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Garmin G5 Installation Manual
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Garmin G5 Electronic Flight
Instrument Part 23 AML STC Installati
on Manual
190
-01112-
10
Rev. 21
Page
178
5.20.1
HSI Co
nfigur
ation
Config Page
Config Option
Configuration Setting
Device
Information
Installation Type
Certified Instrument
Diagnostics/Data Log
Enabled
Attitude Configuration
Ind
icator Type
Normal
Pitch Display
Normal
Roll Display
For Fixed Type Pointers G5 Config =
Ground Pointer
or
For Movable Type Pointers G5 Co
nfig = Sky Pointer
Standard Turn Roll Reference
Hide
Automatic Declutter
Disabled
Air Data
Air Data Sensors
Enabled
Vertical Speed Indicator
(1)(2)
Airspeed
Note: Configure Units prior to
setting airspeeds.
VNE
(1)(2)(3)
VNO
(1)(2)(3)
VSO
(1)(2)(3)
VS1
(1)(2)(3)
VFE
(1)(2)(3)
VA
(1)(2)(3)
VX
(1)(2)(3)
VY
(1)(2)(3)
VG
(1)(2)(3)
VR
(1)(2)(3)
VMC
(1)(2)(3)
VYSE
(1)(2)(3)
Magnetometer
Magnetometer
Enabled
Orientation
Connector Aft
Or
Connector Forward
Or
Connector Port
Or
Connector Starboard
Flight Controls
Garmin Autopilot Servos
None
Analog Autopilot Interface
None
Or
See Section
5.23
if a Non-
Garmin Autopilot is interfaced
Backlight
Current Mode
Automatic
Default Mode
Automatic
Minimum Photocell Input
Default
Minimum Display Brightness
Default
Maximum Photocell Input
Default
Maximum Display Brightness
Default
Filter Time Constant
Default
Display
HSI Page
Enabled
Power Up Page
HSI
Battery
Show Battery Status
When Using Battery
Automatic Power Off
On Ground Only
GPS
Internal GPS Receiver
Disabled
GPS Data Fields
Show
177
179
Table of Contents
Default Chapter
6
Table of Contents
6
1 General Description
13
Introduction
13
Acronyms and Abbreviations
14
Reference Documents
14
Table 1-1: Reference Documents
14
STC Permission
15
Scope
15
Figure 1-4 GMU 11
15
Table 1-2 G5 Attitude and G5 DG/HSI Equipment
15
System Overview
16
Figure 1-1, G5 Electronic Flight Instrument (Attitude)
16
Figure 1-2 G5 Standby Battery
18
Figure 1-3 G5 Electronic Flight Instrument (DG/HSI)
19
Figure 1-5 GAD 29/29B
22
Figure 1-6 - Glare Shield Mounted GPS Antenna
23
Figure 1-8 - GTP 59 (Temperature Probe)
24
Technical Specifications
25
Table 1-3: Physical Characteristics
25
Table 1-4: Power Requirements
25
2 Limitations
26
Installation Limitations
26
Operational Limitations
26
3 Installation Overview
27
Introduction
27
Installation Materials
27
Table 3-1: Contents of the G5 Installation Kit (011-03892-00)
27
Table 3-2: Contents of the GMU 11 Installation Kit (011-04349-90)
27
Table 3-3: Contents of the G5, GMU 11, and GAD 13 Connector Kits (011-03002-00/10)
28
Table 3-4: Contents of the GAD 29/29B Connector Kit (011-03271-00)
28
Table 3-5: G5 Adapter Plate
28
Table 3-6: G5 Recessed Adapter Plate
28
Test Equipment
30
Installation Considerations
30
Table 3-7: G5 and Supporting LRU Circuit Breaker Labels
32
Figure 3-1 CAN Bus Backbone
33
Figure 3-2 Correct CAN Bus Wiring Example and Node Connections
33
Figure 3-3 Incorrect CAN Wiring Example
34
Figure 3-4 CAN Bus Termination (011-02887-00) for G5, GMU 11, and GAD 13
34
Figure 3-5 CAN Bus Termination for GAD 29/29B
35
Figure 3-6 CAN Bus Termination for G5 on M27500 Wire
35
Figure 3-7 GAD 29B Inline Transformer Mounting Instructions
37
Figure 3-8 G5 Diode and Resistor Method a Buildup
38
Figure 3-9 Method a Placement of G5 CAN Bus Resistors
39
Figure 3-10 Method B G5 Resistor Preparation
40
Figure 3-11 Method B Placement of CAN Bus Components
41
Figure 3-12 Wire P/N M27500 Simplified Resistor Connections
41
Figure 3-13 Placement of G5 Power Diode (Bothe Wire Types)
42
4 Installation Procedures
43
Mechanical Installation
43
Figure 4-1 Typical G5 Installations for IFR Approved Aircraft
44
Figure 4-2 G5 Mounting Ring
45
Figure 4-3 Maximum Misalignment of the G5 in the Lateral Axis
45
Figure 4-4 Maximum Misalignment of the G5 in the Longitudinal Axis
46
Figure 4-5 Maximum Misalignment of the G5 in the Vertical Axis
46
Figure 4-6 G5 Alignment Pin
47
Figure 4-7 G5 Hex Driver Insertion
47
Figure 4-8 G5 Captive Mounting Screw Replacement
48
Figure 4-9 Required Vertical Spacing between G5 Units
49
Figure 4-10 Instrument Panel Modification
49
Figure 4-11 G5 Adapter Plate
50
Figure 4-12 G5 Adapter Plate Assembly
50
Figure 4-13, G5 Instrument Hole Dimensions
51
Figure 4-14, Clearance for Connections
52
Figure 4-15 Recessed Adapter Plate
52
Figure 4-16 Recessed Adapter Plate Template Reference Holes
53
Figure 4-17 Single G5 Recessed Adapter Plate Installation
54
Figure 4-18 Single G5 Recessed Installation
54
Figure 4-19 Dual Vertical G5 Recessed Adapter Plate Installation
55
Figure 4-20 Dual Vertical G5 Recessed Installation
55
Figure 4-21 Dual Horizontal G5 Recessed Installation
56
Figure 4-22, Instrument Panel Limitations
57
Figure 4-23 Instrument Panel - View Looking Forward
58
Figure 4-24 Instrument Panel - View with Instruments Removed
58
Figure 4-25 Recessed Adapter Plate Located on Panel
59
Figure 4-26 Match Drilling through Panel - Using Adapter Plate as Template
59
Figure 4-27 Preliminary Trimming of Adapter Plate
60
Figure 4-28 Adapter Plate Located on Far Side of Instrument Panel
60
Figure 4-29 Additional Trimming of Adapter Plate Required
61
Figure 4-30 Trimmed Adapter Plate
61
Figure 4-31 Adapter Plate Mounting Holes
62
Figure 4-32 Dual G5 Panel Cutout - Using Match Drilled Holes for Reference
62
Figure 4-33 Instrument Panel after Cutout for Dual Vertical G5 Units
63
Figure 4-34 Adapter Plate Installed
63
Figure 4-35 Dual Vertical G5 Units Installed
64
Figure 4-36 G5 Flush Mount Adapter Plate Printable Template
65
Figure 4-37 GMU 11 Pitch and Roll Requirements
67
Table 4-1 GMU 11 Supporting Hardware
67
Figure 4-38 GMU 11 Heading Alignment Requirements
68
Figure 4-39 GMU 11 Mounting Hardware
69
Table 4-2 GAD 29/29B, GAD 13 Supporting Hardware
70
Figure 4-40 GAD 29/29B Mounting Hardware
71
Figure 4-41 GAD 13 Mounting Hardware
72
Figure 4-42 - Glare Shield Mounted GPS Antenna Dimensions
74
Figure 4-43 - Glare Shield Mounted GPS Antenna (Screw-Mounted Installation Example)
75
Figure 4-44 - Glare Shield Mounted GPS Antenna (Hook & Loop Installation Example)
76
Figure 4-45 - GTP 59 OAT Probe Dimensions
77
Figure 4-46 - GTP 59 Mounting (Aircraft with Metallic Skin Example)
78
Figure 4-47 - GTP 59 Mounting - Composite Aircraft (Non-Conductive Access Panel)
79
Figure 4-48 - GTP 59 Mounting - Composite Aircraft (Conductive Access Panel)
80
Electrical Installation
81
Table 4-3: Contact Crimp Tooling
81
Table 4-4: G5 (1P51, 2P51), GMU 11 (P111), and GAD 13 (P131) Connector Parts
83
Table 4-5: GAD 29/29B 9-Pin (P291) Connector Parts
84
Table 4-6: GAD 29/29B 25-Pin (P292) Connector Parts
85
Figure 4-49 Wiring Harness Connector Assembly
86
Figure 4-50 Shield Termination Methods
87
Weight and Balance
89
Electrical Load Analysis
89
Table 4-7: LRU Weights
89
Table 4-8: Sample Net Electrical Load Change Calculation
90
Figure 4-51 Ammeter Placement for Current Measurements
92
Figure 4-52 Blank Electrical Load Tabulation Form, Sheet 1 of 2
94
Figure 4-53 Blank Electrical Load Tabulation Form, Sheet 2 of 2
95
Figure 4-54 Sample Completed Electrical Load Tabulation Form, Sheet 1 of 2
96
Figure 4-55 Sample Completed Electrical Load Tabulation Form, Sheet 2 of 2
97
Electrical Bonding
98
Figure 4-56 - Nut and Washer Electrical Bonding
98
Figure 4-57 - Nut Plate Electrical Bonding
98
Figure 4-58 Fiberglass Insulation for Carbon Fiber Material
100
Figure 4-59 Aluminum Tape Joint
100
Figure 4-60 Aluminum Tape Ground Termination
101
Figure 4-61 GAD 29/29B Aluminum Tape Installation (GAD 13 Similar)
102
Table 4-9: Bonding Strap Potential Part Numbers
102
Figure 4-62 #10 Terminal Installation on Garmin Backshell
104
Figure 4-63 - Pan Head Screw Ground Stud Buildup
105
5 System Interconnects
106
G5 Interconnect Notes
107
Figure 5-1 G5 Interconnect Notes
107
Power and Ground
108
Figure 5-2 Power and Ground
108
G5 (ADI) with a GPS Antenna
109
Figure 5-3 G5 (ADI) with a GPS Antenna
109
G5 (ADI) with GPS Position Input
111
Figure 5-4 G5 (ADI) with GPS Position Input
111
G5 (ADI) and GMU 11 with GPS Position Input
115
Figure 5-5 G5 (ADI) and GMU 11 with GPS Position Input
115
G5 (ADI or DG), GMU 11 and GPS Antenna
119
Figure 5-6 G5 (ADI or DG), GMU 11 and GPS Antenna
119
G5 (HSI) with VHF Navigator
122
Figure 5-7 G5 (HSI) with VHF Navigator
122
G5 (HSI) with GPS/VHF Navigator
125
Figure 5-8 G5 (HSI) with GPS/VHF Navigator
125
Figure 5-9 G5 (HSI) with GPS/VHF Navigator Notes
126
Dual G5 Without Navigator
131
Figure 5-10 Dual G5 Without Navigator
131
Dual G5 with VHF Navigator
134
Figure 5-11 Dual G5 with VHF Navigator
134
Dual G5 with GPS/VHF Navigator
138
Figure 5-12 Dual G5 with GPS/VHF Navigator
138
Figure 5-13 Dual G5 with GPS/VHF Navigator Notes
139
G5 (ADI) with GPS/VHF Navigator
144
Figure 5-14 G5(ADI) with GPS/VHF Navigator
144
Figure 5-15 G5 (ADI) with GPS/VHF Navigator Notes
145
G5 (ADI) with VHF Navigator
150
Figure 5-16 G5 (ADI) with VHF Navigator
150
G5 (HSI) with GPS Navigator
154
Figure 5-17 G5 (HSI) with GPS Navigator
154
Dual G5 with GPS Navigator
157
Figure 5-18 Dual G5 with GPS Navigator
157
G5 (ADI) with GPS Navigator
161
Figure 5-19 G5 (ADI) with GPS Navigator
161
G5 (HSI) with Two-Inch GPS Navigator
164
Figure 5-20 G5 (HSI) with GPS Navigator
164
Dual G5 with Two-Inch GPS Navigator
168
Figure 5-21 Dual G5 with Two-Inch GPS Navigator
168
Figure 5-22 Dual G5 with Two-Inch GPS Navigator Notes
169
G5 (ADI) with Two-Inch GPS Navigator
173
Figure 5-23 G5 (ADI) with Two-Inch GPS Navigator
173
Figure 5-24 G5 (ADI) with Two-Inch GPS Navigator Notes
174
G5 Portable Avionics Unit Interface
177
Figure 5-25 G5 Portable Avionics Unit Interface
177
GAD 13 Interface
180
Figure 5-26 GAD 13 Interface
180
GAD 29B Interface to Garmin Autopilots
181
GAD 29B Interface to Non-Garmin Autopilots
182
Table 5-1: Non-Garmin Autopilots
182
Figure 5-27 GAD 29B Interface to Century Autopilots, Sheet 1 of 2
183
Figure 5-28 GAD 29B Interface to Century Autopilots, Sheet 2 of 2
184
Figure 5-29 GAD 29B Interface to Cessna Autopilots, Sheet 1 of 2
186
Figure 5-30 GAD 29B Interface to Cessna Autopilots, Sheet 2 of 2
187
Figure 5-31 GAD 29B Interface to Honeywell Autopilots
188
Figure 5-32 GAD 29B Interface to S-TEC Autopilots
190
Figure 5-33 GAD 29B Interface to Piper Autopilots
192
6 System Configuration and Checkout Procedures
194
Overview
194
Mounting, Wiring, and Power Checks
194
Post-Installation Checkout Procedures
194
Figure 1-7 - GAD 13
198
Table 6-1: Post-Installation Calibration Procedure Summary
198
Figure 6-1, Attitude Calibration Example
200
Figure 6-2, Example of Calibration Equations
200
Figure 6-3 Engine Vibration Test Failure Indication
202
Table 6-2: Heading Verification
205
Figure 6-4 ADI Display of OAT and TAS (Typical Values Shown)
212
Figure 6-5 HSI Display of Crosswind (Typical Values Shown)
213
Figure 6-6 Example EMC Source/Victim Matrix
214
Documentation Checks
217
Figure 6-7 J51 on the G5
219
Appendix
219
Connector Information
219
Figure 6-8 J111 on the GMU 11
220
Figure 6-9 J291 on the GAD 29/29B
222
Figure 6-10 J292 on the GAD 29/29B
222
Figure 6-11 J131 on the GAD 13
224
Figure 6-12 GTP 59
225
Figure 6-13 G5 Outline Drawing
226
Outline and Installation Drawings
226
Figure 6-14 G5 Installation Drawing
227
Figure 6-15 G5 Panel Cutout Measurements (Not to Scale)
228
Figure 6-16 GAD 29/29B Outline Drawing
229
Figure 6-17 GAD 29/29B Install Breakdown
230
Figure 6-18 GMU 11 Outline Drawing
231
Figure 6-19 GMU 11 Install Breakdown
232
Figure 6-20 GAD 13 Outline Drawing
233
Figure 6-21 GAD 13 Install Breakdown
234
Figure 6-22 GTP 59 Outline Drawing
235
Figure 6-23 GTP 59 Install Breakdown
236
Magnetic Interference Survey
237
Figure 6-24 Magnetic Interference Test Harness
238
Gmu 11 Mounting in Nonmetallic Wingtip
241
Figure 6-25 GMU 11 Overbraid Installation
242
Figure 6-26 GMU 11 Overbraid Termination
243
Model Specific Data
244
Table 6-3: Aircraft Model-Specific Data
245
Table 6-4: Lightning Zoning Legend
267
Lightning Protection
267
Figure 6-27 Zoning for Wingtips on Aircraft Not Limited to VFR Operation
268
Figure 6-28 Zoning for Wingtips on Aircraft Limited to VFR Operations
270
Figure 6-29 Zoning for Wings Affected by Landing Gear
271
Figure 6-30 Zoning for a Single Propeller (Low- or High-Wing)
272
Figure 6-31 Zoning for a Low- or High-Wing Canard with a Rear-Mounted Propeller
273
Figure 6-32 Zoning for a Low- or High-Wing Aircraft with a Curved Lower Fuselage
274
Figure 6-33 Zoning for a Single, Rear-Mounted Prop above Fuselage
275
Figure 6-34 Zoning for Front-Mounted Twin Propellers (Low- or High-Wing)
276
Figure 6-35 Zoning for Rear-Mounted Twin Propellers (Low- or High-Wing)
277
Figure 6-36 Zoning for Front- and Rear-Mounted Propellers (Low- or High-Wing)
278
Figure 6-37 Zoning for High-Wing with Front and Rear Propellers Mounted above Fuselage
279
Figure 6-38 Zoning for Low or High Wing Canard with Twin Rear-Facing Props
280
Figure 6-39 Zoning for Single-Propeller Biplane
281
Figure 6-40 Zoning for Empennage
282
Figure 6-41 V-Tail Empennage Zoning
283
Figure 6-42 Dual Vertical Stabilizer with Low Horizontal Stabilizer Zoning
283
Figure 6-43 Example Lightning Zoning for Single-Engine Aircraft
284
Figure 6-44 Example Lightning Zoning for Twin-Engine Aircraft
285
Other manuals for Garmin G5
User Manual
168 pages
Pilot's Guide
96 pages
Install Manual & Pilot's Guide
238 pages
Maintenance Manual
62 pages
4
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Garmin G5 Specifications
General
Brand
Garmin
Model
G5
Category
Avionics Display
Language
English
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