Страница 1: ......
Страница 2: ...rator GARMIN International INC ODA 240087 CE Date 07 30 2010 4 None Rerelease document Robert Grove ODA STC Unit Administrator GARMIN International INC ODA 240087 CE Date 08 24 2010 5 All Changed GPS...
Страница 3: ...e alerter configuration 29 Added detail to section 4 6 regarding GAD 43 interface Corrected description of autopilot interfaces in section 4 6 1 31 Corrected altitude alerter description in section 4...
Страница 4: ...l Re issue complete supplement Robert Grove ODA STC Unit Administrator GARMIN International Inc ODA 240087 CE Date 08 18 2011 Revised section 2 14 limitation on GPS SBAS vertical coupling Added attitu...
Страница 5: ...section 2 4 Clarified applicability of section 2 11 Updated autopilot interface information in section 2 14 Revised external TAWS annunciation information in section 2 16 Added limitation for KFC 275...
Страница 6: ...r Page Number Description FAA Approval 9 All Re issue complete supplement See Page 1 Corrected navigation radio information in Section 1 1 Updated applicable system software in Section 2 2 Corrected A...
Страница 7: ...ON OPERATIONAL AREA 17 2 7 NAVIGATION ANGLE 18 2 8 AHRS NORMAL OPERATING MODE 18 2 9 AIRSPEED LIMITATIONS AND INDICATOR MARKINGS 18 2 10 AEROBATIC MANEUVERS 18 2 11 ELECTRIC STANDBY ATTITUDE GYRO 18 2...
Страница 8: ...VED Page 8 of 40 4 3 ALTITUDE SYNCHRONIZATION 33 4 4 ELECTRIC STANDBY ATTITUDE GYRO 33 4 5 SYNTHETIC VISION TECHNOLOGY 33 4 6 AUTOPILOT OPERATIONS WITH THE G500 SYSTEM 34 SECTION 5 PERFORMANCE 40 SECT...
Страница 9: ...e included in the pilot s normal instrument scan and may be referenced if the PFD data is in question A second G500 system installed on the co pilot s side does not require additional standby instrume...
Страница 10: ...and the PFD attitude display will still be presented see Paragraph 2 8 The G500 HSI can be selected to display course deviation information from up to four independent sources two GPS and two VHF NAV...
Страница 11: ...ay indicating the position of nearby airports that are in the G500 database Runway Highlight a highlighted presentation of the location and orientation of the runway s at the destination airport The s...
Страница 12: ...various airborne weather radars is optionally available on the MFD The G500 supports Garmin GWX weather radar as well as certain 3rd party weather radars 1 8 Video sources The G500 Avionics Display Sy...
Страница 13: ...cted if SVT is enabled Installation of a Mid Continent electric standby attitude indicator is approved by this STC Air Data Computer AHRS Magnetometer GMU 44 GRS 77 GDC 74 Temperature Probe GTP 59 No...
Страница 14: ...e GTP 59 2 No 2 GPS SBAS Navigator required No 2 VOR Localizer GS optional Adapter optional GAD 43 43e to Aircraft Systems optional Existing Equipment already installed in aircraft Standby Attitude Ma...
Страница 15: ...splay Unit GPS Global Positioning System GPSS GPS Roll Steering HDG Heading HSI Horizontal Situation Indicator IFR Instrument Flight Rules IMC Instrument Meteorological Conditions LOI Loss of Integrit...
Страница 16: ...ss against the PFD HSI published charts or other approved sources of navigation information 2 4 Database Cards Databases identified as intended for helicopter use must not be used These databases may...
Страница 17: ...charts database contains procedure charts for the coverage area purchased An own ship position icon will be displayed on these charts This database is updated on a 14 day cycle If not updated within 7...
Страница 18: ...ximum allowable airspeed display is configured to indicate the appropriate maximum allowable airspeed for the airplane including variations for altitude or Mach number The G500 airspeed tape displays...
Страница 19: ...und course pointer prior to initiating any transition on any VHF NAV approach Auto slewing the VHF NAV course pointer to the correct selected course is a database dependent function 2 13 Synthetic Vis...
Страница 20: ...ted TAWS The required TAWS annunciations appear in the upper right of the PFD These annunciations include PULL UP red TERRAIN yellow TERR N A white TERR INHB white These annunciations are not relative...
Страница 21: ...all safety precautions including Do not operate in the vicinity of refueling operations Do not operate while personnel are in the vicinity approximately 20 feet of the radar sweep area WARNING If a r...
Страница 22: ...r ADC 1 or 2 1a 1 Magnetometer GMU 1 or 2 1 Standby Attitude Indicator 1 1 Standby Airspeed Indicator 1 1b 1 Standby Altimeter 1 1b 1 Magnetic Compass 1 1 1 For VFR operations under 14 CFR Part 91 the...
Страница 23: ...he system for EFB applications such as the moving map or electronic charts may require additional evaluation or operational approval 2 24 Surface Operations Do not use SafeTaxi or Chartview functions...
Страница 24: ...fer directly to navigation source for navigation information such as GPS If autopilot is engaged 3 Verify autopilot mode and cross check against standby flight and navigation data 3 1 2 AHRS Failure A...
Страница 25: ...ents to fly the aircraft 3 1 5 Loss of Electrical Power to 3 inch Electric Standby Attitude Indicator flashing amber STBY PWR light When a 3 inch electric standby attitude indicator is installed loss...
Страница 26: ...uminated 3 Verify that the red gyro warning flag is not displayed 4 Seek visual meteorological conditions VMC or land as soon as practical operation of standby attitude indicator is limited by battery...
Страница 27: ...instead of magnetic heading If GPS track is not available 1 Use standby compass for heading reference 2 Verify selected course using CRS button and PFD knob CAUTION No directional references will be...
Страница 28: ...ing CDI 1 2 or BRG softkeys on PFD or refer directly to external navigation data 3 2 4 Synthetic Vision SVT Failure Several data sources are required to display SVT on the PFD GPS terrain database att...
Страница 29: ...r the attitude area AIRSPEED FAIL Use Standby Airspeed Display system is not receiving airspeed input from the air data computer accompanied by a red X through the airspeed display ALTITUDE FAIL Use S...
Страница 30: ...ence detected between displayed attitude airspeed or altitude dual installations only AHRS ALIGN Keep Wings Level Limit aircraft attitude to 10 bank and 5 pitch as AHRS Aligns OK to taxi Attitude and...
Страница 31: ...sories White Annunciation Pilot Action Various Alert Messages may appear under the MFD ALERTS soft key View and understand all advisory messages Typically they indicate communication issues within the...
Страница 32: ...the knob is providing a HDG function Assigning the function of the knob is done by pressing releasing one of the dedicated function buttons to the left of the display The knob defaults back to HDG if...
Страница 33: ...the pilot Reference the Garmin G500 Cockpit Reference Guide for a complete description and the usage of synchronization in dual installations 4 4 Electric Standby Attitude Gyro When an electric stand...
Страница 34: ...Synthetic Vision enabled A GAD 43 Adapter is installed in this aircraft GAD 43 provides attitude to the autopilot GAD 43 provides yaw rate to the yaw damper GAD 43 provides baro correction to the alt...
Страница 35: ...he bug is turned more then 180 degrees the autopilot may turn the airplane in the opposite direction of the desired turn 4 6 4 Roll Steering emulated via HDG mode For autopilots that do not support di...
Страница 36: ...ror signal to the autopilot When the autopilot is operated in HDG mode the autopilot will fly the turn commands from the GPS navigator selected on PFD 1 If the GPSS data is invalid for example if ther...
Страница 37: ...elected altitude bug while ALT SEL mode is selected may result in autopilot mode changes Verify the autopilot mode after changing the selected altitude 4 6 6 3 Bendix King Autopilots To preselect and...
Страница 38: ...appear in the vertical speed PFD knob mode indicator when vertical speed is being reduced automatically Manually changing the selected vertical speed while AUTO is displayed will cancel automatic ver...
Страница 39: ...ce allowed by the G500 the command bars will be displayed at the maximum distance allowed by the G500 As the aircraft pitch changes to satisfy the command bars the bars will continue to be displayed a...
Страница 40: ...opilot disconnects CAUTION Do not use the autopilot if the AP TEST key fails to disengage the autopilot normally NOTE Pressing and holding the AP TEST key for longer than 1 second will prevent the tes...
