Garmin G5000 for Beechjet Owner's manual

Type
Owner's manual
G5000
®
GIFD and AFCS
System Maintenance Manual
Beechcraft Model 400A
Contains Instructions for
Continued Airworthiness
for STC ST01821WI
Document Number:
190-01508-01 Rev. 5
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page ii
© Copyright 2016-2018
Garmin Ltd. or its subsidiaries
All Rights Reserved
Except as expressly provided herein, no part of this manual may be reproduced, copied,
transmitted, disseminated, downloaded or stored in any storage medium, for any purpose
without the express prior 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. 151
st
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
08/29/2016
Initial release
------
2
09/30/2016
Added early serial number airplanes RK1 - RK44,
RK46 - RK48 to STC and other miscellaneous
updates.
149550
3
12/15/2016
Added optional PC920 Fuel Flow Signal Conditioner as
replacement for fuel flow indicators.
150934
4
08/09/2017
Added section 3.14 to update the GEA 7100 sub-
system software from v2.30, included in the G5000
system software v2091.02, to v2.35.
Updated section 4.12.4.
Updated section 8.1.2
161777
5
11/14/2018
Updated Overspeed Alert criteria in section 7.3.2.3
Updated Overspeed Protection Procedure (7.32.1,
7.32.2)
181339
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page iii
DOCUMENT PAGINATION
Section
Pagination
Table of Contents
i ˗˗ xiv
Section 1
1-1 ˗˗ 1-6
Section 2
2-1 ˗˗ 2-28
Section 3
3-1 ˗˗ 3-62
Section 4
4-1 ˗˗ 4-59
Section 5
5-1 ˗˗ 5-92
Section 6
6-1 ˗˗ 6-21
Section 7
7-1 ˗˗ 7-91
Section 8
8-1 ˗˗ 8-22
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page iv
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.
WARNING
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.
CAUTION
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.
IMPORTANT
All G5000 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.
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page v
TABLE OF CONTENTS
SECTION PAGE
1. INTRODUCTION ..................................................................................................................... 1-1
1.1 Content, Scope, Purpose ................................................................................................. 1-1
1.2 Organization ..................................................................................................................... 1-2
1.3 Acronyms & Abbreviations ............................................................................................... 1-3
1.4 Publications ...................................................................................................................... 1-4
1.5 Revision and Distribution ................................................................................................. 1-5
2. SYSTEM DESCRIPTION ......................................................................................................... 2-1
2.1 Equipment Descriptions ................................................................................................... 2-2
2.2 G5000 Optional Interfaces ............................................................................................. 2-15
2.3 Electrical Power Distribution .......................................................................................... 2-20
3. G5000 CONTROL & OPERATION .......................................................................................... 3-1
3.1 GDU 1200W and GTC 570 .............................................................................................. 3-1
3.2 GMC 7250 ........................................................................................................................ 3-4
3.3 GCU 275 .......................................................................................................................... 3-4
3.4 Display Modes .................................................................................................................. 3-5
3.5 MD302 3-in-1 Standby Instrument ................................................................................... 3-9
3.6 Configuration Mode Overview .......................................................................................... 3-9
3.7 G5000 / GFC 700 Software Information ........................................................................ 3-15
3.8 Software Loader Card Creation ..................................................................................... 3-16
3.9 G5000 Software/Configuration Procedure ..................................................................... 3-23
3.10 Load Default GEA Rigging ............................................................................................. 3-32
3.11 400A Max TO Weight ..................................................................................................... 3-33
3.12 400A Performance Kit .................................................................................................... 3-34
3.13 Garmin Optional Equipment and Features .................................................................... 3-35
3.14 GEA 7100 Ver. 2.35 Software Load ............................................................................... 3-36
3.15 Software Load Confirmation .......................................................................................... 3-44
3.16 Non-Garmin Support Options ........................................................................................ 3-45
3.17 Configurations Requiring Enablement Software ............................................................ 3-51
3.18 Splash Sceen Image Loading ........................................................................................ 3-58
3.19 Terrain/Obstacle/Basemap/Safe Taxi/Airport Directory/Charts Database Loading ....... 3-59
3.20 Standby Navigation Database Loading.......................................................................... 3-60
3.21 Aircraft Registration Number Entry ................................................................................ 3-61
3.22 Configuration Confirmation ............................................................................................ 3-61
3.23 Activation of SiriusXM Radio and Weather .................................................................... 3-62
4. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ....................................................... 4-1
4.1 Airworthiness Limitations ................................................................................................. 4-1
4.2 Servicing Information ....................................................................................................... 4-3
4.3 Maintenance Intervals ...................................................................................................... 4-5
4.4 Visual Inspection ............................................................................................................ 4-12
4.5 Electrical Bonding Test .................................................................................................. 4-19
4.6 GRS 77 Earth Magnetic Field Updates .......................................................................... 4-21
4.7 GSM 9100 Servo Mount Inspections ............................................................................. 4-22
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4.8 Garmin LRU Redundant Ground Path Checks .............................................................. 4-23
4.9 Garmin LRU Power Checks ........................................................................................... 4-27
4.10 Pitot Anti-Ice System Checks ......................................................................................... 4-33
4.11 Static Port Anti-Ice System Check ................................................................................. 4-37
4.12 Electrical System Checks............................................................................................... 4-38
4.13 Exterior Skin Inspection Around Antennas .................................................................... 4-44
4.14 Fuel Temperature Zener Diode Check .......................................................................... 4-46
4.15 Emergency Frequency Switch Check ............................................................................ 4-46
4.16 G5000 Display Lighting Check ....................................................................................... 4-47
4.17 G5000 Display Format Mode Check .............................................................................. 4-47
4.18 G5000 HSDB Connection Check ................................................................................... 4-48
4.19 G5000 Redundant Connection Check ........................................................................... 4-51
4.20 Annunciator Panel Power Check ................................................................................... 4-56
4.21 Rudder Boost Movement Check .................................................................................... 4-57
4.22 Rudder Boost Inhibit Active Logic Check ....................................................................... 4-58
5. TROUBLESHOOTING ............................................................................................................. 5-1
5.1 G5000 Alerting System .................................................................................................... 5-1
5.2 G5000 System Failure Annunciations .............................................................................. 5-3
5.3 TAWS Troubleshooting .................................................................................................. 5-28
5.4 Synthetic Vision and Pathways Troubleshooting ........................................................... 5-30
5.5 GFC 700 AFCS Troubleshooting ................................................................................... 5-31
5.6 Backup Communications Path Checks .......................................................................... 5-43
5.7 GDU 1200W Troubleshooting ........................................................................................ 5-44
5.8 GMA Troubleshooting .................................................................................................... 5-54
5.9 GIA 63 Troubleshooting ................................................................................................. 5-55
5.10 GEA Troubleshooting ..................................................................................................... 5-63
5.11 GSD Troubleshooting ..................................................................................................... 5-64
5.12 GTX Troubleshooting ..................................................................................................... 5-65
5.13 GDL 69A Troubleshooting ............................................................................................. 5-66
5.14 GRS and GMU Troubleshooting .................................................................................... 5-67
5.15 GDC Troubleshooting .................................................................................................... 5-73
5.16 GWX Troubleshooting .................................................................................................... 5-74
5.17 GCU Troubleshooting .................................................................................................... 5-74
5.18 GMC Troubleshooting .................................................................................................... 5-75
5.19 GTC Troubleshooting ..................................................................................................... 5-75
5.21 Software/Configuration Troubleshooting........................................................................ 5-78
5.22 System Communication Hierarchy ................................................................................. 5-79
5.23 Aircraft Harness/LRU Connectors .................................................................................. 5-80
5.24 Standby Indicator Troubleshooting ................................................................................ 5-92
6. G5000 EQUIPMENT REMOVAL & REPLACEMENT ............................................................. 6-1
6.1 GDU 1200W Display Unit................................................................................................. 6-1
6.2 GIA 63W Integrated Avionics Unit ................................................................................... 6-2
6.3 GSA 9000 Servo Actuator ................................................................................................ 6-3
6.4 GSM 9100 Servo Mount................................................................................................... 6-3
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Beechcraft Model 400A Rev. 5
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6.5 GMC 7250 Autopilot Mode Controller .............................................................................. 6-4
6.6 GTA 82 Trim Adapter ....................................................................................................... 6-4
6.7 GTC 570 Touchscreen Controller .................................................................................... 6-5
6.8 GCU 275 (Remote) Display Controller ............................................................................. 6-6
6.9 GSD 41 Data Concentrator .............................................................................................. 6-6
6.10 GMA 36 Audio Processor................................................................................................. 6-7
6.11 GDC 7400 Air Data Computer ......................................................................................... 6-8
6.12 GDL 69A Data Link .......................................................................................................... 6-8
6.13 GEA 7100 Engine and Airframe Unit ............................................................................... 6-9
6.14 GRS 77 AHRS ................................................................................................................. 6-9
6.15 GMU 44 Magnetometer.................................................................................................. 6-10
6.16 GTX 3000 Transponder ................................................................................................. 6-10
6.17 GWX 70 Weather Radar ................................................................................................ 6-11
6.18 GSR 56 Satellite Receiver ............................................................................................. 6-11
6.19 Iridium Antenna .............................................................................................................. 6-12
6.20 GPS/WAAS/SXM Antennas ........................................................................................... 6-12
6.21 Nose Avionics Cooling Fans .......................................................................................... 6-13
6.22 Configuration Modules ................................................................................................... 6-14
6.23 MD302 Standby Attitude Module ................................................................................... 6-18
6.24 Emergency Frequency Switch/Annunciator ................................................................... 6-19
6.25 Ground COMM Switch/Annunciator ............................................................................... 6-19
6.26 Display Format and Dimming Panel .............................................................................. 6-20
6.27 Fuel Flow Indicators (Optional Fuel Flow Signal Conditioner) ....................................... 6-20
6.28 Glareshield Cooling Fans ............................................................................................... 6-21
7. G5000 EQUIPMENT CONFIGURATION & TESTING ............................................................ 7-1
7.1 Flap Calibration Procedure .............................................................................................. 7-1
7.2 GCU 275 PFD Controller ................................................................................................. 7-4
7.3 GDC 7400 Air Data Computer ......................................................................................... 7-6
7.4 GDL 69A Data Link ........................................................................................................ 7-11
7.5 GDU 1200W MFD & PFD .............................................................................................. 7-14
7.6 GEA 7100 Engine and Airframe Unit ............................................................................. 7-19
7.7 GIA 63W Integrated Avionics Unit ................................................................................. 7-32
7.8 GMA 36 Audio Processor and Marker Beacon Receiver ............................................... 7-36
7.9 GMC 7250 Autopilot Mode Controller ............................................................................ 7-42
7.10 Radar Altimeter .............................................................................................................. 7-44
7.11 GRS 77 AHRS/GMU 44 Magnetometer ......................................................................... 7-45
7.12 GSD 41 Data Concentrator ............................................................................................ 7-56
7.13 GSA 9000 Servo Actuator .............................................................................................. 7-58
7.14 GSR 56 Satellite Receiver Functional Check ................................................................ 7-59
7.15 GTA 82 Trim Actuator .................................................................................................... 7-61
7.16 GTC 570 Touch Screen Controller ................................................................................ 7-62
7.17 GTX 3000 Transponder ................................................................................................. 7-64
7.18 GWX 70 Airborne Weather Radar ................................................................................. 7-66
7.19 MD 302 Standby Attitude Module .................................................................................. 7-68
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Beechcraft Model 400A Rev. 5
Page viii
7.20 RVSM Checks ................................................................................................................ 7-71
7.21 TAWS Functional Check ................................................................................................ 7-77
7.22 FliteCharts Functional Check ......................................................................................... 7-79
7.23 ChartView Functional Check .......................................................................................... 7-80
7.24 SafeTaxi Functional Check ............................................................................................ 7-81
7.25 Low Speed Awareness .................................................................................................. 7-81
7.26 Non-Garmin Traffic System (TCAS II) Functional Check (Optional) ............................. 7-84
7.27 DME 1 Functional Check (Optional) .............................................................................. 7-85
7.28 DME 2 Functional Check (Optional) .............................................................................. 7-85
7.29 ADF 1 Functional Check (Optional) ............................................................................... 7-86
7.30 ADF 2 Functional Check (Optional) ............................................................................... 7-86
7.31 Cockpit Voice Recorder Functional Check (Optional) ................................................... 7-87
7.32 Autopilot Disengagement Check .................................................................................... 7-89
7.33 Standby Battery Checks................................................................................................. 7-91
7.34 Nose Fan Operational Check ......................................................................................... 7-91
8. SYSTEM RETURN TO SERVICE PROCEDURE ................................................................... 8-1
8.1 Backup Path System Testing ........................................................................................... 8-1
8.2 Miscellaneous System Tests ........................................................................................... 8-7
8.3 GFC 700 Ground Test .................................................................................................... 8-10
8.4 Maintenance Records .................................................................................................... 8-19
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page ix
Figures
Figure Page
Figure 2-1, G5000 Instrument Panel Layout in the Model 400A Beechjet ................................... 2-1
Figure 2-2, Display Unit ................................................................................................................. 2-5
Figure 2-3, Touchscreen Controller .............................................................................................. 2-6
Figure 2-4, Audio Processor ......................................................................................................... 2-7
Figure 2-5, Mode Controller .......................................................................................................... 2-7
Figure 2-6, Display Controller ....................................................................................................... 2-7
Figure 2-7, Transponder ............................................................................................................... 2-8
Figure 2-8, Integrated Avionics Unit .............................................................................................. 2-9
Figure 2-9, Engine and Airframe Unit ........................................................................................... 2-9
Figure 2-10, Air Data Computer .................................................................................................. 2-10
Figure 2-11, Total Air Temperature Probe .................................................................................. 2-10
Figure 2-12, AHRS ...................................................................................................................... 2-11
Figure 2-13, Magnetometer......................................................................................................... 2-11
Figure 2-14, Datalink ................................................................................................................... 2-12
Figure 2-15, Satellite Receiver .................................................................................................... 2-12
Figure 2-16, Data Concentrator .................................................................................................. 2-12
Figure 2-17, Weather Radar ....................................................................................................... 2-13
Figure 2-18, Servo Actuator and Servo Mount ........................................................................... 2-13
Figure 2-19, Trim Adapter ........................................................................................................... 2-14
Figure 2-20, Standby Instrument and Standby Power Switch .................................................... 2-14
Figure 2-21, Optional Fuel Flow Signal Conditioner ................................................................... 2-15
Figure 2-22, G5000 Beechcraft Model 400A Architecture (Summary) ....................................... 2-16
Figure 2-23, Power Generation Overview ................................................................................... 2-21
Figure 2-24, Left Main Bus / Left Load Bus ................................................................................ 2-22
Figure 2-25, Right Main Bus / Right Load Bus............................................................................ 2-23
Figure 2-26, Emergency Bus ...................................................................................................... 2-24
Figure 2-27, Battery / Standby Bus / L-R Overhead Bus ............................................................ 2-25
Figure 2-28, L-R Nonessential / Galley Buses ............................................................................ 2-26
Figure 2-29, Left Radio Master / Right Radio Master Buses ...................................................... 2-27
Figure 2-30, Dual Powered Units / Ground Comm ..................................................................... 2-28
Figure 3-1, Example Image GDU 1200W .................................................................................. 3-1
Figure 3-2, Example Image - G5000 Softkeys .............................................................................. 3-2
Figure 3-3, Example Images - GTC 570 ....................................................................................... 3-3
Figure 3-4, Example Image GMC 7250 ..................................................................................... 3-4
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Beechcraft Model 400A Rev. 5
Page x
Figure 3-5, Example Image GCU 275 ........................................................................................ 3-4
Figure 3-6, Normal Mode, Full PFD (Example) ......................................................................... 3-5
Figure 3-7, Normal Mode, 40/60 Format PFD (Example) .......................................................... 3-5
Figure 3-8, Normal Mode, Full MFD (Example) ......................................................................... 3-6
Figure 3-9, Normal Mode, Split MFD (Example) ........................................................................ 3-6
Figure 3-10, Beechcraft Model 400A EIS ..................................................................................... 3-7
Figure 3-11, Concept Display Format and Dimming Panel ....................................................... 3-7
Figure 3-12, Reversionary Mode (Example) ................................................................................. 3-8
Figure 3-13, Beechcraft Model 400A EIS 60/40 Reversionary ..................................................... 3-8
Figure 3-14, MD302 (Example) ..................................................................................................... 3-9
Figure 3-15, SET>ACTV Diagram .............................................................................................. 3-12
Figure 3-16, Loss of Communication .......................................................................................... 3-12
Figure 3-17, Configuration Status ............................................................................................... 3-13
Figure 3-18, System Status Indicators ........................................................................................ 3-14
Figure 3-19, G5000 LRU Configuration File Storage .................................................................. 3-21
Figure 3-20, GRS/GDC Configuration Setting Storage .............................................................. 3-22
Figure 3-21, Software/Configuration Overview ........................................................................... 3-23
Figure 4-1, GSM 9100 Servo Mount Inspection Items ................................................................ 4-22
Figure 4-2, Exterior Skin Inspection Around Antennas ............................................................... 4-45
Figure 5-1, Avionics Status Page .................................................................................................. 5-1
Figure 5-2, G5000 Alerting Notification ......................................................................................... 5-2
Figure 5-3, System Annunciations (PFD) ..................................................................................... 5-2
Figure 5-4, G5000 Major System Failure Annunciations (GDU in Reversionary Mode) ............ 5-19
Figure 5-5, GFC Status Page ..................................................................................................... 5-36
Figure 5-6, Magnetometer Interference Test .............................................................................. 5-70
Figure 5-7, GIA1 and GIA2 Connector Arrangement ................................................................. 5-80
Figure 5-8, View of J601 (COM) Connector from back of GIA .................................................. 5-80
Figure 5-9, View of J602 (VOR/ILS) Connector from back of GIA ............................................. 5-80
Figure 5-10, View of J603 (Main Serial) Connector from back of GIA ....................................... 5-81
Figure 5-11, View of J604 (Main Discrete) Connector from back of GIA ................................... 5-81
Figure 5-12, View of J605 (I/O 1) Connector from back of GIA ................................................. 5-81
Figure 5-13, View of J606 (I/O 2) Connector from back of GIA ................................................. 5-81
Figure 5-14, GEA1 and GEA2 Connector Arrangment .......................................................... 5-82
Figure 5-15, View of P71001 Connector from front of GEA ....................................................... 5-83
Figure 5-16, View of P71002 Connector from front of GEA ....................................................... 5-83
Figure 5-17, View of P71003 Connector from front of GEA ....................................................... 5-84
Figure 5-18, GMA1 and GMA2 Connector Arrangment ............................................................. 5-84
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page xi
Figure 5-19, View of J3471 Connector from back of GMA ........................................................ 5-85
Figure 5-20, View of J3472 Connector from back of GMA ........................................................ 5-85
Figure 5-21, GMA1 and GMA2 Connector Arrangment ............................................................. 5-85
Figure 5-22, View of J3301 Connector looking at the GTX ....................................................... 5-86
Figure 5-23, View of J3302 Connector looking at the GTX ........................................................ 5-86
Figure 5-24, View of J12001 Connector from the back of the GDU ........................................... 5-86
Figure 5-25, View of J771 Connector from back of GRS ........................................................... 5-87
Figure 5-26, View of J441 Connector on the GMU .................................................................... 5-87
Figure 5-27, View of J74001 Connector on the GDC ................................................................ 5-87
Figure 5-28, GDL 69A Connector Arrangment ........................................................................... 5-88
Figure 5-29, View of J1 Connector on the GDL69A .................................................................. 5-88
Figure 5-30, View of J1 Connector on the GCU ........................................................................ 5-88
Figure 5-31, View of J7101 Connector on the GMC .................................................................. 5-89
Figure 5-32, View of J5701 Connector on the GTC ................................................................... 5-89
Figure 5-33, GSD1 and GSD2 Connector Arrangment ............................................................. 5-90
Figure 5-34, View of J411 Connector on the GSD .................................................................... 5-90
Figure 5-35, View of J412 Connector on the GSD .................................................................... 5-90
Figure 5-36, View of J701 Connector on the GWX .................................................................... 5-91
Figure 5-37, View of J821 Connector on the GTA ..................................................................... 5-91
Figure 5-38, View of J90001 Connector on the GSA ................................................................. 5-91
Figure 5-39, GSR Connector Arrangment .................................................................................. 5-92
Figure 5-40, View of J561 Connector on the GSR .................................................................... 5-92
Figure 6-1, GTC Avionics Status Page ......................................................................................... 6-1
Figure 6-2, GSM 9100 O-ring ....................................................................................................... 6-3
Figure 6-3, Center Pedestal - DFDP Installation........................................................................... 6-5
Figure 6-4, Center Pedestal - GTA 82 Mounting Plate ................................................................. 6-5
Figure 6-5, GDU1200W (PFD1) Configuration Module Installation ............................................ 6-14
Figure 6-6, GRS77 Configuration Module Installation ................................................................ 6-15
Figure 6-7, GEA7100 Configuration Module with Thermocouple (Typical) Installation .............. 6-16
Figure 7-1, PFD Normal Operation (SVS Enabled) .................................................................... 7-18
Figure 7-2, Normal Engine Instrument Markings (MFD) ............................................................. 7-20
Figure 7-3, GPS Status Page (MFD) .......................................................................................... 7-34
Figure 7-4, Marker Beacon Symbology ...................................................................................... 7-40
Figure 7-5, Pitch/Roll Offset ........................................................................................................ 7-48
Figure 7-6, GRS/GMU Calibration .............................................................................................. 7-48
Figure 7-7, GRS/GMU Calibration Procedure ............................................................................. 7-49
Figure 7-8, GRS/GMU Calibration .............................................................................................. 7-51
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Beechcraft Model 400A Rev. 5
Page xii
Figure 7-9, Magnetometer Calibration ........................................................................................ 7-51
Figure 7-10, Magnetometer Verification ...................................................................................... 7-52
Figure 7-11, Engine Run Up ....................................................................................................... 7-53
Figure 7-12, Engine Run Up Page .............................................................................................. 7-53
Figure 7-13, AHRS Information Valid .......................................................................................... 7-55
Figure 7-14, GSD Status Page ................................................................................................... 7-58
Figure 7-15, GSR56 Configuration Page .................................................................................... 7-60
Figure 7-16, Aircraft Registration Configuration.......................................................................... 7-66
Figure 7-17, MD302 Configure Menu ......................................................................................... 7-69
Figure 7-18, RVSM Critical Region ............................................................................................. 7-72
Figure 7-19, Paint Stripe Limitations ........................................................................................... 7-73
Figure 7-20, Dial Indicator ........................................................................................................... 7-74
Figure 7-21, Static Port Measurement ........................................................................................ 7-75
Figure 7-22, Static Port Measurement Locations ....................................................................... 7-76
Figure 7-23, Squat Switch Air/Gnd ............................................................................................. 7-82
Figure 7-24, Low Speed Awareness Band and Approach Cue Symbolization ........................... 7-83
Figure 7-25, Squat Switch Air/Ground ........................................................................................ 7-87
Figure 8-1, Squat Switch Air/Gnd ................................................................................................. 8-1
Figure 8-2, GDU Data Verification (ARINC 429).......................................................................... 8-5
Figure 8-3, GIA Data Verification (ARINC429/RS-232) ............................................................... 8-6
Figure 8-4, GIA Data Verification (RS-485) ................................................................................. 8-7
Figure 8-5, Pre-Flight Test ......................................................................................................... 8-10
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Page xiii
Tables
Table Page
Table 1-1, Required Documents ................................................................................................... 1-4
Table 2-1, G5000 and Supporting Equipment ............................................................................ 2-17
Table 2-2, Non-Garmin Interface Support ................................................................................... 2-18
Table 2-3, Notable G5000 Features ........................................................................................... 2-18
Table 3-1, Data Indicator Symbols .............................................................................................. 3-13
Table 3-2, Successful Criteria ..................................................................................................... 3-24
Table 4-1, Maintenance Intervals .................................................................................................. 4-5
Table 4-2, Nose Section Visual Inspection Procedure ............................................................... 4-12
Table 4-3, Nose Avionics Compartment Visual Inspection Procedure ....................................... 4-12
Table 4-4, Pilot’s Compartment Visual Inspection Procedure .................................................... 4-13
Table 4-5, Pedestal G5000 Equipment Visual Inspection Procedure ......................................... 4-13
Table 4-6, Instrument Panel G5000 Equipment Visual Inspection Procedure ........................... 4-14
Table 4-7, Cabin Area Visual Inspection Procedure ................................................................... 4-15
Table 4-8, Rear Fuselage and Empennage Visual Inspection Procedure .................................. 4-17
Table 4-9, Wing Visual Inspection Procedure ............................................................................. 4-18
Table 4-10, Aircraft Exterior (Antennas) Inspection Procedure .................................................. 4-18
Table 4-11, Lightning Strike Inspection Procedure ..................................................................... 4-18
Table 4-12, Nose Bay LRUs ....................................................................................................... 4-23
Table 4-13, Nose Bay LRU Ground Continuity Check ................................................................ 4-23
Table 4-14, Flight Deck LRUs ..................................................................................................... 4-25
Table 4-15, Flight Deck LRU Ground Continuity Check ............................................................. 4-25
Table 5-1, SVS Troubleshooting ................................................................................................. 5-30
Table 5-2, SVS-Related Alert Messages .................................................................................... 5-30
Table 5-3, AFCS Annunciation Troubleshooting......................................................................... 5-31
Table 5-4, AFCS General Troubleshooting ................................................................................. 5-34
Table 5-5, Magnetometer Interference Test Sequence .............................................................. 5-71
Table 5-6, Troubleshooting ......................................................................................................... 5-78
Table 6-1, Configuration Module Kit, Part Number 011-00979-20 ............................................ 6-14
Table 6-2, Configuration Module Kit, Part Number 011-00979-03 ........................................... 6-15
Table 6-3, Configuration Module with Thermocouple Kit, Part Number 011-02582-01 ............ 6-17
Table 7-1, Flap Position Test ........................................................................................................ 7-3
Table 7-2, Altitude/Airspeed .......................................................................................................... 7-9
Table 7-3, Vertical Speed ............................................................................................................ 7-10
Table 7-4, Engine Indication Test Equipment ............................................................................. 7-21
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page xiv
Table 7-5, Fuel Flow Test Points ................................................................................................ 7-22
Table 7-6, Fuel Temperature Test Points ................................................................................... 7-22
Table 7-7, Oil Temperature Test Points ...................................................................................... 7-23
Table 7-8, N1 Test Points ........................................................................................................... 7-24
Table 7-9, N2 Test Points ........................................................................................................... 7-25
Table 7-10, Oil Pressure Test Points .......................................................................................... 7-28
Table 7-11, ITT Test Points......................................................................................................... 7-30
Table 7-12, Required GRS/GMU Calibrations ............................................................................ 7-47
Table 7-13, MD302 Range Marking Menu .................................................................................. 7-70
Table 7-14, Static Port Measurement Log .................................................................................. 7-76
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page 1-1
1. INTRODUCTION
1.1 Content, Scope, Purpose
This document provides Instructions for Continued Airworthiness (ICA) for the Garmin G5000 Integrated
Flight Deck including the GFC700 Automatic Flight Control System (AFCS) as installed in the Beechcraft
Model 400A series under STC ST01821WI which defines each of the installation configurations required
to safely operate the aircraft.
This document satisfies the requirements for continued airworthiness as defined by 14 CFR Part 25.1529.
Information in this document is required to maintain the continued airworthiness of the G5000 and
GFC700 systems.
1.1.1 Applicability
This document applies to all Beechcraft Model 400A series aircraft equipped with the G5000 and GFC700
AFCS systems.
Modification of an aircraft by Supplemental Type Certificate (STC) ST01821WI obligates the aircraft
operator to include the 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.
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page 1-2
1.2 Organization
This manual is structured as described below:
Section 2: G5000 System Description & Operation
Provides a complete description of the type design changes associated with installing the G5000 software
upgrade and optional configurations under this STC including basic operational information. An overview
of the G5000 and GFC 700 system interface is also provided.
Section 3: G5000 Control & Operation
Presents basic control and operation information specifically tailored to maintenance practices. Basic
G5000 Configuration Mode operation is also described.
Section 4: Instructions for Continued Airworthiness
Provides maintenance instructions for continued airworthiness of the G5000 system.
Section 5: Troubleshooting
Provides troubleshooting information to aid in diagnosing and resolving potential problems with
equipment and functions installed by this STC.
Section 6: G5000 Equipment Removal & Replacement
Gives instructions for the removal and replacement of G5000 and GFC700 equipment.
Section 7: G5000 Equipment Configuration & Testing
Gives instructions for loading software, configuring, and testing of G5000 equipment.
Section 8: System Return to Service Procedure
Specifies return-to-service procedures to be performed upon completion of maintenance of the G5000
system.
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page 1-3
1.3 Acronyms & 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
CES: Cabin Entertainment System
CFR: Code of Federal Regulations
DFDP Display Format and Dimming Panel
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
LWD: Left Wing Down
MFD: Multi-Function Display
MFW: Multi-Function Window
OAT: Outside Air Temperature
PFD: Primary Flight Display
RAT: Ram Air Temperature
RCCB: Remote Controlled Circuit Breaker
RVSM: Reduced Vertical Separation Minimum
RWD: Right Wing Down
SAT: Static Air Temperature
STBY: Standby
STC: Supplemental Type Certificate
TAWS: Terrain Awareness & Warning System
WAAS: Wide Area Augmentation System
VHF: Very High Frequency
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page 1-4
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 1-1, Required Documents
Document Number
Document Title
005-00756-00
Master Drawing List, G5000/GFC 700, Beechjet 400A
005-00756-01
Garmin ODA Certification Plan, Beechjet 400A
005-00756-02
General Arrangement, G5000GFID &GFC 700, Beechcraft Model 400A
005-00756-04
Existing Equipment Removals, Beechjet Model 400A
005-00756-05
Wire Harness Routing/Inst, Nose, Beechjet Model 400A
005-00756-06
Wire Harness Routing, Cabin, Beechjet Model 400A
005-00756-07
Wire Harness Routing/Inst, Tail Beechjet Model 400A
005-00756-08
Nose Avionics Install, Beechjet Model 400A
005-00756-09
Main Instrument Panel Install, Beechjet Model 400A
005-00756-10
Circuit Breaker Panels Modification, Beechjet 400A
005-00756-13
Antenna Install, Beechjet 400A
005-00756-14
Roll Servo Install, Beechjet Model 400A
005-00756-15
Pitch Servo Install, Beechjet Model 400A
005-00756-16
Yaw Servo Install, Beechjet Model 400A
005-00756-19
Pedestal Equipment Install, Beechjet Model 400A
005-00756-46
Console Panel Beechjet Model 400A
005-00756-50
Pitot/Static Modification, Beechjet Model 400A
005-00756-54 Wire Harness Routing/Inst, Tail Beechjet Model 400A, Older S/N
005-00756-60 Wire Harness Routing/Inst, Cabin Beechjet Model 400A, Older S/N
005-00756-95 Wire Harness Routing/Inst, Nose Beechjet Model 400A, Older S/N
005-00756-C4
RVSM Static Port Markings
005-00756-D2 Circuit Breaker Panels Modification, Early S/N Beechjet Model 400A
005-W0230-00
Wiring Diagram, G5000/GFC 700, Beechjet Model 400A
005-W0236-00
Wiring Diagram, G5000/GFC 700, Beechjet Model 400A, Early S/N
320-00750-XX
Wiring Harness Assembly, Beechjet Model 400A
320-01005-XX
Wiring Harness Assembly, Beechjet Model 400A, Early S/N
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page 1-5
Document Number
Document Title
190-00836-00
GSR 56 Installation Manual
190-00355-07
GDL 69 Series TSO Installation Manual
190-00303-75
GCU 275/47X Installation Manual
190-00303-74
GTA 82 Trim Adapter Installation Manual
190-01360-00
GEA 7100 Installation Manual
190-00303-10
GRS 77/GMU 44 Installation Manual
190-01100-00
GDC 7400 Air Data Computer Installation Manual
190-00303-85
GSA 9000/GSM 9100 Installation Manual
190-00987-00
GTC 570 Installation Manual
190-00829-01
GWX 70 Weather Radar Installation Manual
190-00836-00
GSR 56 Installation Manual
190-00303-26
GSD 41 Installation Manual
190-00926-01
GTX 3000 Installation Manual
190-00858-01
GMA 36 Installation Manual
190-00303-29
GDU 1200W Installation Manual
190-00303-05
GIA 63 Installation Manual
190-00355-07
GDL 69 Series TSO Installation Manual
190-00355-04
GDL 69 Series SiriusXM® Satellite Radio Activation Instructions
190-00313-63
GMU 44 Installation Location Magnetic Interference Survey Procedure
190-01508-03
FAA Approved Airplane Flight Manual Supplement
9017782
Model MD302 Series Standby Attitude Module, Installation Manual and
Operating Instructions*
*Non-Garmin Document
TP-336
Emergency Power Supply JET Model PS-835 Installation Manual
128-590001-9
Beechjet Model 400/400A Maintenance Manual*
*Non-Garmin Document
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 Revision and Distribution
This document is required for maintaining the continued airworthiness of the aircraft. When this document
is revised, each page will also be revised to indicate the current revision level.
G5000 System Maintenance Manual 190-01508-01
Beechcraft Model 400A Rev. 5
Page 1-6
Garmin Dealers may obtain the latest revision of this document on the Garmin Dealer Resource Center
website.
Owners/operators may obtain the latest revision of this document by one of the following methods:
Visit https://fly.garmin.com/support
Contact a Garmin dealer
Contact Garmin Product Support at 913-397-8200, toll free 866-739-5687, or use around the world
contact information on https://fly.garmin.com/
A Garmin Service Bulletin describing the revision to this document will be sent to aircraft owners and
operators if the revision is determined to be significant.
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Garmin G5000 for Beechjet Owner's manual

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Owner's manual

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