190-00355-00 February 2020 Revision G
System Maintenance Manual
GDL 69/69A Part 23 AML STC
Contains Instructions for Continued Airworthiness
for STC SA01487SE-D
Aircraft Make, Model, Registration Number, and Serial
Number along with the applicable STC configuration
information must be completed in Appendix A and
saved with aircraft permanent records.
190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
Rev. G Page A
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®
and GDL
®
, are registered trademarks of Garmin International or its subsidiaries.
Garmin Pilot™ is a trademark of Garmin International or its subsidiaries. These trademarks may not be
used without the express permission of Garmin.
© 2020 Google, Inc. All rights reserved. Android™ is a trademark of Google, Inc.
© 2020 The Bluetooth
®
word mark and logos are registered trademarks owned by Bluetooth SIG, Inc. and
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®
is a registered trademark of Cisco in the U.S. and other countries.
SiriusXM
®
, Sirius
®
, XM
®
and all related marks and logos are trademarks of Sirius XM Radio Inc.
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190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
Rev. G Page B
RECORD OF REVISIONS
CURRENT REVISION DESCRIPTION OF CHANGES
Revision Revision Date Description
E 05/09/11
Update referenced documents (2.1). Add periodic bonding test
(2.5.2, 2.12). Add GRC 10 battery service (2.4). Clarify ODA role
(2.15).
F 06/11/15
Combined maintenance manual and ICA. Added Flight Stream 110
to manual.
G
02/12/20
Updated part numbers and software version for new SXM tuner
models.
Section Description
1.3 Added new second generation tuner part numbers.
7.1
Added a note about required software version for installations with GI 275 or new tuner
models.
190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
Rev. G Page i
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 Code of Federal Regulations (CFR), Chapter
VII, Subchapter C) and which may not be exported, released, or disclosed to foreign nationals inside or
outside of the United States without first obtaining an export license. A violation of the EAR may be
subject to a penalty of up to 10 years imprisonment and a fine of up to $1,000,000 under Section 2410 of
the Export Administration Act of 1979. Include this notice with any reproduced portion of this document.
This information in this document is subject to change without notice. Visit the Garmin website at
w
ww.garmin.com for current updates and supplemental information concerning the operation of Garmin
products.
DEFINITIONS OF WARNINGS, CAUTIONS, AND NOTES
WARNING
Warnings indicate that immediate attention must be given to avoid potential
equipment damage and personal injury should the instructions be disregarded.
CAUTION
Cautions indicate an alert to potential damage to the equipment if the
procedural step is not directly followed.
NOTE
Notes indicate additional information is needed.
190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
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TABLE OF CONTENTS
1 INTRODUCTION .............................................................................................................................1-1
1.1 Content, Scope and Purpose ......................................................................................................1-2
1.2 Organization ..............................................................................................................................1-2
1.3 Definitions and Abbreviations ..................................................................................................1-3
1.4 Publications ...............................................................................................................................1-4
1.5 ICA Revision and Distribution ..................................................................................................1-4
2 SYSTEM OVERVIEW .....................................................................................................................2-1
2.1 System Interfaces ......................................................................................................................2-2
2.2 Ground Plane .............................................................................................................................2-3
3 GDL 69/69A CONTROL AND OPERATION ...............................................................................3-1
3.1 GDL 69/69A Controls ...............................................................................................................3-1
3.2 GDL 69/69A Configuration ......................................................................................................3-1
4 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ........................................................4-1
4.1 Airworthiness Limitations .........................................................................................................4-2
4.2 Servicing Information ...............................................................................................................4-3
4.3 Maintenance Intervals ...............................................................................................................4-4
5 TROUBLESHOOTING ...................................................................................................................5-1
5.1 GDL 69/69A General Troubleshooting .....................................................................................5-2
5.2 GRT 10/GRC 10 General Troubleshooting ..............................................................................5-4
5.3 Flight Stream 110 General Troubleshooting .............................................................................5-5
6 REMOVAL AND REPLACEMENT INFORMATION ...............................................................6-1
6.1 Unit Return ................................................................................................................................6-2
6.2 GDL 69/69A Removal and Reinstallation ................................................................................6-3
6.3 GRT 10 Removal and Reinstallation ........................................................................................6-5
6.4 GRC 10 Remote Control Battery Replacement ........................................................................6-6
6.5 Flight Stream 110 ......................................................................................................................6-7
6.6 Configuration Module ...............................................................................................................6-8
6.7 Flight Stream 110 Bonding Strap ............................................................................................6-10
7 RETURN TO SERVICE ..................................................................................................................7-1
7.1 Return-to-Service Procedures ...................................................................................................7-2
7.2 Test Procedures .........................................................................................................................7-5
APPENDIX A AIRCRAFT SPECIFIC INFORMATION .................................................................A-1
A.1 GDL 69/69A Configuration Log ..............................................................................................A-2
A.2 GRT 10/GRC 10 Configuration Log ........................................................................................A-3
A.3 Flight Stream 110 Configuration Log ......................................................................................A-4
A.4 Wire Routing ............................................................................................................................A-5
A.5 Aircraft Wiring Diagrams ........................................................................................................A-7
APPENDIX B SPECIAL BONDING PROCEDURES ...................................................................... B-1
B.1 Considerations for Untreated or Bare Dissimilar Metals ......................................................... B-2
B.2 Preparation of Aluminum Surfaces .......................................................................................... B-3
B.3 Composite Aircraft ................................................................................................................... B-3
B.4 Tube and Fabric Aircraft .......................................................................................................... B-8
190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
Rev. G Page iii
LIST OF FIGURES
Figure 2-1 GDL 69/69A ........................................................................................................................2-1
Figure 2-2 GDL 69 System Interface Diagram .....................................................................................2-2
Figure 6-1 GDL 69/69A Mounting Rack Assembly .............................................................................6-4
Figure 6-2 GRT 10 .................................................................................................................................6-5
Figure 6-3 GRC 10 Remote Control Battery Department .....................................................................6-6
Figure 6-4 Flight Stream Assembly Overview ......................................................................................6-7
Figure 6-5 Backshell Assembly .............................................................................................................6-9
Figure 6-6 Flight Stream Bonding .......................................................................................................6-11
Figure A-1 Wire Routing - Single Engine .............................................................................................A-5
Figure A-2. Wire Routing - Twin Engine ...............................................................................................A-6
Figure B-1 Electrical Bonding Preparation - Nut Plate ......................................................................... B-2
Figure B-2 Electrical Bonding Preparation - Bolt/Nut Joint ................................................................. B-2
Figure B-3 Electrical Bonding Preparation - Terminal Lug .................................................................. B-2
Figure B-4 Fiberglass insulation for Carbon Material .......................................................................... B-4
Figure B-5 Aluminum Tape Joint .......................................................................................................... B-5
Figure B-6 Aluminum Tape Ground Termination ................................................................................ B-6
Figure B-7 GDL 69/69A Aluminum Tape Installation ......................................................................... B-7
Figure B-8 Bonding Clamp Assembly .................................................................................................. B-9
190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
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LIST OF TABLES
Table 1-1 Garmin Publications ...............................................................................................................1-4
Table 2-1 Ground Plane Definitions and Ground Path Resistance Requirements .................................2-3
Table 4-1 Periodic Maintenance .............................................................................................................4-4
Table 5-1 GDL 69/69A Troubleshooting Guide ....................................................................................5-2
Table 5-2 GRT 10/GRC 10 Troubleshooting .........................................................................................5-4
Table 5-3 Flight Stream 110 Troubleshooting .......................................................................................5-5
Table 6-1 Flight Stream Bonding Hardware ........................................................................................6-11
Table 7-1 Configuration and Checkout Procedures ...............................................................................7-5
Table B-1 Composite Airframe Bonding Hardware .............................................................................. B-5
Table B-2 Materials Required but Not Supplied .................................................................................... B-8
190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
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1 INTRODUCTION
1.1 Content, Scope and Purpose ............................................................................................................1-2
1.2 Organization .....................................................................................................................................1-2
1.3 Definitions and Abbreviations .........................................................................................................1-3
1.4 Publications ......................................................................................................................................1-4
1.5 ICA Revision and Distribution ........................................................................................................1-4
190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
Rev. G Page 1-2
1.1 Content, Scope and Purpose
This document provides Instructions for Continued Airworthiness (ICA) of the GDL 69/69A SiriusXM
®
satellite receiver, optional GRT 10/GRC 10 wireless remote, and optional Flight Stream 110 Bluetooth
®
transceiver as installed under STC SA01487SE-D.
1.2 Organization
The following outline briefly describes the organization of this manual:
Section 2: System Description
Section 2 provides a description of the equipment installed by STC SA01487SE-D. An overview of the
GDL 69/69A, GRT 10/GRC 10, and Flight Stream 110 system interface is also provided.
Section 3: GDL 69/69A Control and Operation
Section 3 provides information on basic control, operation, configuration, and software loading
specifically tailored to maintenance practices. Basic GDL 69/69A and GRT 10/GRC 10 configuration
mode operation and software loading is also described.
Section 4: Instructions for Continued Airworthiness
Section 4 provides instructions for continued airworthiness of the GDL 69/69A, GRT 10/GRC 10, and
Flight Stream 110 systems.
Section 5: Troubleshooting
Section 5 provides troubleshooting information to aid in diagnosing and resolving potential problems with
the GDL 69/69A, GRT 10/GRC 10, and Flight Stream 110 equipment.
Section 6: Equipment Removal and Reinstallation
Section 6 provides instructions for the removal and reinstallation of the GDL 69/69A, GRT 10/GRC 10,
and Flight Stream 110 equipment.
Section 7: Return to Service
Section 7 provides instructions for testing the GDL 69/69A, GRT 10/GRC 10, and Flight Stream 110
equipment along with return to service procedures to be performed upon completion of maintenance of the
GDL 69/69A, GRT 10/GRC 10, and Flight Stream 110 equipment.
Appendix A: Installation Specific Information
APPENDIX A provides a template to record general installation information and the system configuration
log for a specific installation of the GDL 69/69A, GRT 10/GRC 10, and Flight Stream 110 equipment.
190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
Rev. G Page 1-3
1.3 Definitions and Abbreviations
Definitions
Except where specifically noted, references made to the GDL 69/69A will be synonymous with all
GDL 69 Series unit part numbers.
First generation models are GDL 69 (P/N 011-00986-00) and GDL 69A (P/N 011-00987-00).
Second generation models are GDL 69 SXM (P/Ns 011-03177-00 or 011-03177-05) and GDL 69A SXM
(P/Ns 011-03177-10 or 011-03177-15).
Throughout this document, references will be made to metallic and nonmetallic aircraft. For the purpose of
this manual, metallic aircraft will be those with an aluminum skin. Nonmetallic aircraft will refer to all
other aircraft (e.g., wooden aircraft, aircraft with composite skin, or aircraft with tube and fabric
construction).
Abbreviations
The following abbreviations/acronyms are used within this document:
AML: Approved Model List
CFR: Code of Federal Regulations
EAR: Export Administration Regulations
FAA: Federal Aviation Administration
HSDB: High Speed Data Bus
IAW: In Accordance With
ICA: Instructions for Continued Airworthiness
LRU: Line Replaceable Unit
ODA: Organization Designation Authorization
PED: Portable Electronic Device
RMA: Return Merchandise Authorization
STC: Supplemental Type Certificate
190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
Rev. G Page 1-4
1.4 Publications
Table 1-1 lists publications related to the operation and maintenance of the GDL 69/69A, optional
GRT 10/GRC 10, and optional Flight Stream 110 devices.
Table 1-1 Garmin Publications
1.5 ICA Revision and Distribution
This manual is a requirement for maintaining the continued airworthiness of the aircraft. Garmin dealers
may obtain the latest revision of this document at the Garmin Dealer Resource Center
website.
Dealers are notified of manual revision changes via a Garmin Service Bulletin.
Owners and operators may obtain the latest revision of this manual at www.flyGarmin.com
or by
contacting a Garmin dealer. Garmin contact information is available at www.flyGarmin.com
.
Part Number Garmin Document
190-01532-00
Garmin Pilot User’s Guide for Android™
190-01501-00
Garmin Pilot User’s Guide for iOS
®
005-C0217-00 GDL 69/69A Part 23 AML STC Master Data List
190-00355-04 GDL 69 Series SiriusXM Satellite Radio Activation Instructions
190-00355-02 GDL 69/69A Part 23 AML STC Installation Manual
190-00355-11 GRC 10 User’s Guide
190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
Rev. G Page 2-1
2 SYSTEM OVERVIEW
2.1 System Interfaces .............................................................................................................................2-2
2.1.1 GDL 69/69A Data Link .........................................................................................................2-2
2.1.2 GRT 10 ...................................................................................................................................2-2
2.1.3 Flight Stream 110 ...................................................................................................................2-2
2.2 Ground Plane ...................................................................................................................................2-3
The GDL 69/69A is a SiriusXM satellite radio data link receiver (see Figure 2-1) performing the following
system functions:
Reception of graphical and textual weather data
Reception of audio entertainment data (GDL 69A only)
Output of weather data to interfaced control display device or Portable Electronic Device (PED)
via Flight Stream.
Output of audio entertainment data (GDL 69A only)
The optional GRT 10/GRC 10 is a wireless remote system for passengers to control the audio functions of
the Garmin GDL 69A data link receiver. The system consists of two components: (1) the GRT 10 wireless
transceiver installed in the aircraft and connected to the GDL 69A serial port, and (2) the GRC 10 wireless
remote with an LCD display.
The optional Flight Stream 110 Bluetooth transceiver is used to interface the GDL 69/69A to a compatible
PED. SiriusXM weather data can be displayed and audio functions (GDL 69A only) can be controlled on
the PED.
Figure 2-1 GDL 69/69A
190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
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2.1 System Interfaces
2.1.1 GDL 69/69A Data Link
The GDL 69/69A utilizes High Speed Data Bus (HSDB), RS-232, discrete inputs/outputs, and analog
audio inputs/outputs to communicate with other Line Replaceable Units (LRU) and systems on the aircraft.
See Figure 2-2 for a summary of the GDL 69/69A interfaces.
Figure 2-2 GDL 69 System Interface Diagram
2.1.2 GRT 10
The GRT 10 utilizes RS-232 and discrete inputs to communicate with the GDL 69A.
2.1.3 Flight Stream 110
The Flight Stream 110 communicates with PEDs using Bluetooth technology. RS-232 is used to
communicate with the GDL 69/69A and RS-422 is used to communicate with other LRUs.
Garmin
GDL 69/69A
Flight Stream
(Optional)
PED
Audio Panel
(GDL 69A Only)
Garmin Display
(GDU, GTN, GNS, GMX, etc.)
SiriusXM Antenna
GRT 10 Transceiver
(Optional, GDL 69A Only)
GRC 10 Remote
Remote Audio
Switches
(Optional, GDL 69A Only)
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Rev. G Page 2-3
2.2 Ground Plane
For the purpose of this STC, aircraft ground plane definitions vary according to airframe type and aircraft
model as defined in Table 2-1. Refer to the periodic test and reconditioned resistance values corresponding
to these ground plane definitions when performing the equipment bonding test in Section 4.3. Ensure that
all GDL 69 Series antenna coaxial cables are disconnected during resistance checks.
Table 2-1 Ground Plane Definitions and Ground Path Resistance Requirements
Aircraft Type/Model
Ground
Reference
Maximum Resistance Between
GDL 69 Series Unit Chassis and
Ground Reference (mΩ)
Notes
Periodic Test Reconditioned
Metal airframe
Nearby Metal
Structure
10.0 2.5
Tube and fabric airframe
Nearby Metal
Structure
10.0 2.5
Composite VFR-only Models
Aermacchi S.211A Instrument Panel 50.0 25.0
Diamond
DA20-A1,
DA20-C1
Instrument Panel 50.0 25.0
DA 40 Instrument Panel 50.0 25.0
Grob
G115,
G115A,
G115B
Instrument Panel 50.0 25.0
G115C,
G115C2,
G115D,
G115D2,
G115EG
Instrument Panel 50.0 25.0 [2]
G120A Instrument Panel 50.0 25.0 [2]
G520 Egrett,
G520T
Instrument Panel 50.0 25.0 [2]
Slingsby
T67M260,
T67M260-T3A
Instrument Panel 50.0 25.0
Composite IFR Models
Beech 390
Nearby structure
lightning ground
foil
10.0 5.0
Cessna
LC40-550FG,
LC41-550FG,
LC42-550FG
Nearby aluminum
lightning ground
bar/strip
10.0 5.0
Cirrus
SR20,
SR22
Local grounded
structure (such as
seat support
structure, entry
step)
10.0 5.0
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[1] Diamond DA 40 and DA 40F with Diamond OSB 40-004/3 incorporated, or aircraft with
similar factory-installed lightning protection supporting IFR operation.
[2] Some S/N are IFR from the factory. IFR models must use values of 10.0 and 5.0 for bonding
tests, and LRU must be grounded to available lightning ground per manufacturer SRM or other
approved data.
Diamond DA 40
Nearby structure
lightning ground
tube
10.0 5.0 [1]
Aircraft Type/Model
Ground
Reference
Maximum Resistance Between
GDL 69 Series Unit Chassis and
Ground Reference (mΩ)
Notes
Periodic Test Reconditioned
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3 GDL 69/69A CONTROL AND OPERATION
3.1 GDL 69/69A Controls
The GDL 69/69A does not have a direct pilot interface. The GDL 69/69A is controlled via a separately
installed control display device, or through a PED, if the Flight Stream 110 is installed. The GDL 69A
audio features can be controlled by optional mounted switches (located in the cabin), the optional GRC 10
wireless remote controller if a GRT 10 wireless transceiver is installed, or a PED if a Flight Stream 110 is
installed. Refer to the applicable control display pilot’s guide. For GRT 10/GRC 10 installations, refer to
GRC 10 User’s Guide for additional information. For Flight Stream 110 installations, refer to Garmin Pilot
User’s Guide for iOS or Garmin Pilot User’s Guide for Android, depending on your PED operating
system.
3.2 GDL 69/69A Configuration
Configuration and software loading of the GDL 69/69A is performed through the control display device.
Refer to the applicable control display device installation manual for configuration procedures and
software loading steps.
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4 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
4.1 Airworthiness Limitations ...............................................................................................................4-2
4.2 Servicing Information ......................................................................................................................4-3
4.2.1 Periodic Maintenance .............................................................................................................4-3
4.2.2 Special Tools ..........................................................................................................................4-3
4.3 Maintenance Intervals ......................................................................................................................4-4
This manual is designed for use by the installing agency of the Garmin GDL 69/69A system as Instructions
for Continued Airworthiness (ICA), in accordance with 14 CFR 23.1529, and part 23, appendix G. This
ICA includes information required by the operator to adequately maintain the GDL 69/69A system
installed under the AML STC.
190-00355-00 System Maintenance Manual GDL 69/69A Part 23 AML STC
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4.2 Servicing Information
The GDL 69/69A does not require servicing. In the event of a system failure, troubleshoot the
GDL 69/69A in accordance with Section 5.
GRC 10 Remote Control Battery Replacement
If the unit does not turn on, or the battery level indicator on the display shows no bars, replace the batteries.
See Section 6.4 for details.
NOTE
Failure of the GRC 10 (i.e. dead batteries) has no impact on normal aircraft operations
and is only used for passengers to control audio entertainment.
4.2.1 Periodic Maintenance
All antennas connected to the GDL 69/69A should be maintained in accordance with appropriate
inspection data for the antenna installation.
4.2.2 Special Tools
A milliohm meter with an accuracy of +/- 0.1 m
Ω (or better) is required to measure the electrical bonding
between the GDL 69/69A system components and aircraft ground.
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4.3 Maintenance Intervals
Table 4-1 Periodic Maintenance
Item Description/Procedure Interval
Equipment Removal
and Replacement
Removal and replacement of the following items. See Section 6
for instructions.
• GDL 69/69A unit
• GRT 10 unit
• Flight Stream 110
On Condition
Battery
Replacement
Removal and replacement of GRC 10 batteries. See Section 6.4
for instructions.
On Condition
Visual Inspection
The GDL 69/69A, GRT 10 (if installed), Flight Stream 110 (if
installed), switches, and wiring harnesses should be inspected to
ensure continued integrity of the installation.
Visual inspection of the GDL 69/69A.
1. Inspect the GDL 69/69A for security of attachment, including
visual inspection of mounting rack and other supporting
structure attaching the rack to aircraft.
2. Verify the countersunk fastener heads are in full contact with
unit mounting rack holes. If fasteners are loose, re-torque to
12 to 15 in-lbs and complete the electrical bonding test.
3. Inspect for signs of corrosion. If corrosion is found, treat in
accordance with aircraft maintenance manual.
4. Inspect condition of wiring, switches, shield terminations,
routing, and attachment/clamping. Correct any issues
identified by replacing damaged wiring/shield terminations
and re-attaching as necessary. Replace any damaged
switches.
Visual inspection of the GRT 10 (if installed).
1. Inspect the GRT 10 for security of attachment.
2. Verify fastener heads are secure. Tighten to snug plus
one-quarter turn if necessary.
3. Inspect condition of wiring, shield terminations, routing, and
attachment/clamping. Correct any issues identified by
replacing damaged wiring/shield terminations and
re-attaching as necessary.
Visual inspection of the Flight Stream 110 (if installed).
1. Inspect the Flight Stream 110 for security of attachment.
2. Verify fastener heads are secure. Tighten to snug plus
one-quarter turn if necessary.
3. Inspect condition of wiring, shield terminations, routing, and
attachment/clamping. Correct any issues identified by
replacing damaged wiring/shield terminations and
re-attaching as necessary.
12 Calendar
Months
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