Home

Garmin Pilatus PC_6 Cockpit Reference Guide

1. 1 Enter a Transponder s s s s s sss s ssss s sss s sin isss s ssss 1 Enter or Change Flight ID s s s s s s s sss s ssss s ssis 1 Selecting a COM Radio seen 2 Selecting a NAV Radio 2 NAV COM Tuning nnne 2 Digital Clearance Recorder and 2 Intercom System ICS Isolation 3 AUTOMATIC FLIGHT CONTROL SYSTEM 5 S TEC Fifty Five X 5 5 GPS NAVIGAHON el 7 Direct to Navigation ssssssssseseenee nnne 7 Activate a Stored Flight Plan 8 Activate a Flight Plan Leg 8 Stop Navigating a Flight 755 9 Vertical Navigation VNAV sssssee nnne 9 21 Trip Planning re ayda i ca a a rue E e YR 21 Create a User Waypoint Defined by Latitude amp Longitude 23 Create a User Waypoint Defined by Radials from Other Waypoints 23 Create a User Waypoint Defined by a Radial amp Distance from Another Way
2. HDG FAULT AHRS2 magnetometer fault has occurred A fault has occurred in the 2 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced MANIFEST GMU1 software mismatch communication halted MANIFEST GMU2 software mismatch communication halted The GMU 44 has incorrect software installed The system should be serviced GWX 68 ALERT MESSAGES Message Comments GWX CONFIG GWX config error Config service req d GWX 68 configuration settings do not match those of the GDU configuration The system should be serviced GWX FAIL GWX is inoperative GWX SERVICE GWX needs service Return unit for repair 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 A failure has been detected in the GWX 68 The GWX 68 may still be usable MANIFEST GWX software mismatch communication halted The GWX 68 has incorrect software installed The system should be serviced WX ALERT Possible severe weather ahead Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm 190 00851 02 Rev A 85 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 saunqea4 2 AEN Sd 24V olpny uqax s q siu u
3. eft external fuel transfer pump inactive Right external fuel transfer pump inactive Left fuel tank is low Right fuel tan Fuel pressure is low Generator has failed is low 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 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 69 SaJnjeoJ 2 buluueld AEN Sd5 241V oipny uadx 93 siu umn sul 2 ni uio AeN ui jeuonippy uoneiedo jJeuuouqv iic Dou x pul Annunciations amp Alerts A GARMIN Annunciation Text Alerts Window Message Audio Alert 52 ER Landing light is on Left external fuel transfer pump is active z Right external fuel transfer pump is active T m one Prop deice is on Tow cable attached 55 ALERT MESSAGE 9 Alerts Window Message Audio Alert PFD FAN FAIL The cooling fan for the PFD is inoperative None amp MFD FAN FAIL The cooling fan for the MFD is inoperative None 5 TERRAIN SVS ALERTS BE PFD MFD s Tert Tune Terrain SVS MFD Aural
4. 93 PED Softkey Map ctt ttti etti tet ente eb 93 MED Softkey Map nennen nnne 98 Loading Updated Databases 100 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Table of Contents GARMI N Blank Page Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A 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 02 Rev A Garmin G950 Co
5. 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 ofall 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 G950 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
6. 4 Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 21 sjuauimasu nubi olpny uqax si UI0JNeN 52 SoJnpa20Jd buluueld AEN Sd5 nubi aoueplony paezey suelv uoneiedo s n e 4 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 5 6 7 A GARMIN turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints 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 7 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 o
7. Arriving at waypoint xxxx where xxxx is the waypoint name FPL TRUNC Flight plan has been truncated This occurs when a newly installed navigation 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 LOCKED FPL Cannot navigate locked flight plan 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 MAG VAR WARN Large magnetic variance Verify all course angles The GDU internal model cannot determine the 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 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 190 00851 02 Rev A 87 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 so1njeoJ 2 Buruuejg AEN Sd 24V oipny uddx sia syu unysu paezey nubi Wil jeuonippy uoneiedo
8. Selected Altitude VNV Target Altitude Extreme Pitch Indication Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN Abnormal 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 DR Modeis indicated 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 SBAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation
9. 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 4 Turn the large FMS Knob to highlight the desired arrival 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 37 oipny uddx 59 sjuauimasu U105 AEN 16114 52 AEN 540 Duruue d ni s mp old aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures 000000 GARMIN 5 6 7 8 9 10 11 12 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
10. COM2 SERVICE COM2 needs service Return unit for repair The system has detected a fault in COM1 and or COM2 COM1 and or COM2 may still be usable The system should be serviced when possible COMI PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the system should be serviced COM1 RMT XFR 1 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 system should be serviced 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 soJnjeoJ 2 AEN Sd 24V olpny uqax sia syu unysu paezey nubi wi0 gt AeN Wil jeuonippy uoneiedo Jeuuouqy R 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 Comments LOI GPS integrity lost Crosscheck with other NAVS
11. Jeppesen 57 L Lightning 43 44 M Magnetic Field Variation Database Update 104 Message advisories 75 79 81 89 Minimums 74 MKR MUTE 12 Mode 97 Mode selection softkeys 11 Multi Function Display MFD Softkeys 98 N NAV 12 NAV1 1 12 NAV2 1 12 Navigation database 20 90 Index 2 A GARMIN 0 OBS 2 Obstacles 78 79 80 Oil Pressure 6 7 Temperature 6 7 P Pathways 55 Povver up page 62 Pressure oil 6 7 Propeller speed 6 R Range aircraft 9 10 Reversionary mode 65 ROC 70 72 73 S Safelaxi amp 56 SBAS 38 49 50 67 80 82 Sector scan 53 Secure Digital SD card 62 STAB 53 Standby 51 Standby Navigation Database 103 104 Store Flight Plan 33 Stormscope lightning data 43 44 Strike 43 Strike mode 44 SVT 55 89 Synchronization 100 Synthetic Vision Technology 55 T TA 74 TAS 46 84 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN TAWS 49 50 72 Temperature Interstage Turbine 6 Temperature oil 6 7 Terrain 47 48 49 78 94 99 Terrain SVT 15 48 49 Tilt line 51 Timer 86 Topographical data 94 99 Torque 6 Traffic 43 45 98 Traffic advisory 45 Traffic Advisory 74 Traffic map page 45 46 47 Transponder 11 96 97 Trim 6 V Vertical speed guidance 20 Vertical track 74 Video 59 VNV 17 66 88 Voltmeter 6 8 Vspeed 2 W WATCH 53 Waypoint Selection Submenu 27 28 Weather Attenuate
12. airports to the aircraft s current position c 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 c 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 c Turn the large FMS Knob to select 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 Tum the large FMS Knob to select the WPT page group 2 Tum 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 02 Rev A GARMIN FlightPlamning 4 Turn the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the
13. 9 Page Pop Up Alert Message Annunciation Reduced Required Terrain TERRAIN Warning Terrain Clearance Warning RTC Terrain 2 8 Imminent Terrain Impact TERRAIN Waring Terrain Warning ITI Terrain 5 Reduced Required Obstacle TERRAIN Warning Obstacle i Clearance Warning ROC Obstacle Imminent Obstade Impact TERRAIN Warning Obstade ES Warning 10 Obstacle 5 5 Reduced Required Terrain TERRAIN CAUTION TERRAIN Caution Terrain Clearance Caution RTC Terrain Imminent Terrain Impact TERRAIN 1 CAUTION TERRAIN Caution Terrain Caution ITI Terrain Reduced Required Obstacle TERRAIN cautton OBSTACLE Caution Obstacle a Clearance Caution ROC Obstacle Imminent Obstade Impact TERRAIN CAUTTON OBSTACLE Caution Obstacle Caution 101 Obstacle 70 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN Amnunciations amp Alerts Terrain SVS System Status Annunciations SjueuinJjsu sub PFD MFD Alert Terrain SVS Page Aural Alert Type d e Annunciation Annunciation Message System Test in Progress TER TEST one Terrain System System Test Pass None None Test OK 3 z Terrain System 3 Terrain System Test Fail TER FAIL 7 s Failure Terrain or Obstacle gt database unavailable or sg ate
14. Available VOICE ALERTS Voice Alert Description Minimums minimums 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 Traffic Traffic Played when a Traffic Advisory TA is issued TAS system TAS System Test OK 1 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 74 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Annunciations amp Alerts 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 the MFD amp PFD with preferred settings if desired XTALK ERROR A flight display crosstalk error has occurred The MFD and PFD are not communicating with each other The system should be serviced PFD1 SERVICE PFD1 needs ervice Return unit for repair un MFD1 SERVICE MFD1 needs ervice Return unit for repair MANIFEST PFD1
15. 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 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 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 Depictions of equipment may differ slightly from the actual equipment 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 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 Califo
16. Cockpit Reference Guide for the Pilatus PC 6 49 AeN Sd5 S24V oipny uadx si sjueumasuj u102 AEN Yubil buluueld Ubila aoueploay s mp oold paezey saunqea4 jeuonippy sue v uoneiedo junuuy Jeuuouqy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 46 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 Tum the large FMS Knob to select the Map Page Group 2 Tum 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
17. Day Auto and Night Options In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity Press the FMS Knob when finished to remove the Chart Setup Menu AIRPORT DIRECTORY The Aircraft Owners and Pilots Association AOPA and optional AC U KWIK Airport Directory add enhanced airport information when viewing airports on the WPT Airport Information Page Both Airport Directories are available for downloading at flygarmin com However copy only one of the databases to the Supplemental Data Card The system cannot recognize both databases simultaneously View Airport Directory Information 58 While viewing the VVPT Airport Information Page if necessary press the INFO 1 Softkey to change the softkey label to display INFO 2 AOPA airport information is displayed on the right half of the display Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Additional Features AUXILIARY VIDEO OPTIONAL NOTE lmages provided on the Aux Video page are for supplemental use only There are four modes of operation of the optional auxiliary video display Full Screen Full Screen with Digital Zoom Split Screen with Map and Split Screen with Map and Digital Zoom Displaying auxiliary video 1 Tum the large FMS Knob to select the AUX page grou
18. Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features GARMIN 5 If desired return the display to the default settings by pressing the RESET Softkey 6 Press the BACK Softkey to return to the previous softkey level Display Selection Pressing the HIDE MAP Soltkey removes the map and displays video on the full screen The softkey label changes to grey with black characters Pressing the HIDE MAP Softkey again restores the map view and the small video image The softkey label returns to white characters on a black background Zoom Range Pressing the VID ZM or VID ZM Softkeys increases or decreases video display magnification between 1x and 10x The RANGE Knob can be used to increase or decrease the range setting on the map display or zoom in and out on the video display While in the Split Screen mode pressing the MAP ACTV or VID ACTV Softkey determines which display the RANGE Knob adjusts Pressing the softkey to display MAP ACTV allows the RANGE Knob to control the range setting of the map display Pressing the softkey to display VID ACTV allows the RANGE Knob to control the zoom setting of the video display SCHEDULER Scheduler messages appear in the Alerts Window on the PFD When a scheduler message is waiting the ALERTS Softkey label changes to ADVISOR
19. GPS integrity is insufficient for the current phase of flight GPS NAV LOST Loss of GPS navigation Insufficient satellites f 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 SBAS is unavailable use LNAV only minimums TRUE APR True north approach Change HDG reference to TRUE Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs nf service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A fault has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The system should be serviced NAV1 SERVICE NAV1 needs nf Service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair A fault has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The system should be serviced NAV1 RMT XFR NAV1 remote transfer key
20. Jeuuouqy ic x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix pd Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT A GARMIN Message Comments ARSPC NEAR Airspace near and ahead Special use airspace is near and ahead of the aircraft position ARSPC NEAR Airspace near less Special use airspace is withi n 2 nm of the aircraft frequency for approach than 2 nm position APR INACTV Approach is not active The system notifies the pilot the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate The system notifies the pilot to load the approach frequency for the approp iate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for approach PTK FAIL Parallel track unavailable bad geometry The system notifies the pi correct NAV receiver Set the CDI to the correct NAV receiver Bad parallel track geometry ot to set the CDI to the PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for pa allel offset PTK FAIL Parallel track unavailable past IAF IAF waypoint for parallel offset has been passed UNABLE V WPT Can t reach current vertical waypoint Th
21. Key highlight Hold At Wpt and press the ENT Key The HOLD AT window appears with the course field highlighted Use the FMS Knobs to edit the entry course and press the ENT Key Use the small FMS Knob to select INBOUND or OUTBOUND course direction and press the ENT Key Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key Use the FMS Knobs to edit the length and press the ENT Key Use the small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key Press the ENT Key while LOAD is highlighted to add the hold into the flight plan Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN ight Planning Creating a user defined hold at the aircraft present position 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the MENU Key highlight Hold At Present Position and press the ENT Key The HOLD AT window appears with the Length mode highlighted 3 Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key 4 Use the FMS Knobs to edit the length and press the ENT Key 5 Use the small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key 6 Use the FMS Knobs to edit the Expec
22. ROC o Obstacle Ahead Pull Up Obstade Ahead Pull Up Imminent Obstade PULL UP Obstacle Ahead Pull Up Impact Warning or Obstacle Ahead Pull Up 01 OBSTACLE PULP or Obstacle Obstacle Pull Up Pull Up Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance or Terrain GR 5 5 Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN ERRINAHERD Terrain Ahead Terrain Impact Caution ITI or Ahead Olin 1 d Caution Terrain Caution Terrain 72 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Annunciations 8 Alerts PFD MFD MFD Alert Type 1 TAWS B Page Aural Message o Pop Up Alert Annunciation Reduced Required TERRAIN CAUTION OBSTACLE Caution Obstacle Obstacle Clearance or Caution Obstacle Caution 400 B 25 a Obstacle Ahead Obstacle Ahead Imminent Obstacle TERRAIN OBSTACLE AHEAD 1 Obstacle Ahead Obstacle Impact Caution 101 or Ahead Caution Obstacle Caution Obstacle Premature Descent TERRAIN TO0LOW TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Five Hundred 500 Excessive Descent TERRAIN S K Sink Rate Rate Caution EDR Negative Cimb TERRAIN 7 BWTSiK Don t Rate Caution NCR or or iron ray Low Terai Defau
23. The cursor is placed in the OFFSET 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 turn 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 highlight 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 18 1 2 3 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 On the MFD press the ACT LEG Softkey 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 02 Rev A A
24. 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 lost 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 of the 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 SBAS 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 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 67 sepeooid uluueld AEN 540 rki oipny uadx si syuaumasul uo2 AEN paezey saunyea4 Jeuolppy sue v unuuy xipuaddy x pul 3 Wfl Nav Com XPDR Audio Hazard Additional Flight Instruments Flight Planning EIS AFCS GPS Nav Avoidance Procedures Features Annun Appendix Alerts Index Abnormal Operation 68 A GARMIN CDI DR Indication on PFD Symbolic Aircraft Map pag
25. epum invalid invalid software TER FAIL Er configuration system audio fault F MFD Terrain or Obstacle database unavailable ES or invalid S 8 777 None None operating with PFD Terrain or Obstacle 3 databases 8 No GPS position TER N ertain System ot Available 2 Excessively degraded ula gi GPS signal or out of TER N A None ot Available database coverage area ze Sufficient GPS signal T received after loss or Terrain System None None num database coverage area Available 92 entered ES gt o 2 x x pul 190 00851 02 Rev A Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations 8 Alerts A GARMIN TAWS B ALERTS PFD MFD MED Alert Type 1 TAWS B Page Aural Message ee Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP RES ee 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 07 Terrain Terrain Pull Up Pull Up Reduced Required PULL UP BSU Obstacle Obstacle Pull Obstacle Clearance or Up Pull Warning
26. for maneuvering the aircraft on the ground This database is updated on a 56 day cycle ChartView if installed ChartView resembles the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts if installed FliteCharts resemble the paper version of AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts The selected Display Pane depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Press the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and press the SHW CHRT Softkey 2 Press the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available wi
27. special or se the software or related advised of the extent allowed ated on daims or losses re ation Some jurisdictions do not allow the or consequential damages ganizations duded in this dhantability d as is and AC U KWIK g its accuracy reliability or nd to the maximum extent zations from any cause of s in the information arising isdictions do not allow the or consequential damages Printed in the U S A amp GARMIN Warnings Cautions 5 Notes e eo 6 WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance 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 avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING 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 Do not use outdated database information Databases used in the G950 system must be updated regularly in order to ensure
28. startup screen Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show active navigation database information for each display MFD1 DB PFD1 DB Verify the correct active navigation database cycle information is shown for each display Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN SSS Appendix Loading the Jeppesen Navigation Database as the Standby Navigation Database sjuaumasu nubi The purpose of the Standby Navigation Database is to allow the loading of the next cycle of the Jeppesen Navigation Database to the bottom SD card prior to its effective date The Jeppesen Navigation Database is available from Jeppesen seven days prior to its effective date oipny uddx UI0JNeN NOTE After the navigation database is loaded or copied the top SD card may be removed 52 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD 2 Verify that an SD card is inserted in the bottom slot of the PFD and the MFD 3 Turn the system ON A prompt similar to the following is displayed 4 Press the YES Softkey The navigation database is copied to the SD card in the bottom card slot of the MFD 5 After the navigation database files are copied to the bottom SD card the display will appe
29. 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 hazardous weather penetration thunderstorm penetration Stormscope information as displayed on the G950 MFD is to be used only for weather avoidance not penetration WARNING 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 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 A Wamings Cautions amp Notei
30. 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 may also be selected as follows 2 AEN 540 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 c Press the ENT Key 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 25 si SjueuinJjsu JU05 AEN iui olpny uqax 52 aoueplony paezey suelv uoneiedo s n e 4 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
31. the system user waypoints No flight plans modified 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 The flight plan on the SD card contains more waypoints truncated than the system can support The flight plan was imported with as many waypoints as possible Some waypoints not loaded The flight plan on the SD card contains one or more Waypoints locked waypoints that the system cannot find in the navigation database The flight plan has been imported but must be edited within the system before it can be activated for use User waypoint database full Not all The flight plan file on the SD card contains user loaded 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 a
32. transponder configuration settings do not match those of backup configuration memory The system should be serviced MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The system should be serviced XPDR1 SRVC XPDR1 needs service Return unit for repair The 1 transponder should be serviced when possible XPDR1 FAIL XPDR1 is inoperative There is no communication with the 1 transponder 190 00851 02 Rev A 83 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 So1nje24 e uepioAy s mp oold Buruue d AEN Sd5 yi oipny uddx 913 Sjueumasu paezey nubi u102 AEN Wil jeuonippy uoneiedo Jeuuouqy 5 R x pul Flight Instruments Nav Com XPDR Audio Flight Planning Additional Hazard Avoidance Abnormal EIS AFCS Procedures GPS Nav Features Operation Index Appendix m Annunciations 8 Alerts GRS 77 MESSAGE ADVISORIES A GARMIN 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 system should be serviced AHRS1 GPS AHRS1 using backup GPS source The 1 AHRS is using the backup GPS path Primary GPS path has failed The system should be serviced when possible AHRS1 GPS AHRS1 not receiving an
33. 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 enter 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 t
34. 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 10 A GARMIN NAV COM TRANSPONDER AUDIO PANEL Nav Com XPDR Audio Panel ADF TUNING OPTIONAL Tune the ADF using the remote ADF control head DME TUNING OPTIONAL 1 Press the DME Softkey 2 Tum the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection ENTER A TRANSPONDER CODE 1 Press the XPDR Softkey to display the transponder mode selection softkeys 2 Press the CODE Softkey to display the transponder code selection softkeys for digit entry 3 Press the digit softkeys to enter the code in the code field VVhen 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 ENTER OR CHANGE FLIGHT ID 1 Press the TMR REF Softkey then turn the large FMS Knob to highlight the Flight ID field 2 Turn the small FMS Knob to enter the first character 3 Turn the large FMS Knob to select the next field 4 Tum the small FMS Knob to enter the next desired character 5 Repeat steps 3 and 4 until the desired Flight ID is entered 6 Press the ENT Key to update the Flight ID 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Sjueumasu S24V o
35. 3 S24V oipny uddx JUI05 AEN sual uonesado s n e 4 s mp oold Buruue d AEN Sd5 junuuy jeuuouqy feuonippv xipuaddy x pul qwbil4 2 GARMIN Nav Com XPDR Audio Panel Sjueuinijsu fila 59 oipny uadx U10 AeEN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 14 A GARMIN 5 AUTOMATIC FLIGHT CONTROL SYSTEM A NOTE Refer to the Aircraft Flight Manual AFM 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 G950AFCS 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 Inadditionto the 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 02 Rev A Garmin G950 Cockpit
36. 32 PLAN 1 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 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Flight Planning c 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 title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedure s waypoints 3 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 MENU 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 MED then turn the small FMS Knob to display the Flight Plan Catalog 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 Enter th
37. 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show database information for each display MFD1 DB or PFD1 DB Verify the correct database cycle information is shown for each database for each display Remove power from the system Updating the Active Jeppesen Navigation Database not using the Dual Navigation Database or Automatic Database Synchronization Features 1 2 3 4 5 6 7 8 9 10 11 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the display PFD or MFD to be updated label of SD card facing left Turn the system ON A prompt similar to the following is displayed in the upper left corner of the display Press the NO Softkey to proceed to loading the active database A prompt similar to the following is displayed press the YES Softkey to update the active navigation database After the update completes the display starts in normal mode Do not remove power while the display is starting Turn the system OFF and remove the SD card from the top card slot Repeat steps 1 through 6 for the other display PFD or MFD Remove the SD card when finished Apply power to the system and press the ENT Key to acknowledge the
38. ALUR 261 4 7NH By CEGIX faf 351 5 9NH 5 CEGIX faf 351 5 9NH s H RW35R map 351 5 1NM RW35R map 351 5 1NM z 6368FT 348 5NM B3BBET 6368FT 348 5NM ENT MOGAL mahp 0 MOGAL mahp E t HOLD 168 6 0NH HOLD 168 6 0NM o 26 Altitudes Displayed Without Altitudes Displayed With Temperature Compensation Temperature Compensation Annun Alerts Enabling temperature compensated altitude 1 From the Active Flight Plan Page press the MENU Key The Page Menu is displayed Appendix 2 Turn the FMS Knob to highlight Temperature Compensation 3 Press the ENT Key The TEMPERATURE COMPENSATION Window is displayed Index 40 Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN 5 4 5 6 Use the small FMS Knob to select the temperature at the lt airport gt The compensated altitude is computed as the temperature is selected Press the ENT Key ACTIVATE COMPENSATION is highlighted Press the ENT Key The compensated altitudes for the approach are shown in the flight plan Disabling temperature compensated altitude 1 2 3 4 5 From the Active Flight Plan Page press the MENU Key The Page Menu is displayed Turn the FMS Knob to highlight Temperature Compensation Press the ENT Key The TEMPERATURE COMPENSATION Window is displayed Press the ENT Key CANCEL COMPENSATION is highlighted Press the ENT Key The tempe
39. AUTION Never disconnect power to the system when loading a database Power interuption during the database loading process could result in maintenance being required to reboot the system A NOTE When loading database updates the DB Mismatch message will be displayed until database synchronization is complete followed by turning system power off then on Synchronization can be monitored on the AUX SYSTEM STATUS Page In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features If an error occurs during synchronization an error message will be displayed followed by the affected display in the Sync Status section of the Database Window If synchronization completes on one display but an error occurs on another the error message will be displayed with the affected diaplays listed after it When an error message is displayed the problem must be corrected before synchronization can be completed A power cycle is required to restart synchronization when Card Full or Err is shown Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all other errors th
40. CS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 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 Black below aircraft altitude 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 TAWS Inhibit Inhibit TAWS While the TAWS B Page is displayed press the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit TAWS 3 Press the ENT Key Enable TAWS While the TAWS B Page is displayed press the INHIBIT Softkey Or 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable TAWS 3 Press the ENT Key 50 NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02
41. E A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Tum 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 Tum 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 copied 5 Press the COPY Softkey A Copy to flight plan 22 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 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 34 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN ight Planning 4 Turn the large FMS Knob to highlight the flight plan to be deleted 5 Press the DELETE Softkey A Delete flight plan 4 confirmation window is displayed 6 With OK highlighted press the
42. ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key sjuauimasu nubi 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 insertion 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 olpny uqax 0105 AEN 52 SoJnpa20Jd 4 AEN 540 nubi 5 To change the user waypoint name follow the procedure for modifying a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD aoueplony paezey saunqea4 jeuonippy NOTE See the Annunciations amp Alerts section for flight plan export message descriptions uoneiedo Jeuuouqy 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 t
43. Fix sss 40 Activate A Missed Approach in the Active Flight 7 5 40 Temperature Compensated Altitude sssssseeee 40 HAZARD AVOIDANCE 43 Customizing the Hazard Displays on the Navigation 43 STORMSCOPE Optional 0 ccccccscsssssssssssccsssssssssscsssssssssecesssssssssecessssssssseeesansssssnsess Traffic Systems Terrain And Obstacle Proximity Terrain SVS scere trum aden A Terrain Awareness amp Warning System TAWS B Display Optional 49 Airborne Color Weather Radar Optional sse 51 ADDITIONAL FEATURES ertt ttes 55 Synthetic Vision Optional V s s s s s s 55 Terminal Procedure Charts sen 56 Airport Directory Auxiliary Video Optional Scheduler esae ate nen at eet d hd Electronic Checklists if installed 62 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN of Contents ABNORMAL OPERATION Reversionary Mode Abnormal COM Operation ssssss
44. G950 Integrated Flight Deck Cockpit Reference Guide for the Pilatus PC 6 Pe A GARMIN Copyright 2009 2010 2012 2014 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0935 06 or later Some differences in operation may be observed when comparing the information in this manual to earlier or later f software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Hounsdown Business Park Southampton Hampshire 040 9LR U K Tel 44 0 23 8052 4000 Fax 44 0 23 8052 4004 Aviation Support 44 0 87 0850 1243 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 fj For after 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 Web Site Address www garmin com Except 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 without the express written permission of Garmin Garmin hereby grants permission to download a singl
45. GARMIN 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 flig VERTICAL NAVIGATION VNAV The aviation 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 be entered manually ACTIVE FLIGHT PLAN GPS Navigation ht plan eG Large White 12400FT Text Insertion Large Light M Ee Blue Text Indicator a nh Na ai RIVET iof Small Light Blue Text Quick Small Light Blue Subdued Text Small White Text with Altitude Restriction Bar SIUS Cross AT or ABOVE 5 000 fi A l Cross AT 2 300 fi Cinn SE Cross AT or BELOW 3 000 ft 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 413 sjuaumasu sub olpny uqax uo2 AEN suelv uoneiedo SaJnjeaJ s mp ooud Duruue d junuuy jeuuouqy feuonippv p EZzeH nubi xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS AFCS Procedures Appendix Al
46. 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 c 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 to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the 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 38 1 2 3 NOTE If certain GPS parameters SBAS 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 Press the ENT Key A list of available approaches for the destination airport is displayed Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN 5 4 Turn either FMS to highlight the desired 5 Press the ENT Key A list of av
47. 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 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 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 sjuaumasu nubi 59 oipny uddx JUI0JNeN ACN 540 52 Suelv uoneiedo sainjea4 aoueplony sainpadold Duruue d unuuy Jeuuouqy Jeuonippy 2 Wfil4 x pu ddy 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 7 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
48. QRs A NOTE Garmin requests the flight crew report any observed discrepancies related to database information These discrepancies could come in the form of an incorrect procedure incorrectly identified terrain obstacles and fixes or any other displayed item used for navigation or communication in the air or on the ground Go to FlyGarmin com and select Report An Aviation Data Error Report 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 A Warnings Gators amp Notes GARMIN Blank Page Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Fesouisf Hevill ni Change Summary 190 00851 00 RevA RevB 190 00851 01 190 00851 02 Initial release Added WX 500 Stormscope Added TAWS B Added KTA 870 TAS Various clerical changes Added Synthetic Vision System Added ChartView and FliteCharts Added AOPA Airport Directory Added SiriusXM Satellite Radio Added Auxiliary Video Added Electronic Checklists Added GDU 12 01 Added AC U KWIK Airport Directory Added User Defined Holding Patterns Added Landing Field Elevation enty Added temperature compensated altitude Updated System Message Advisories Updated Warnings Cautions and Notes Updated database loading procedures Changed Synthetic Vision System SVS to Synthetic Vision Technology SVT Removed SiriusXM Weather and SiriusXM Satellite Radio Added other GDU 14 02
49. Reference Guide for the Pilatus PC 6 sia sjueunasu olpny uqax 0105 AEN ARN Sd5 52 Sue v uoneiedo sainjea4 aoueplony 2 Duruue d junuuy Jeuuouqy Jeuonippy p EzeH xipuaddy x pul iui nu GARMIN AFCS Sjueuinijsu fila 593 oipny uadx U105 AEN 52 AeN 5492 4 r Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 16 A GARMIN GPS Navigation GPS NAVIGATION DIRECT TO NAVIGATION Direct to 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
50. Rev A A GARMIN ___ Hazard Avaldante 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 Displaying Weather on the Weather Radar Page 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Weather Radar Page Press the MODE Softkey 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 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 Turn the Joystick to select the desired range 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
51. System Status Page 19 Press the Display Database Selection Softkey to shovv standby navigation database information for each display MFD1 DB PFD1 DB Verify the correct standby navigation database cycle information is shown for each display Magnetic Field Variation Database Update At startup the system compares this version of the MV DB with that presently being used by the AHRS GRS If the system determines the MV DB needs to be updated a prompt is displayed on the Navigation Map Page as shown in the following figure GRS MY DB Update Available Update from 2005 to 2010 OK or CANCEL GRS Magnetic Field Variation Database Update Prompt Loading the magnetic field variation database update With OK highlighted as shown in the previous figure press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure Uploading GRS Mag Var Database STARTING UPLOAD 6 0 Uploading Database to GRS When the upload is complete the system is ready for use Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN A Activate a flight plan 18 Active database 102 AC U KWIK 58 ADF 11 12 66 ADS B 97 AHRS 84 85 Aircraft range 9 10 Airport Directory 58 Airport Signs 55 56 Airways 99 Alert messages 85 ALT 46 Altitude mode 46 Altitude volume 46 Ammeter 6 8 Antenna stabilization 53 Antenna tilt 51 AOPA 58 Audio panel controls NAV1 NAV2 12 Auxil
52. Y 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 60 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN Additional Features 4 5 6 7 8 9 10 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 e 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
53. 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 02 Rev A GARMIN Engine indication System SYSTEM DISPLAY Sjueuinijsu sub SE 2s d e 53 o Buruue d AEN 540 S21V 1ubil4 SeJnpa20Jd aoueplony paezey ELECTRICAL GEN A BAT A GEN V o BAT V sounjeo4 Jeuonippy uoneiedo Jeuuouqy System Display 25 Oil Pressure Displays engine oil pressure in pounds per square inch PRES PSI psi x pu ddy Oil Temperature Displays engine oil temperature in C TEMP C x pul 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 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 0 Ammeter GEN A ALT A Voltmeter BUS 1 V BUS 2 V FUEL DISPLAY o 5 5 9 8 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Displays DC bus voltages PRES PSI TEMP C 115 FFLOW GPH PRES PSI QTY L GAL 48 QTY R GAL 48 FUEL CALC GAL REM 167 GAL USED 3 ENDUR 4 16 RANGE N 684 Fuel Display A GARMIN Displays DC current in amperes amps for the generator
54. ailable transitions for the selected approach procedure is novv 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 TEMP COMP or optional RAD ALT 9 Press 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 procedure 10 Press the ENT Key If BARO or OFF was selected step 8 proceed to step 11 If TEMP COMP was selected in step 8 the cursor moves to the TEMP AT field Turn the small FMS Knob to enter the temperature at the destination airport The temperature compensated altitude minimum is displayed below the previously enter minimum altitude value Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 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
55. ain or obstacle databases required for TAWS in the PFD or MFD is missing or invalid GMA 347 MESSAGE ADVISORIES Message Comments GMAT FAIL GMAT is inoperative The audio panel self test has detected a fault The audio panel is unavailable The system should be serviced GMA1 CONFIG GMAT config error Config service req d The audio panel configuration settings do not match backup configuration memory The system should be serviced MANIFEST GMA1 software mismatch communication halted The audio panel has incorrect software installed The system should be serviced GMA1 SERVICE GMA1 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 system should be serviced when possible 190 00851 02 Rev A 19 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 so1njeoJ 2 Buruuejg AEN Sd 24V oipny uadx sia siu un sul paezey u102 AEN Wil jeuonippy uoneiedo Jeuuouqy ic E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES A GARMIN Message Comments GIA1 CONFIG GIA1 config Co
56. and the alternator ALT A is not used 190 00851 02 Rev A 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 of 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 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 sub Suelv uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld ARN SdD 2 olpny uqax unuuy jeuuouqy jeuonippy paezey wd U105 AEN xipuaddy x pul GARMIN Engine Indication System S3u uin sul sub U105 AEN Duruue d 16i Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy x pul 190
57. apable The GIA1 and or GIA 2 has incorrect software installed The system should be serviced 80 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Annunciations 8 Alerts GIA 63W MESSAGE ADVISORIES CONT Config service req d Message Comments MANIFEST GFC software Incorrect servo software is installed or gain mismatch communication halted settings are incorrect MANIFEST COM1 software mismatch communication halted COM1 and or COM2 software mismatch The MANIFEST COM2 software system should be serviced mismatch communication halted MANIFEST NAV1 software mismatch communication halted NAV1 and or NAV2 software mismatch The MANIFEST NAV2 software system should be serviced mismatch communication halted COM1 CONFIG COM config error mM Config service req d COM and or COM2 configuration settings do not match backup configuration memory The system COM2 CONFIG COM config error should be serviced 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 system should be serviced COM1 SERVICE COM1 needs service Return unit for repair
58. ar 6 As instructed on the display press any key to continue The display will now appear 7 Press any key to continue The display will now appear 8 Press the NO Softkey The display now starts in normal mode Since the database effective date is not yet valid it should not be loaded as the active database The display now starts in normal mode Do not remove power while the display is starting so1njeo4 aoueplony SoJnpa204d Duruue d AEN 540 puezey 3461 jeuonippy uoneiedo Jeuuouqy 9 Press the ENT Key to acknowledge the startup screen 10 Turn the large FMS Knob to select the AUX Page group on the MFD 11 Turn the small FMS Knob to select the System Status Page 12 The new database is copied to the SD card in the bottom card slot of the PFD Progress can be monitored in the SYNC STATUS field When copying is finished Complete is displayed sue v unuuy 13 Turn system power OFF 14 Remove the SD card from the top card slot of the MFD 15 Turn system power ON Feed 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts A Appendix 0808080 GARMIN 16 Press the ENT Key to acknowledge the startup screen 17 Turn the large FMS Knob to select the AUX Page group on the MFD 18 Turn the small FMS Knob to select the
59. as been reached Pilot profile import failed Displayed if the importing operation fails for any other reason Pilot profile import succeeded Displayed if the importing operation succeeds Overwrite existing file Displayed if the filename matches the name of an existing file on the SD card Pilot profile export failed Displayed if the export operation fails Pilot profile export succeeded Displayed if the export operation succeeds 91 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 s mip q e uepioAy SaJnpa20Jd Duruue d AEN Sd5 241V oipny uddx Sia siu uinnsu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy x pul GARMIN Annunciations amp Alerts Sjueuinijsu fila 59 oipny uadx U105 AEN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey soinjeod Jeuonippy uoneiedo jeuuouqy OA xipu ddy 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 92 A GARMIN Appendix APPENDIX PFD SOFTKEY MAP optional r mu m r 7 mu uu m r CDI NAV1 CD NAV2 CDI GPS Top Level PFD Softkeys optional DST ae 285 Ez r1 owe 1 566 fer REY ST ERTS p nnuannnunnunnonnn n vu um m REC Press the BACK Softkey to return to the top level softkeys TRFC 2 Inset Map Softkeys INSET Displays Inset Map in PFD lower left corn
60. at may cause the synchronization process to be halted Timeout System timed out prior to the database transfer completing 100 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Appendix Updating Basemap SafeTaxi Obstacle and Airport Directory Databases These databases may be copied to one Supplemental Data Card then automatically synchronized to other card in the system 1 With system power OFF remove the MFD database card from the bottom card slot of the MFD 2 Update the basemap SafeTaxi obstacle and or airport directory databases on the MFD card 3 Insert the MFD database card into the bottom card slot of the MFD 4 Apply power to the system check that the databases are initialized and displayed on the power up screen If a Verifying message is seen wait for the system to finish loading before proceeding to step 5 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey 6 Turn the large FMS Knob to select the AUX Page group on the MFD 7 Turn the small FMS Knob to select the System Status Page 8 Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed 9 Remove and reapply power to the system 10 11 12 Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Sta
61. bottom card slot of the PFD or MFD The SD card needs to be einserted PFD1 or MFD1 CARD 1 ERR Card 1 is invalid The SD card in the top card slot of the PFD or MFD contains invalid data PFD1 or MFD1 CARD 2 ERR Card 2 is invalid The SD card in the bottom card slot of the PFD or MED contains invalid data 190 00851 02 Rev A 89 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 saunqea4 2 AEN SdD 24V oipny uadx s q siu un su paezey nubi Wil jeuonippy uoneiedo Jeuuouqy cA E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix eee Annunciations amp Alerts FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others A GARMIN Flight Plan Import Export Description Results Flight plan successfully imported A flight plan file stored on the SD card was successfully imported as a stored flight plan File contained user waypoints only The file stored on the SD card did not contain a flight User waypoints imported success plan only user waypoints These waypoints have been fully No stored flight plan data was saved to
62. ckpit Reference Guide for the Pilatus PC 6 sual uonesado s n e 4 aoueplony s mp oold Buruue d AEN Sd5 yi oipny uadx sia junuuy jeuuouqy paezey nubi u102 AEN xipuaddy x pul is T Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun Instruments 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 DOWN 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
63. comes 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 GPS Position 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 65 eouepioAy Senpa204d Buruue d ARN 540 52 oipny uddx 513 5149 1115 puezey ubi U105 AEN BUTLER saunqea4 jeuonippy xipuaddy suelv junuuy 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 66 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
64. d 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 temperature 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 02 Rev A GARMIN FlightPlamning CREATE A USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Turn the large FMS Knob on the MFD to select the WPT page group 2 Tum 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 Enter the 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 ste
65. d Color Highlight 53 Weather radar 51 Wind data 95 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Index Index 3 sainjea4 aoueplony 2 buluueld AEN Sd5 S24JV olpny uqax sia sjuauimasu jeuonippy 2 Wil Tuo2 NeN uoneiedo Jeuuouqy Sue v unuuy 1821 GARMIN index Sjueuinijsu fila 593 U105 AEN S24V AeN Sd5 Duruue d r Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy e E 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Index 4 A GARMIN arminAT Ine 2345 Turner Road SE S Salem OR 97302 USA p 503 391 3411 f 503 364 2138 S Garmin Europe Ltd Liberty House Hounsdown Business Park s Southampton Hampshire 5040 9LR U K p 44 0 23 8052 4000 fb 1 44 0 23 8052 4004 Aviation Support 44 Er 5 886 2 2642 9199 f 886 2 2642 90 2009 2010 2012 2014 Garmin Ltd or its subsidiaries 190 00851 02 Rev A
66. d inserted into the bezel slot If the SD card contains an invalid checklist file or no checklist the Power up Page messages display Checklist File Invalid or Checklist File N A not available and the CHKLIST Softkey is not available Accessing and Navigating Checklists 1 2 3 4 5 6 7 8 9 10 62 From any page on the MFD except EIS Pages press the CHKLIST Softkey Turn the large FMS Knob to select the GROUP field Turn the small FMS Knob to select the desired procedure and press the ENT Key Turn the large FMS Knob to select the CHECKLIST field Turn the FMS Knob to select the desired checklist and press the ENT Key The selected checklist item is indicated with white text surrounded by a white box Press the ENT Key or CHECK Softkey to check the selected checklist item The line item turns green and a checkmark is placed in the associated box The next line item is automatically selected for checking Either FMS Knob can be used to scroll through the checklist and select the desired checklist item Press the CLR Key or UNCHECK Softkey to remove a check mark from an item When all checklist items have been checked Checklist Finished is displayed in green text at the bottom left of the checklist window If all items in the checklist have not been checked CHECKLIST NOT FINISHED will be displayed in yellow text Press the ENT Key GO TO NEXT CHECKLIST wil
67. 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 FLIGHT PLAN NOTE When creating a 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 counter 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 Tum the small FMS Knob clockwise to display the Flight Plan Catalog Page 3 Press 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
68. e 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 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 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 33 sjuauimasu sub olpny uqax si UI0JNeN 52 2 4 AEN 540 nubi aoueplony paezey Ssuelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy 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 GARMI N 2 3 4 5 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 waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window 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 ACTIVAT
69. e copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited co G950 is a trademark of Garmin Ltd or its subsidiaries Garmin WATCH FliteCharts and SafeTaxi are registered trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc Stormscope is a registered trademark of L 3 Communication n AC U KWIK is a registered trademark of Penton Business Media Inc AOPA Membership Publications Inc and it AOPA expressly disclaim all warranties with data express or imp apa rant or make an ces in damages that result documentation even if AOPA or an AOPA aut uch damages User ag d harmless AOPA fro and fitness fo wa no circumstan consequential possibility of s by lim 50 and f and fitness Organization th aw to release and ho to any actual or alleged inaccuracies in the in itation or exclusion of i the above limitations o its relate expressly disclaim data express or implied including but no
70. e 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 Unsupported leg type in flight plan The lateral flight plan contains a procedure turn unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint vector or other VNV Unavailable Excessive track The cu rent 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 selected A parallel course has been selected causing the deviation to go invalid vertica 88 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message Comments NON WGS84 WPT Do not use GPS for navigation to xxxx The position of the selected waypoint xxxx 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 TRAFFIC FAIL Traffic device has failed The is no longer receiving data from the traffic sys
71. e in the desired position The location of the Bearing Line becomes the center point of the Sector Scan 2 Press the FMS Knob to display the cursor 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field 4 Turn the small FMS Knob to select FULL 60 40 or 20 scan 5 If desired readjust the Bearing Line with the Joystick to change the center of the Sector Sca n 6 Press the FMS Knob to remove the cursor Antenna Stabilization 1 To activate or deactivate the antenna stabilization press the MODE Softkey 2 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 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 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 53 AeN Sd5 S24V oipny uadx si sjueumasu u105 AEN buluueld Wil uep ony s mp oold paezey suelv uoneiedo
72. elect the Map Page Group 2 Turn the small FMS Knob to select the Terrain SVS Page 3 If desired select the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select 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 Black below aircraft altitude Enable Disable Aviation Data 1 While the Terrain SVS 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 Terrain SVS Inhibit Inhibit Terrain While the Terrain SVS Page is displayed select the INHIBIT Softkey Or Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN Hazard avoidance 1 Press the MENU Key 2 Tum the small FMS Knob to select Inhibit Terrain 3 Press the ENT Key Enable Terrain While the Terrain SVS Page is displayed select the INHIBIT Softkey Or 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable Terrain 3 Press the ENT Key A NOTE If Terrain SVS alerts are inhibited w
73. endix Alerts Operation Features Avoidance Index Flight Planning GARMI N Removing a user defined hold created at the aircraft present position or at a Direct To waypoint 1 Press the Direct To Key to display the DIRECT TO Window PFD or MFD 2 Press the MENU Key to display the PAGE MENU vvith the cursor on the Cancel Direct To NAV selection 3 Press the ENT Key The holding pattern is removed Removing a user defined hold created at an active flight plan vvaypoint 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highlight the HOLD waypoint 3 Press the CLR Key A Remove Holding Pattern confirmation window is displayed 4 Select OK and press the ENT Key The holding pattern is removed from the active flight plan Select CANCEL and press the ENT Key to cancel the removal of the holding pattern INVERT AN ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 Press the MENU Key to display the Page Menu 3 Turn the large FMS Knob to highlight Invert Flight Plan 4 Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location 5 With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT
74. er e Horizon Heading Marks e Terrain and Obstacle Alerting Three dimensional Traffic Airport Signs e Runway Display Displaying Synthetic Terrain 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 Press the SYN TERR Softkey 4 Press the BACK Softkey to return to the previous page Displaying Pathways 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 99 xipuaddy suelv uoneiedo sainjea4 aoueplony saunpadoid Duruue d AEN Sd5 S24JV oipny uddx sia sjuauimasu junuuy Jeuuouqy Jeuonippy p EzeH ubi u05 AeN BUTLER x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional beatus GARMIN 4 Press the PATHWAY Softkey 5 Press the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Sof
75. er OFF Removes Inset Map 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 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 33 Sonjeo4 e ueproAy SoJnpa204d Duruue d AEN 540 S24JV olpny uqax 513 sjueumasu puezey U10 AEN jeuonippy uoneiedo Jeuuouqy Sue v unuuy gt s o z m x x pul ii Wfi l4 Hight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index A Appendix 0h8hxy7 GARMIN TRAFFIC Cycles through traffic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map window TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map optional 31 Coe Ge ST YT mn p p nnunnnunn n SYNVIS n nn rs Press the BACK Softkey to return to the top level softkeys BRG1 OFF L IL IL L IL Yursil e a E V3 75 7 EEE 75 n onm ppnnm
76. erts 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 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 It 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 by the Altitude has been entered The system cannot system estimating the by the pilot Altitude is use this altitude in altitude of the ai
77. es 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 display to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DIK 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 G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN Amunciations 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 Electrical load reduction recommended Engine oil contamination detected F L uel filter is blocked
78. fault 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 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 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 4 AEN Sd5 S24V oipny duadx 99 s u umnnsul u102 AEN bila Duruue d Wil uep ony s mp oold paezey Sue v uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy 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 Aveidanes GARMINI TERRAIN SVS A NOTE Terrain SVS is only available when the Synthetic Vision System SVT option is installed and the TAWS option has not been installed A NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Display Terrain on the Terrain SVS Page 1 Tum the large FMS Knob to s
79. 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 navigation database update Verify that stored flight plans contain correct waypoint locations TIMER EXPIRD Timer has expired The system notifies the pilot that the timer has expired 86 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message Comments 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 navigation 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 This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database This alert is issued only after an navigation database update Verify use of airways in stored flight plans and reload airways as needed WPT ARRIVAL Arriving at waypoint XXxx
80. for the Pilatus PC 6 190 00851 02 Rev A GARMIN avoidance TRAFFIC SYSTEMS e 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 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 Traffic Advisory TA dosing rate distance and vertical separation meet TA citeria Traffic Advisory Off Scale Traffic Symbol Description Traffic Information Service TIS NOTE If the G950 is configured to use a Traffic Advisory System TAS TIS is not available for use 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 02 Rev A Garmin G950
81. g 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 MFD1 DB ERR MFD1 ChartView database error exists The MFD and or PFD detected a fault in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists The system should be serviced The MFD and or PFD detected a fault in the ChartView database optional feature Ensure that the data card is properly inserted Replace data ard If problem persists The system should be serviced o MFD1 DB ERR MFD1 FliteCharts database error exists The MFD and or PFD detected a fault in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The system should be serviced MFD1 DB ERR MFD1 Airport Directory database error exists The MFD detected a fault in the Airport Directory database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 multiple database errors exist PFD1 DB ERR PFD1 multiple database errors exist The MFD and or PFD detected a fault in more than one database If problem persist
82. he 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 02 Rev A GARMIN FlightPlamning 12 Press the ENT Key 13 Repeat step 10 to enter the next waypoint name 14 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 USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM ANOTHER WAYPOINT 1 Tum the large FMS Knob on the MFD to select the WPT page group 2 Tum 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 Enter the 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
83. hen the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOWALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix TERRAIN AWARENESS amp WARNING SYSTEM TAWS B DISPLAY OPTIONAL 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 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 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 49 AEN Sd5 S24V oipny uadx 99 s u umnnsul u102 AEN bila Duruue d Wil aoueploay s mp oold paezey Sue v uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AF
84. 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 OFF 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 02 Rev A A GARMIN __Flight instruments SET BAROMETRIC MINIMUM DESCENT ALTITUDE mal g 2 o 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 59 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 Wil s mp 01d 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 di
85. iary video 59 Aviation database 19 Barometric Altitude Minimums 3 Barometric pressure 96 Bearing line 52 53 Bus voltage 6 8 C CDI 1 12 88 Cell 43 44 Cell mode 44 ChartView 56 57 Checklists 62 63 Clearance player 12 Clearance Recorder 12 Code selection softkeys 11 COM 12 65 D Database Synchronization 102 DB Mismatch 100 DCLTR Softkey 56 Dead Reckoning 67 Declutter 66 93 99 Direct to 17 DME 11 12 DR mode 67 68 E Edit a flight plan 33 Electrical indications 6 Electronic checklists 62 63 Emergency checklist 63 Enable Terrain 49 Endurance 9 F Flaps 6 Flight ID 11 Flight path marker 55 FliteCharts 56 57 Frequency Transfer 12 Fuel Flow 6 9 Quantity 6 9 Remaining 9 Used 9 G Gain 52 Generator speed 6 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Index Index 1 sainjea4 aoueplony 2 buluueld AEN Sd5 S24JV olpny uqax sia sjuauimasu jeuonippy 2 Wil Tuo2 NeN uoneiedo Jeuuouqy Sue v unuuy m Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts ud Appendix Index H Horizon heading 55 Horizontal scan 52 Inhibit 48 50 Inhibit TAWS 50 Inhibit Terrain 48 49 Inset Map 93 94 Intercom isolation 13 Interstage Turbine Temperature ITT 6 IOI 70 72 73 ITT 6 J
86. int identifier and GPS derived distance information Displays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HSI in an arc format Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information 95 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 s n e 4 auepiony SoJnpa20Jd Duruue d AEN Sd5 S241V olpny uqax sia s tin sul jeuonippy puezey nubi qb uoneiedo Jeuuouqy Sue v unuuy ER z Hazard Flight Nav Com Hight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Features A GARMIN Appendix 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 o Es Lk FE D m n n FE D n L STBY ON ALT GND VFR CODE IDENT BACK ALERTS F WF vvv mn n n n F mrs nm Press the BACK Softkey to return to the top level softkeys ETT IE AES 7 Tom Esse TE qns Press the BACK Softkey to return to the previous level softkeys Transponder Softkeys Abnormal Operation Annun Alerts Appendix Index XPDR Displays transponder mode selection softkeys STBY Selects Standby Mode transponder does not repl
87. into the active flight plan and activates the s mp old 11 12 siu uinnsu iui aoueplony AEN 549 52 oipny sadx paezey 346 U105 AEN soJnjeoJ jeuonippy first leg of the approach 13 Press the ENT Key ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC 2 Tum the large FMS Knob to highlight ACTIVATE APPROACH Key 3 Press the ENT Key 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 39 xipuaddy suelv uoneiedo junuuy Jeuuouqy x pul A Procedures GARMIN ACTIVATE A VECTOR TO FINAL APPROACH FIX Flight Instruments 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key EIS 4 final approach course becomes the active leg 25 3 3 ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 2 1 Press the PROC Key E 2 Tum the large FMS Knob to highlight ACTIVATE MISSED APPROACH R 3 Press the ENT Key A confirmation window is displayed R 4 With ACTIVATE highlighted press the ENT Key Or Press the go around button Flight Planning TEMPERATURE COMPENSATED ALTITUDE When temperature compensated altitude is enabled for the loaded approach the altitudes associated with the approach waypoints are displayed in slanted text M 2 5 3 2 a E E 28 HABUK iaf 021 5 7NM HABUK iaf 021 5 7NM FALUR 261 4 7NH F
88. ion Map Page Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN II Appendix TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map TERRAIN Displays terrain information on Navigation Map AIRVVAYS Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed BACK Returns to top level softkeys DCLIR Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLIR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan SHW CHRT When available displays optional airport and terminal procedure charts CHKLIST When available displays optional checklists 99 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 nubi soinjeo4 e2uepioAy s mp old buluueld ACN 540 S24V oipny duadx Jeuonippy p ezeH fia Juo neN uoneiedo Jeuuouqy Sue v unuuy k Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix LOADING UPDATED DATABASES A GARMIN A C
89. ions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Obstacle database mismatch 78 Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 The PFD and MFD have different obstacle database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on 190 00851 02 Rev A A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message Comments DB MISMATCH Airport Terrain database mismatch The PFD and MFD have different airport terrain database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on NAV DB UPDATED Active navigation database updated System has updated the active navigation database from the standby navigation database TERRAIN DSP PFD1 or MFD1 Terrain awareness display unavailable One of the terrain airport terr
90. ipny uadx sia JUI05 AEN Suelv uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld ARN Sd5 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul iui nu Flight Instruments Nav Com AFCS XPDR Audio EIS Abnormal Additional Hazard Flight Planning Annun GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN 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 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 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 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned 2 Tum 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 3 Press the Frequency Transfer Key to place the frequency into the active frequency field DIGITAL CLEARANCE RECORDER AND PLAYER NOTE Only the audio for the selected COM MIC Key is recorded Audi
91. 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 system should be serviced 6 51 FAIL G S1 is inoperative 6 52 FAIL 6 52 is inoperative A fault has been detected in glideslope receiver 1 and or receiver 2 The system should be serviced 82 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Annunciations 8 Alerts GIA 63W MESSAGE ADVISORIES CONT Message Comments G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair A fault has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The 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 system should be serviced MANIFEST GEA1 software mismatch communication halted GTX 33 33ES MESSAGE ADVISORIES The 1 GEA 71 has incorrect software installed The system should be serviced Message Comments XPDR1 CONFIG XPDR1 config error Config service req d The
92. l be highlighted by the Cursor Press the ENT Key to advance to the next checklist Press the EXIT Softkey to exit the Checklist Page and return to the page last viewed Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Additional Features Immediately Accessing Emergency Procedures 1 From any page on the MFD press the CHKLIST Softkey 2 Press the EMERGCY Softkey 3 Turn the FMS Knob to select the desired emergency checklist and press the ENT Key 4 Press the ENT Key or CHECK Softkey to check the selected emergency checklist item The line item turns green and a checkmark is placed in the box next to it The next line item is automatically highlighted for checking Either FMS Knob can be used to scroll through the checklist and select the desired checklist item olpny uqax s q sjuauimasu U10 AEN 3463 52 Press the CLR Key or UNCHECK Softkey to remove a check mark from an item 5 When all checklist items have been checked Checklist Finished is displayed in green text at the bottom left of the checklist window If all items in the checklist have not been checked CHECKLIST NOT FINISHED will be displayed in yellow text 6 Press the ENT Key GO TO NEXT CHECKLIST will be highlighted by the AEN Sd5 Duruue d LITE cursor 7 Press the ENT Key to advance to the next checklist 8 Press the RETURN Softkey to return to the previous checklis
93. led The system should be serviced 190 00851 02 Rev A 75 Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 saunqee4 2 AEN 5649 S24V oipny uadx sia siu un su paezey nubi u102 AEN Wil jeuonippy uoneiedo Jeuuouqy ic Eu 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 MFD amp PFD MESSAGE ADVISORIES CONT Message Comments PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The system should be serviced DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 navigation database error exists PFD1 DB ERR PFD1 navigation database error exists The MFD and or PFD detected a fault in the navigation database Attempt to reload the navigation database If problem persists the system should be serviced MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists The MFD and or PFD detected a fault in the basemap databa
94. lt setting for the PC 6 when more than one option is available TAWS B SYSTEM STATUS ANNUNCIATIONS 190 00851 02 Rev A unu TAWS B Page Aural Alert Type Alert mee Annunciation Message Annunciation System Test in Progress TAWS TEST M MD NMM e TANS 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 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 73 So1nje24 eouepioAy s mp oold Buruue d AEN Sd5 2 oipny uddx 913 Sjueumasu paezey Wfila u102 AEN Wil jeuonippy uoneiedo Jeuuouqy R x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 1224 Annunciations GARMIN PFD MFD Alert Annunciation Aural Message TAWS B Page Alert Type Annunciation TANS System TAWS B System Test Fail di ail Failure Terrain or Obstacle database unavailable or invalid invalid software configuration system audio fault TANS System Failure No GPS position Excessively degraded GPS signal Out of database None m Available Coverage area Sufficient GPS signal received TAWS None sic Lp after loss
95. min com by selecting Database Exclusions List NOTE The FAA has asked Garmin to remind pilots who fly with Garmin database dependent avionics of the following t is the pilot s responsibility to remain familiar with all FAA regulatory and advisory guidance and information related to the use of databases in the National Airspace System Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen Databases obtained from Garmin or Jeppesen are assured compliance with all data quality requirements DQRs by virtue of a Type 2 Letter of Authorization LOA from the FAA A copy of the Type 2 LOA is available for each database and can be viewed at http fly garmin com by selecting Type 2 LOA Status Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with established FAA regulatory guidance but does not constitute authorization to fly any and all terminal procedures that may be presented by the system It is the pilot s responsibility to operate in accordance with established AFM S and regulatory guidance or limitations as applicable to the pilot the aircraft and installed equipment Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Warnings Cautions 5 Notes NOTE the pilot operator wants or needs to adjust the database contact Garmin Product Support to coordinate the revised D
96. n 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 ENT 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 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 190 00851 02 Rev A Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 21 oipny uddx s q sjuauimasu U105 AEN 1461 4 52 2 4 AEN 540 nubi aoueplony paezey suelv uoneiedo s n e 4 u
97. n sul paezey nubi wi0 gt AeN nubi jeuonippy uoneiedo Jeuuouqy R x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts GDC 74A MESSAGE ADVISORIES A GARMIN Message Comments ADC1 ALT EC ADC1 altitude error correction is unavailable GDC1 or GDC2 is reporting that the altitude error correction is unavailable ADC1 AS EC ADCT airspeed error correction is unavailable GDC1 or GDC2 is reporting that the airspeed error correction is unavailable MANIFEST GDC1 software mismatch communication halted The GDC 74A has incorrect software installed The system should be serviced ADC1 SERVICE ADC1 needs service Return unit for repair The GDC1 and or GDC2 self test has detected a problem in the unit The system should be serviced MANIFEST ADC1 needs service Return unit for repair The GDC1 and or GDC2 self test has detected a problem in the unit The system should be serviced MISCELLANEOUS MESSAGE ADVISORIES Message Comments FPL WPT LOCK Flight plan waypoint is locked Upon power up the system detects that a stored flight plan waypoint is locked This occurs when an navigation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and
98. n 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 available 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 02 Rev A 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 way
99. ndix Alerts Operation Features Index Torque Gauge TRQ PSI Interstage Turbine Temperature Gauge ITT C Propeller Speed Gauge NP RPM 4 Gas Generator Speed Gauge NG 96 G Fuel Flow FFLOW GPH Oil Pressure Indicator OIL PSI Oil Temperature Indicator OIL C VOLTS Fuel Quantity Indicator FUEL QTY 1 Aileron and Rudder Trim Bars AIL RUD 2 Elevator Trim Bar ELEV 3 Flap Position Indicator FLAPS Engine Indication System GARMIN Displays engine torque in pounds per square inch 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
100. nfig service req d error GIA2 CONFIG GIA2 config Config service req d error The GIA1 and or GIA2 configuration settings do not match backup configuration memory The system should be serviced error Config service req d GIA1 CONFIG G A1 audio confi error Config service req d too low GIA1 COOLING GIA1 temperat GIA2 CONFIG GIA2 audio confi too low GIA2 COOLING GIA2 temperat The GIA1 and or GIA2 have an error in the audio configuration The system should be serviced The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the system should be serviced Return the unit for repair GIA1 SERVICE G A1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service The GIA1 and or GIA2 self test has detected a problem in the unit The system should be serviced halted HW MISMATCH GIA hardware mismatch GIA1 communication halted MANIFEST G A1 software mismatch communication ha HW MISMATCH GIA hardware mismatch GIA2 communicati on ted MANIFEST GIA2 software mismatch communication ha ted A GIA mismatch has been detected where only one is SBAS c
101. nnunnnunnnntovntu IL Tom TL erm omes oe L L 10 L 1E see J faces EY V3 V3 V3 V3 MEN nsn nmn nmn m Excess paveo pesens TE rreee Ies uu im 3 PFD Configuration Softkeys PFD Displays second level softkeys for additional PFD configurations SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features 94 Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN DFLTS WIND DME BRGI HSI FRMT BRG2 190 00851 02 Rev A PATHWAY SYN TERR HRZN HDG APTSIGNS OPTN I OPTN 2 OPTN3 OFF 360 HSI ARC HSI Appendix Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan Enables synthetic terrain depiction Displays compass heading along the Zero Pitch line Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm Resets PFD to default settings including changing units to standard Displays softkeys to select wind data parameters Headwind tailwind and crosswind arrows with numeric speed components Wind direction arrow and numeric speed Wind direction arrow with headwind tailwind and crosswind speed components Information not displayed Displays the DME Information Window Cycles the Bearing 1 Information Window through NAVI or GPS waypo
102. nuuy Jeuuouqy Jeuonippy 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 7 8 9 10 11 12 13 A GARMIN 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 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 airspee
103. o 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 xipuaddy suelv junuuy x pul 190 00851 02 Rev A Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 35 GARMIN Flight Planning Ssjueuinijsu fila 59 oipny uadx U105 AEN s24v AeN Sd5 buluueld 346 Blank Page 5 2 4 puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 36 GARMIN Procedures PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Tum 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
104. o 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 02 Rev A 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 radios and music PILOT KEY COPLT KEY pides 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 mm radios aural alert copi pass musi Copi pass s pilot ot engers C lot engers mus Copi ic lot Selected radios aural alerts pilot copilot ICS Isolation Modes 190 00851 02 Rev A 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 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 sjueumansu 5
105. of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp 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 longitude 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 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Warnings Cautions 5 Notes 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 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
106. p 2 Turn the small FMS Knob to select VIDEO and display the AUX VIDEO Page The video display softkeys shown below appear on the AUX VIDEO Page Control of the AUX VIDEO Page can also be accessed through the Page Menu Selecting video menu options 1 While viewing the AUX VIDEO Page press the MENU Key to display the Page Menu OPTIONS 2 Turn the large FMS Knob to highlight the desired video adjustment option and press the ENT Key Once the ENT key is pressed on any option the page menu closes and returns to the AUX VIDEO Page Video Setup Video brightness contrast and saturation may be adjusted be selecting the setup function While viewing the setup function softkeys after 45 seconds of softkey inactivity the system reverts to the AUX VIDEO Page softkeys Adjusting the video settings 1 With the AUX VIDEO Page displayed press the SETUP Softkey 2 Press the BRIGHT or BRIGHT to adjust display brightness in five percent increments from 0 to 100 3 Press the CNTRST or CNTRST to adjust display contrast in five percent increments from 0 to 100 4 Press the SAT or SAT to adjust display saturation in five percent increments from 0 to 100 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 9 s mp o4d Buruuejd AeN Sd5 S24V oipny uadx sia siu u nnsul Tu102 AEN 3463 aoueplony paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul
107. p 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 sainpadold AEN 540 nubi CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 1 Tum the large FMS Knob on the MFD to select the WPT page group 2 Tum 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 Enter the desired waypoint name 5 Press the ENT Key 6 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 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 23 sia sjueuinsu U05 AEN iui olpny uqax 52 2 Suelv uoneiedo sainjea4
108. parameters Revision Date of Revision Affected Pages October 2014 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 RR 1 Record of Revisions GARMI Blank Page RR 2 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN Tale of Contents FLIGHT 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 s s s s s ss s sss s sss s sssss n 1 Enable Disable OBS Mode While Navigating with GPS 2 Generic TIGE occorre e ac c an omen 2 Configure Vspeed Bugs 2 Set Barometric Minimum Descent Altitude sss 3 Displaying Wind Data 3 Changing HSI Format nnns 3 ENGINE INDICATION 5 9 5 Engine Display een etn tenerae eun 5 System Display eene eite rere ted inerenti HR RA Ren 7 Fuel Display ee HRA A i e EUR 8 NAV COM TRANSPONDER AUDIO PANEL 1 ADF Tuning 7 2 1 DME Tuning 5
109. point 25 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 Table of Contents GARMI N Delete a User Vlaypoint U s s s s s s ss nnne 26 Create a Flight Plan s s nennen 27 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 User Defined Holding Patterns 30 Invert An Active Flight Plan sss 32 Remove a Departure Arrival Approach or Airway from a Flight Plan 32 Store a Flight Plan nennen nnn rnnt Edit a Stored Flight Plan Delete a Waypoint from the Flight Plan sss Invert and Activate a Stored Flight Plan Copy a Flight Pl n ee eere eb en eii ee diae Delete a Flight Plan Graphical Flight Plan Creation Export a Flight Plan to an SD Card ssssssss PROCEDURES a Da ss Load and Activate a Departure Procedure Activate A Departure Leg ccccccssusssssssssssssessssssessssssssssssvsessssnsnessssnsnessssennessssennss Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure sl s sl 38 Activate An Approach in the Active Flight Plan 39 Activate a Vector to Final Approach
110. point 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 the 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 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 29 oipny uddx 593 sjuauimasu U10 AEN 1461 4 52 2 4 AEN 540 nubi aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Fligh
111. rature compensated altitude at the FAF is cancelled 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 sjuauimasu nubi oipny udax si UI0JNeN 52 AEN 540 Duruue d nubi s mp olqd aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul GARMIN Procedures Sjueuinijsu fila 59 oipny uadx U105 AEN s24v AeN Sd5 buluueld Blank Page um aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 42 GARMIN 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 G950 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
112. rcraft as it designated for use in determining vertical passes over the navigation giving vertical flight path flight path guidance point This altitude is guidance Altitude does provided as a reference not match the published and is not designated to altitude in navigation be used in determining database or no published vertical flight path altitude exists guidance 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 vertical 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 02 Rev A GARMIN FLIGHT PLANNING TRIP PLANNING 1 Turn the large FMS Knob to select the AUX page group 2 Turn the small FMS Knob to select the first rectangular page icon 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 positio
113. re locked in the flight plan The flight plan must be edited within the system before it can be activated for use 90 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN Amunciations amp Alerts Flight Plan Import Export Description Results One or more user waypoints One or more imported user waypoints were renamed 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 PILOT PROFILE IMPORT EXPORT MESSAGES R Pilot Profile Import Export Results Description No pilot profile plan files found to import Displayed if the SD card does not have one or more valid pilot profile filenames Overwrite existing profile Displayed if the profile name matches the name of existing profile Profile name invalid Enter a different Displayed if the profile name is invalid profile name All available pilot profiles in use Delete a Displayed if the maximum number for pilot profile before importing another profiles h
114. rnia 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 Use of polarized eyewear may cause the flight displays to appear dim or blank 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 A Wamings Cautions amp Notei 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 The purpose 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 NOTE The pilot operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation The database alerts can be viewed at www flygarmin com by selecting Aviation Database Alerts NOTE The pilot operator must review and be familiar with Garmin s database exclusion list as discussed in SAIB CE 14 04 to determine what data may be incomplete The database exclusion list can be viewed at www flygar
115. s the system should be serviced 190 00851 02 Rev A 7 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 soJnjeoJ 2 AEN 5649 2 olpny uqax s q paezey nubi u102 NEN Wil jeuonippy uoneiedo Jeuuouqy es E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message Comments DB MISMATCH Navigation database mismatch Xtalk is off The PFD and MFD have different navigation database versions or regions installed Crossfill is off Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Standby Navigation database mismatch The PFD and MFD have different standby navigation database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Terrain database mismatch The PFD and MFD have different terrain database vers
116. sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul GARMIN Hazard Avoidance Sjueuinijsu fila 59 olpny uddX u102 AEN S2dV AeN Sd5 Duruue d Blank Page 6 2 4 eouepioAy DX Se1njeoJ jeuonippy uoneiedo jeuuouqy suay junuuy xipuaddy x pul 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 54 GARMIN 0 Additional Features ADDITIONAL FEATURES SYNTHETIC VISION OPTIONAL o V ARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVT is intended as an aid to situational awareness only and may not provide the accuracy and or fidelity upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic Synthetic Vision Technology SVT functionality is offered as an optional enhancement to the G950 Integrated Flight Deck System SVT is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVT information is shown on the primary flight display PFD SVT offers a three dimensional view of terrain and obstacles Terrain and obstacles that pose a threat to the aircraft in flight are shaded yellow or red In addition to SVT enhancement to the PFD the following feature enhancements have been added to the PFD e Pathways e Flight Path Mark
117. 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 2 3 Press the MENU Key Turn the large FMS Knob to select Show Tilt Line Press the ENT Key 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 AEN Sd5 S24V oipny uddx sia siu umnsul uo2 AEN iui Duruue d aoueploay s mp oold paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 0 GARMIN 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 field 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 2 3 Press the MENU Key Turn the large FMS Knob to select Show Bearing Line Press the ENT Key Vertically Scan a Storm Cell 1 2 3 4 5 While in the Horizontal Scan view move the Joystick to place the Bearing Line on the desired storm cell or other area to be vertically scanned Press the VERTICAL Sof
118. se The MFD and or PFD detected a fault in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists The system should be serviced MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists The MFD and or PFD detected a fault in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists The 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 but is missing on the specified LRU 76 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Annunciations 8 Alerts DATABASE MESSAGE ADVISORIES CONT Message Comments 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 fault in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists The system should be serviced MFD1 DB ERR MFD1 airport terrain database missin
119. software mismatch communication halted un MANIFEST MFD1 software mismatch communication halted The PFD and or MFD self test has detected a problem The system should be serviced The PFD and or MFD has incorrect software installed The system should be serviced PFD1 CONFIG PFD1 config error Config service req d The PFD configuration settings do not match backup configuration memory The system should be serviced MFD1 CONFIG MFD1 config error Config service req d The MFD configuration settings do not match backup configuration memory The system should be serviced SW MISMATCH GDU software version mismatch Xtalk is off The MFD and PFD have different software versions installed The system should be serviced PFD1 COOLING PFD1 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage PFD1 KEYSTK PFD1 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the system should be serviced A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has fai
120. splay the arc style HSI aoueplony paezey suelv uoneiedo s n e 4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul 190 00851 02 Rev A Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 amp GARMIN Flight Instruments I x oipny uadx U105 AEN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00851 02 Rev A Garmin G950 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 EM TRG PSI Floatplane Option FFLOW GPH OIL PSI OIL C AMPS G oO OOO 9 FUEL QTY E E A F Engine Display 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 S3u u nnsul Suelv uone1edo So1njeoJ Fuluueld AEN 540 S24V olpny uqax yunuuy jeuuouqy jeuonippy paezey wd u102 AEN xipuaddy x pul nubi E Flight Instruments iw Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS Procedures GPS Nav Appe
121. ssssseeenennnnnn Hazard Displays with Loss of GPS Position Unusual Attitudes sseeennnnnnnnnnnne MEC O eee eee ite erbe en eer id ANNUNCIATIONS amp 69 WARNING Annunciation sss 69 CAUTION Annunciation sse 69 Safe Operating Annunciation ssssssseeeenen 69 Alert M ssage eese eee den s Ee ss i aiebat 70 Terrain SVS Alerts 70 TAWS B Alerts eee ote HR LU Rep EAE Ce edet 72 TAWS B System Status Annunciations sssssseenes 73 Voice Alerts MFD amp PFD Message Advisories ssssssssene 15 Database Message 150165 76 GMA 347 Message Advisories GIA 63W Message Advisories GEA 71 Message Advisorles ss s ss s s ss sss s ssis GTX 33 33ES Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories GWX 68 Alert 55 65 GDC 74A Message Advisories Miscellaneous Message Advisories Flight Plan Import Export Messages Pilot Profile Import Export Messages APPENDIX Gm
122. t particular purpose The s do not warrant or ma erwise Licensee agrees not to s Or a ied induding b ticular purpose duding neglige mplied wa exclusion all warranties wi y representation S related organizatio espect to the AOPA ut not lim s regardin nce sha from the AOPA be liable for use or inability to u ees not to m any causes of acti form ranties or liabi s may not app lity for incidenta y to you d organizations hereafter collectively AC U KWIK 0 th respect to the AC U KWIK information in ied warranties of me imited to the imp information is provide e any representations regardin ue AC U KWIK Organizations a ted to the implied warranties The information is provided as is and AOPA does not g its accuracy reliability or horized representative has been sue AOPA and to the maximum 0 d d 0 owed by ction daim aw to release and hold ha s or losses related to any act ut of Garm in s use of the information i m ual or alleged inaccuracie the datasets Some jur n ess AC U KWIK Organi m S October 2014 itation or exclusion of implied warranti the above limitations or exclusions may n 1 es or liability for incidenta ot apply to licensee 90 00851 02 Rev A f ns hereina information of ter collectively included in this merchantability otherwise Under any incidental
123. t 9 Press the EXIT Softkey to exit the Checklist Page and return to the page last viewed 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 63 SeJnpa20Jd eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul GARMIN itional Features Add Blank Page 6 2 4 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 64 GARMIN 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 be
124. t Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 4 5 6 7 A GARMIN Turn the small FMS Knob one click clockwise 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 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 USER DEFINED HOLDING PATTERNS A holding pattern can be defined at any active flight plan waypoint or at the aircraft present position 30 Creating a user defined hold at an active flight plan waypoint 1 2 3 4 5 6 7 8 9 10 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan VVindovv PFD Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highlight the waypoint for the hold Press the MENU
125. t Further Clearance Time EFC TIME and press the ENT Key 7 Press the ENT Key while ACTIVATE is highlighted to immediately activate the hold olpny uqax si UI0JNeN 52 AEN 540 pu i8 ea Creating a User Defined Hold at a Direct To Waypoint 1 Press a Direct to Key and set up the Direct To waypoint as desired but select HOLD instead of ACTIVATE when finished 2 Use the FMS Knobs to edit the entry course and press the ENT Key 5 Use the small FMS Knob to select INBOUND or OUTBOUND course direction and press the ENT Key 6 Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key 7 Use the FMS Knobs to edit the length and press the ENT Key 8 Use the small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key 9 Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key Press the ENT Key while ACTIVATE is highlighted to activate the Direct To with the user defined hold defined at the Direct To waypoint soJnjeoJ 2 jeuonippy paezey uoneiedo Jeuuouqy Sue v unuuy 10 xipuaddy x pul 190 00851 02 Rev A Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav App
126. tem The traffic device should be serviced STRMSCP FAIL Stormscope has failed Stormscope has failed The system should be serviced FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63W has failed FAILED PATH An autopilot servo data path has failed A data path connected to an autopilot servo has failed Only available if Garmin AFCS is installed SVT SVT DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVT SVT DISABLED Terrain DB resolution too low Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER message Message criteria entered by the user CHECK CRS Database course for LOC1 LOC ID is CRS Selected course for LOC1 differs from published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS Selected course for LOC2 differs from published localizer course by more than 10 degrees PFD1 or MFD1 CARD 1 REM Card 1 was removed Reinsert card The SD card was removed from the top card slot of the PFD or MFD The SD card needs to be reinserted PFD1 or MFD1 CARD 2 REM Card 2 was removed Reinsert card The SD card was removed from the
127. th ChartView 3 Press the GO BACK Softkey to return to the previous page View Charts from the Active Flight Plan Page 1 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 37 saunpar0dd Buruuejd AeN Sd5 S24V olpnyyuqax sia siu u nnsul nubi Tu102 AEN UTE eouepioAy paezey s m e q jeuonippy xipueddy suelv uoneiedo junuuy Jeuuouqy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional beatur GARMIN 3 4 Press the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected Press the GO BACK Softkey to return to the previous page Change Day Night View 1 2 3 4 5 6 7 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between
128. 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 4 Strike is between 6 and 60 seconds old m Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old owe 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 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 43 AEN Sd5 S24V oipny duadx 99 s u u nnsul u102 AEN bila buluueld ni e uepioAy s mp oold paezey Sue v uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy 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 44 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 Naviga
129. 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 Select 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 02 Rev A 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 Tum 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 de
130. tion 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 that 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 vievving area Press the CLEAR Softkey to remove all Stormscope lightning data from the display Garmin 6950 Cockpit Reference Guide
131. tkey A vertical slice of the selected area is now displayed Move the Joystick right or left to move the scanned slice a few degrees right or left Turn the Joystick to adjust the range 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 1 2 3 4 52 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 Press the GAIN Softkey to activate the cursor in the GAIN field 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 position Press the FMS Knob to remove the cursor Press the GAIN Softkey again to recalibrate the gain CALIBRATED is displayed in the GAIN field Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN Ground Mapping 1 Press the MODE 2 Press the GROUND Softkey to place the radar in Ground Map Mode Hazard Avoidance Softkey 3 Press the BACK Softkey Sector Scan 1 While in the Horizontal Scan Mode move the Joystick right or left to place the Bearing Lin
132. tkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts it may be necessary to carry another source of charts on board the aircraft SafeTaxi SafeTaxi 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 36 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A GARMIN Additional Features position in relation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis
133. 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 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 deleted 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 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 sual uonesado s n e 4 aoueplony s mp oold Buruue d AEN Sd5 yi olpnyygqax sia sjueumansu unuuy jeuuouqy jeuonippy paezey bil U105 AEN ubi xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN ELECTRONIC CHECKLISTS IF INSTALLED The system accesses the checklists from an SD car
134. tus Page Press the Display Database Selection Softkey to show database information for each display MFD1 DB or PFD1 DB Verify the correct database cycle information is shown for each database for each display Updating Terrain FliteCharts and ChartView Databases 1 With system power OFF remove the Supplemental Data Card from the bottom card slot of the MFD and PFD 2 Copy the updated terrain database to both Supplemental Data Cards Copy the updated FliteCharts or ChartView database to one Supplemental Data Card 3 Insert the updated Supplemental Data Cards into the bottom card slot of the MFD and PFD The Supplemental Data Card containing the FliteCharts or ChartView database is inserted in the MFD 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 s n e 4 aoueplony 2 Duruue d AEN Sd5 52 oipny uddx sia sjuauimasu jeuonippy 2 Wil Tuo2 NeN ui uoneiedo Jeuuouqy sue v unuuy Annun Abnormal Additional Hazard Flight Nav Com Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Index Appendix A Appendix CCUG ARMIN 4 5 6 7 8 9 Apply power to the system check that the databases are initialized and displayed on the power up screen A Verifying message may be seen If this message is present wait for the system to finish loading before proceeding to step
135. uouqy Sue v unuuy Feed Flight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index Appendix MFD SOFTKEY MAP enone we CCC _ A GARMIN optional optional SHW CHRT CHKLIST Press the BACK Softkey on this level to return to the top softkey level y ENGINE SYSTEM FUEL BACK XT Kw Press the BACK Softkey on this level to return to the top softkey level TRAFFIC PROFILE TOPO TERRAIN ES ES AIRWAYS l l 5x 1 AIRWY ON AIRWY LO AIRWAY HI Press the BACK Softkey on ENGINE FUEL DEC FUEL INC FUEL RsT FUEL ENGINE 08 SYSTEM FUEL TRAFFIC PROFILE BACK 4 this level to return to the top ES ES wz A softkey level MFD Softkeys DEC FUEL INC FUEL RST FUEL BACK Displays the LEAN and SYSTEM softkeys Displays oil oxygen and electrical Displays fuel system details and softkeys Press to decrease fuel quantity in l gallon increments Press to increase fuel quantity in l gallon increments Press to reset to full fuel Press to return to the top level softkeys Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays removes Profile View on Navigat
136. y GPS information The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced AHRS1 GPS AHRS1 not receiving backup GPS information The 1 AHRS is not receiving backup GPS nformation The system should be serviced AHRS1 GPS AHRS1 operating exdusively in no GPS mode he 1 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS and 2 AHRS magnetic model database versions do not match 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 software installed The System should be serviced 84 Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN GMU 44 MESSAGE ADVISORIES Annunciations 8 Alerts Message Comments HDG FAULT AHRS1 magnetometer fault has occurred A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced
137. y to any interrogations e ON Selects Mode A transponder replies to interrogations AIT Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations 96 Garmin 6950 Cockpit Reference Guide for the Pilatus PC 6 190 00851 02 Rev A A GARMIN GND VFR CODE IDENT 0 7 BKSP IDENT ADS B TX TMR REF NRST ALERTS Appendix 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 Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Use numbers to enter code Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Activates deactivates transmission of the aircrafts three dimensional position and aircraft heading for reception by ADS B systems Displays Timer References Window Displays Nearest Airports Window Displays Alerts Window 97 190 00851 02 Rev A Garmin G950 Cockpit Reference Guide for the Pilatus PC 6 sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 S24JV oipny uddx sia sjuauimasu jeuonippy piezeg nubi Tulo2 NeN Yid uoneiedo Jeu

Garmin Pilatus PC_6 Cockpit Reference Guide

Contents

Download Pdf Manuals

Related Search

Related Contents