowledges the scheduler message The softkey label reverts to ALERTS when pressed the Alerts Window is removed from the display and the scheduler message is deleted from the message queue Message timers set to periodic alerting automatically reset to the original timer value once the message is displayed When power is cycled all messages are retained until deleted and message timer countdown is resumed Enter a Scheduler Message 1 Select the AUX Utility Page 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Tum the large FMS Knob to highlight the first empty scheduler message naming field 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 49 sainpa20dd Buluuejd AEN Sd5 523 oipny uadx sia Sjueumajsul u102 AEN aoueplony paezey s m e q jeuonippy uoneiedo Jeuuouqy Sue v unuuy xipueddy x pul iui Wfil4 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EI
74. min G950 Cockpit Reference Guide for the Pilatus PC 6 sjuauimasu nubi 59 oipny uddx UI0JNeN ACN 540 52 suelv uoneiedo sainjea4 aoueplony 2 Duruue d unuuy Jeuuouqy Jeuonippy paezey bi xipueddy x pul Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EIS GPS Nav AFCS Appendix Alerts Operation Features Avoidance Procedures Index GPS Navigation 1 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET distance field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or tum the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key on the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlig
75. n 101 or Ahead CAUTION OBSTACLE C l Caution Obstacle Caution Obstacle Premature Descent TOOLOW TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Five Hundred 500 Excessive Descent TERRAIN S NK RATE Sink Rate Rate Caution EDR Negative Cimb TERRAIN Evans Don t Sink Rate Caution NCR or or aeee Tern Default setting for the PC 6 when more than one option is available 190 00851 00 Rev B 57 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 saunqea4 aoueplony SoJnpa204d Duruue d AEN 540 2 oipny uadx 513 sjueumasu puezey ubi U10 AEN ubiu jeuonippy uoneiedo Jeuuouqy EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN TAWS B SYSTEM STATUS ANNUNCIATIONS FED MED TAWS B Page Aural Alert Type Alert cae ET Annunciation Message Annunciation wee wes TANSTEST N TAWS System System Test Pass None None Test OK TAWS Alerting is disabled TAWS INH None None MFD Terrain or Obstacle database unavailable or invalid None None TAWS operating with PFD Terrain or Obstacle databases TAWS B System Test Fail ITAWS FAIL 7
76. nformation on Inset Map Press to display the Stormscope lightning data on the Inset Map within a 200 nm radius of the aircraft optional Ez CS owe pa Deer peser Bn nN 75 75 77 74 gt J pers wind owe ene sreRwr BRc atun sTo sarol Back ALERTS mo 1 BAGH NAVI BAGH GPS BRG2 OFF Press the BACK Softkey to return to the top level softkeys METERS JE LA ALERTS nmpysmumnnnstu L TL erm omes L om L L L L Eee Acenrs F3 V3 A V3 F3 P8 056 n9 nn 75 onm PFD Configuration Softkeys PFD DFLTS WIND OPTN 1 OPTN 2 74 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Displays second level softkeys for additional PFD configurations Resets PFD to default settings including changing units to standard Displays softkeys to select wind data parameters Longitudinal and lateral components Total direction and speed 190 00851 00 Rev B A GARMIN 640 Appendix OPTN 3 Total direction with head and crosswind speed components OFF Information not displayed DME Displays the DME Information Window BRGI Cycles the Bearing 1 Information Window through NAV1 or GPS vvaypoint identifter and GPS derived distance information HSI FRMT Displays the HSI formatting softkeys 360 HSI Displays the HSI in a 360 deg
77. ngs do not match backup configuration memory The GIA1 CONFIG GIA1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d serviced The GIA1 and or GIA2 have an error in the audio configuration The G950 system should be too low GIA1 COOLING GIA1 temperatu too low GIA2 COOLING GIA2 temperatu operating temperature The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to emperature GIA1 COOLING GIA1 over emperature GIA2 COOLING GIA2 over serviced The GIA1 and or GIA2 temperature is too high If problem persists the G950 system should be n GIA1 SERVICE GIA1 needs ervice Return the unit for repai n GIA2 SERVICE GIA2 needs ervice Return the unit for repai serviced T The GIA1 and or GIA2 self test has detected a problem in the unit The G950 system should be halted halted HW MISMATCH GIA hardware mismatch GIA1 communication A GIA mismatch has been detected where only HW MISMATCH GIA hardware 1 one is WAAS capable mismatch GIA2 communication MANIFEST GIA1 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software MANIFEST GIA2 software installed The G950 system should be serviced mismatch communication halte
78. o Navigation from the MFD 1 Press the Direct to E Key 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 6 Enter the desired altitude 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Tum the small FMS Knob to select MSL or AGE 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field 10 Enter the desired offset distance before the waypoint 11 Press the ENT Key The Activate field is highlighted 12 Press the ENT Key to activate Direct to Navigation from the PFD 1 Press the Direct to Key 8 2 Tum the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the ALT altitude field 190 00851 00 Rev B Gar
79. o select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 4 Enterthe desired waypoint name 5 Press the ENT Key 6 The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one dlick to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 23 sia sjuounasu U105 AEN 3461 olpny uqax 52 eouepioAy paezey spay uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 24 A GARMIN 7 With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD RAD radial radial Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to en
80. oint for parallel offset has been passed 190 00851 00 Rev B 69 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 saunqee4 sanpa20Jq Buruuejd AEN 5640 24V oipny uadx sia siu umn sul paezey nb u102 AEN nubi jeuonippy uoneiedo Jeuuouqy 3 PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix end Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT UNABLE V WPT vertical waypoint Message Can t reach current Comments The current vertical waypoint can not be reached within the maximum flight path angle and vertical Speed constraints The system automatically transitions to the next vertical waypoint VNV Unavailable type in flight plan Unsupported leg The lateral flight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track The current track angle error exceeds the limit angle error causing the vertical deviation to go invalid VNV Unavailable Excessive The current crosstrack exceeds the limit causing crosstrack error vertical deviation to go invalid VNV Unavailable Parallel course 1 A parallel course has been selected causin
81. ongitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand A WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed A CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings A CAUTION The Garmin G950 does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations A NOTE All visual depictions contained within this document including screen images of the G950 panel and displays are subject to change and may not reflect the most current G950 system and aviation databases Depic
82. os and music PILOT KEY COPLT KEY Pilot Hears Passenger Hears Annunciator Annunciator Selected radios aural alerts pilot copilot passengers music Selected radios aural alerts pilot radios aural alerts pilot passengers music Selected radios aural alerts pilot copilot Selected ON radios aural alerts pilot copilot passengers music Copilot passengers music Copilot Selected radios aural alerts pilot copilot ICS Isolation Modes Nav Com XPDR Audio Panel Selected radios aural alerts pilot copilot passengers music Copilot passengers music Selected radios aural alerts pilot passengers music Passengers music 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Sjueumansu 59 S24V oipny uddx JUI05 AEN sual uone1edo saunjeaj s mp oold Buruue d AEN Sd5 junuuy jeuuouqy feuonippv xipueddy x pul iui bi paezey GARMIN Nav Com XPDR Audio Panel Sjueuinijsu fila 59 oipny uadx U10 AeEN S2dV AeN Sd5 Buluuejd Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00851 00 Rev B Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 14 A GARMIN 0 AFCS AUTOMATIC FLIGHT CONTROL SYSTEM NOTE Refer to the Aircraft Flight Manual AF
83. ost or not available the DR function may not be capable of estimating your position and consequently the system may display a path that is different than the actual movement ofthe aircraft Estimated position information displayed by the G950 through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lack of satellite measurements needed to determine a position Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 3 sepeooid ujuuejd AEN 540 52 oipny uadx si syuaumasu U105 AeN paezey saunyea4 Jeuolppy Sue v unuuy xipueddy x pul iui bi Nav Com XPDR Audio Hazard Avoidance Additional Flight Instruments Flight Planning EIS AFCS Procedures GPS Nav Features Annun Appendix Alerts Index Abnormal Operation 54 A GARMIN CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the d
84. r clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints 4 Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key The active flight plan is modified as each waypoint is entered 5 Repeat step numbers 3 and 4 to enter each additional flight plan waypoint 6 When all waypoints have been entered press the FMS Knob to remove the cursor Creating a stored flight plan 1 Press the FPL Key 2 Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page 3 Select the NEW Softkey or press the MENU Key highlight Create New Flight Plan and press the ENT Key to display a blank flight plan for the first empty storage location 4 Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 27 sjuauimasu sub oipny uadx si U105 AeN 52 2 Buluuejd AEN Sd5 nubi uoneiado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS
85. ree format ARC HSI Displays the HSI in an arc format BRG2 Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information ALT UNIT Displays softkeys for setting the altimeter and BARO settings to metric units METERS When enabled displays altimeter in meters IN Press to display the BARO setting as inches of mercury HPA Press to display the BARO setting as hectopacals STD BARO Sets barometric pressure to 29 92 in Hg 1013 hPa 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 75 sjuauimasu nubi 59 soJnjeoJ seinpa2o0Jd Buruuejd AEN 5649 S24V oipny uadx Jeuonippy paezey ni uo2 AEN uoneiedo Jeuuouqy Sue v unuuy End Flight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index Appendix pner XPDR 76 n A GARMIN optional Press the BACK Softkey to return to the top level softkeys 3E 3E IE EAE 7 Tom Tser TE Yaram STBY ON ALT GND VFR CODE Press the BACK Softkey to return to the previous level softkeys Transponder Softkeys 0 7 BKSP Displays transponder mode selection softkeys Selects Standby Mode transponder does not reply to any interrogations Selects Mode A transponder replies to interrogations Selects Mode C
86. s the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach buluueld s mp old procedure 10 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 11 Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and activates the first leg of the approach 12 Press the ENT Key eouepioAy soJnjeoJ jeuonippy ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN uoneiedo Jeuuouqy 1 Press the PROC Key 34 bi paezey 2 Tum the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 37 xipueddy suelv junuuy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index A Procedures GARMIN ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL Press the ENT Key The final approach course becomes the active leg ACTIVATE A MISSED APPROACH IN THE A
87. s written permission of Garmin Garmin hereby grants permission to oad a single copy of this manual and of any revision to this manual onto a hard drive or electronic storage medium to be viewed for personal use provided that such electronic nted copy of this manual or revision must contain the complete text of this copyright hat any unauthorized commercial distribution of this manual or any ot G950 is a trademark of Garmin Ltd or its subsidiaries Garmin WATCH and SafeTaxi are registered trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used witho ut the express permission of Garmin NavData is a registered trademark of Jeppesen Inc June 2010 190 00851 00 Rev B Printed in the U S A A Warnings Cantans amp Notes GARMIN e e WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain function The G950 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNIN
88. ser waypoints imported successfully No stored flight plan data was modified The file stored on the SD card did not contain a flight plan only user waypoints These waypoints have been saved to the system user waypoints No flight plans stored in the system have been modified No flight plan files found to import The SD card contains no flight plan data Flight plan import failed Flight plan data was not successfully imported from the SD card Flight plan partially imported Some flight plan waypoints were successfully imported from the SD card however others had errors and were not imported A partial stored flight plan now exists in the system File contained user waypoints only The file stored on the SD card did not contain a flight plan only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan truncated Th Th e flight plan on the SD card contains more waypoints than the system can support e flight plan was imported with as many waypoints as possible Some waypoints not loaded Waypoints locked Th e flight plan on the SD card contains one more waypoints that the system cannot in the navigation database The flight has been imported but must be edited thin the system before it can be activated use 190 00851 00 Rev B Garmin G950 Cockpit R
89. serviced 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 9 saunqea4 aDueplony seinpe2oJd Buruuejd AEN 5640 24V olpny uqax sia syu unysu paezey Wfila nubi jeuonippy uoneiedo Jeuuouqy 0 EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix sd Annunciations amp Alerts A GARMIN MFD amp PFD MESSAGE ADVISORIES CONT Message Comments PFD1 KEYSTK PFD1 key name Key is stuck Key is stuck MFD1 KEYSTK MFD key name A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The G950 system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The G950 system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The G950 system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The G950 system should be serviced DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 aviation database error exists PFD1 DB ERR PFD1 aviation database error exists The MFD and or PFD detected a failure in the aviation database
90. splayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs af service Return unit for repair GPS2 SERVICE GPS2 needs service Return uni A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G950 system should be serviced NAV1 SERVICE NAV1 needs Service Return unit for repair NAV2 SERVICE NAV2 needs if Service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G950 system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cycle its operation If the problem persists the 6950 system should be serviced 6 51 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G950 system should be serviced Return unit for repair G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The
91. stacle is more than 1000 Black below aircraft altitude Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed press the MAP Softkey 2 Press the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 43 AEN 540 S24V olpnyyuqax sia siu umnnsul Tuo2 AEN iui Duruue d nubi s mp oold paezey Suelv uoneiedo s m Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN TERRAIN AWARENESS amp WARNING SYSTEM TAWS B DISPLAY OPTIONAL 44 NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Manual System Test 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Display Terrain on the TAWS B Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS B Page 3 If desired press the VIEW Softkey to
92. t the TEST Softkey 4 Self test takes approximately eight seconds to complete When completed successfully traffic symbols are displayed and a voice alert is heard see Alerts and Annunciations section If the self test fails the system reverts to Standby Mode and a voice alert is heard Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN Hazard avoidance Displaying Traffic on the Navigation Map 1 Ensure TAS is operating 2 With the Navigation Map displayed select the MAP Softkey 3 Select the TRAFFIC Softkey Traffic is now displayed on the map TERRAIN AND OBSTACLE PROXIMITY NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Displaying Terrain and Obstacles on the Terrain Proximity Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the last rectangular page icon 3 If desired press the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Ob
93. ter the desired waypoint name Waypoints may also be selected as follows 8 9 10 11 a b o Or a b o d Or a b d Or a b o d When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN Flight Planning 12 Press the ENT Key 13 Repeat step 10 to enter the next waypoint name 14
94. the SYSTEM and FUEL PE softkeys HE SYSTEM Displays the engine leaning softkeys au BACK Press to return to the top level softkeys 1f FUEL Displays fuel system softkeys DEC FUEL Press to decrease fuel quantity in 1 gallon increments Sue unuuy INCFUEL Press to increase fuel quantity in 1 gallon increments RST FUEL Press to reset fuel to full BACK Press to return to the top level softkeys gt s 3 m x x pul 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 7 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix DCLTR 78 TRAFFIC TOPO TERRAIN AIRWAYS STRMSCP BACK A GARMIN Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map Displays terrain information on Navigation Map Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON AIl airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed Displays Stormscope weather and coverage information on Navigation Map optional feature Returns to top level softkeys Selects desired amount of map detai
95. tion Submenu 27 28 Weather Attenuated Color Highlight 48 Weather radar 45 Wind data 74 190 00851 00 Rev B A GARMIN 3armimAT Ine 2345 Turner Road Ellis Salem OR 97302 U S A p 503 391 3411 f 503 364 2 C ae NDA Garmin Europe Ltd F Liberty House Bulls Copse Road gt Hounsdown Business Park Southampton S040 9RB U K EET p 44 0870 8501241 f 2009 2010 Garmin Ltd or its subsidiaries 190 00851 00 Rev B
96. tion point 4 Press the LD WPT Softkey The selected waypoint is inserted at the selected point The default user waypoint naming is USR000 USR001 USR002 and so On 5 To change the user waypoint name follow the procedure for modifying a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD NOTE See the Annunciations amp Alerts section for flight plan export message descriptions 1 Insert the SD card into the top card slot on the MFD 2 Press the FPL Key to display the Active Flight Plan Page on the MFD 3 Turn the small FMS Knob to select the Flight Plan Catalog Page 4 Press the FMS Knob to activate the cursor 5 Turn the large FMS Knob to highlight the flight plan to be exported 6 Press the EXPORT Softkey 7 Press the ENT Key to confirm the export 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 33 oipny uddx 59 sjuauimnasu U10 AEN 346 3 52 2 Buluuejd AEN Sd5 nubi uonesado saunyea4 aoueplony Junuuy jeuuouqy jeuonippy paezey xipueddy x pul GARMIN Flight Planning Ssjueuinijsu fila 59 U105 AEN s24v AeN Sd5 Buluuejd 34 Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00851 00 Rev B Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 34 A GARMIN Pro
97. tions of equipment may differ slightly from the actual equipment A NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B amp GARMIN Notes NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The p
98. to the Utility Page for the actual flight departure time Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings The flashing cursor moves to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system The flashing cursor moves to the fuel flow field Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system The flashing cursor moves to the fuel onboard field Enter the fuel onboard Press the ENT Key when finished Note that in AUTOMATIC page mode fuel onboard is provided by the fuel totalizer The flashing cursor moves to the calibrated airspeed CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated airspeed is provided by the system The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press the ENT Key when finished Note that in AUTOMATIC page mode the baro setting is provided by the setting entered on the PFD The flashing cursor moves to the air temperat
99. ure TOTAL AIR TEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN flight Planning CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Turn the large FMS Knob on the MFD to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 4 Enterthe desired waypoint name 5 Press the ENT Key 6 The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field 7 With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types 8 Turn the small FMS Knob to select LAT LON latitude and longitude 9 Press the ENT Key 2 4 AEN 540 nubi CREATE A NEW USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 1 Turn the large FMS Knob on the MFD t
100. urpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G950 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G950 Pilot s Guide for this aircraft 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 A Warnings tantens 2 Hot GARMIN Blank Page Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMI N Record of Revisions Change Summary 190 00851 00 RevA Initial release eed Date of Revision Affected Pages June 2010 All Added WX 500 Stormscope Added TAWS B Added KTA 870 TAS Various clerical changes 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 RR 1 Record of Revisions GARMIN Blank Page RR 2 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B GARMIN LLL Table of Contents FLIGHT INSTRUMENTS 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg 1 Change Altimeter Barometric Pressure Setting Units 1 Change Navigation Sources w s s s s s ss s sss s sss s sssss n 1 Enable Disable OBS Mode While Navigating with GPS 2
101. us PC 6 190 00851 00 Rev B GARMIN flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG 1 Press the PFD Softkey 2 Press the STD BARO Softkey to set standard barometric pressure CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Press the PFD Softkey to display the second level softkeys 2 Press the ALT UNIT Softkey 3 Press the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Press the HPA Softkey to display the barometric pressure setting in hectopascals 4 Press the BACK Softkey to return to the top level softkeys CHANGE NAVIGATION SOURCES 1 Press the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD 2 Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue tuning box over the NAV2 standby frequency 3 Press the CDI Softkey a third time to return to GPS 190 00851 00 Rev B Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 xipueddy Suelv uoneiedo s m aoueplony SoJnpa20Jd Duruue d AEN Sd5 S24JV olpny uqax 913 unuuy Jeuuouqy Jeuonippy paezey bi U10 AEN x pul Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Planning
102. zardous weather penetration thunderstorm penetration Stormscope information as displayed on the G950 MFD is to be used only for weather avoidance not penetration Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 00 Rev B A GARMIN 7 ng Cautions 5 Notes V ARNING The Garmin G950 has a very high degree of functional integrity However the pilot must recognize that providing monitoring and or self test capability for all conceivable system failures is not practical Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the G950 It is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G950 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G950 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G950 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G

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