Garmin G500 Instructions Manual Download Page 292

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AFMS, GARMIN G500/G600 SYSTEM

190-00601-01 Rev. L

FAA APPROVED

Page 10 of 52

TABLE OF CONTENTS

SECTION 1. GENERAL ................................................................................. 12

1.1

G500/G600

RIMARY

LIGHT

ULTI

-F

UNCTION

ISPLAY

YSTEM

.. 12

1.2

YSTEM

OWER

OURCES

................................................................... 13

1.3

AVIGATION

OURCES

........................................................................ 13

1.4

YNTHETIC

ISION

ECHNOLOGY

(SVT) ............................................ 14

1.5

UTOPILOT

NTERFACE

....................................................................... 15

1.6

UDIO

ANEL

...................................................................................... 16

1.7

RAFFIC

ISPLAY

................................................................................ 16

1.8

EATHER

ATA

................................................................................. 16

1.9

IDEO

ISPLAY

................................................................................... 16

1.10

ADAR

LTIMETER

............................................................................. 16

1.11

IGH

PEED

ATA

NTERFACE

.................................................... 17

1.12

INGLE

G500/G600

PERATIONAL

LOCK

IAGRAM

......................... 18

1.13

UAL

G500/G600

PERATIONAL

LOCK

IAGRAM

........................... 19

1.14

EFINITIONS

........................................................................................ 20

SECTION 2. LIMITATIONS ......................................................................... 21

2.1

OCKPIT

EFERENCE

ILOT

’

UIDE

.............................................. 21

2.2

YSTEM

OFTWARE

EQUIREMENTS

................................................... 21

2.3

OVING

...................................................................................... 21

2.4

ATABASE

ARDS

.............................................................................. 21

2.5

ADAHRS

AND

AHRS

PERATIONAL

REA

....................................... 21

2.6

AGNETIC

ARIATION

PERATIONAL

REA

...................................... 22

2.7

AVIGATION

NGLE

........................................................................... 22

2.8

ADAHRS

AND

AHRS

ORMAL

PERATING

ODE

........................... 22

2.9

IRSPEED

IMITATIONS AND

NDICATOR

ARKINGS

.......................... 22

2.10

EROBATIC

ANEUVERS

.................................................................... 23

2.11

OURSE

OINTER

UTO

LEWING

....................................................... 23

2.12

YNTHETIC

ISION

ECHNOLOGY

....................................................... 23

2.13

UTOPILOT

NTERFACE

....................................................................... 23

2.14

ERRAIN

ROXIMITY

UNCTION

......................................................... 23

2.15

TAWS

UNCTION

[GDU

620

NITS WITH INTERNAL

TAWS] ............ 24

2.16

ATALINKED

EATHER

ISPLAY

(XM,

GFDS,

FIS-B

WEATHER

) ...... 24

2.17

RAFFIC

ISPLAY

................................................................................ 24

2.18

CTIVE

EATHER

RADAR ................................................................ 25

2.19

TORM

COPE

ISPLAY

..................................................................... 25

2.20

INDS OF

PERATIONS

........................................................................ 26

2.21

KFC

275/325

LTITUDE

RESELECT

.................................................. 26

2.22

YPE

ATINGS

.................................................................................... 26

2.23

LECTRONIC

TANDBY

NSTRUMENT

OWER

..................................... 27

2.24

LECTRONIC

LIGHT

(EFB)

PPLICATIONS

................................. 27

2.25

URFACE

PERATIONS

........................................................................ 27

2.26

MFD

IDEO

ISPLAY

......................................................................... 27

Summary of Contents for G500

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Page 268: ...maintenance instructions Added new special inspection requirements G 03 21 11 Update referenced IM Specify overbraid bonding strap foil corrosion inspections periodic bonding test Clarify TVS test Fo...

Page 269: ...ation 3 2 4 Servicing Information 4 2 5 Periodic Maintenance Instructions 5 2 6 Troubleshooting Information 7 2 7 Removal and Replacement Information 8 2 8 Diagrams 8 2 9 Special Inspection Requiremen...

Page 270: ......

Page 271: ...M Reduced Vertical Separation Minima 14 STC Supplemental Type Certificate 15 TSO Technical Standard Order 16 TVS Transient Voltage Suppressor 2 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 2 1 Introductio...

Page 272: ...FD AHRS and ADC circuit breakers are suffixed with the numbers 1 and 2 i e PFD 1 and PFD 2 If an LRU is optionally powered from multiple circuit breakers then the circuit breakers will be suffixed wit...

Page 273: ...the unit overnight approx 15 hours at the rated voltage 2 Float Charging Disconnect the battery or batteries from the indicator or module Connect the battery or batteries to a constant voltage source...

Page 274: ...led may have a TVS located at the indicator and or at the power bus See G500 G600 AML STC Installation Manual Table K 2 to help locate TVS installations These components must be tested every 24 calend...

Page 275: ...tery may be permanently damaged if it is left in a discharged state Recharge a discharged battery as soon as possible and maintain with a float charge for maximum battery life Within the preceding 12...

Page 276: ...and performance requirements The encoding altimeter must be checked as specified in the Socata Maintenance Manual section 05 10 01 ATA 34 The RVSM critical areas must be inspected as specified in Soca...

Page 277: ...d verify ADC 1 ADC 2 switch is operating normally as specified in the G500 G600 AML STC Installation Manual section P 3 1 Refer to the manufacturer s instructions for additional calibration and return...

Page 278: ...If the Mid Continent Standby Attitude Indicator if installed has not been operated for more than 3 months charge each battery pack using one of the methods described in section 2 4 2 10 Application o...

Page 279: ...espond to questions regarding this ICA In addition the customer may refer questions regarding this equipment and its installation to the manufacturer Garmin Garmin customer assistance may be contacted...

Page 280: ...for grounding Description of Location GDU 620 1 Yes N A GSU 75 B 1 Yes No Yes No GRS 77 1 Yes No Yes No GDC 74 1 Yes No Yes No GMU 44 1 Yes N A GTP 59 1 Yes N A GAD 43 43e Yes No Yes No MCI 4300 4 Ye...

Page 281: ...601 00 Rev M Instructions for Continued Airworthiness Page 12 of 13 3 3 Wire Routing Single Engine The following diagram depicts the wire routing for the G500 G600 LRUs throughout the aircraft structu...

Page 282: ...00601 00 Rev M Instructions for Continued Airworthiness Page 13 of 13 3 4 Wire Routing Twin Engine The following diagram depicts the wire routing for the G500 G600 LRUs throughout the aircraft structu...

Page 283: ......

Page 284: ...01 Rev L FAA APPROVED Page 2 of 52 LOG OF REVISIONS Rev Page Description FAA Approval A All Complete Supplement Seyed Joussef Hashemi Manager Flight Test Branch ANM 160L FAA Los Angeles ACO Transport...

Page 285: ...ded AHRS operational area in section 2 4 Added section 2 5 16 Added section 2 6 17 Added section 2 10 18 Added section 2 13 Updated section 2 14 to account for SVT 19 Added section 2 17 Updated sectio...

Page 286: ...section 2 8 Robert Grove ODA STC Unit Administrator GARMIN International Inc ODA 240087 CE Date September 15 2009 D 11 12 16 Remove requirement for standby ADI for VFR operations installations Add ma...

Page 287: ...ter databases and SD card usage with GSR 56 datalink Added information on airport directory database 14 Updated section 2 8 to reflect current airspeed tape behavior 16 Updated sections 2 14 2 15 and...

Page 288: ...erted new section 2 3 for moving map limitations 20 21 Moved rate of turn failure description from section 3 3 1 to section 3 3 2 25 Added checkbox for disabled altitude alerter in section 4 4 G All R...

Page 289: ...tions in section 2 4 Clarified applicability of section 2 11 Updated autopilot interface information in section 2 13 Added limitation for KFC 275 325 interface in section 2 21 Added Type Ratings limit...

Page 290: ...1 Moved Traffic and Weather Systems to separate sections 1 7 and 1 8 Updated software versions in section 2 2 Moved sections 2 4 DB Card and 2 11 Elec Stby to section 7 Added TAWS Annun from Garmin Na...

Page 291: ...01 Rev L FAA APPROVED Page 9 of 52 Added check box for GAD 43 function to section 4 6 Added description of GDU control capabilities for GWX weather radars to section 7 9 Edited information about obsta...

Page 292: ...REQUIREMENTS 21 2 3 MOVING MAP 21 2 4 DATABASE CARDS 21 2 5 ADAHRS AND AHRS OPERATIONAL AREA 21 2 6 MAGNETIC VARIATION OPERATIONAL AREA 22 2 7 NAVIGATION ANGLE 22 2 8 ADAHRS AND AHRS NORMAL OPERATING...

Page 293: ...ND 4300 SERIES 39 4 5 SYNTHETIC VISION TECHNOLOGY 39 4 6 AUTOPILOT OPERATIONS WITH THE G500 G600 SYSTEM 40 4 7 TAWS 46 4 8 RADAR ALTIMETER 46 SECTION 5 PERFORMANCE 47 SECTION 6 WEIGHT AND BALANCE 47 S...

Page 294: ...dio panels video sources radar altimeters ADF receivers DME receivers and autopilots The G500 G600 system can optionally provide Terrain Alerting functions and display of Terminal Procedures The prima...

Page 295: ...stem GSU 75 B AHRS Attitude and Heading Reference System GRS 77 ADC Air Data Computer GDC 74A B GAD Garmin Adapter GAD 43 43e STBY ATT Electric Standby Attitude Indicator Except L 3 Trilogy and Mid Co...

Page 296: ...affic surrounding the aircraft A typical SVT display is shown below SVT provides additional features on the G500 G600 primary flight display PFD which display the following information Synthetic Terra...

Page 297: ...ended to aid the pilot awareness of the terrain and obstacles in front of the airplane It may not provide either the accuracy or fidelity or both on which to solely base decisions and plan maneuvers t...

Page 298: ...f weather data include the Garmin GDL 69 A and GDL 69 A SXM Sirius XM receivers Garmin GSR 56 Iridium Transceiver Garmin GDL 88 ADS B transceiver and GTX 345 Transponder If one of these optional weath...

Page 299: ...be passed through intermediate hub units Interfaced equipment that uses HSDB includes the GTN 6XX 7XX navigators GDL 69 series datalink receivers GDL 88 ADS B transceiver GWX 68 70 R weather radars G...

Page 300: ...ate standby instruments approved under this STC refer to Sections 2 5 2 and 3 2 2 or Electronic Standby Instruments System ESIS shown to be compatible with this STC This STC does not approve the ESIS...

Page 301: ...e optional 4 Video Source optional 5 Video Source optional 5 ARINC 708 WXR Only GAD 43e only analog nav receiver altitude preselect analog radar altimeter DME ADF Marker Beacon Only if GDU 1 is not co...

Page 302: ...quipment FD Flight Director FPM Flight Path Marker GDU Garmin Display Unit GPS Global Positioning System GPSS GPS Roll Steering HDG Heading HSI Horizontal Situation Indicator IFR Instrument Flight Rul...

Page 303: ...orrectness against the PFD HSI published charts or other approved sources of navigation information 2 4 Database Cards The SD database card must not be removed or inserted during flight and or while t...

Page 304: ...S is not receiving GPS or Air Data Note In dual GPS installations only one GPS needs to be available to the ADAHRS or AHRS for IFR flight 2 9 Airspeed Limitations and Indicator Markings The original t...

Page 305: ...nfirm the inbound course pointer is set to the proper course prior to initiating any transition on any VHF NAV approach 2 12 Synthetic Vision Technology The use of the synthetic vision display element...

Page 306: ...inked Weather Display XM GFDS FIS B weather This limitation applies to datalinked weather products from SiriusXM via a GDL 69 69A FIS B via a Garmin ADS B receiver and Connext via a GSR 56 Do not use...

Page 307: ...microwave radiation and improper use or exposure may cause serious bodily injury DO NOT OPERATE THE RADAR EQUIPMENT UNTIL YOU HAVE READ AND CAREFULLY FOLLOWED THE SAFETY PRECAUTIONS AND INSTRUCTIONS...

Page 308: ...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 aircraft shall have one source of altitude and airs...

Page 309: ...em for EFB applications such as the moving map or electronic charts is not authorized if additional evaluation or operational approval is required unless that approval has been obtained 2 25 Surface O...

Page 310: ...ged 4 Verify autopilot mode and cross check against standby flight and navigation data 3 1 2 ADAHRS Failure Failure of a combined Air Data Attitude and Heading Reference System ADAHRS may result in ei...

Page 311: ...the aircraft 3 1 6 Loss of Electrical Power to 3 inch Electric Standby Attitude Indicator flashing amber STBY PWR light MidContinent 4300 Series When a 3 inch electric standby attitude indicator is in...

Page 312: ...teadily illuminated 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...

Page 313: ...le of climb airspeed VX After warning ceases 3 Climb and maintain safe altitude 4 Advise ATC of altitude deviation if appropriate NOTE Only vertical maneuvers are recommended unless either operating i...

Page 314: ...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 d...

Page 315: ...may be indicated by any or all of following Loss of course deviation information on HSI Loss of glideslope glidepath information on PFD Loss of bearing pointer on HSI 1 Select alternate navigation so...

Page 316: ...on TAWS Cautions include an amber or or annunciator on the PFD and one of the following aural messages Terrain Ahead or Caution Terrain Obstacle Ahead or Caution Obstacle Wire Ahead or Caution Wire To...

Page 317: ...a red X over the attitude area AIRSPEED FAIL Use Standby Airspeed Display system is not receiving airspeed input from the ADAHRS or ADC accompanied by a red X through the airspeed display ALTITUDE FA...

Page 318: ...itch as AHRS Aligns OK to taxi Attitude and Heading Reference System is aligning ADAHRS or AHRS may not align with excessive pitch bank angles AHRS ALIGN Remain Stationary Note Only appears with GSU 7...

Page 319: ...that data from the interfaced sensor is not available Loss of connection or failure of interfaced sensor 3 3 3 Advisories White Annunciation Pilot Action Various Alert Messages may appear under the M...

Page 320: ...signing 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 it is not rotated for a period of 10 se...

Page 321: ...e the Garmin G500 G600 Cockpit Reference Guide for a complete description and the usage of synchronization in dual installations 4 4 Electric Standby Attitude Gyro Mid Continent 4200 and 4300 Series W...

Page 322: ...bled 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 altitude preselector GAD...

Page 323: ...g If the bug is turned more than 180 degrees the autopilot may turn the airplane in the opposite direction of the desired turn 4 6 4 GPSS emulated via HDG mode For autopilots that do not support digit...

Page 324: ...GPS the annunciated GPSS text will be yellow and a zero turn command will be sent to the autopilot 4 6 5 Roll Steering capable autopilots If the autopilot is already designed to receive Roll Steering...

Page 325: ...ure ALT is displayed in white text in the upper right corner of the PFD When altitude capture mode is active ALTC is displayed in green text in the upper right corner of the PFD When a KA 315 annuncia...

Page 326: ...reduced automatically Manually changing the selected vertical speed while AUTO is displayed will cancel automatic vertical speed reduction 4 6 7 2 Bendix King Autopilots To select and maintain a verti...

Page 327: ...llowed by the G500 G600 the command bars will be displayed at the maximum distance allowed by the G500 G600 As the aircraft pitch changes to satisfy the command bars the bars will continue to be displ...

Page 328: ...er than 1 second will prevent the test from running and the AP TEST key will remain displayed Do not engage the autopilot if advisory AC Reference Lost or Reference Timeout Fault is present 4 6 10 Dua...

Page 329: ...AFMS GARMIN G500 G600 SYSTEM 190 00601 01 Rev L FAA APPROVED Page 47 of 52 Section 5 PERFORMANCE No change Section 6 WEIGHT AND BALANCE See current weight and balance data...

Page 330: ...d periodically have no expiration date and provide worldwide coverage The obstacle database contains data for obstacles and wires that pose a potential hazard to aircraft Obstacles 200 feet and higher...

Page 331: ...ained A poorly maintained battery will suffer accelerated degradation Extended storage in a discharged state and over charging will permanently damage the battery Complete charging is required to brin...

Page 332: ...ations are not relative to the terrain displayed on the MFD or the yellow red terrain shading of the Synthetic Vision displayed on the PFD of the G500 G600 system Refer to the Garmin navigator Airplan...

Page 333: ...be getting closer to your aircraft independent of the direction the target is pointed A green relative motion vector pointed towards your ownship indicates that the traffic target is converging on you...

Page 334: ...les at zoom scales of 10 nautical miles or less and depict wire obstacles at zoom scales of 5 nautical miles or less The obstacle or wire overlay icon will be shown near the bottom of the display when...

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