Garmin G5000 for Beechjet 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. 1

G5000 System Maintenance Manual 190-01508-01

Beechcraft Model 400A Rev. 1

Page ii

Garmin Ltd. or its subsidiaries

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 ------

G5000 System Maintenance Manual 190-01508-01

Beechcraft Model 400A Rev. 1

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DOCUMENT PAGINATION

Section Pagination

Table of Contents i  xiii

Section 1 1-1  1-5

Section 2 2-1  2-27

Section 3 3-1  3-54

Section 4 4-1  4-58

Section 5 5-1  5-86

Section 6 6-1  6-21

Section 7 7-1  7-89

Section 8 8-1  8-21

G5000 System Maintenance Manual 190-01508-01

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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. 1

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 ............................................................................................. 2-14

2.3 Electrical Power Distribution .......................................................................................... 2-19

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 Engine and Serial Number ................................................................................... 3-33

3.12 400A Max TO Weight ..................................................................................................... 3-34

3.13 400A Performance Kit .................................................................................................... 3-35

3.14 Garmin Optional Equipment and Features .................................................................... 3-36

3.15 Software Load Confirmation .......................................................................................... 3-37

3.16 Non-Garmin Support Options ........................................................................................ 3-38

3.17 Configurations Requiring Enablement Software ............................................................ 3-44

3.18 Terrain/Obstacle/Basemap/Safe Taxi/Airport Directory/Charts Database Loading ....... 3-51

3.19 Standby Navigation Database Loading .......................................................................... 3-52

3.20 Aircraft Registration Number Entry ................................................................................ 3-53

3.21 Configuration Confirmation ............................................................................................ 3-53

3.22 Activation of SiriusXM Radio and Weather .................................................................... 3-54

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

4.8 Garmin LRU Redundant Ground Path Checks .............................................................. 4-23

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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 .......................................................................... 4-45

4.15 Emergency Frequency Switch Check ............................................................................ 4-45

4.16 G5000 Display Lighting Check ....................................................................................... 4-46

4.17 G5000 Display Format Mode Check .............................................................................. 4-46

4.18 G5000 HSDB Connection Check ................................................................................... 4-47

4.19 G5000 Redundant Connection Check ........................................................................... 4-50

4.20 Annunciator Panel Power Check ................................................................................... 4-55

4.21 Rudder Boost Movement Check .................................................................................... 4-56

4.22 Rudder Boost Inhibit Active Logic Check ....................................................................... 4-57

5. TROUBLESHOOTING ............................................................................................................. 5-1

5.1 G5000 Alerting System .................................................................................................... 5-2

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 GTX Troubleshooting ..................................................................................................... 5-65

5.12 GDL 69A Troubleshooting ............................................................................................. 5-66

5.13 GRS and GMU Troubleshooting .................................................................................... 5-67

5.14 GDC Troubleshooting .................................................................................................... 5-73

5.15 GWX Troubleshooting .................................................................................................... 5-74

5.16 GCU Troubleshooting .................................................................................................... 5-74

5.17 GMC Troubleshooting .................................................................................................... 5-75

5.18 GTC Troubleshooting ..................................................................................................... 5-75

5.19 Software/Configuration Troubleshooting ........................................................................ 5-76

5.20 System Communication Hierarchy ................................................................................. 5-79

5.21 Aircraft Harness/LRU Connectors .................................................................................. 5-80

5.22 Standby Indicator Troubleshooting ................................................................................ 5-92

6. G5000 EQUIPMENT REMOVAL & REPLACEMENT ............................................................. 6-1

6.1 GDU 1200W Display Unit................................................................................................. 6-2

6.2 GIA 63W Integrated Avionics Unit ................................................................................... 6-2

6.3 GSA 9000 Servo Actuator ................................................................................................ 6-3

6.4 GSM 9100 Servo Mount................................................................................................... 6-4

6.5 GMC 7250 Autopilot Mode Controller .............................................................................. 6-4

6.6 GTA 82 Trim Adapter ....................................................................................................... 6-4

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6.7 GTC 570 Touchscreen Controller .................................................................................... 6-6

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 ............................................................................................. 6-12

6.19 Iridium Antenna .............................................................................................................. 6-12

6.20 GPS/WAAS/SXM Antennas ........................................................................................... 6-13

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 ....................................................................................................... 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 ................................................................................................. 7-3

7.3 GDC 7400 Air Data Computer ......................................................................................... 7-5

7.4 GDL 69A Data Link ........................................................................................................ 7-10

7.5 GDU 1200W MFD & PFD .............................................................................................. 7-13

7.6 GEA 7100 Engine and Airframe Unit ............................................................................. 7-18

7.7 GIA 63W Integrated Avionics Unit ................................................................................. 7-31

7.8 GMA 36 Audio Processor and Marker Beacon Receiver ............................................... 7-35

7.9 GMC 7250 Autopilot Mode Controller ............................................................................ 7-41

7.10 Radar Altimeter .............................................................................................................. 7-43

7.11 GRS 77 AHRS/GMU 44 Magnetometer ......................................................................... 7-44

7.12 GSD 41 Data Concentrator ............................................................................................ 7-55

7.13 GSA 9000 Servo Actuator .............................................................................................. 7-57

7.14 GSR 56 Satellite Receiver Functional Check ................................................................ 7-58

7.15 GTA 82 Trim Actuator .................................................................................................... 7-60

7.16 GTC 570 Touch Screen Controller ................................................................................ 7-61

7.17 GTX 3000 Transponder ................................................................................................. 7-63

7.18 GWX 70 Airborne Weather Radar ................................................................................. 7-65

7.19 MD 302 Standby Attitude Module .................................................................................. 7-67

7.20 RVSM Checks ................................................................................................................ 7-70

7.21 TAWS Functional Check ................................................................................................ 7-76

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7.22 FliteCharts Functional Check ......................................................................................... 7-78

7.23 ChartView Functional Check .......................................................................................... 7-79

7.24 SafeTaxi Functional Check ............................................................................................ 7-80

7.25 Low Speed Awareness .................................................................................................. 7-80

7.26 Non-Garmin Traffic System (TCAS II) Functional Check (Optional) ............................. 7-83

7.27 DME 1 Functional Check (Optional) .............................................................................. 7-84

7.28 DME 2 Functional Check (Optional) .............................................................................. 7-84

7.29 ADF 1 Functional Check (Optional) ............................................................................... 7-85

7.30 ADF 2 Functional Check (Optional) ............................................................................... 7-85

7.31 Cockpit Voice Recorder Functional Check (Optional) ................................................... 7-86

7.32 Autopilot Disengagement Check .................................................................................... 7-88

7.33 Standby Battery Checks................................................................................................. 7-90

7.34 Nose Fan Operational Check ......................................................................................... 7-90

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

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

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Figure 2-20, Standby Instrument and Standby Power Switch .................................................... 2-14

Figure 2-21, G5000 Beechcraft Model 400A Architecture (Summary) ....................................... 2-15

Figure 2-22, Power Generation Overview ................................................................................... 2-20

Figure 2-23, Left Main Bus / Left Load Bus ................................................................................ 2-21

Figure 2-24, Right Main Bus / Right Load Bus............................................................................ 2-22

Figure 2-25, Emergency Bus ...................................................................................................... 2-23

Figure 2-26, Battery / Standby Bus / L-R Overhead Bus ............................................................ 2-24

Figure 2-27, L-R Nonessential / Galley Buses ............................................................................ 2-25

Figure 2-28, Left Radio Master / Right Radio Master Buses ...................................................... 2-26

Figure 2-29, Dual Powered Units / Ground Comm ..................................................................... 2-27

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

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 ............................................................... 4-44

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

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Page x

Figure 5-5, GFC Status Page...................................................................................................... 5-35

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

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

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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) .................................................................... 7-17

Figure 7-2, Normal Engine Instrument Markings (MFD) ............................................................. 7-19

Figure 7-3, GPS Status Page (MFD) .......................................................................................... 7-33

Figure 7-4, Marker Beacon Symbology ...................................................................................... 7-39

Figure 7-5, Pitch/Roll Offset ........................................................................................................ 7-47

Figure 7-6, GRS/GMU Calibration .............................................................................................. 7-47

Figure 7-7, GRS/GMU Calibration Procedure ............................................................................. 7-48

Figure 7-8, GRS/GMU Calibration .............................................................................................. 7-50

Figure 7-9, Magnetometer Calibration ........................................................................................ 7-50

Figure 7-10, Magnetometer Verification ...................................................................................... 7-51

Figure 7-11, Engine Run Up ....................................................................................................... 7-52

Figure 7-12, Engine Run Up Page .............................................................................................. 7-52

Figure 7-13, AHRS Information Valid .......................................................................................... 7-54

Figure 7-14, GSD Status Page ................................................................................................... 7-57

Figure 7-15, GSR56 Configuration Page .................................................................................... 7-59

Figure 7-16, Aircraft Registration Configuration.......................................................................... 7-65

Figure 7-17, MD302 Configure Menu ......................................................................................... 7-68

Figure 7-18, RVSM Critical Region ............................................................................................. 7-71

Figure 7-19, Paint Stripe Limitations ........................................................................................... 7-72

Figure 7-20, Dial Indicator ........................................................................................................... 7-73

Figure 7-21, Static Port Measurement ........................................................................................ 7-74

Figure 7-22, Static Port Measurement Locations ....................................................................... 7-75

Figure 7-23, Squat Switch Air/Gnd ............................................................................................. 7-81

Figure 7-24, Low Speed Awareness Band and Approach Cue Symbolization ........................... 7-82

Figure 7-25, Squat Switch Air/Ground ........................................................................................ 7-86

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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Tables

Table Page

Table 1-1, Required Documents ................................................................................................... 1-4

Table 2-1, G5000 and Supporting Equipment ............................................................................ 2-16

Table 2-2, Non-Garmin Interface Support ................................................................................... 2-17

Table 2-3, Notable G5000 Features ........................................................................................... 2-17

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 .......................................................................................................... 7-8

Table 7-3, Vertical Speed .............................................................................................................. 7-9

Table 7-4, Engine Indication Test Equipment ............................................................................. 7-20

Table 7-5, Fuel Flow Test Points ................................................................................................ 7-20

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Page xiii

Table 7-6, Fuel Temperature Test Points ................................................................................... 7-21

Table 7-7, Oil Temperature Test Points ...................................................................................... 7-22

Table 7-8, N1 Test Points ........................................................................................................... 7-23

Table 7-9, N2 Test Points ........................................................................................................... 7-24

Table 7-10, Oil Pressure Test Points .......................................................................................... 7-27

Table 7-11, ITT Test Points ......................................................................................................... 7-29

Table 7-12, Required GRS/GMU Calibrations ............................................................................ 7-46

Table 7-13, MD302 Range Marking Menu .................................................................................. 7-69

Table 7-14, Static Port Measurement Log .................................................................................. 7-75

G5000 System Maintenance Manual 190-01508-01

Beechcraft Model 400A Rev. 1

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. 1

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. 1

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. 1

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

005-00756-08 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-C4 RVSM Static Port Markings

005-W0230-00 Wiring Diagram, G5000/GFC 700, Beechjet Model 400A

320-00750-XX Wiring Harness Assembly, Beechjet Model 400A

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

G5000 System Maintenance Manual 190-01508-01

Beechcraft Model 400A Rev. 1

Page 1-5

Document Number Document Title

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

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.

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.

G5000 System Maintenance Manual 190-01508-01

Beechcraft Model 400A Rev. 1

Page 2-1

2. SYSTEM DESCRIPTION

This section provides an overview of the G5000 GIFD and GFC 700 AFCS that is installed on the

Beechcraft Model 400A in accordance with STC ST01821WI.

The installation incorporates three high-resolution 12-inch flight displays, along with two touch screen

display/controllers that serve as the primary crew interface for the system. The landscape oriented flight

displays have multi-pane capability that allow essential flight data to be displayed with electronic maps &

charts, TAWS, TCAS, flight plan and weather information on multiple flight display windows

simultaneously. A GMC 7250 autopilot controller and GCU 275 Display controller are installed above the

MFD and both PFDs respectively. A 3-in-1 digital standby instrument (Mid Continent Instruments Model

MD302) is installed beneath the MFD, along with the relocated fuel quantity indicators. The forward

pedestal transition panel includes two GTC 570 touch-screen controllers. A new display format and

dimming panel and miscellaneous switch panel is installed in the aft pedestal (not shown, see Section 3.4

for additional detail). There are additional modifications to the electrical power distribution system,

overhead dimming panel and circuit breaker panels.

Refer Figure 2-1 for the instrument panel layout.

Figure 2-1, G5000 Instrument Panel Layout in the Model 400A Beechjet

Engine indications are normally shown on the MFD engine indicating window or on the PFD during

display reversion mode, except as noted in the list below. There are no changes in engine gauge limits or

markings with the implementation of the G5000; engine gauge limits are incorporated based on existing

AFM/AFMS limitation data.

Gauges/indicators removed and incorporated into the G5000 are as follows:

• ITT

• N1 fan

• N2 turbine

• Oil pressure

• Oil temperature

G5000 System Maintenance Manual 190-01508-01

Beechcraft Model 400A Rev. 1

Page 2-2

• Fuel flow

• Fuel temperature

• Consumed fuel totalizer

• Engine vibration (provided on the GTC summary page)

Additionally, the G5000 will perform automated calculation of the target N1 speed (N1 bug) based on

equations that have been derived using approved AFM/AFMS data and charts.

The AOA indicator, hydraulic pressure indicator, pressurization control and indicators, and crew alerting

system are retained by this installation. Some of these items are relocated within the instrument panel to

accommodate the new equipment placement.

2.1 Equipment Descriptions

2.1.1 GFC 700 Operation

The GFC 700 is a digital Automatic Flight Control System (AFCS), fully integrated within the G5000

system avionics architecture. The GFC 700 AFCS functionality is distributed across the following Line

Replaceable Units (LRUs):

• GDU 1200W Primary Flight Displays (PFDs) – 2 LRUs

• GDU 1200W Multi-Function Display (MFD) – 1 LRU

• GIA 63W Integrated Avionics Units – 2 LRUs

• GSA 9000 Servos – 3 LRUs

• GSM 9100 Gearbox – 3 LRUs

• GMC 7250 A/P Mode Controller – 1 LRU

• GTA 82 Trim Adapter – 1 LRU

The GFC 700 AFCS is designed as a three-axis fail passive digital flight control. The following functions

are provided by the GFC 700 in this installation:

• Flight Director

• Autopilot

• Yaw Damper

• Rudder Boost

Flight Director:

The Flight Directors operate within the GIA 63Ws and use data from the G5000 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 7250 allows the pilot to switch the active

director between flight director #1 (GIA1) and flight director #2 (GIA2). The Flight Director provides:

• Command Bars showing pitch/roll guidance

• Vertical/lateral mode selection and processing

• Autopilot communication

Autopilot:

The autopilot operates with two Garmin Servo Actuators (GSA) 9000 servos used to provide primary pitch

and roll control. A Garmin Trim Adapter (GTA) 82 interfaces to the existing pitch trim control system for

automatic pitch trim control. The LH/RH GIA interface to the existing roll trim system for automatic roll

trim control. Flight director data is processed within the servos and turned into aircraft primary and

secondary flight control surface commands. The autopilot cannot operate unless the flight director is

engaged. The autopilot provides servo monitoring and Automatic Flight Control in response to Flight

Director steering commands, utilizing AHRS and ADC sensor information.

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