Garmin G1000 NXi - Beechcraft King Air 200/A200/B200 Operating instructions

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Operating instructions

This manual is also suitable for

190-00915-N1 April 2019 Revision 5
System Maintenance Manual
King Air 200 Series
Includes Instructions for Continued Airworthiness
for STC SA01535WI-D
G1000 NXi System Maintenance Manual Page i
King Air 200 Series Revision 5
190-00915-N1
© Copyright 2016, 2017, 2018, 2019
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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this manual or revision must contain the complete text of this copyright notice and provided further that
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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 9LR, UK
Phone: +44 (0) 23 8052 4000
Fax: +44 (0) 23 8052 4004
Garmin AT, Inc.
2345 Turner Rd., SE
Salem, OR 97302 USA
Telephone: 503.391.3411
RECORD OF REVISIONS
Revision Revision Date Description ECO #
1 8/18/2016 Initial Release ---
2 1/30/2017
Various updates.
151146
3 7/3/2017
Added two B200 Airframe Configurations
160679
4 7/16/18
Updated for sw v2286.06
175812
5 04/30/19
Modified to support major changes to STC per
MDL 005-00421-00 Rev. 28 as part of V2286.07
software update.
188087
DOCUMENT PAGINATION
Section Pagination
Table of Contents i
x
Section 1 1 - 6
Section 2 7 - 38
Section 3 39 - 91
Section 4 94 - 134
Section 5 136 - 227
Section 6 229 - 256
Section 7 258 - 338
Section 8 340 - 379
Section 9 380 - 396
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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
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TABLE OF CONTENTS
PARAGRAPH PAGE
1. INTRODUCTION .................................................................................................................... 1
1.1 Content, Scope, Purpose ................................................................................................. 1
1.2 Organization ..................................................................................................................... 2
1.3 Definitions/Abbreviations ................................................................................................. 3
1.4 Units of Measure .............................................................................................................. 4
1.5 Publications...................................................................................................................... 4
1.6 Revision and Distribution ................................................................................................. 6
2. SYSTEM DESCRIPTION ....................................................................................................... 7
2.1 Equipment Descriptions ................................................................................................... 7
2.2 G1000 Optional Interfaces ............................................................................................. 23
2.3 Electrical Power Distribution .......................................................................................... 24
2.4 Pitot/Static System ......................................................................................................... 27
2.5 Shield Block Grounds .................................................................................................... 29
2.6 G1000NXi /GFC700 Block Diagrams ............................................................................. 30
2.7 GDU 1050A and GDU 1550 Displays ............................................................................ 32
2.8 Softkeys ......................................................................................................................... 33
2.9 FMS Knob ...................................................................................................................... 33
2.10 GCU 477 - MFD Controller ............................................................................................ 34
2.11 GMC 710 - AFCS Controls ............................................................................................ 34
2.12 GMA Audio Panels ......................................................................................................... 35
2.13 G1000 Normal Mode ...................................................................................................... 37
2.14 Reversionary Mode ........................................................................................................ 38
3.
SOFTWARE AND CONFIGURATION ................................................................................. 39
3.1 Configuration Mode Overview ........................................................................................ 39
3.2 G1000 System Software Information ............................................................................. 44
3.3 Configuration Mode ........................................................................................................ 49
3.4 G1000 Hardware/Software Compatibility Check ............................................................ 49
3.5 Equipment Verification (Third Party/Optional Equipment Documentation) .................... 50
3.6 Configuration Checklist .................................................................................................. 55
3.7 G1000 Software/Configuration Procedure ..................................................................... 57
3.8 System Software and Configuration Load ..................................................................... 58
3.9 Feature Enablement ...................................................................................................... 68
3.10 Aircraft Registration Number Entry ................................................................................ 76
3.11 Configuration Manager .................................................................................................. 78
3.12 Splash Screen Loading .................................................................................................. 79
3.13 Clearing Default User Settings ....................................................................................... 79
3.14 Database Loading .......................................................................................................... 79
3.15 Configuration of Navigation Map for Traffic System ...................................................... 81
3.16 Enter Flight ID for GTX 3000 Installations ..................................................................... 81
3.17 GRA5500 Legacy Software and Configuration (Non Integrated) ................................... 82
3.18 Interface Confirmation .................................................................................................... 84
3.19 MD 302 Configuration and Sensor Calibration .............................................................. 86
3.20 Flight Stream 510 (FS 510) Firmware Update ............................................................... 91
4. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS .................................................... 94
4.1 Airworthiness Limitations ............................................................................................... 94
4.2 Servicing Information ..................................................................................................... 95
4.3
Maintenance Intervals .................................................................................................... 98
4.4 Visual Inspection .......................................................................................................... 104
4.5 Electrical Bonding Test ................................................................................................ 109
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4.6 GSU 75B, GRS 77, or GRS 7800 Earth Magnetic Field Updates ................................ 113
4.7 GSA 80 Greasing Procedure ....................................................................................... 113
4.8 Flaps-in-motion Discrete Input Check .......................................................................... 113
4.9 GSM 85A/GSM 86 Slip Clutch Torque Check Procedure ............................................ 114
4.10 G1000 Redundant Connection Check ......................................................................... 117
4.11 Engine Data Check ...................................................................................................... 121
4.12 Trim Annunciator Check .............................................................................................. 124
4.13 G1000 Miscompare Checks ......................................................................................... 126
4.14 Nose Avionics Compartment Fans Operational Check ................................................ 127
4.15 Instrument Panel Fans Operational Check .................................................................. 127
4.16 Standby Battery Periodic Checks ................................................................................ 128
4.17 Power Bus Check ........................................................................................................ 132
4.18 Exterior Skin Inspection Around Antennas .................................................................. 134
5. TROUBLESHOOTING ....................................................................................................... 136
5.1 System Annunciations ................................................................................................. 137
5.2 G1000 Alerting System ................................................................................................ 161
5.3 Aural Alerts .................................................................................................................. 162
5.4 King Air 200 Series Specific Alerts .............................................................................. 164
5.5 TAWS Troubleshooting ................................................................................................ 165
5.6 Synthetic Vision and Pathways Troubleshooting ......................................................... 166
5.7 GFC 700 AFCS Troubleshooting ................................................................................. 167
5.8 General Troubleshooting ............................................................................................. 168
5.9 Backup Communications Path Checks ........................................................................ 180
5.10 GDU 105X Troubleshooting ......................................................................................... 180
5.11 GDU 105X Alerts ......................................................................................................... 182
5.12 GIA Troubleshooting .................................................................................................... 190
5.13 GIA Alert Messages ..................................................................................................... 191
5.14 GEA Troubleshooting ................................................................................................... 197
5.15 GTX Troubleshooting ................................................................................................... 198
5.16 GDL 69A or GDL69A SXM Troubleshooting ................................................................ 199
5.17 GSU 75B, GRS 77, or GRS 7800 and GMU 44 Troubleshooting ................................ 201
5.18 GSU 75B/GDC 74B/GDC 7400 Troubleshooting ......................................................... 207
5.19 GWX 68, GWX 70, or GWX 75 Troubleshooting ......................................................... 208
5.20 GMC 710 Troubleshooting ........................................................................................... 209
5.21 GCU 477 Troubleshooting ........................................................................................... 210
5.22 Software/Configuration Troubleshooting ...................................................................... 211
5.23 Backshell/Backplate Connectors ................................................................................. 213
5.24 Mechanical Standby Attitude Indicator Troubleshooting .............................................. 221
5.25 Mechanical Standby Airspeed Indicator Troubleshooting ............................................ 221
5.26 Mechanical Standby Altimeter Troubleshooting ........................................................... 222
5.27 MD 302 Standby Indicator Troubleshooting ................................................................. 222
5.28 Safe Flight Lift Computer Troubleshooting .................................................................. 222
5.29 GDL 59 Troubleshooting .............................................................................................. 225
5.30 GSR 56 Troubleshooting ............................................................................................. 225
5.31 GTS 820/850 Troubleshooting ..................................................................................... 225
5.32 GTS Traffic Processor Troubleshooting ....................................................................... 227
6. EQUIPMENT REMOVAL AND INSTALLATION ............................................................... 229
6.1
GDU 1050A/1550 ......................................................................................................... 230
6.2 GMA 1347D or GMA 1360D Audio Panel .................................................................... 230
6.3 GIA 63W or GIA 64E Integrated Avionics Units ........................................................... 231
6.4 GEA 71 or GEA 71B Engine/Airframe Unit .................................................................. 231
6.5 GTX 33( ) or GTX 3000 Transponder .......................................................................... 232
6.6 GTX 335R/GTX 345R Transponder ............................................................................. 233
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6.7 GDC 74B/GDC 7400 Air Data Computer ..................................................................... 233
6.8 GTP 59 OAT Probe ...................................................................................................... 234
6.9 GRS 77 or GRS 7800 AHRS or GSU 75B ADAHRS ................................................... 234
6.10 GMU 44 Magnetometer ............................................................................................... 235
6.11 GDL 69A or GDL 69A SXM ......................................................................................... 237
6.12 GSA 80 Servos ............................................................................................................ 237
6.13 GSM 85A/86 Servo Gearbox ....................................................................................... 239
6.14 GCU 477 ...................................................................................................................... 239
6.15 GMC 710...................................................................................................................... 239
6.16 GWX 68, GWX 70, or GWX 75 .................................................................................... 240
6.17 Configuration Modules ................................................................................................. 240
6.18 GEA 71/71B Backshell Thermocouple Removal & Replacement ................................ 245
6.19 GPS/WAAS Antennas .................................................................................................. 246
6.20 Diversity Transponder Antenna ................................................................................... 246
6.21 Iridium Antenna ............................................................................................................ 247
6.22 Wi-Fi Antenna .............................................................................................................. 247
6.23 Signal Conditioners ...................................................................................................... 248
6.24 Instrument Panel Annunciators (Prop Synch and Standby Battery) ............................ 248
6.25 L-3 Avionics (BF Goodrich) PS-835(C or D Model) Emergency Battery ...................... 249
6.26 MD 302 Standby Attitude Module (SAM) ..................................................................... 249
6.27 Mechanical Standby Indicators .................................................................................... 251
6.28 GIA Cooling Fans ......................................................................................................... 253
6.29 GDU Cooling Fans ....................................................................................................... 253
6.30
GTS 820/850 and GTS Processor Traffic Units ........................................................... 254
6.31 GPA 65 PA/LNA Unit ................................................................................................... 254
6.32 GA 58 Traffic Antennas ................................................................................................ 255
6.33 GDL 59 Wi-Fi Datalink ................................................................................................. 255
6.34 GSR 56 Satellite Transceiver ....................................................................................... 256
6.35 GRA 5500 Radar Altimeter .......................................................................................... 256
7. GARMIN G1000 LRU REPLACEMENT/CONFIGURATION & TESTING ......................... 258
7.1 GDU 1050A/1550 PFD & MFD .................................................................................... 258
7.2 GMA 1347D or GMA 1360D Audio Panel .................................................................... 262
7.3 GIA 63W or GIA 64E Integrated Avionics Unit ............................................................. 268
7.4 GEA 71/71B Engine/Airframe Unit ............................................................................... 279
7.5 GTX 335R, GTX 345R, GTX 33( ), or GTX 3000 Transponder ................................... 293
7.6 GSU 75B ADAHRS ...................................................................................................... 296
7.7 GDC 74B or GDC 7400 Air Data ................................................................................. 298
7.8 GRS 77 or 7800 AHRS and GMU 44 Magnetometer .................................................. 304
7.9 GMU 44 Magnetometer ............................................................................................... 306
7.10 GSU/GRS/GMU Calibration Procedures ..................................................................... 307
7.11 GDL 69A or GDL 69A SXM Data Link ......................................................................... 316
7.12 GSA 80 Servos ............................................................................................................ 319
7.13 GCU 477 FMS Controller ............................................................................................. 321
7.14 GMC 710 AFCS Controller .......................................................................................... 324
7.15 GWX 68, GWX 70, or GWX 75 Weather Radar ........................................................... 326
7.16 GRA 5500 Radar Altimeter .......................................................................................... 329
7.17 Garmin Traffic Systems (GTS 8XX/GTS 8XXX) .......................................................... 331
7.18
GDL 59......................................................................................................................... 335
7.19 GSR 56 ........................................................................................................................ 338
8. SUBSYSTEM FUNCTIONAL CHECKS ............................................................................. 340
8.1 Non-Garmin Traffic System Functional Check ............................................................. 340
8.2 Stormscope Functional Check ..................................................................................... 341
8.3 TAWS Functional Check .............................................................................................. 343
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8.4 FliteCharts Functional Check ....................................................................................... 346
8.5 ChartView Functional Check ........................................................................................ 347
8.6 SafeTaxi Functional Check .......................................................................................... 348
8.7 fsigSynthetic Vision (SVS) Functional Check .............................................................. 349
8.8 DME Functional Check ................................................................................................ 349
8.9 ADF Functional Check ................................................................................................. 351
8.10 GRA 5500 Radar Altimeter Functional Check ............................................................. 351
8.11 Non-Garmin Radar Altimeter Check (Optional) ........................................................... 351
8.12 Weight on Wheels and Low Speed Awareness Band Check ...................................... 352
8.13 RVSM Checks .............................................................................................................. 353
8.14 Safe Flight Lift Computer Ground Calibration .............................................................. 359
8.15 ESP Functional Check ................................................................................................. 368
8.16 GTS Traffic System Functional Check ......................................................................... 372
8.17 Activation of Garmin Connext ...................................................................................... 375
8.18 GDL 59 Wi-Fi Data Link Functional Check .................................................................. 377
8.19 GSR 56 Satellite Transceiver Functional Check .......................................................... 377
8.20 Search and Rescue Functional Check ......................................................................... 379
9. G1000 SYSTEM RETURN TO SERVICE PROCEDURE .................................................. 380
9.1 Display Test ................................................................................................................. 380
9.2 Display Failure Test ..................................................................................................... 383
9.3 Reversion Mode Check ................................................................................................ 384
9.4 Cooling Fan Fail Annunciation Check .......................................................................... 385
9.5 GPS Signal Acquisition ................................................................................................ 385
9.6
GPS Failure Test ......................................................................................................... 386
9.7 GIA Failure Test ........................................................................................................... 387
9.8 GEA Functional Check ................................................................................................. 388
9.9 Standby Instrument Electrical Power Checks .............................................................. 389
9.10 G1000 Backup Path Test ............................................................................................. 391
9.11 GFC 700 Ground Checkout ......................................................................................... 391
9.12 Maintenance Records .................................................................................................. 396
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LIST OF ILLUSTRATIONS
FIGURE PAGE
Figure 2-1, Display Units ............................................................................................................... 8
Figure 2-2 Flight Stream 510 ....................................................................................................... 9
Figure 2-3, Audio Panel ................................................................................................................ 9
Figure 2-4, AFCS Controller ....................................................................................................... 10
Figure 2-5, FMS Controller ......................................................................................................... 10
Figure 2-6, Transponders ........................................................................................................... 11
Figure 2-7, GIA unit ..................................................................................................................... 13
Figure 2-8, GEA unit ................................................................................................................... 14
Figure 2-9 GSU-75B ADAHRS with Connector and Mounting Tray .......................................... 15
Figure 2-10, Air Data Computer .................................................................................................. 15
Figure 2-11, OAT probe .............................................................................................................. 16
Figure 2-12, AHRS ...................................................................................................................... 16
Figure 2-13, Magnetometer ........................................................................................................ 17
Figure 2-14, GDL 69A/69A SXM Datalink ................................................................................... 17
Figure 2-15, GDL 59 Wi-Fi Datalink ............................................................................................ 18
Figure 2-16, GSR 56 Satellite Transceiver ................................................................................. 18
Figure 2-17, GTS 820/850 Traffic System .................................................................................. 19
Figure 2-18, GTS Traffic Processor ............................................................................................ 19
Figure 2-19, Weather Radar ....................................................................................................... 20
Figure 2-20, Servo ...................................................................................................................... 20
Figure 2-21, GRA 5500 Radar Altimeter ..................................................................................... 21
Figure 2-22, MD 302 Standby Attitude Module ........................................................................... 22
Figure 2-23, 200 Series Electrical Distribution (Post G1000 STC) ............................................. 25
Figure 2-24, G1000 Component Power Sources ........................................................................ 26
Figure 2-25, Pitot/Static System with ADC(s) and AHRS(s) Installed ......................................... 27
Figure 2-26, Pitot/Static System with GDU 75 ADAHRS(s) Installed.......................................... 28
Figure 2-27, G1000NXi/GFC 700 Block Diagram with GSU 75B ADAHRS................................ 30
Figure 2-28, G1000NXi/GFC 700 Block Diagram with Separate ADC and AHRS...................... 31
Figure 2-29, GDU 1050A Control Interface ................................................................................. 32
Figure 2-30, GDU 1550 Control Interface ................................................................................... 32
Figure 2-31, G1000 Softkeys ...................................................................................................... 33
Figure 2-32, MFD Controls (GCU 477 shown) ............................................................................ 34
Figure 2-33, AFCS Controls (GMC 710 shown) ......................................................................... 34
Figure 2-34, GMA 1347D Controls ............................................................................................. 35
Figure 2-35, GMA 1360D Controls ............................................................................................. 36
Figure 2-36, Normal Mode .......................................................................................................... 38
Figure 2-37, Automatic Reversion with MFD failure ................................................................... 38
Figure 2-38, Manual Reversion with pilot PFD failure ................................................................. 38
Figure 3-1, SET>ACTV Diagram ................................................................................................ 40
Figure 3-2, Loss of Communication ............................................................................................ 41
Figure 3-3, Configuration Status ................................................................................................. 41
Figure 3-4, Data Transmission Indicators ................................................................................... 41
Figure 3-5, G1000 LRU Configuration File Storage .................................................................... 47
Figure 3-6, GSU/GRS/GDC Configuration Settings Storage ...................................................... 48
Figure 3-7, Garmin Unit S/N Location ......................................................................................... 51
Figure 3-8, Garmin Unit Listed if Installed ................................................................................... 52
Figure 3-9, Ethernet Connections Page ...................................................................................... 53
Figure 3-10, ESP Status Field .................................................................................................... 54
Figure 3-11, Software/Configuration Overview ........................................................................... 57
Figure 3-12, MFD Aux - Database Page DB Transfer ................................................................ 80
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Figure 3-13, Stormscope Configuration Page ............................................................................. 84
Figure 3-14, Stormscope Configuration ...................................................................................... 84
Figure 3-15, Servo Mount Configuration Verification .................................................................. 86
Figure 4-1, GIA I/O Page .......................................................................................................... 113
Figure 4-2, Discrete Indications ................................................................................................ 113
Figure 4-3, GFC Status Page ................................................................................................... 115
Figure 4-4, Ambient Temperature Conversion Chart ................................................................ 123
Figure 4-5, Standby Battery ...................................................................................................... 129
Figure 4-6, Power Supply Connection ...................................................................................... 132
Figure 4-7, Exterior Skin Inspection Around Antennas ............................................................. 135
Figure 5-1, Aux – System Status Page ..................................................................................... 136
Figure 5-2, System Annunciations ............................................................................................ 137
Figure 5-3, Alerts & Annunciations ........................................................................................... 161
Figure 5-4, Alerts Softkey Annunciation .................................................................................... 161
Figure 5-5, AFCS Annunciation Field ....................................................................................... 167
Figure 5-6, GFC Status Page ................................................................................................... 170
Figure 5-7, Magnetometer Interference Test ............................................................................ 204
Figure 5-8, GIA 63W/64E Backplate Connectors ..................................................................... 213
Figure 5-9, GEA 71/71B Backplate Connectors ....................................................................... 214
Figure 5-10, GMA 1347D/1360D Backplate Connectors .......................................................... 214
Figure 5-11, GTX 33/33D Backplate Connectors ..................................................................... 214
Figure 5-12, GTX 3000 Connectors (P3301 and P3302) .......................................................... 215
Figure 5-13, GTX 335R/345R Looking at Front of Connector (P3251) ..................................... 215
Figure 5-14, GTX 345R (Only) Looking at Front of Connector (P3252).................................... 216
Figure 5-15, GDU 1050A/1550 Backshell Connector (P10401 or P15001) .............................. 216
Figure 5-16, GRS 77 Backshell Connector (P771) ................................................................... 216
Figure 5-17, GRS 7800 Backshell Connector (P78001) ........................................................... 217
Figure 5-18, GSU 75B Connector View from Front (P751) ....................................................... 217
Figure 5-19, GDC 74B Backshell Connector (P74B1) .............................................................. 217
Figure 5-20, GDC 7400 Mating Connector (P74001) ............................................................... 217
Figure 5-21, GDL 69A/GDL 69A SXM Backplate Connector (P69A1) ...................................... 218
Figure 5-22, GCU 477 Backshell Connector (P4751) ............................................................... 218
Figure 5-23, GMC 710 Backshell Connector (P7101) .............................................................. 218
Figure 5-24, GWX 68 Backshell Connector (P681) .................................................................. 218
Figure 5-25, GWX 70/75 Backshell Connector (P751) ............................................................. 218
Figure 5-26, GTS 820/850 Mating Connectors (P8001 and P8002) ......................................... 219
Figure 5-27, GTS 820/850 Mating Connector (P8003) (Rear View) ......................................... 219
Figure 5-28, GTS Processor Connector (P8001) ...................................................................... 219
Figure 5-29, GPA 65 Mating Connector (P651) (Rear View) .................................................... 219
Figure 5-30, Signal Conditioner (1PVIB1 and 2PVIB1) ............................................................ 220
Figure 5-31, GDL 59 Mating Connector (1P591) ...................................................................... 220
Figure 5-32, GSR 56 Mating Connector (1P561) ...................................................................... 220
Figure 5-33, GRA 5500 Connector (P55001) ........................................................................... 220
Figure 6-1, Servo Gear ............................................................................................................. 238
Figure 6-2, Configuration Module Installation ........................................................................... 241
Figure 6-3, GRS 7800 Configuration Module Installation ......................................................... 242
Figure 6-4, GSU 75B Configuration Module Installation ........................................................... 243
Figure 6-5, GEA Backshell Thermocouple ................................................................................ 245
Figure 6-6, MD 302 Backshell and Config Module ................................................................... 250
Figure 7-1, G1000 Normal Mode Check ................................................................................... 261
Figure 7-2, Aux – GPS Status Page (MFD) .............................................................................. 276
Figure 7-3, Normal Engine Instrument Markings (MFD) ........................................................... 282
Figure 7-4, Ambient Temperature Conversion Chart ................................................................ 285
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Figure 7-5, Aircraft Registration ................................................................................................ 295
Figure 7-6, GRS/GMU Calibration, Pitch/Roll Offset ................................................................ 309
Figure 7-7, GRS/GMU Calibration, Engine Run-Up .................................................................. 313
Figure 7-8, Normal Mode AHRS Check .................................................................................... 315
Figure 8-1, Low Speed Awareness Band Symbolization .......................................................... 353
Figure 8-2, RVSM Critical Region ............................................................................................. 355
Figure 8-3, Dial Indicator ........................................................................................................... 356
Figure 8-4, Static Port Measurement ........................................................................................ 357
Figure 8-5, Static Port Measurement locations ......................................................................... 357
Figure 8-6, C-05606-1 Lift Computer ........................................................................................ 365
Figure 8-7, Breakout Box .......................................................................................................... 366
Figure 8-8, Force Applicator Usage Instructions ....................................................................... 367
Figure 8-9, Traffic Map .............................................................................................................. 372
Figure 8-10, GSR56 Configuration Page .................................................................................. 378
Figure 8-11, Aux-Telephone page ............................................................................................ 378
Figure 9-1, MFD Power Up Page .............................................................................................. 380
Figure 9-2, PFD Power-up System Annunciations ................................................................... 381
Figure 9-3, PFD Normal Operation ........................................................................................... 382
Figure 9-4, GDU Reversionary Mode ....................................................................................... 384
Figure 9-5, AUX-GPS Status Page ........................................................................................... 385
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LIST OF TABLES
TABLE .................................................................................................................................. PAGE
Table 1-1, Required Documents ................................................................................................... 4
Table 1-2, Reference Publications ................................................................................................ 5
Table 3-1, Garmin Unit S/N Prefixes ........................................................................................... 50
Table 2-2, MD302 Range Markings Configuration ...................................................................... 87
Table 2-3, MD302 VNE Setup .................................................................................................... 88
Table 2-4, MD302 Dimming Curve ............................................................................................. 89
Table 4-1, Maintenance Intervals ................................................................................................ 98
Table 4-2, Discontinued Maintenance Intervals ........................................................................ 103
Table 4-3, Nose Section Visual Inspection Procedure .............................................................. 104
Table 4-4, Nose Avionics Compartment Visual Inspection Procedure ..................................... 104
Table 4-5, Pilot’s Compartment Visual Inspection Procedure ................................................... 105
Table 4-6, Instrument Panel G1000 Equipment Visual Inspection Procedure .......................... 106
Table 4-7, Cabin Area Visual Inspection Procedure ................................................................. 107
Table 4-8, Rear Fuselage and Empennage Visual Inspection Procedure ................................ 108
Table 4-9, Lightning Strike Inspection Procedure ..................................................................... 109
Table 4-10, GSM 85A/GSM 86 Slip Clutch Torque Settings .................................................... 117
Table 4-11, Engine Data Check Test Equipment ...................................................................... 121
Table 4-12, Oil Pressure Indication Test Points ........................................................................ 121
Table 4-13, ITT Indication Test Points ...................................................................................... 122
Table 4-14, Torque Indication Test Points ................................................................................ 123
Table 4-15, Standby Battery Required Equipment ................................................................... 128
Table 5-1, SVS Troubleshooting ............................................................................................... 166
Table 5-2, SVS-Related Alert Messages .................................................................................. 167
Table 5-3, AFCS Annunciation Troubleshooting ....................................................................... 168
Table 5-4, AFCS General Troubleshooting ............................................................................... 169
Table 5-5, Magnetometer Interference Test Sequence ............................................................ 205
Table 6-1, Configuration Module Kit – 011-00979-00 ............................................................... 241
Table 6-2, GRS 7800 Configuration Module Parts ................................................................... 242
Table 6-3, GSU 75B Configuration Module Kit – 011-00979-20 ............................................... 243
Table 6-4, Thermocouple Kit (011-00981-00) ........................................................................... 245
Table 7-1, ITT Indication Test Points ........................................................................................ 284
Table 7-2, Torque Indication Test Points .................................................................................. 286
Table 7-3, N1 Indication Test Points ......................................................................................... 287
Table 7-4, N2 Indication Test Points ......................................................................................... 289
Table 7-5, Fuel Flow Indication Test Points .............................................................................. 290
Table 7-6, Oil Pressure Test Points .......................................................................................... 291
Table 7-7, Oil Temperature Test Points .................................................................................... 292
Table 7-8, Air Data System Test ............................................................................................... 301
Table 7-9, Vertical Speed Table ............................................................................................... 303
Table 7-10, Required GRS/GMU Calibrations .......................................................................... 308
Table 8-1, RVSM Required Avionics ........................................................................................ 354
Table 8-2, Static Port Measurement Log .................................................................................. 358
Table 8-3, In-Flight Altitude Hold Performance Test ................................................................. 359
G1000 NXi System Maintenance Manual Page 1
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1. INTRODUCTION
1.1 Content, Scope, Purpose
This document provides Instructions for Continued Airworthiness (ICA) for the G1000NXi
Integrated Flight Deck, including the GFC700 Automatic Flight Control System (AFCS) as
installed in the Textron Aviation Inc. (Beechcraft) King Air 200 Series 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.
Throughout this document, the Garmin Integrated Flight Deck is referred to as the G1000
system. With the installation of the updated G1000 NXi as part of this amendment to the STC all
references to the G1000 system in this document include the G1000 NXi system. In addition,
the GFC-700 autopilot system is included for the G1000 NXi system and is only identified
separately when needed.
References to “200 Series” throughout this document include 200, 200C, B200, B200C,
B200GT, and B200CGT models. Items in this document that are aircraft model(s) specific will
identify the model(s) instead of “200 Series”.
References to “Beechcraft” throughout this document include other Manufacturer names
including Textron Aviation, Hawker Beechcraft, and Raytheon.
1.1.1 Applicability
This document applies to all King Air Model 200 Series aircraft equipped with the G1000NXi
system. All G1000 NXi King Air 200 Series airplanes are configured per General Arrangement
drawing 005-00421-N3 Rev 1 or subsequent.
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
The General Arrangement drawing lists the G1000 System Software Version numbers approved
for this STC.
This STC allows multiple engine and prop combinations for the King Air 200 Series. The
correct configuration for a particular aircraft is loaded by choosing the applicable
airframe/engine/propeller configuration using Table 6 of the General Arrangement Drawing for
eligible engine and propeller combinations included in this STC.
G1000 NXi System Maintenance Manual Page 2
King Air 200 Series Revision 5
190-00915-N1
IMPORTANT!
If 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 G1000NXi 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
‘2286.01’ = Software Image P/N 006-B2286-01
Restart the MFD in configuration mode (see Section 3) and use the FMS knob on the GCU 477
controller to 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 B200 PT6A-42” with a “McCauley 3-BLADE
propeller, the AIRFRAME section should display:
SERIES: B200
ENGINE: PT6A-42
PROP: MCCAULEY 3
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 King Air 200 Series. An overview of the G1000 system
interface is also provided.
Section 3: Software and Configuration
Provides software and configuration loading instructions for a complete system software load.
Section 4: Instructions for Continued Airworthiness
Provides maintenance instructions for continued airworthiness of the G1000 system.
Section 5: Troubleshooting
Provides troubleshooting information to aid in diagnosing and resolving potential problems with
the G1000 system.
Section 6: Equipment Removal & Replacement
Gives instructions for the removal and replacement of G1000 equipment.
Section 7: Garmin G1000 LRU Replacement/Configuration & Testing
Gives instructions for loading software, configuring, and testing of G1000 equipment.
Section 8: Subsystem Functional Checks
Gives instructions for testing G1000 subsystems.
Section 9: G1000 System Return to Service Procedure
Specifies return-to-service procedures to be performed upon completion of maintenance of the
G1000 system.
G1000 NXi System Maintenance Manual Page 3
King Air 200 Series Revision 5
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1.3 Definitions/Abbreviations
ADAHRS: Air Data and Attitude Heading Reference System
ADF: Automatic Direction Finder
ADS-B: Automatic Dependent Surveillance – Broadcast
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
FIS-B: Flight Information Services – Broadcast
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
MMC: Multi-Media Card
OAT: Outside Air Temperature
PED: Personal Electronic Device
PFD: Primary Flight Display
PVT: Position Velocity Time
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
TIS: Traffic Information Services
TIS-A: Traffic Information Services – A
TIS-B: Traffic Information Services – Broadcast
WAAS: Wide Area Augmentation System
VHF: Very High Frequency
G1000 NXi System Maintenance Manual Page 4
King Air 200 Series Revision 5
190-00915-N1
1.4 Units of Measure
Unless otherwise stated, all units of measure are English units.
1.5 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 1-1, Required Documents
Part Number Garmin Document
005-00421-00
Master Drawing List, Garmin G1000/GFC 700 in Hawker Beechcraft Model 200/B200
Series King Air
005-00421-30 Main Instrument Panel Installation, King Air 200/B200
005-00421-31 Pedestal Re-Configuration, King Air 200/B200
005-00421-32 GWX Radar Install, King Air 200/B200
005-00421-33 Antenna Install, King Air 200/B200
005-00421-34 Electrical Equipment Install, Nose Bay, King Air 200/B200
005-00421-35 Roll Servo Install, w/GSM 85A King Air 200/B200
005-00421-36 Yaw Servo Install, w/GSM 85A King Air 200/B200
005-00421-37 Pitch Servo Install, w/GSM 85A King Air 200/B200
005-00421-38 Pitch Trim Servo Install, w/GSM 85A King Air 200/B200
005-00421-39 Magnetometer Install, King Air 200/B200
005-00421-40 OAT Sensor Install, King Air 200/B200
005-00421-41 Transponder Install, King Air 200/B200
005-00421-42 Datalink Install, King Air 200/B200
005-00421-45 Roll Servo Install, w/GSM 86 King Air 200/B200
005-00421-46 Yaw Servo Install, w/GSM 86 King Air 200/B200
005-00421-47 Pitch Servo Install, w/GSM 86 King Air 200/B200
005-00421-48 Pitch Trim Servo Install, w/GSM 86 King Air 200/B200
005-00421-51 Wire Harness Installation, Nose, King Air 200/B200
005-00421-52 Wire Harness Installation, Cabin, King Air 200/B200
005-00421-53 Wire Harness Installation, Tail, King Air 200/B200
005-00421-54 Control Wheel Modification, King Air 200/B200
005-00421-55 Overhead Control Panel Modification, King Air 200/B200
005-00421-56 Circuit Breaker Panel Modification, King Air 200/B200
005-00421-58 Glareshield Lighting Modification, King Air 200/B200
005-00421-A9 Optional Equipment Install, Tail Shelf, King Air 200/B200
320-00426-XX Harness Assembly, G1000/GFC 700, King Air 200/B200
005-00421-D5 Pitot/Static System Modification, King Air 200 Series
005-00421-N3 General Arrangement, G1000 King Air 200 Series
005-W0025-00 Wiring Diagram, G1000/GFC 700 King Air 200/B200
G1000 NXi System Maintenance Manual Page 5
King Air 200 Series Revision 5
190-00915-N1
101-590010-133 Super King Air Wiring Diagram Manual
101-590010-161 Super King Air Wiring Diagram Manual
101-590010-19 Super King Air 200 Series Maintenance Manual
101-590010-39 Beech Super King Air 200 and 200T Wiring Diagram Manual
101-590010-453 Super King Air 200 Series Airworthiness Limitations Manual
101-590097-13 King Air Series Component Maintenance Manual
85-292-1-1033 Signal Conditioner Installation Manual (Meggitt/Vibro-Meter)
9016182
Mid-Continent Instruments - Installation Manual and Operating Instructions,
4200 Series Attitude Indicator
9017782
Mid-Continent Instruments - Installation Manual and Operating Instructions Model MD302
Series SAM Standby Attitude Module.
98-39006 Structural Inspection and Repair Manual
Part Number Other Documents
TP-336 L-3 Avionics Systems – Emergency Power Supply Installation Manual, PS-835
The following publications are recommended to be on hand during the performance of
maintenance activities.
Table 1-2, Reference Publications
Part Number Garmin Document
190-00303-10 GRS77/GMU44 Installation Manual
190-00303-72 GSA8X/GSM85(A) Installation Manual
190-00303-83 GSM 86 Servo Gear Box Installation Manual
190-00313-12 Circular Connector (and Configuration Module) Installation Instructions
190-00313-63 GMU 44 Installation Location Magnetic Interference Survey Procedure
190-00355-04 GDL 69 Series SiriusXM Satellite Radio Activation Instructions
190-00355-07 GDL 69 Series TSO Installation Manual
190-00836-00 GSR 56 Satellite Radio Installation Manual
190-00837-00 GDL 59 Datalink Installation Manual
190-00907-00 G1000/G1000H System Maintenance Manual (Standard Piston/Turboprop/Helicopter)
190-00915-N2
Airplane Flight Manual Supplement, G1000 NXi Integrated Avionics System and GFC 700
AFCS In Beechcraft Models 200, 200C, B200, B200C, B200GT and B200CGT King Air
Aircraft
190-01091-00 GRS 7800 Installation Manual
190-01277-00 GRA 5500 Installation Manual
190-01501-00 Garmin Pilot for iOS User’s Guide
190-01532-00 Garmin Pilot for Android User’s Guide
190-01532-01 User's Guide, Garmin Pilot for Android (Phone)
190-01639-00 GSU 75 Installation Manual
190-02009-00 GWX Processor Installation Manual
190-02040-00 G1000 Cockpit Reference Guide for the Beechcraft 200 Series
190-02040-01
G1000 Cockpit Reference Guide for the Beechcraft 200 Series (for MDL 005-00421-00,
Rev 27 & Subsequent)
G1000 NXi System Maintenance Manual Page 6
King Air 200 Series Revision 5
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Generic installation manuals for individual Garmin LRUs are also available through the ‘Dealer
Resource Center’ section of the Garmin web site; refer to Section 1.6 for details.
1.6 Revision 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 NXi System Maintenance Manual Page 7
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2. SYSTEM DESCRIPTION
2.1 Equipment Descriptions
2.1.1 GFC 700 Operation
The GFC 700 is a fail-passive digital flight control system composed of multiple G1000 LRUs
and servos. The following functions are provided by the GFC 700 in this installation:
Flight Director
Autopilot
Pitch Trim
Yaw Damper
Electronic Stability and Protection (optional)
Flight Director:
The Flight Directors operate within the GIA 63Ws or GIA 64Es and use data from the G1000
system, including air, attitude and flight data, to calculate commands for display to the pilot and
for the Autopilot. Flight director command bars and mode annunciations are sent to the PFDs
through a high-speed Ethernet connection for display to the pilot and copilot. The flight
directors operate independently of the autopilot and allow the pilot to hand-fly the command
bars, if desired. The GMC 710 allows the pilot to switch the active director between flight
director #1 (GIA1) and flight director #2 (GIA2).
Autopilot:
The autopilot operates within one high-speed GSA 80 servo (pitch trim) and three GSA 80
servos (pitch, roll and yaw). Flight director data is processed within the servos and turned into
aircraft flight control surface commands. The autopilot cannot operate unless the flight director
is engaged.
Manual Electric Trim:
When the autopilot is not engaged, the pitch trim servo may be used to provide a Manual
Electric Pitch Trim (MEPT) function. This allows the pilot or co-pilot to adjust pitch trim from the
PITCH TRIM switch on the control wheel in lieu of using the elevator trim wheel. Trim speeds
are scheduled to provide easier control over a wide speed or configuration range. The PITCH
TRIM switch is split into two halves. The left half arms MEPT. The right half controls direction.
Both halves must be actuated at the same time to command the pitch trim servo to operate. If
only one half of the PITCH TRIM switch is actuated for more than 3 seconds, a red PTRM
message will appear on the PFDs.
Yaw Damper:
The yaw damper reduces Dutch roll tendencies and coordinates turns. It can operate
independently of the autopilot and may be used during normal hand-flight maneuvers.
Electronic Stability and Protection:
Electronic Stability and Protection (ESP) is an optional function that is intended to assist the
pilot in maintaining the airplane in a safe flight condition within the aircraft flight envelope. This
envelope is defined by pitch, roll, and airspeed. This feature is only active when in flight and the
autopilot is off. There are two versions of the ESP option available: ESP with Angle of Attack
(AOA) modes and ESP without Angle of Attack (AOA) modes. The ESP option with AOA
modes requires a new lift computer. The ESP option without AOA modes uses the existing lift
computer.
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Underspeed Protection:
The optional Underspeed Protection (USP) system is available when the ESP system is
installed and the autopilot is on. It is designed to discourage aircraft operation below minimum
established airspeeds. When the aircraft decelerates to stall warning, the autopilot will provide
input causing the aircraft to pitch down and wings to level. The pitch down force will continue
until the aircraft reaches a pitch attitude at which IAS equals the IAS at which stall warning turns
off, plus two knots.
2.1.2 GDU 1050A PFD (2) & GDU 1550 MFD
Two Garmin GDU 1050A displays and one GDU 1550 display are installed in the King Air
instrument panel. The GDU 1050A units, 10.4 inch LCD displays with 1024x768 resolution, are
configured as PFD 1 and PFD 2; the GDU 1550 unit, a 15 inch LCD display with 1400 x1050
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 or GMA 1360D 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 1550 communicates with the GDU 1050A units, GDL 69A /GDL69 SXM datalink,
GWX68, GWX 70, or GWX 75 weather radar, optional GDL59 Wi-Fi datalink and optional GTS
820/850 or GTS Processor traffic through a high-speed data bus (HSDB) Ethernet connection.
The GDU 1550 communicates with the GCU 477 via RS-232 digital interface.
The GDU 1050A units communicate with each other and the GIA 63W or GIA 64E units through
a high-speed data bus (HSDB) Ethernet connection.
PFD 1 receives primary electrical power from the new Essential Bus and secondary electrical
power from Dual Fed Bus No. 1. PFD 2 receives electrical power from Dual Fed Bus No. 2.
Electrical power to the MFD is also provided by the Essential 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
G1000 NXi System Maintenance Manual Page 9
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2.1.3 Flight Stream 510
The Flight Stream™ 510 (FS 510) is a Wi-Fi/Bluetooth capable multi-media card (MMC) that is
installed in the bottom SD slot of the MFD. It sends position, velocity, time, attitude, heading,
FIS-B, TIS-B traffic, Sirius XM audio control, Sirius XM weather data, and flight plan transfer to
mobile devices via Bluetooth. The FS 510 can also interface with a mobile device via Wi-Fi
pairing for the purposes of updating databases used by the GDU(s). Bluetooth and Wi-Fi are
mutually exclusive with only one interface functional at a time. Connecting via Wi-Fi requires a
pilot-configurable Wi-Fi Protected Access WPA2 security password. By updating databases
wirelessly, new databases may be transferred to the G1000 system without taking the data card
out of the aircraft.
Figure 2-2 Flight Stream 510
2.1.4 GMA 1347D or GMA 1360D Audio Panel (2)
The Garmin GMA 1347D or GMA 1360D Audio Panel integrates NAV/COM digital audio,
intercom system and marker beacon controls. The 200 Series installation includes two GMA
1347D or GMA 1360D panels. The GMA 1347D or GMA 1360D 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 or GMA 1360Ds is processed by and received from the GIA 63W or GIA 64E
Integrated Avionics Units (IAUs). Electrical power to GMA 1 is provided from the Essential bus.
Electrical power to GMA 2 is provided from Avionics Bus No. 1. 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 or GMA 1360D units interface with the existing
marker beacon antenna, as well as existing mic and phone jacks and oxygen mask mic.
Figure 2-3, Audio Panel
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Garmin G1000 NXi - Beechcraft King Air 200/A200/B200 Operating instructions

Type
Operating instructions
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