Garmin Cessna Caravan G1000 User manual
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190-00716-01 May 2012 Revision 1
G1000 / GFC 700
System Maintenance Manual
Hawker Beechcraft
Model 300/B300 Series King Air
Contains Instructions
For Continued Airworthiness
For STC SA01535WI-D
This page intentionally left blank.
Page A G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 1 190-00716-01
© Copyright 2012
Garmin Ltd. or its subsidiaries
All Rights Reserved
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted,
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written consent of Garmin. Garmin hereby grants permission to download a single copy of this manual
and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed and
to print one copy of this manual or of any revision hereto, 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.
Garmin International, Inc.
1200 E. 151st Street
Olathe, KS 66062 USA
Telephone: 913-397-8200
www.garmin.com
Garmin (Europe) Ltd.
Liberty House
Bulls Copse Road
Hounsdown Business Park
Southampton, SO40 9RB, UK
Phone: +44 (0) 23 8052 4000
Fax: +44 (0) 23 8052 4004
RECORD OF REVISIONS
Revision Revision Date Description ECO #
1 5/11/12 Initial release ------
DOCUMENT PAGINATION
Section Pagination
Table of Contents i – vi
Section 1 1-1 – 1-6
Section 2 2-1 – 2-18
Section 3 3-1 – 3-52
Section 4 4-1 – 4-34
Section 5 5-1 – 5-88
Section 6 6-1 – 6-20
Section 7 7-1 – 7-58
Section 8 8-1 – 8-16
Page B G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 1 190-00716-01
INFORMATION SUBJECT TO EXPORT CONTROL LAWS
This document may contain information which is subject to the Export Administration Regulations
(“EAR”) issued by the United States Department of Commerce (15 CFR, Chapter VII Subchapter C) and
which may not be exported, released or disclosed to foreign nationals inside or outside the United States
without first obtaining an export license. The preceding statement is required to be included on any and
all reproductions in whole or in part of this manual.
This product, its packaging, and its components contain chemicals known to the State of California to
cause cancer, birth defects, or reproductive harm. This Notice is being provided in accordance with
California's Proposition 65. If you have any questions or would like additional information, please refer
to our web site at www.garmin.com/prop65.
The GDU lens is coated with a special anti-reflective coating that is very sensitive to skin oils, waxes and
abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE
COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens
cleaner that is specified as safe for anti-reflective coatings.
All G1000 screen shots used in this document are current at the time of publication. Screen shots are
intended to provide visual reference only. All information depicted in screen shots, including software
file names, versions and part numbers, is subject to change and may not be up to date.
CAUTION
WARNING
IMPORTANT
G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air Page i
190-00716-01 Revision 1
TABLE OF CONTENTS
SECTION PAGE
1INTRODUCTION ............................................................................................................................1-1
1.1CONTENT,SCOPE,PURPOSE ........................................................................................................1-1
1.2ORGANIZATION............................................................................................................................1-3
1.3DEFINITIONS/ABBREVIATIONS ....................................................................................................1-4
1.4PUBLICATIONS .............................................................................................................................1-5
1.5REVISON AND DISTRIBUTION ......................................................................................................1-6
2SYSTEM DESCRIPTION ...............................................................................................................2-1
2.1EQUIPMENT DESCRIPTIONS .........................................................................................................2-1
2.2G1000 OPTIONAL INTERFACES..................................................................................................2-12
2.3ELECTRICAL POWER DISTRIBUTION..........................................................................................2-13
2.4PITOT/STATIC SYSTEM ..............................................................................................................2-16
2.5SHIELD BLOCK GROUNDS .........................................................................................................2-17
2.6G1000 /GFC700 BLOCK DIAGRAM ...........................................................................................2-17
3G1000 CONTROL & OPERATION...............................................................................................3-1
3.1GDU 1040A AND GDU 1500 DISPLAYS......................................................................................3-1
3.2GCU 477 -MFD CONTROLLER ...................................................................................................3-3
3.3GMC 710 -AFCS CONTROLS......................................................................................................3-3
3.4GMA 1347D AUDIO PANEL ........................................................................................................3-4
3.5G1000 NORMAL MODE................................................................................................................3-5
3.6REVERSIONARY MODE ................................................................................................................3-6
3.7CONFIGURATION MODE OVERVIEW ............................................................................................3-7
3.8G1000 /GFC 700 SOFTWARE INFORMATION ............................................................................3-11
3.9G1000 SOFTWARE/CONFIGURATION PROCEDURE ....................................................................3-18
3.10TAWS-A SUPPORT CONFIGURATION ....................................................................................3-24
3.11TAWS-A VOICE NO CALLOUT OPTION CONFIGURATION.....................................................3-25
3.12TAWS-A VOICE CALLOUT OPTION CONFIGURATION...........................................................3-26
3.13ADF OPTION CONFIGURATION ..............................................................................................3-27
3.14DME OPTION CONFIGURATION .............................................................................................3-28
3.15RAD ALT OPTION CONFIGURATION .....................................................................................3-29
3.16TCAS II TRAFFIC SYSTEM OPTION CONFIGURATION............................................................3-30
3.17TAS/TCAS ITRAFFIC SYSTEM OPTION CONFIGURATION ....................................................3-31
3.18GTS 8XX TAS/TCAS1 TRAFFIC SYSTEM CONFIGURATION.................................................3-32
3.19LIGHTNING SYSTEM OPTION CONFIGURATION .....................................................................3-33
3.20LIGHTNING SYSTEM OPTION CONFIGURATION LOAD CONFIRMATION.................................3-34
3.21GTX 33/33D CONFIGURATION ..............................................................................................3-35
3.22ESP SUPPORT OPTION CONFIGURATION................................................................................3-36
3.23GDL 59 WI-FI DATA LINK OPTION CONFIGURATION ...........................................................3-37
3.24GSR 56 SATELLITE RECIEVER OPTION CONFIGURATION......................................................3-38
3.25POTS HANDSET CONFIGURATION .........................................................................................3-38
3.26FLIGHT DATA RECORDER OPTION CONFIGURATION.............................................................3-39
3.27FLITECHARTS CONFIGURATION.............................................................................................3-41
3.28CHARTVIEW ENABLE.............................................................................................................3-41
3.29TAWS-B ENABLE ..................................................................................................................3-42
3.30TAWS-A ENABLE..................................................................................................................3-43
3.31SUPPLEMENTAL DATABASE LOADING...................................................................................3-44
3.32SVS/PATHWAYS ENABLE ......................................................................................................3-45
3.33ESP ENABLE ..........................................................................................................................3-46
3.34AIRCRAFT REGISTRATION NUMBER ENTRY ..........................................................................3-47
Page ii G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 1 190-00716-01
3.35GDL 69 ALTERNATE ANTENNA LOCATION CONFIGURATION...............................................3-48
3.36SPLASH SCREEN LOADING .....................................................................................................3-49
3.37NAVIGATION DATABASE LOADING .......................................................................................3-50
3.38CONFIGURATION OF NAVIGATION MAP FOR TRAFFIC SYSTEM.............................................3-52
3.39CLEARING DEFAULT USER SETTINGS....................................................................................3-52
4INSTRUCTIONS FOR CONTINUED AIRWORTHINESS........................................................4-1
4.1AIRWORTHINESS LIMITATIONS ...................................................................................................4-1
4.2SERVICING INFORMATION ...........................................................................................................4-2
4.3MAINTENANCE INTERVALS .........................................................................................................4-4
4.4VISUAL INSPECTION ..................................................................................................................4-10
4.5ELECTRICAL BONDING TEST .....................................................................................................4-15
4.6GRS 77 EARTH MAGNETIC FIELD UPDATES .............................................................................4-18
4.7GSA 80 GREASING PROCEDURE................................................................................................4-18
4.8FLAPS-IN-MOTION DISCRETE INPUT CHECK..............................................................................4-19
4.9GSM 86 SLIP CLUTCH TORQUE CHECK PROCEDURE................................................................4-20
4.10G1000 REDUNDANT CONNECTION CHECK ............................................................................4-22
4.11ENGINE DATA CHECK (GIA 1OR GIA 2INOPERATIVE) ........................................................4-25
4.12TRIM ANNUNCIATOR CHECK .................................................................................................4-25
4.13G1000 MISCOMPARE CHECKS ...............................................................................................4-27
4.14GIA COOLING FANS OPERATIONAL CHECK ..........................................................................4-28
4.15GDU COOLING FANS OPERATIONAL CHECK.........................................................................4-28
4.16STANDBY BATTERY PERIODIC CHECKS.................................................................................4-29
4.17RUDDER BOOST OPERATIONAL CHECK .................................................................................4-32
5TROUBLESHOOTING ...................................................................................................................5-1
5.1G1000 ALERTING SYSTEM ..........................................................................................................5-2
5.2SYSTEM ANNUNCIATIONS ...........................................................................................................5-4
5.3300/B300 SPECIFIC ALERTS ......................................................................................................5-25
5.4TAWS TROUBLESHOOTING.......................................................................................................5-26
5.5SYNTHETIC VISION AND PATHWAYS TROUBLESHOOTING ........................................................5-27
5.6GFC 700 AFCS TROUBLESHOOTING.........................................................................................5-27
5.7BACKUP COMMUNICATIONS PATH CHECKS..............................................................................5-43
5.8GDU 104X TROUBLESHOOTING................................................................................................5-44
5.9GDU 104X ALERTS ...................................................................................................................5-46
5.10GIA 63 TROUBLESHOOTING ..................................................................................................5-54
5.11GIA ALERT MESSAGES ..........................................................................................................5-56
5.12GEA TROUBLESHOOTING ......................................................................................................5-63
5.13GTX TROUBLESHOOTING ......................................................................................................5-64
5.14GDL 69A TROUBLESHOOTING ..............................................................................................5-65
5.15GRS 77/GMU 44 TROUBLESHOOTING...................................................................................5-67
5.16GDC 7400 TROUBLESHOOTING .............................................................................................5-74
5.17GWX 68 TROUBLESHOOTING ................................................................................................5-75
5.18GMC 710 TROUBLESHOOTING ..............................................................................................5-76
5.19GCU 477 TROUBLESHOOTING ...............................................................................................5-77
5.20SOFTWARE/CONFIGURATION TROUBLESHOOTING ................................................................5-78
5.21MATING/BACKPLATE CONNECTORS......................................................................................5-80
5.22STANDBY ATTITUDE INDICATOR TROUBLESHOOTING ..........................................................5-85
5.23STANDBY AIRSPEED INDICATOR TROUBLESHOOTING...........................................................5-85
5.24STANDBY ALTIMETER TROUBLESHOOTING...........................................................................5-86
5.25GDL 59 TROUBLESHOOTING .................................................................................................5-86
5.26GSR 56 TROUBLESHOOTING..................................................................................................5-87
5.27GTS 820/850 TROUBLESHOOTING .........................................................................................5-87
G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air Page iii
190-00716-01 Revision 1
6EQUIPMENT REMOVAL & INSTALLATION..........................................................................6-1
6.1GDU 1040A AND GDU 1500.......................................................................................................6-2
6.2GMA 1347D AUDIO PANEL ........................................................................................................6-2
6.3GIA 63W INTEGRATED AVIONICS UNITS....................................................................................6-3
6.4GEA 71 ENGINE/AIRFRAME UNIT ...............................................................................................6-3
6.5GTX 33( )TRANSPONDER ...........................................................................................................6-4
6.6GDC 7400 AIR DATA COMPUTER ...............................................................................................6-4
6.7GTP 59 OAT PROBE....................................................................................................................6-4
6.8GRS 77 AHRS.............................................................................................................................6-5
6.9GMU 44 MAGNETOMETER ..........................................................................................................6-5
6.10GDL 69A .................................................................................................................................6-5
6.11GSA 80 AND GSA 9000 SERVOS .............................................................................................6-6
6.12GSM 86 AND GSM 9100 SERVO GEARBOX.............................................................................6-2
6.13GCU 477 ..................................................................................................................................6-2
6.14GMC 710 .................................................................................................................................6-3
6.15GWX 68 ...................................................................................................................................6-3
6.16CONFIGURATION MODULE REMOVAL &REPLACEMENT ........................................................6-4
6.17GEA 71 BACKSHELL THERMOCOUPLE REMOVAL &REPLACEMENT......................................6-6
6.18GPS/WAAS ANTENNAS ..........................................................................................................6-7
6.19DIVERSITY TRANSPONDER ANTENNA......................................................................................6-7
6.20IRIDIUM ANTENNA ...................................................................................................................6-8
6.21WI-FI ANTENNA.......................................................................................................................6-8
6.22SIGNAL CONDITIONERS............................................................................................................6-8
6.23INSTRUMENT PANEL SWITCH/ANNUNCIATOR (PROP SYNCH AND STANDBY BATTERY)........6-9
6.24EMERGENCY FREQUENCY SWITCH/ANNUNCIATOR.................................................................6-9
6.25STANDBY BATTERY ...............................................................................................................6-10
6.26STANDBY AIRSPEED INDICATOR............................................................................................6-10
6.27STANDBY ALTIMETER............................................................................................................6-10
6.28STANDBY ATTITUDE INDICATOR ...........................................................................................6-11
6.29GIA COOLING FANS...............................................................................................................6-11
6.30GDU COOLING FANS .............................................................................................................6-12
6.31GTS 8XX TRAFFIC UNIT .......................................................................................................6-12
6.32GPA 65 PA/LNA UNIT ..........................................................................................................6-13
6.33GA 58 TRAFFIC ANTENNAS ...................................................................................................6-13
6.34GDL 59 WI-FI DATALINK......................................................................................................6-13
6.35GSR 56 SATELLITE RECEIVER ...............................................................................................6-14
6.36GSD 41 DATA CONCENTRATOR ............................................................................................6-15
7G1000 EQUIPMENT CONFIGURATION & TESTING.............................................................7-1
7.1GDU 1040A/1500 MFD &PFD ..................................................................................................7-1
7.2GMA 1347D AUDIO PANEL ........................................................................................................7-3
7.3GIA 63W INTEGRATED AVIONICS UNIT......................................................................................7-6
7.4GEA 71 ENGINE/AIRFRAME UNIT ...............................................................................................7-9
7.5GTX 33( )TRANSPONDER .........................................................................................................7-12
7.6GDC 7400 AIR DATA COMPUTER .............................................................................................7-13
7.7GRS 77 AHRS /GMU 44 MAGNETOMETER .............................................................................7-18
7.8GDL 69A XM DATA LINK ........................................................................................................7-26
7.9GSA 80/9000 SERVOS ...............................................................................................................7-26
7.10GCU 477 FMS CONTROLLER ................................................................................................7-27
7.11GMC 710 AFCS CONTROLLER..............................................................................................7-29
7.12GWX 68 WEATHER RADAR ..................................................................................................7-30
7.13GTS 8XX TRAFFIC SYSTEM FUNCTIONAL CHECK ................................................................7-31
7.14NON-GARMIN TRAFFIC SYSTEM (TAS/TCAS I) FUNCTIONAL CHECK .................................7-33
Page iv G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 1 190-00716-01
7.15NON-GARMIN TRAFFIC SYSTEM (TCAS II) FUNCTIONAL CHECK ........................................7-34
7.16LIGHTNING SYSTEM FUNCTIONAL CHECK ............................................................................7-35
7.17TAWS FUNCTIONAL CHECK..................................................................................................7-37
7.18FLITECHARTS FUNCTIONAL CHECK ......................................................................................7-40
7.19CHARTVIEW FUNCTIONAL CHECK ........................................................................................7-41
7.20SAFETAXI FUNCTIONAL CHECK ............................................................................................7-42
7.21DME FUNCTIONAL CHECK ....................................................................................................7-43
7.22ADF FUNCTIONAL CHECK .....................................................................................................7-44
7.23RADIO ALTIMETER CHECK ....................................................................................................7-44
7.24WEIGHT ON WHEELS AND LOW SPEED AWARENESS BAND CHECK......................................7-45
7.25RVSM CHECKS......................................................................................................................7-46
7.26ESP FUNCTIONAL CHECK ......................................................................................................7-52
7.27ACTIVATION OF GARMIN FLIGHT DATA SERVICES ...............................................................7-55
7.28GDL 59 WI-FI DATA LINK FUNCTIONAL CHECK ..................................................................7-57
7.29GSR 56 SATELLITE RECEIVER FUNCTIONAL CHECK.............................................................7-58
8SYSTEM RETURN TO SERVICE PROCEDURE ......................................................................8-1
8.1BACKUP PATH SYSTEM TESTING.................................................................................................8-2
8.2GFC 700 GROUND CHECKOUT ..................................................................................................8-10
8.3MAINTENANCE RECORDS ..........................................................................................................8-15
G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air Page v
190-00716-01 Revision 1
LIST OF ILLUSTRATIONS
FIGURE PAGE
Figure 2-1, Display Units...........................................................................................................................2-1
Figure 2-2, Audio Panel.............................................................................................................................2-2
Figure 2-3, AFCS Controller .....................................................................................................................2-2
Figure 2-4, FMS Controller .......................................................................................................................2-3
Figure 2-5, Transponder.............................................................................................................................2-3
Figure 2-6, GIA unit ..................................................................................................................................2-4
Figure 2-7, GEA unit .................................................................................................................................2-5
Figure 2-8, Air Data Computer..................................................................................................................2-6
Figure 2-9, OAT probe ..............................................................................................................................2-6
Figure 2-10, AHRS ....................................................................................................................................2-7
Figure 2-11, Magnetometer .......................................................................................................................2-7
Figure 2-12, GDL 69A Datalink................................................................................................................2-8
Figure 2-13, GDL 59 Wi-Fi Datalink ........................................................................................................2-8
Figure 2-14, GSR 56 Satellite Receiver.....................................................................................................2-9
Figure 2-15, GSD 41 Data Concentrator ...................................................................................................2-9
Figure 2-16, GTS 8XX Traffic System......................................................................................................2-9
Figure 2-17, Weather Radar.....................................................................................................................2-10
Figure 2-18, GSA 80 / GSM 86 ...............................................................................................................2-10
Figure 2-19, GSA 9000 / GSM 9100 .......................................................................................................2-11
Figure 2-20, 300/B300 Electrical Distribution (Post G1000 STC)..........................................................2-14
Figure 2-21, G1000 Component Power Sources......................................................................................2-15
Figure 2-22, Pitot/Static System (Post G1000 STC)................................................................................2-16
Figure 2-23, G1000/GFC 700 Block Diagram.........................................................................................2-17
Figure 3-1, GDU 1040A Control Interface................................................................................................3-1
Figure 3-2, GDU 1500 Control Interface...................................................................................................3-2
Figure 3-3, G1000 Softkeys.......................................................................................................................3-2
Figure 3-4, MFD Controls (GCU 477 shown)...........................................................................................3-3
Figure 3-5, AFCS Controls (GMC 710 shown).........................................................................................3-3
Figure 3-6, GMA 1347D Controls.............................................................................................................3-4
Figure 3-7, Normal Mode ..........................................................................................................................3-5
Figure 3-8, Automatic Reversion with MFD failure.................................................................................3-6
Figure 3-9, Manual Reversion with pilot PFD failure ..............................................................................3-6
Figure 3-10, SET>ACTV Diagram...........................................................................................................3-8
Figure 3-11, Loss of Communication .......................................................................................................3-9
Figure 3-12, Configuration Status.............................................................................................................3-9
Figure 3-13, Data Transmission Indicators...............................................................................................3-9
Figure 3-14, G1000 LRU Configuration File Storage ............................................................................3-16
Figure 3-15, GRS/GDC Configuration Settings Storage ........................................................................3-17
Figure 3-16, Software/Configuration Overview .....................................................................................3-18
Figure 3-17, Airframe Options ................................................................................................................3-20
Figure 3-18, Propeller Options ................................................................................................................3-20
Figure 3-19, Configuration/Software Load Page....................................................................................3-21
Figure 3-20, System Status ......................................................................................................................3-22
Figure 3-21, TAWS-A Support Configuration ........................................................................................3-24
Figure 3-22, TAWS-A No Voice Callout Installation Configuration......................................................3-25
Figure 3-23, TAWS-A Voice Callout Installation Configuration............................................................3-26
Figure 3-24, ADF Configuration .............................................................................................................3-27
Figure 3-25, DME Configuration.............................................................................................................3-28
Figure 3-26, RAD ALT Configuration ....................................................................................................3-29
Figure 3-27, TCAS II System Configuration...........................................................................................3-30
Figure 3-28, Non-Garmin Traffic System Configuration ........................................................................3-31
Page vi G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 1 190-00716-01
Figure 3-29, GTS 8XX TAS/TCAS1 Configuration ...............................................................................3-32
Figure 3-30, Lightning System Option Configuration.............................................................................3-33
Figure 3-31, Stormscope Configuration Page.........................................................................................3-34
Figure 3-32, Stormscope Configuration..................................................................................................3-34
Figure 3-33, GTX33/33D Configuration .................................................................................................3-35
Figure 3-34, ESP Support Configuration.................................................................................................3-36
Figure 3-35, GDL 59 Configuration ........................................................................................................3-37
Figure 3-36, GSR 56 Configuration.........................................................................................................3-38
Figure 3-37, FDR Configuration..............................................................................................................3-40
Figure 3-38, ChartView Enable ...............................................................................................................3-41
Figure 3-39, TAWS-B Enable .................................................................................................................3-42
Figure 3-40, TAWS-A Enable .................................................................................................................3-43
Figure 3-41, Supplemental Database Synchronization ............................................................................3-44
Figure 3-42, SVS Enable .........................................................................................................................3-45
Figure 3-43, ESP Enable..........................................................................................................................3-46
Figure 3-44, Aircraft Registration............................................................................................................3-47
Figure 3-45, GDL 69 Cable Loss.............................................................................................................3-48
Figure 3-46, GDL 69 Cable Loss Configured..........................................................................................3-48
Figure 3-47, Navigation Database Synchronization ................................................................................3-51
Figure 4-1, GIA I/O Page........................................................................................................................4-19
Figure 4-2, Discrete Valid/Invalid Indications ........................................................................................4-19
Figure 4-3, GFC Status Page...................................................................................................................4-20
Figure 4-4, Standby Battery .....................................................................................................................4-29
Figure 4-5, Power Supply Connection....................................................................................................4-31
Figure 5-1, AUX – System Status Page....................................................................................................5-1
Figure 5-2, Alerts & Annunciations..........................................................................................................5-2
Figure 5-3, ADVISORY Softkey Annunciation .......................................................................................5-2
Figure 5-4, System Annunciations............................................................................................................5-4
Figure 5-5, AFCS Annunciation Field....................................................................................................5-28
Figure 5-6, GFC Status Page ...................................................................................................................5-31
Figure 5-7, Magnetometer Interference Test ..........................................................................................5-70
Figure 5-8, GIA 63W Backplate Connectors..........................................................................................5-80
Figure 5-9, GEA 71 Backplate Connectors ............................................................................................5-81
Figure 5-10, GMA 1347D Backplate Connectors...................................................................................5-81
Figure 5-11, GTX 33/33D Backplate Connectors...................................................................................5-81
Figure 5-12, GDU 1040A/1500 Mating Connector (P10401 or P15001)...............................................5-81
Figure 5-13, GRS 77 Mating Connector (P771) .....................................................................................5-82
Figure 5-14, GDC 7400 Mating Connector (P74001) ............................................................................5-82
Figure 5-15, GDL 69A Mating Connector (P69A1)...............................................................................5-82
Figure 5-16, GCU 477 Mating Connector (P4751) ................................................................................5-82
Figure 5-17, GMC 710 Mating Connector (P7101)................................................................................5-82
Figure 5-18, GWX 68 Mating Connector (P681) ...................................................................................5-83
Figure 5-19, GTS 820/850 Mating Connectors ......................................................................................5-83
Figure 5-20, GPA 65 Mating Connector (P651).....................................................................................5-83
Figure 5-21, Signal Conditioner Mating Connector (PVIB1).................................................................5-83
Figure 5-22, GDL 59 Backplate Connector (P591) ................................................................................5-84
Figure 5-23, GSR 56 Backplate Connector (P561)..................................................................................5-84
Figure 5-24, GSD 41 Backplate Connector (P411) .................................................................................5-84
Figure 5-25, GSA 9000 Mating Connector (P90001)..............................................................................5-84
Figure 6-1, GSA 80 Servo Gear.................................................................................................................6-6
Figure 6-2, GSM 9100 O-ring ...................................................................................................................6-6
Figure 6-3, Configuration Module Installation .........................................................................................6-4
Figure 6-4, GEA Backshell Thermocouple...............................................................................................6-6
G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air Page vii
190-00716-01 Revision 1
Figure 7-1, G1000 Normal Mode Check ..................................................................................................7-2
Figure 7-2, Marker Beacon Symbology....................................................................................................7-4
Figure 7-3, AUX – GPS STATUS Page (MFD).......................................................................................7-6
Figure 7-4, Normal Engine Instrument Markings (MFD) ........................................................................7-9
Figure 7-5, Aircraft Registration..............................................................................................................7-12
Figure 7-6, Engine Run-Up Test Page.....................................................................................................7-24
Figure 7-7, Normal Mode AHRS Check ................................................................................................7-25
Figure 7-8, GTS 8XX GND TEST softkey..............................................................................................7-31
Figure 7-9, Low Speed Awareness Band Symbolization........................................................................7-45
Figure 7-10, Static Port Measurement .....................................................................................................7-46
Figure 7-11, RVSM Critical Region........................................................................................................7-47
Figure 7-12, Dial Indicator ......................................................................................................................7-48
Figure 7-13, Static Port Measurement .....................................................................................................7-48
Figure 7-14, Static Port Measurement locations......................................................................................7-49
Figure 7-15, Static Port Measurement Log..............................................................................................7-49
Figure 7-16, GSR56 Configuration Page.................................................................................................7-58
Figure 7-17, AUX-TELEPHONE page ...................................................................................................7-58
Figure 8-1, GDU Data Verification (ARINC 429) ....................................................................................8-7
Figure 8-2, GIA Data Verification (ARINC429/RS-232)..........................................................................8-8
Figure 8-3, GIA Data Verification (RS-485) .............................................................................................8-9
Figure 8-4, Pre-Flight Test......................................................................................................................8-10
Page viii G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 1 190-00716-01
LIST OF TABLES
TABLE................................................................................................................................................ PAGE
Table 1-1, G1000 System Software Version ............................................................................................1-1
Table 1-2, Required Documents ...............................................................................................................1-5
Table 1-3, Reference Publications ............................................................................................................1-6
Table 3-1, Software Verification .............................................................................................................3-23
Table 3-2, Flight Data Recorder Parameters............................................................................................3-39
Table 4-1, Maintenance Intervals..............................................................................................................4-4
Table 4-2, Discontinued Maintenance Intervals .......................................................................................4-9
Table 4-3, Nose Section Visual Inspection Procedure............................................................................4-10
Table 4-4, Nose Avionics Compartment Visual Inspection Procedure ..................................................4-10
Table 4-5, Pilot’s Compartment Visual Inspection Procedure................................................................4-11
Table 4-6, Instrument Panel G1000 Equipment Visual Inspection Procedure .......................................4-11
Table 4-7, Cabin Area Visual Inspection Procedure...............................................................................4-13
Table 4-8, Rear Fuselage and Empennage Visual Inspection Procedure................................................4-14
Table 4-9, Lightning Strike Inspection Procedure ...................................................................................4-15
Table 4-10, Measured Torque.................................................................................................................4-21
Table 4-11, Standby Battery Required Equipment ..................................................................................4-29
Table 5-1, SVS Troubleshooting .............................................................................................................5-27
Table 5-2, SVS-Related Alert Messages.................................................................................................5-27
Table 5-3, AFCS Annunciation Troubleshooting ...................................................................................5-29
Table 5-4, AFCS General Troubleshooting ............................................................................................5-30
Table 5-5, Magnetometer Interference Test Sequence ...........................................................................5-72
Table 6-1, Configuration Module Kit – 011-00979-00 or -03 ..................................................................6-4
Table 6-2, Thermocouple Kit (011-00981-00) .........................................................................................6-6
Table 7-1, Fuel Flow Indication Special Equipment ...............................................................................7-10
Table 7-2, Fuel Flow Test Points.............................................................................................................7-10
Table 7-3, Oil Pressure Indication Special Equipment ............................................................................7-11
Table 7-4, Oil Pressure Test Points..........................................................................................................7-11
Table 7-5, Air Data System Test.............................................................................................................7-15
Table 7-6, Vertical Speed Table .............................................................................................................7-17
Table 7-7, Required GRS/GMU Calibrations.........................................................................................7-19
Table 7-8, In-Flight Altitude Hold Performance Test..............................................................................7-51
G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air Page 1-1
190-00716-01 Revision 1
1 INTRODUCTION
1.1 Content, Scope, Purpose
This document provides Instructions for Continued Airworthiness (ICA) for the Garmin G1000
Integrated Flight Deck including the GFC700 Automatic Flight Control System (AFCS) as installed in
the Hawker Beechcraft Model 300/B300 series King Air, under STC SA01535WI-D. This document
satisfies the requirements for continued airworthiness as defined by 14 CFR Part 23.1529 and Appendix
G. Information in this document is required to maintain the continued airworthiness of the G1000 and
GFC700.
1.1.1 Applicability
This document applies to all Model 300/B300 series King Air aircraft equipped with the G1000 and
GFC700 AFCS systems.
Modification of an aircraft by this Supplemental Type Certificate (STC) obligates the aircraft operator to
include the maintenance information provided by this document in the operator’s Aircraft Maintenance
Manual and the operator’s Aircraft Scheduled Maintenance Program.
Aircraft modified by this STC have been shown to qualify for operation in Reduced Vertical Separation
Minimum (RVSM) airspace as a group aircraft in accordance with Title 14 of the Code of Federal
Regulations (14 CFR) Part 91, Appendix G, “Operations in Reduced Vertical Separation Minimum
(RVSM) Airspace”, and Federal Aviation Administration (FAA) Document No. 91-RVSM, Change 2
dated 2/10/2004, “Guidance Material On The Approval Of Operators/Aircraft For RVSM Operations”.
This qualification is based on analysis of the configuration and performance of the air data, automatic
altitude control, altitude alerting, and altitude reporting systems. These systems must be maintained in
accordance with the inspections and tests specified in this document and other current maintenance
practices to guarantee continued compliance to RVSM specifications.
1.1.2 Identifying an STC Configuration
Table 1-1 lists the G1000 System Software Version numbers approved for this STC.
Table 1-1, G1000 System Software Version
Aircraft Model G1000 System
Software Version Notes
300/B300 Series King Air 0985.04 Initial approval
This STC allows multiple configurations for the King Air series. The correct configuration for a
particular aircraft is loaded by choosing the applicable airframe/engine/propeller configuration.
Page 1-2 G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 1 190-00716-01
IMPORTANT!
If the technician is unsure of an aircraft’s STC configuration, perform the
following:
After acknowledgement of the splash screen, use the FMS knob on the GCU 477 controller to go to the
AUX – SYSTEM STATUS page on the MFD. In the AIRFRAME section (upper right corner,) the
display shows the current G1000 airframe configuration and system software version number. The
airframe configuration is shown in the AIRFRAME field and the system software version number is
shown in the following format: ‘SYS SOFTWARE VERSION XXXX.XX’. It correlates to the software
image used to load the software to the system:
EXAMPLE:
System Software Version ‘0985.04’ = Software Image P/N 006-B0985-04
With the PFD in configuration mode (see section 3.7), go to the GDU-AIRFRAME CONFIGURATION
page. In the AIRFRAME section (upper right corner), verify the correct configuration for SERIES,
ENGINE and PROP.
EXAMPLE:
For a configuration that loaded “King Air B300 PT6A-60A”, the AIRFRAME section should display:
SERIES: B300
ENGINE: PT6A-60A
PROP: HARTZELL 4
G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air Page 1-3
190-00716-01 Revision 1
1.2 Organization
The following outline briefly describes the organization of this manual:
Section 2: System Description
Provides a complete description of the type design change associated with installing the G1000 integrated
cockpit system in the 300/B300 Series King Air. An overview of the G1000 and GFC 700 system
interface is also provided.
Section 3: G1000 Control & Operation
Presents basic control and operation information specifically tailored to maintenance practices. Basic
G1000 Configuration Mode operation is also described.
Section 4: Instructions for Continued Airworthiness
Provides maintenance instructions for continued airworthiness of the G1000 and GFC 700 systems.
Section 5: Troubleshooting
Provides troubleshooting information to aid in diagnosing and resolving potential problems with the
G1000 and GFC 700 systems.
Section 6: G1000 Equipment Removal & Replacement
Gives instructions for the removal and replacement of G1000 and GFC700 equipment.
Section 7: G1000 Equipment Configuration & Testing
Gives instructions for loading software, configuring, and testing of G1000 equipment.
Section 8: System Return to Service Procedure
Specifies return-to-service procedures to be performed upon completion of maintenance of the G1000
system.
Page 1-4 G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 1 190-00716-01
1.3 Definitions/Abbreviations
ADF: Automatic Direction Finder
ADTS: Air Data Test Set
AFCS: Automatic Flight Control System
AFM: Airplane Flight Manual
AFMS: Airplane Flight Manual Supplement
AHRS: Attitude Heading Reference System
CDU: Control Display Unit
CFR: Code of Federal Regulations
DME: Distance Measuring Equipment
EAU: Engine/Airframe Unit
ESP Electronic Stability and Protection
GPS: Global Positioning System
GPWS: Ground Proximity Warning System
HSDB: High-Speed Data Bus (Ethernet)
IAU: Integrated Avionics Unit
ICS: Inter-Com System
ITT: Interstage Turbine Temperature
LRU: Line Replaceable Unit
MFD: Multi-Function Display
OAT: Outside Air Temperature
PFD: Primary Flight Display
RVSM: Reduced Vertical Separation Minimum
STBY: Standby
STBY ATT: Standby Attitude Indicator
STBY ALT: Standby Altimeter
STBY A/S: Standby Airspeed Indicator
STC: Supplemental Type Certificate
TAWS: Terrain Awareness & Warning System
WAAS: Wide Area Augmentation System
VHF: Very High Frequency
1.3.1 Units of Measure
Unless otherwise stated, all units of measure are English units.
G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air Page 1-5
190-00716-01 Revision 1
1.4 Publications
The following documents are required by this maintenance manual to perform maintenance. It is the
responsibility of the owner / operator to ensure latest versions of these documents are used during
operation, servicing or maintenance of the airplane.
Table 1-2, Required Documents
Part Number Garmin Document
005-00629-00 Master Drawing List, Garmin G1000/GFC 700 in Hawker Beechcraft Model 300/B300
Series King Air
005-00629-02 General Arrangement, G1000/GFC 700, King Air 300/B300 Series
005-00629-40 Main Instrument Panel Installation, King Air 300/B300
005-00629-41 Pedestal Re-Configuration, King Air 300/B300
005-00629-42 GWX 68 Radar Install, King Air 300/B300
005-00629-43 Antenna Install, King Air 300/B300
005-00629-44 Electrical Equipment Install, Nose Bay, King Air 300/B300
005-00629-45 Roll Servo Install, King Air 300/B300
005-00629-46 Yaw & Pitch Servo Install, King Air 300/B300
005-00629-48 Pitch Trim Servo Install, King Air 300/B300
005-00629-49 Magnetometer Install, King Air 300/B300
005-00629-50 OAT Sensor Install, King Air 300/B300
005-00629-52 Optional Equipment Install, Tail Shelf, King Air 300/B300
005-00629-54 Wire Harness Installation, Nose, King Air 300/B300
005-00629-55 Wire Harness Installation, Cabin, King Air 300/B300
005-00629-56 Wire Harness Installation, Tail, King Air 300/B300
005-00629-57 Control Wheel Modification, King Air 300/B300
005-00629-59 Circuit Breaker Panel Modification, King Air 300/B300
005-00629-61 Lighting Modification, King Air 300/B300
005-W0226-00 Wiring Diagram, G1000/GFC 700, King Air 300/B300
Hawker Beechcraft Document
101-590097-9 Super King Air 300 and 300LW Maintenance Manual
101-590097-15 Super King Air 300 and 300LW Wiring Diagram Manual
101-590097-161 Super King Air 300 Airworthiness Limitations Manual
130-590031-7 Super King Air B300 and B300C Electrical Wiring Diagram Manual
130-590031-11 Super King Air B300 and B300C Maintenance Manual
130-590031-197 Super King Air B300 and B300C Avionics Wiring Diagram Manual (Proline 21)
130-590031-211 Super King Air B300 and B300C Airworthiness Limitations Manual
101-590097-13 King Air Series Component Maintenance Manual
98-39006 King Air Structural Inspection and Repair Manual
Other Documents
85-292-1-1033 Signal Conditioner Installation Manual (Meggitt Sensing Systems)
9016182 Mid-Continent Instruments - Installation Manual and Operating Instructions,
4200 Series Attitude Indicator
TP-336 L-3 Avionics Systems – Emergency Power Supply Installation Manual, PS-835
Page 1-6 G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 1 190-00716-01
The following publications are recommended to be on hand during the performance of maintenance
activities.
Table 1-3, Reference Publications
Part Number Garmin Document
190-00716-02 Airplane Flight Manual Supplement, G1000 Integrated Avionics System and
GFC 700 AFCS in Hawker Beechcraft 300 and 300LW King Air
190-00716-03 Airplane Flight Manual Supplement, G1000 Integrated Avionics System and
GFC 700 AFCS in Hawker Beechcraft B300 and B300C King Air
190-01344-00 G1000 King Air 300/B300 Cockpit Reference Guide
190-00355-04 GDL 69/69A XM Satellite Radio Activation Instructions
190-00907-00 G1000 System Maintenance Manual
190-00303-72 GSA8X/GSM85(A) Installation Manual
190-00303-83 GSM 86 Installation Manual
190-00303-85 GSA9000/GSM9100 Installation Manual
190-00313-63 GMU 44 Installation Location Magnetic Interference Survey Procedure
Generic installation manuals for individual Garmin LRUs are also available through the ‘Dealer Resource
Center’ section of the Garmin web site; refer to Section 1.5 for details.
1.5 Revison and Distribution
This document is required for maintaining the continued airworthiness of the aircraft. When this
document is revised, every page will be revised to indicate current revision level.
Garmin Dealers may obtain the latest revision of this document on the Garmin Dealer Resource Center
website.
Owner/operators may obtain the latest revision of this document from the https://fly.garmin.com/ Support
page, or by contacting a Garmin dealer, contacting Garmin Product Support at 913-397-8200, toll free
866-739-5687, or using around the world contact information on https://fly.garmin.com/.
A Garmin Service Bulletin describing the revision to this document will be sent to Garmin dealers if the
revision is determined to be significant.
G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air Page 2-1
190-00716-01 Revision 1
2 SYSTEM DESCRIPTION
2.1 Equipment Descriptions
2.1.1 GDU 1040A PFD (2) & GDU 1500 MFD
Two Garmin GDU 1040A displays and one GDU 1500 display are installed in the King Air instrument
panel. The GDU 1040A units, 10.4 inch LCD displays with 1024x768 resolution, are configured as PFD 1
and PFD 2; the GDU 1500 unit, a 15 inch LCD display with 1024x768 resolution, is configured as a MFD.
All displays provide control and display of nearly all functions of the G1000 integrated cockpit system. The
PFD displays are located on either side of the MFD, with the stand-by instruments located between the
Pilot’s PFD (PFD 1) and the MFD. GMA 1347D Audio Panels are located outboard of each PFD.
Additionally, a GMC 710 AFCS Controller is located in the upper instrument panel, above the MFD, and a
GCU 477 is installed in the pedestal. The GCU 477 provides the control interface for the MFD.
The GDU 1500 communicates with the GDU 1040A units, GDL 69A datalink, GWX68 weather radar,
optional GSD41 data concentrator, optional GDL59 wi-fi datalink and optional GTS 8XX traffic through a
high-speed data bus (HSDB) Ethernet connection. The GDU 1500 communicates with the GCU 477 via
RS-232 digital interface.
The GDU 1040A units communicate with each other and the GIA 63W units through a high-speed data bus
(HSDB) Ethernet connection.
PFD 1 receives primary electrical power from No. 1 Triple Fed Bus and secondary electrical power from
Center Bus. PFD 2 receives electrical power from No. 3 Triple Fed Bus. Electrical power to the MFD is
provided by No. 2 Triple Fed Bus. The displays will power-up immediately with external or aircraft power
or battery operation.
All displays are installed in the King Air panel using ¼-turn fasteners. Three CDU cooling fans are also
installed behind the panel for PFD and MFD cooling.
Figure 2-1, Display Units
Page 2-2 G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 1 190-00716-01
2.1.2 GMA 1347D Audio Panel (2)
The Garmin GMA 1347D Audio Panel integrates NAV/COM digital audio, intercom system and marker
beacon controls. The 300/B300 installation includes two GMA 1347D panels. The GMA 1347D panels
provide control of all cockpit intercom/mic systems as well as NAV/COM/ILS audio. The units also
provide display reversion mode control through a large red button. Warning and alert audio received by the
GMA 1347Ds is processed by and received from the GIA 63W Integrated Avionics Units (IAUs). Electrical
power to GMA 1 is provided from No. 1 Triple Fed Bus. Electrical power to GMA 2 is provided from Left
Gen Avionics Bus. GMA 1 will be powered immediately with external or aircraft power or battery
operation. GMA 2 will operate after selecting Avionics Master on. The GMA 1347D units interface with
the existing marker beacon antenna, as well as existing mic and phone jacks and oxygen mask mic.
Figure 2-2, Audio Panel
2.1.3 GMC 710 AFCS Control Unit
The dedicated AFCS controls on the GMC 710 allow crew control interface with the various GFC 700
autopilot / flight director functions. GMC 710 controls are discussed in detail in the G1000/King Air
300/B300 Series Cockpit Reference Guide. The GMC 710 is powered by No. 1 Triple Fed Bus.
Figure 2-3, AFCS Controller
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