Garmin 0140000 Users Manual
SPECIFICATION |
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REVISIONS |
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DESCRIPTION |
ECO NO. |
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CONTROL |
Q |
12/29/09 |
Added antenna note |
68178 |
DRAWING |
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03/23/10 |
Added Standalone Rack info |
70476 |
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07/29/10 |
Added updated NAV/COM unit |
73976 |
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8.5" |
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GIA 63/GIA 63W |
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Installation Manual |
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3-Hole |
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DER REVIEW REQUIRED |
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NOTES: |
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1. |
DESCRIPTION: G1000 Installation Documentation - GIA 63/GIA 63W Installation Manual |
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PAGE SIZE: |
Letter: Width = 8.5 inches, Height = 11 inches |
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Tabloid: Width = 11.0 inches, Height = 17.0 inches |
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3. |
PAGINATION: 48 double-sided letter sheets. |
11 single-sided tabloid sheets. |
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4.MATERIAL: 24 pound bond. Approved equivalents allowed.
5.COLOR: Black Ink on White Paper Stock.
6.BINDERY: Three-hole punch, shrink-wrap. Digital output preferred
7.FOLDS: Z-Fold tabloid sheets at end of document.
8.ELECTRONIC ARTWORK: Shall Conform to Garmin Archive, Filename: 190-00303-05.pdf
The following files have been archived under the above ARCHIVE FILENAME.
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190-00303-05.pdf |
Portable Document Format, contains Installation Manual and Release Specification |
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release.indd |
Adobe InDesign Format, Release Specification |
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Manual Elements |
Word 97 for PC, Formatted Files and Figures |
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CONFIDENTIAL |
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Garmin Ltd. or its subsidiaries |
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This drawing and the specifications contained herein are the property of Garmin |
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c/o Garmin International, Inc. |
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Ltd. or its subsidiaries and may not be reproduced or used in whole or in part as |
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1200 E. 151st Street |
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the basis for manufacture or sale of products without written permission . |
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Olathe, Kansas 66062 U.S.A. |
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Date: |
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Drafter: |
John Sherman |
11/17/03 |
TITLE: GIA 63/GIA 63W Installation Manual |
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Checker: |
Daniel Cobb |
11/17/03 |
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PART NO: |
190-00303-05 |
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Project Engineer: |
Craig Parker |
11/17/03 |
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DER REVIEW REQUIRED |
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1 of 1 |
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Released By: |
SDT |
11/18/03 |
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GIA 63/GIA 63W
Installation Manual
190-00303-05 |
July, 2010 |
Revision S |
© Copyright 2010 Garmin Ltd. or its subsidiaries
All Rights Reserved
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express prior written consent of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed and to print one copy of this manual or of any revision hereto, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin International, Inc.
1200 E. 151st Street
Olathe, KS 66062 USA
Telephone: 913-397-8200
Aviation Dealer Technical Support Line (Toll Free): (888) 606-5482
www.garmin.com
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Garmin (Europe) Ltd |
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Liberty House |
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Bulls Copse Road |
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Hounsdown Business Park |
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Southampton, SO40 9RB, UK |
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Telephone: 44/ (0) 870.8501241 |
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RECORD OF REVISIONS |
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Revision |
Revision |
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Description |
Date |
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A |
11/15/04 |
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Production Release |
B |
3/16/05 |
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Updated pinout list, removed EQF and ETSO 2C37e deviation |
C |
6/23/05 |
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Added additional interconnects, TSO-C9c, and TSO-C52b |
D |
10/26/05 |
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Added TSO-C151b and boot block instructions |
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E |
6/8/06 |
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Edited document to include the GIA 63W |
F |
7/21/06 |
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Corrected WAAS TSO |
G |
9/19/06 |
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Added RTCA/DO-229C deviation |
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H |
10/18/06 |
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Added Comant antennas |
J |
4/10/07 |
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Added Comant antenna and revised ICAW |
K |
6/6/07 |
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Added the 011-01105-01 unit |
L |
8/23/07 |
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Changed operational limitations and added antennas |
M |
2/29/08 |
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Added ETSO information |
N |
5/27/09 |
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Added TSO-C92c and other TSO info |
P |
09/09/09 |
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Added Level A CLD information |
Q |
12/29/09 |
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Added antenna note |
R |
03/23/10 |
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Added standalone rack info |
S |
7/29/10 |
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Added updated NAV/COM unit |
Page A |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
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CURRENT REVISION DESCRIPTION |
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Revision |
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Section |
Description of Change |
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Number(s) |
Number |
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1-2 |
1.3.1 |
Clarified RS-485 channel information |
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Added annunciator outputs |
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1-4 |
1.4.5 |
Corrected Antenna power supply at GPS port spec |
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1-5 |
1.4.6 |
Clarified transmitter power spec |
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1-8 |
1.4.10 |
Clarified power requirements |
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1-9 |
1.4.11 |
Added 011-01105-20 |
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1-14 – 1-16 |
1.6.3 |
Updated software part number range |
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1-21 – 1-25 |
1.6.5 |
Added updated NAV/COM TSO compliance info |
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1-27 |
1.6.9 |
Clarified regulatory criteria |
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2-1 |
2.1.1 |
Added updated NAV/COM unit |
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2-10 |
2.4 |
Removed wire guidance and added barrel contacts info |
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3-4 |
3.8 |
Added 011-01105-20 |
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4-1 |
4.1.1 |
Added -20 pins |
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4-3 |
4.1.2 |
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4-4 |
4.1.2 |
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S |
4-7 |
4.1.4 |
Corrected pin 3 to read “OUT” |
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4-15 |
4.4.1.2 |
Corrected labeling of RS-485/422 pins |
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4-17 |
4.5 |
Corrected ANNUNCIATE pin designation and spec |
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4.6.2.3 |
Deleted “GROUND” and added VOICE ALERT AUDIO |
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4-19 |
specs |
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4.6.2.4 |
Added -20 pins |
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4-20 |
4.7.1 |
Added GLIDESLOPE COMPOSITE OUT explanation |
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and -20 pins |
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Added -20 pins |
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4-1 – 4-30 |
4 |
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Added note indicating some pins are not currently |
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supported and removed pins that are not supported from |
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descriptions |
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C-1 |
C-1 |
Added wire length guidance |
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C-3 |
C-1 |
Added references to Note 7 and 8 |
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C-5 |
C-1 |
Added cross side interconnects |
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DOCUMENT PAGINATION
Section |
Page Range |
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Table of Contents |
i – vi |
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Section 1 |
1-1 |
– 1-32 |
Section 2 |
2-1 |
– 2-16 |
Section 3 |
3-1 |
– 3-6 |
Section 4 |
4-1 |
– 4-30 |
Appendix A |
A-1 |
– A-4 |
Appendix B |
B-1 |
– B-8 |
Appendix C |
C-1 |
– C-14 |
GIA 63/GIA 63W Installation Manual |
Page i |
190-00303-05 |
Revision S |
This manual reflects the operation of main software version 5.31 for the GIA 63 and main software version 6.00 for the GIA 63W. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions.
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.
WARNING
Perchlorate Material – special handling may apply, See www.dtsc.ca.gov./hazardouswaste/perchlorate.
Page ii |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
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TABLE OF CONTENTS |
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PARAGRAPH |
PAGE |
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1 |
GENERAL DESCRIPTION.............................................................................................................. |
1-1 |
1.1 |
Introduction........................................................................................................................................ |
1-1 |
1.2 |
Equipment Description ...................................................................................................................... |
1-1 |
1.3 |
Interface Summary............................................................................................................................. |
1-2 |
1.4 |
Technical Specifications .................................................................................................................... |
1-3 |
1.5 |
License Requirements...................................................................................................................... |
1-10 |
1.6 |
Certification ..................................................................................................................................... |
1-10 |
1.7 |
Referenced Documents .................................................................................................................... |
1-30 |
1.8 |
Limited Warranty............................................................................................................................. |
1-31 |
2 |
INSTALLATION OVERVIEW ........................................................................................................ |
2-1 |
2.1 |
Introduction........................................................................................................................................ |
2-1 |
2.2 |
Installation Considerations ................................................................................................................ |
2-5 |
2.3 |
Rack Considerations .......................................................................................................................... |
2-9 |
2.4 |
Cabling and Wiring.......................................................................................................................... |
2-10 |
2.5 |
Cooling Air ...................................................................................................................................... |
2-10 |
2.6 |
GIA 63 Minimum Installation Requirements .................................................................................. |
2-11 |
2.7 |
GIA 63W Minimum Installation Requirements .............................................................................. |
2-12 |
2.8 |
Mounting Requirements .................................................................................................................. |
2-13 |
3 |
INSTALLATION PROCEDURE...................................................................................................... |
3-1 |
3.1 |
Unpacking Unit.................................................................................................................................. |
3-1 |
3.2 |
Wiring Harness Installation ............................................................................................................... |
3-1 |
3.3 |
Antenna Installation........................................................................................................................... |
3-2 |
3.4 |
Cable Installation .............................................................................................................................. |
3-2 |
3.5 |
Backshell Assembly........................................................................................................................... |
3-3 |
3.6 |
Unit Installation ................................................................................................................................. |
3-3 |
3.7 |
Post Installation Configuration & Checkout...................................................................................... |
3-4 |
3.8 |
Continued Airworthiness ................................................................................................................... |
3-4 |
4 |
SYSTEM INTERCONNECTS.......................................................................................................... |
4-1 |
4.1 |
Pin Function List................................................................................................................................ |
4-1 |
4.2 |
Power and Antennas ........................................................................................................................ |
4-13 |
4.3 |
GIA System ID Program.................................................................................................................. |
4-14 |
4.4 |
Serial Data ....................................................................................................................................... |
4-14 |
4.5 |
Discrete I/O...................................................................................................................................... |
4-17 |
4.6 |
COM/VOR/ILS/Digital Audio ........................................................................................................ |
4-18 |
4.7 |
VOR/ILS Indicator .......................................................................................................................... |
4-20 |
4.8 |
RMI/OBI.......................................................................................................................................... |
4-23 |
4.9 |
DME Tuning and ADF .................................................................................................................... |
4-24 |
4.10 |
Auto Pilot......................................................................................................................................... |
4-26 |
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GIA 63/GIA 63W Installation Manual |
Page iii |
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190-00303-05 |
Revision S |
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PARAGRAPH |
PAGE |
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APPENDIX A GIA 63 MAIN BOOT BLOCK UPLOADING INSTRUCTIONS................................. |
A-1 |
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A.1 |
Introduction....................................................................................................................................... |
A-1 |
A.2 |
Determining Current Boot Block...................................................................................................... |
A-1 |
A.3 |
Loading Boot Block Version 4.01 .................................................................................................... |
A-2 |
A.4 |
Loading GIA Main Software (only if GIA main software was cancelled in Section A.2) ............... |
A-3 |
APPENDIX B OUTINE & INSTALLATION DRAWINGS.................................................................. |
B-1 |
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APPENDIX C INTERCONNECT EXAMPLES..................................................................................... |
C-1 |
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LIST OF FIGURES |
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FIGURE |
PAGE |
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2-1 |
GPS Antenna Considerations............................................................................................................. |
2-7 |
2-2 |
GIA 63(W) Modular Rack............................................................................................................... |
2-13 |
2-3 |
GIA 63(W) Standalone Rack........................................................................................................... |
2-14 |
2-4 |
GIA 63(W) Standalone Rack, Suggested Mounting Locations ....................................................... |
2-15 |
3-1 |
Coaxial Cable Installation.................................................................................................................. |
3-2 |
3-2 |
GIA STATUS Page ........................................................................................................................... |
3-5 |
B-1 |
GIA 63(W) Modular Installation Outline Drawing .......................................................................... |
B-1 |
B-2 |
GIA 63(W) Modular Installation Drawing ....................................................................................... |
B-3 |
B-3 |
GIA 63(W) Standalone Installation Outline Drawing ...................................................................... |
B-5 |
B-4 |
GIA 63(W) Standalone Installation Drawing ................................................................................... |
B-7 |
C-1 |
GIA 63(W) Example Interconnect (Sheet 1 of 7)............................................................................. |
C-1 |
C-1 |
GIA 63(W) Example Interconnect (Sheet 2 of 7)............................................................................. |
C-3 |
C-1 |
GIA 63(W) Example Interconnect (Sheet 3 of 7)............................................................................. |
C-5 |
C-1 |
GIA 63(W) Example Interconnect (Sheet 4 of 7)............................................................................. |
C-7 |
C-1 |
GIA 63(W) Example Interconnect (Sheet 5 of 7)............................................................................. |
C-9 |
C-1 |
GIA 63(W) Example Interconnect (Sheet 6 of 7)........................................................................... |
C-11 |
C-1 |
GIA 63(W) Example Interconnect (Sheet 7 of 7)........................................................................... |
C-13 |
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LIST OF TABLES |
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TABLE |
PAGE |
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3-1 |
Pin Contact Part Numbers.................................................................................................................. |
3-1 |
3-2 |
Recommended Crimp Tools .............................................................................................................. |
3-1 |
3-3 |
Long Term Power Interrupt Category A (200 mS) Mod Status ........................................................ |
3-4 |
Page iv |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
GIA 63 HARDWARE MOD LEVEL HISTORY
The following table identifies hardware modification (Mod) Levels for the GIA 63. Mod Levels are listed with the associated service bulletin number, service bulletin date, and the purpose of the modification. The table is current at the time of publication of this manual (see date on front cover) and is subject to change without notice. Authorized Garmin Sales and Service Centers are encouraged to access the most up-to-date bulletin and advisory information on the Garmin Dealer Resource web site at www.garmin.com using their Garmin-provided user name and password.
APPLICABLE |
MOD |
SERVICE |
SERVICE |
PURPOSE OF MODIFICATION |
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LRU PART |
BULLETIN |
BULLETIN |
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LEVEL |
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DATE |
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This modification consists of |
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1 |
0416 |
9/13/2004 |
modifying the voice alert audio output |
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circuit, enabling it to power down |
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when not in use. |
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This Service Bulletin consists of |
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2 |
0418 |
9/8/2004 |
visually inspecting the GIA 63 Main2 |
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board for incorrectly installed |
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011-00781-00 |
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capacitors. |
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This modification addresses a |
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3 |
0505 |
1/19/2005 |
potential GIA 63 COM transceiver |
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interference condition. |
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4 |
N/A |
N/A |
More robust capacitors installed in the |
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power supply backup circuit. |
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011-00781-01 |
1 |
N/A |
N/A |
More robust capacitors installed in the |
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power supply backup circuit. |
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GIA 63/GIA 63W Installation Manual |
Page v |
190-00303-05 |
Revision S |
GIA 63W HARDWARE MOD LEVEL HISTORY
The following table identifies hardware modification (Mod) Levels for the GIA 63W. Mod Levels are listed with the associated service bulletin number, service bulletin date, and the purpose of the modification. The table is current at the time of publication of this manual (see date on front cover) and is subject to change without notice. Authorized Garmin Sales and Service Centers are encouraged to access the most up-to-date bulletin and advisory information on the Garmin Dealer Resource web site at www.garmin.com using their Garmin-provided user name and password.
APPLICABLE |
MOD |
SERVICE |
SERVICE |
PURPOSE OF MODIFICATION |
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LRU PART |
BULLETIN |
BULLETIN |
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LEVEL |
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NUMBER |
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DATE |
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011-01105-00 |
1 |
N/A |
N/A |
More robust capacitors installed in the |
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power supply backup circuit. |
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Page vi |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
1 GENERAL DESCRIPTION
1.1Introduction
This manual presents mechanical and electrical installation requirements for installing the GIA 63(W) as part of a Garmin Integrated Flight Deck. The GIA 63(W) can be integrated into a variety of airframes under an appropriate TC or STC. Each airframe installation may vary. Use only approved (type or supplemental type) data for specific installation instructions in a particular aircraft.
1.2Equipment Description
The GIA 63(W) is a microprocessor-based input/output Line Replaceable Unit (LRU) used in a Garmin Integrated Flight Deck. The GIA 63(W) communicates with the GDU via Ethernet high-speed data bus (HSDB), and with other LRUs using RS-232, RS-485/422, and ARINC 429. All configuration is done through the GDU. The GIA 63(W) contains the following sub-assemblies:
•A main processor that interfaces with all LRUs in the G1000 sub-system and performs calculations for the GFC 700 autopilot (if equipped).
•A twelve channel parallel GPS receiver that simultaneously tracks and uses up to 12 satellites. The GIA 63W includes a 15 channel WAAS certified GPS receiver.
•A VHF COM transceiver that provides tuning from 118.00 to 136.992 MHz in 25 kHz or 8.33 kHz spacing for 760 or 2280 channel configuration respectively.
•A VOR/ILS localizer receiver that provides tuning from 108.00 to 117.95 MHz in 50 kHz increments.
•An ILS glideslope receiver that provides tuning from 328.6 to 335.4 MHz as paired with the frequency tuned on the VOR/ILS localizer receiver.
CAUTION
The operation of unapproved cellular telephones or other unapproved cellular devices aboard aircraft while airborne is prohibited by FCC rules. Due to the potential for interference with onboard systems, the operation of unapproved cellular communication devices while onboard an aircraft that is on the ground is subject to FAA regulations 14 CFR 91.21.
FCC regulation 47 CFR 22.925 prohibits airborne operation of unapproved cellular telephones installed in or carried aboard aircraft. Unapproved cellular telephones must not be operated aboard any aircraft while the aircraft is off the ground. When any aircraft leaves the ground, all unapproved cellular telephones on board that aircraft must be turned off.
Unapproved cellular telephones that are on, even in a monitoring state, can disrupt GPS performance.
GIA 63/GIA 63W Installation Manual |
Page 1-1 |
190-00303-05 |
Revision S |
1.3Interface Summary
1.3.1 Primary Interfaces
The GIA 63(W) is designed as an open architecture system that provides the following interfaces:
•1 dedicated Ethernet High-Speed Data Bus (HSDB) input/output channel
•2 Controller Area Network (CAN) I/O channels
•8 Main ARINC 429 inputs
•3 Main ARINC 429 outputs
•1 VOR/ILS ARINC 429 input
•1 VOR/ILS ARINC 429 output
•5 RS-485 input/output channels (any two RS-485 channels can be configured to form a single RS-422 channel)
•8 RS-232 input/output channels
•41 Discrete inputs
•14 Discrete outputs
•24 Annunciator outputs
1.3.2Additional Interfaces
The GIA 63(W) can provide interfaces for the following additional equipment:
•Autopilot
•Altitude encoder/serializer
•Fuel management systems
•Lightning detection systems
•Traffic awareness systems
•Data link systems
•External annunciators
•DME (including King Serial)
•ADF
Page 1-2 |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
1.4Technical Specifications
1.4.1 Environmental Qualification Form
It is the responsibility of the installing agency to obtain the latest revision of the GIA 63(W) Environmental Qualification Form. This form is available directly from Garmin under the following part number:
GIA 63 Environmental Qualification Form, Garmin part number 005-00148-02 GIA 63W Environmental Qualification Form, Garmin part number 005-00235-00
To obtain a copy of this form, see the dealer/OEM portion of the Garmin web site (www.garmin.com).
1.4.2 Physical Characteristics
Characteristics |
Specifications |
Modular Rack Width |
3.83 inches (9.73 cm) |
Modular Rack Height |
7.26 inches (18.44 cm) |
Standalone Rack Width |
3.88 inches (9.86 cm) |
Standalone Rack Height |
6.91 inches (17.55 cm) |
Depth w/connectors (Modular and Standalone) |
10.20 inches (25.91 cm) |
Unit Weight |
5.3 lbs. (2.40 kg) |
Modular Rack & Connector Weight |
1.9 lbs. (0.86 kg) |
Standalone Rack & Connector Weight |
2.2 lbs. (1.01 kg) |
1.4.3 General Specifications
For detailed specifications, see the Environmental Qualification Form.
Characteristics |
Specifications |
Operating Temperature Range |
-40°C to +65°C. For more details see Environmental |
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Qualification Form. |
Humidity |
95% non-condensing |
Altitude Range |
-1,500 ft to 50,000 ft |
1.4.4 GPS Specifications (GIA 63 only)
Characteristics |
Specifications |
Acquisition Time |
a) Search-the-Sky (without almanac, without initial position |
|
or time): 5 minutes |
|
b) AutoLocate™ (with almanac, without initial position or |
|
time): 5 minutes |
|
c) Cold Start (position known to 300 nm, time known to 10 |
|
minutes, with valid almanac): 45 seconds |
|
d) Warm Start (position known to 10 nm, time known to 10 |
|
minutes, with valid almanac and ephemeris): 15 seconds |
Max Velocity |
1000 knots |
Dynamics |
6 g |
Antenna power supply |
20 mA typical, 40 mA max at 4.6 VDC |
GIA 63/GIA 63W Installation Manual |
Page 1-3 |
190-00303-05 |
Revision S |
1.4.5 WAAS Specific GPS Specifications (GIA 63W only)
Characteristics |
Specifications |
|
Number of channels |
15 (12 GPS and 3 GPS/WAAS/SBAS) |
|
Frequency |
1575.42 MHz L1, C/A code |
|
Sensitivity (acquisition) |
-116 dBm to -134.5 dBm GPS |
|
|
-116 dBm to -134.5 dBm WAAS |
|
Sensitivity (drop lock) |
-144 dBm |
|
Lat/Long position accuracy |
<1.25 meter RMS horizontal, <2 meter vertical, with WAAS |
|
Velocity |
1000 knots maximum (above 60,000 ft) |
|
TTFF (time to first fix) |
1:45 min. typical with current almanac, position, and time |
|
Reacquisition |
10 seconds typical for signal outages of 30 seconds or less |
|
Position update interval |
0.2 sec (5 Hz) |
|
1 pps (pulse per second) |
±275 nsec of UTC second during steady-state navigation |
|
Datum |
WGS-84 |
|
SATCOM compatibility |
Compatible on aircraft equipped with SATCOM (see Section |
|
|
2.1.3.2 for SATCOM compatible antennas) |
|
Antenna power supply at GPS |
4.3 VDC to 4.8 VDC @ 60 mA |
|
port |
||
|
Page 1-4 |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
1.4.6 COM Transceiver Specifications
Characteristics |
Specifications |
Audio Output |
100 mW minimum into a 500 Ω load. |
Audio Response |
Less than 6 dB of variation between 350 and 2500 Hz. |
Audio Distortion |
The distortion in the receiver audio output shall not exceed |
|
25% at all levels up to 100 mW. |
AGC Characteristics |
The audio output shall not vary by more than 6 dB when the |
|
level of the RF input signal, modulated 30% at 1000 Hz, is |
|
varied from 5 μV to 100,000 μV (hard). |
Sensitivity |
(S+N)/N on all channels shall be greater than 6 dB when the |
|
RF level is 2 μV (hard) modulated 30% at 1000 Hz at rated |
|
audio. |
Squelch |
2 μv (hard) ±6 dB for 25 kHz channels. |
|
3 μv (hard) ±6 dB for 8.33 kHz channels. |
Selectivity |
6 dB BW is greater than ±8 kHz for 25 kHz channeling. |
|
60 dB BW is less than ±25 kHz for 25 kHz channeling. |
|
6 dB BW is greater than ±2.778 kHz for 8.33 kHz |
|
channeling. |
|
60 dB BW is less than ±7.37 kHz for 8.33 kHz channeling. |
Spurious Response |
Greater than 80 dB. |
Transmitter Power |
At Least 16 watts when Vin = 28 VDC |
|
At least 10 watts when Vin = 14 VDC (011-01105-2X only) |
Transmitter Duty Cycle |
Recommended 10% maximum. |
Modulation Capability |
The modulation shall not be less than 70% and not greater |
|
than 98% with a standard modulator signal applied to the |
|
transmitter. |
Carrier Noise Level |
Shall be at least 45 dB (S+N)/N. |
Frequency Stability |
0.0005% |
Demodulated Audio Distortion |
Less than 10% distortion when the transmitter is modulated |
|
at least 70%. |
Sidetone |
1.4 VRMS into a 500 Ω load when the transmitter is |
|
modulated at least 70%. |
Demodulated Audio Response |
Shall be less than 6 dB when the audio input frequency is |
|
varied from 350 to 2500 Hz. |
GIA 63/GIA 63W Installation Manual |
Page 1-5 |
190-00303-05 |
Revision S |
1.4.7 VOR Specifications
Characteristics |
Specifications |
Receiver Audio Sensitivity |
At -103.5 dBm (S+N)/N shall not be less than 6 dB. |
Course Deviation Sensitivity |
At –103.5 dBm deviation output shall not be less than 60% |
|
of standard deflection (90 mV) when a VOR deviation test |
|
signal is applied (10 degrees course difference). |
Flag |
The VLOC Course Deviation Flag must be flagged: |
|
a) in the absence of an RF signal. |
|
b) in the absence of the 9960 Hz modulation. |
|
c) in the absence of either one of the two 30 Hz |
|
modulations. |
|
d) When the level of a standard VOR deviation test signal |
|
produces less than a 50% of standard deflection. |
AGC Characteristics |
From -99 dBm to -13 dBm input of a Standard VOR Audio |
|
Test Signal, audio output levels shall not vary more than |
|
3 dB. |
Spurious Response |
Greater than 60 dB. |
VOR OBS Bearing Accuracy |
The bearing information as presented to the pilot shall not |
|
have an error in excess of 2.7° as specified by |
|
RTCA DO-196 and EuroCAE ED-22B. |
Audio Output |
A minimum 100 mW into a 500 Ω load. |
Audio Response |
Less than 6 dB of variation between 350 and 2500 Hz. In |
|
voice mode, an ident tone of 1020 Hz shall be attenuated at |
|
least 20 dB. |
Audio Distortion |
The distortion in the receiver audio output shall not exceed |
|
10% at all levels up to 100 mW. |
Selectivity |
6 dB BW is greater than 16.5 kHz. |
Page 1-6 |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
1.4.8 LOC Specifications
Characteristics |
Specifications |
Receiver Audio Sensitivity |
At -103.5 dBm (S+N)/N shall not be less than 6 dB. |
Course Deviation Sensitivity |
At –103.5 dBm, deviation output shall not be less than 60% |
|
of standard deflection when a LOC deviation test signal is |
|
applied. |
Flag |
The VLOC Course Deviation Flag must be flagged: |
|
a) When the level of a standard deviation test signal |
|
produces 50% or less of standard deflection of the deviation |
|
indicator. |
|
b) In the absence of 150 Hz modulation. |
|
c) In the absence of 90 Hz modulation. |
|
d) In the absence of both 90 Hz and 150 Hz modulation. |
|
e) In the absence of RF. |
AGC Characteristics |
From –99 dBm and –13 dBm input of a Standard VOR |
|
Audio Test Signal, audio output levels shall not vary more |
|
than 3 dB. |
Selectivity |
6 dB BW is greater than 9 kHz. |
|
69 dB BW is less than 36 kHz. |
Standard Deflection |
a) With a standard deflection ‘FLY LEFT’ condition (90 Hz |
|
dominant), the output shall be +90 mV ± 9 mV. |
|
b) With a standard deflection ‘FLY RIGHT’ condition (150 Hz |
|
dominant), the output shall be -90 mV ± 9 mV. |
Spurious Response |
Greater than 60 dB. |
Centering Accuracy |
Typical 0 ± 3 mV (Max error 9.9 mV per RTCA DO-195). |
Audio Output |
A minimum 100 mW into a 500 Ω load. |
Audio Response |
Less than 6 dB of Variation between 350 and 2500 Hz. In |
|
voice mode, an ident tone of 1020 Hz shall be attenuated at |
|
least 20 dB. |
Audio Distortion |
The distortion in the receiver audio output shall not exceed |
|
10% at all levels up to 100 mW. |
GIA 63/GIA 63W Installation Manual |
Page 1-7 |
190-00303-05 |
Revision S |
1.4.9 Glideslope Specifications
Characteristics |
Specifications |
Sensitivity |
At –93 dBm, deviation output shall not be less than 60% of |
|
standard deflection when glideslope deviation test signal is |
|
applied. |
Centering Accuracy |
0 ± .0091 ddm or 0 ± 7.8 mV. |
Selectivity |
6 dB BW is greater than 17 kHz. |
|
69 dB BW is less than 132 kHz. |
Standard deflection |
a) With a standard deflection ‘FLY DOWN’ condition (90 Hz |
|
dominant), the output shall be -78 mV ± 7.8 mV. |
|
b) With a standard deflection ‘FLY UP’ condition (150 Hz |
|
dominant), the output shall be +78 mV ± 7.8 mV. |
Flag |
The GS Course Deviation Flag must be flagged: |
|
a) When the level of a standard deviation test signal |
|
produces 50% or less of standard deflection of the |
|
deviation indicator. |
|
b) In the absence of 150 Hz modulation. |
|
c) In the absence of 90 Hz modulation. |
|
d) In the absence of both 90 Hz and 150 Hz modulation. |
|
e) In the absence of RF. |
1.4.10 Power Requirements
Characteristics |
|
Specifications |
Input Voltage Range |
28 Vdc for PJ601 (14/28 Vdc for 011-01105-20 unit) |
|
|
14/28 Vdc for PJ605 |
|
|
See the Environmental Qualification Form for details on |
|
|
surge ratings and minimum/maximum operating voltages. |
|
Power Requirements for P601 |
0.3 A max @ 27.5 Vdc (not transmitting); |
|
(COM Connector) |
4.3 |
A max @ 27.5 Vdc (transmitting) |
011-01105-20 |
0.6 |
A max @ 13.75 Vdc (not transmitting); |
Power Requirements for P601 |
6.0 A max @ 13.75 Vdc (transmitting) |
|
(COM Connector) |
|
|
Superflag Power |
Power depends upon loads present on Superflag output pins |
|
Requirements for P605 |
(see Sections 4.7.2.1 and 4.10.7) |
|
(Main 2 Connector) |
|
|
Power Requirements for P605 |
1.0 |
A max @ 27.5 Vdc (Without Superflags Active) |
(Main 2 Connector) |
2.0 |
A max @ 13.75 Vdc (Without Superflags Active) |
Page 1-8 |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
1.4.11 Power Interrupt
|
|
Mod |
Long Term Power |
|
Unit Name |
Unit Part Number |
Interrupt Category |
||
Status* |
||||
|
|
Per RTCA DO-160D** |
||
|
|
|
||
|
011-00781-00 |
4 |
A (200mS) |
|
GIA 63 |
0, 1, 2, 3 |
B (50mS) |
||
|
||||
011-00781-01 |
1 |
A (200mS) |
||
|
||||
|
0 |
B (50mS) |
||
|
|
|||
|
011-01105-00 |
1 |
A (200mS) |
|
GIA 63W |
0 |
B (50mS) |
||
|
||||
011-01105-01 |
0 |
A (200mS) |
||
|
||||
|
011-01105-20 |
0 |
A (200mS) |
*Refer to Mod Status Table in front of manual for applicable mod levels.
**Refer to the Section 3.8 for Continued Airworthiness.
GIA 63/GIA 63W Installation Manual |
Page 1-9 |
190-00303-05 |
Revision S |
1.5License Requirements
The Telecommunications Act of 1996, effective February 8, 1996, provides the FCC discretion to eliminate radio station license requirements for aircraft and ships. The GIA 63(W) installation must comply with current transmitter licensing requirements. To find out the specific details on whether a particular installation is exempt from licensing, please visit the FCC web site http://wireless.fcc.gov/aviation.
Transmitter Description: |
Aviation-band VHF transceiver with 25 and 8.33 kHz channel spacing. |
Antenna Characteristics: |
Broad band, 50 ohm, vertically polarized. |
Rated Power: |
16 Watts |
Emission Type: |
6K00A3E |
Frequency of Operation: |
118.00 – 136.992 MHz |
If an aircraft license is required, make application for a license on FCC form 404, application for Aircraft Radio Station License. The FCC also has a fax-on-demand service to provide forms by fax. The GIA 63(W) owner accepts all responsibility for obtaining the proper licensing before using the transmitter.
International transmitter license procedures vary by country. Contact the local spectrum agency for license requirements.
CAUTION
The VHF transmitter in this equipment is guaranteed to meet federal communications commission acceptance over the operating temperature range. Modifications not expressly approved by Garmin could invalidate the license and make it unlawful to operate the equipment.
1.6Certification
The GIA 63 GPS receiver is certified for IFR enroute, terminal, and non-precision approaches. The GIA 63W GPS receiver is WAAS certified.
The GIA 63(W) has been qualified to RTCA/DO-160 Section 20 RF susceptibility and Section 22 lightning requirements. Special installation considerations are required, refer to the Environmental Qualification Form.
The GIA 63(W) meets the requirements for GPS as a Primary Means of Navigation for Oceanic/Remote Operations per FAA Notice N8110.60.
The GIA 63(W) is eligible for B-RNAV in accordance with AMC 20-4.
Eligible for PRNAV in accordance with PRNAV requirements: JAA Administrative & Guidance Material Section One: General Part 3: Temporary Guidance Leaflets, Leaflet No 10: Airworthiness and Operational Approval for Precession RNAV Operations in Designated European Airspace 7.1 Required Functions.
The conditions and tests required for TSO approval of this article are minimum performance standards. It is the responsibility of those installing this article either on or within a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards. TSO articles must have separate approval for installation in an aircraft. The article may be installed only if performed under 14 CFR part 43 or the applicable airworthiness requirements. At the time of publication, installations of this TSO approved article are only approved when installed in an aircraft as part of a Garmin Integrated Flight Deck.
Page 1-10 |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
1.6.1 GIA 63 TSO/ETSO Compliance
Function |
TSO/ETSO |
Category |
Applicable LRU SW Part |
Applicable CLD |
||||
Numbers |
Part Numbers |
|||||||
|
|
|
||||||
|
|
|
|
All |
006-C0046-() |
|||
|
|
|
006-B0190-() |
|
|
|||
|
TSO-C9c |
|
006-C0044-() |
|||||
Automatic Pilots |
|
except |
||||||
ETSO-C9c |
|
006-B0190-00 |
006-C0047-() |
|||||
|
|
|||||||
|
|
|
through |
|
|
|||
|
|
|
006-C0039-01 |
|||||
|
|
|
006-B0190-19 |
|||||
|
|
|
|
|
||||
|
|
|
All |
|
|
006-C0046-() |
||
|
|
|
006-B0190-() |
|
|
|
|
|
Glideslope |
TSO-C34e |
|
|
|
006-C0044-() |
|||
|
except |
|
006-B0083-01 |
|||||
|
|
|
|
|||||
Receiver |
ETSO-2C34f |
|
006-B0190-00 |
|
006-C0047-() |
|||
|
|
|
||||||
|
|
|
through |
|
|
|
|
|
|
|
|
|
|
006-C0039-01 |
|||
|
|
|
006-B0190-04 |
|
|
|||
|
|
|
|
|
|
|
||
|
|
|
All |
|
|
006-C0046-() |
||
|
|
|
006-B0190-() |
|
|
006-C0044-() |
||
Localizer Receiver |
TSO-C36e |
Class A |
except |
|
006-B0082-02 |
|
|
|
|
006-C0047-() |
|||||||
ETSO-2C36f |
006-B0190-00 |
|
||||||
|
|
|
|
006-C0039-01 |
||||
|
|
|
through |
|
|
|||
|
|
|
006-B0190-04 |
|
|
|
|
|
|
|
|
|
|
006-C0053-00 |
|||
|
|
|
|
|
|
|||
VHF COM |
TSO-C37d |
|
All |
|
All |
006-C0046-() |
||
Class 3 and 5 |
|
006-C0044-() |
|
|||||
006-B0190-() |
|
006-B0081-0() |
|
|||||
Transmitter |
ETSO-2C37e |
|
|
|||||
|
except |
|
except |
|
|
|||
|
|
006-C0047-() |
||||||
|
|
|
|
|||||
|
|
|
006-B0190-00 |
006-B0081-00 |
|
|
||
VHF COM |
TSO-C38d |
|
|
|
||||
Class C and E |
through |
|
through |
006-C0039-01 |
||||
Receiver |
ETSO-2C38e |
006-B0190-04 |
|
006-B0081-04 |
||||
|
|
|
|
|||||
|
|
|
|
|
|
|
||
|
|
|
All |
|
|
006-C0046-() |
||
|
|
|
|
|
|
|
||
|
TSO-C40c |
|
006-B0190-() |
|
|
006-C0044-() |
||
VOR Receiver |
|
except |
|
006-B0082-02 |
|
|
||
|
|
006-C0047-() |
||||||
ETSO-2C40c |
|
006-B0190-00 |
|
|||||
|
|
|
|
|
|
|||
|
|
|
|
006-C0039-01 |
||||
|
|
|
through |
|
|
|||
|
|
|
006-B0190-04 |
|
|
|
|
|
|
|
|
|
|
006-C0053-00 |
|||
|
|
|
|
|
|
|||
|
|
|
|
|
|
|
|
|
|
|
|
|
|
All |
006-C0046-() |
||
|
|
|
006-B0190-() |
|
|
|||
Flight Director |
TSO-C52b |
|
006-C0044-() |
|||||
|
except |
|||||||
Equipment |
ETSO-C52b |
|
006-B0190-00 |
006-C0047-() |
||||
|
|
|
through |
|
|
|||
|
|
|
006-C0039-01 |
|||||
|
|
|
006-B0190-19 |
|||||
Ground Proximity |
|
|
|
All |
006-C0046-() |
|||
|
|
006-B0190-() |
|
|
||||
Warning – Glide |
|
|
006-C0044-() |
|||||
|
|
except |
||||||
Slope Deviation |
TSO-C92c |
|
006-B0190-00 |
|
|
|||
|
006-C0047-() |
|||||||
Alerting |
|
|
||||||
|
|
through |
||||||
Equipment |
|
|
006-C0039-01 |
|||||
|
|
006-B0190-29 |
||||||
|
|
|
||||||
|
|
|
All |
|
|
006-C0046-() |
||
|
|
|
006-B0190-() |
|
|
|
|
|
|
TSO-C129a |
|
|
006-B0093-00 |
006-C0044-() |
|||
GPS |
Class A1 |
except |
|
|||||
|
|
|
||||||
ETSO-C129a |
006-B0190-00 |
|
006-B0093-01 |
006-C0047-() |
||||
|
|
|
||||||
|
|
|
through |
|
|
|||
|
|
|
006-B0190-04 |
|
|
|
|
|
|
TSO-C151b |
Class A and B |
|
|
All |
006-C0046-() |
||
|
006-B0190-() |
|
|
|||||
|
006-C0044-() |
|||||||
TAWS |
|
|
except |
|||||
ETSO-C151a |
Class B |
006-B0190-00 |
006-C0047-() |
|||||
|
||||||||
|
through |
|
|
|||||
|
006-C0039-01 |
|||||||
|
|
|
006-B0190-29 |
|||||
|
|
|
|
|
||||
GIA 63/GIA 63W Installation Manual |
Page 1-11 |
190-00303-05 |
Revision S |
1.6.2 GIA 63 TSO/ETSO Deviations
TSO/ETSO |
|
Deviation |
|
TSO-C9c |
1. Garmin was granted a deviation from TSO-C9c to use SAE AS 402B instead of AS- |
|
|
|
402A. |
|
|
|
|
|
|
|
2. |
Garmin was granted a deviation from TSO-C9c to use DO-160D instead of specified |
|
|
environmental tests. |
|
|
|
3. |
Garmin was granted a deviation from TSO-C9c subpart A (c), which requires marking |
|
|
the weight of the unit on the unit. Garmin will provide this information in the installation |
|
|
|
manual in lieu of marking on the serial tag. Garmin does not currently list the weight on |
|
|
|
other avionics units. |
|
|
|
4. |
Garmin was granted a deviation from SAE AS 402B paragraph 4.4.1 to limit autopilot |
|
|
engagement to attitudes considered safe for the certified aircraft. |
|
|
|
5. |
Garmin was granted a deviation from SAE AS 402B paragraph 4.3.2 to not provide |
|
|
servo effort indications when the automatic pilot is not engaged. |
|
|
ETSO-C9c |
1. Garmin was granted a deviation from ETSO-C9c to use SAE AS-402B instead of AS- |
|
|
|
402A. |
|
|
|
2. |
Garmin was granted a deviation from ETSO-C9c to use DO-160D instead of the |
|
|
specified environmental tests. |
|
|
|
3. |
Garmin was granted a deviation from AS-402B paragraph 4.3.2 to not provide servo |
|
|
effort indications when the automatic pilot is not engaged. |
|
|
|
4. |
Garmin was granted a deviation from AS-402B paragraph 4.4.1 to limit autopilot |
|
|
engagement to attitudes considered safe for the certified aircraft. |
|
|
TSO-C34e |
1. Garmin was granted a deviation from TSO-C34e to use DO-160D Change 3 instead of |
|
|
|
DO-160B, and DO-178B instead of DO-178A. |
|
|
TSO-C36e |
1. Garmin was granted a deviation from TSO-C36e to use DO-160D Change 3 instead of |
|
|
|
DO-160B, and DO-178B instead of DO-178A. |
|
|
TSO-C37d |
1. Garmin was granted a deviation from TSO-C37d to use DO-160D Change 3 instead of |
|
|
|
DO-160B, and DO-178B instead of DO-178A. |
|
|
|
2. |
Garmin was granted a deviation from TSO-C37d paragraph (a)(1) to allow using RTCA |
|
|
document DO-186a Change 2 instead of RTCA document DO-186 to specify minimum |
|
|
|
performance standards. |
|
|
|
3. |
Garmin was granted a deviation from TSO-C37d by allowing a 6dB reduction of |
|
|
transmitter power during the Normal Operating Conditions - Emergency Operation Voltage |
|
|
|
as described in RTCA document DO-186a paragraph 2.5.13.1 and RTCA document DO- |
|
|
|
160C paragraph 16.5.2.1. |
|
|
|
4. |
Garmin was granted a deviation from TSO-C37d paragraph (a)(5) to allow 8.33 kHz |
|
|
spacing in addition to the 25 kHz spacing. |
|
|
|
5. |
Garmin was granted a deviation from TSO-C37d paragraph (b)(1) to allow the marking |
|
|
to call out 8.33 kHz spacing in addition to the 25 kHz spacing. |
|
|
TSO-C38d |
1. Garmin was granted a deviation from TSO-C38d to use DO-160D Change 3 instead of |
|
|
|
DO-160B, and DO-178B instead of DO-178A. |
|
|
|
2. |
Garmin was granted a deviation from TSO-C38d paragraph (a)(1) to allow using RTCA |
|
|
document DO-186a Change 2 instead of RTCA document DO-186 to specify minimum |
|
|
|
performance standards. |
|
|
|
3. |
Garmin was granted a deviation from TSO-C38d paragraph (a)(5) to allow 8.33 kHz |
|
|
spacing in addition to the 25 kHz spacing. |
|
|
TSO-C40c |
1. Garmin was granted a deviation from TSO-C40c to use DO-160D Change 3 instead of |
|
|
|
DO-160B, and DO-178B instead of DO-178A. |
|
|
TSO-C52b |
1. Garmin was granted a deviation from SAE AS 8008 paragraph 3.6 to limit flight director |
|
|
|
operation to attitudes considered safe for the certified aircraft. |
|
|
|
2. |
Garmin was granted a deviation from TSO-C52b to use DO-160D instead of DO-160C. |
|
ETSO-C52b |
1. Garmin was granted a deviation from AS-8008 paragraph 3.6 to limit flight director |
|
|
|
operation to attitudes considered safe for the certified aircraft. |
|
|
|
|
|
|
Page 1-12 |
|
GIA 63/GIA 63W Installation Manual |
|
Revision S |
|
190-00303-05 |
|
|
TSO/ETSO Deviations, continued |
TSO/ETSO |
Deviation |
TSO-C92c 1. Garmin was granted a deviation from TSO-C92c to use DO-160D Change 3 instead of DO-160C.
2. Garmin was granted a deviation from TSO-C92c to not include the version and levels of software or the modification status of hardware in the appliance number.
TSO-C129a 1. Garmin was granted a deviation from TSO-C129a to use DO-160D Change 3 instead of DO-160C.
2.Garmin was granted a deviation from TSO-C129a to eliminate the annunciation for pending CDI scale change 3.0 NM from the FAF.
3.Garmin was granted a deviation from TSO-C129a involving the use of GPS calibrated altitude in approach mode based on the enclosed TSO deviation request dated August 24, 1994 and the approval letter dated November 29, 1994.
4.Garmin was granted a deviation from TSO-C129a to extend automatic CDI sensitivity changes to non-approach mode navigation.
5.Garmin was granted a deviation from TSO-C129a to eliminate the requirement in (a)(3)(xi)1.b.ii to “alert the pilot of the need to manually insert the barometric pressure”.
6.Garmin was granted a deviation from TSO-C129a to eliminate the requirement in (a)(3)(xv)4.b to provide a “means to manually identify a satellite that is expected to be unavailable at the destination (for scheduled maintenance as identified in FAA Notice to Airmen) shall be provided” for the RAIM prediction process.
7.Garmin was granted a deviation from TSO-C129a to change the requirement in (a)(6)(iii) from “The navigation data contains all 1’s or 0’s” to “All data bits in subframe 1, 2, or 3 are 0’s”.
8.Garmin was granted a deviation from TSO-C129a to change the requirement in paragraph (a)(7)(ii) to match the WAAS TSO-C145a and DO-229 requirements for Power input testing.
ETSO-C129a 1. Garmin was granted a deviation from ED-72A 3.2.2.1.f (list item 3) and 3.2.2.4.j.4 to eliminate the annunciation for pending CDI scale change 3.0 nm from the FAF.
2.Garmin was granted a deviation from ED-72A 3.2.2.4.j.3 to extend automatic CDI sensitivity changes for approach mode navigation to non-approach mode navigation as well.
3.Garmin was granted a deviation from ED-72A 3.2.2.1.f (list item 4) and 3.2.2.3.e.4 and 3.2.2.4.j.2 to eliminate the requirement to alert the pilot of the need to manually insert the barometric pressure.
4.Garmin was granted a deviation from ED-72A 3.2.2.3.d.2 to eliminate the requirement to provide a means to manually identify a satellite that is expected to be unavailable at the destination (for scheduled maintenance as identified in FAA Notice to Airmen) for the RAIM prediction process.
5.Garmin was granted a deviation from ED-72A 3.1.4.1.c to change the requirement from “the navigation data contains all 1’s or 0’s” to “all data bits in subframe 1,2, or 3 are 0’s”.
6.Garmin was granted a deviation from ED-72A 4.16.2 to eliminate the requirement for valid position within 10 seconds of power interrupt for abnormal operating conditions power input tests. For abnormal operating conditions power input tests, satellite acquisition time of 5 minutes applies.
TSO-C151b 1. Garmin was granted a deviation from TSO-C151b 4.a. to mark the unit with the serial number instead of the date of manufacture.
GIA 63/GIA 63W Installation Manual |
Page 1-13 |
190-00303-05 |
Revision S |
1.6.3 GIA 63W TSO/ETSO Compliance
Function |
TSO/ETSO |
Category |
Applicable LRU SW Part |
Applicable CLD Part |
|||
Numbers |
Numbers |
||||||
|
|
|
|||||
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All |
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All |
006-C0084-0() |
||
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|
except |
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|
006-B0544-1() |
||||
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|
006-C0084-00 |
||||
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through |
||||
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|
006-C0072-0() |
||||
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|
006-B0544-3() |
||||
Automatic Pilots |
TSO-C9c |
|
and all |
006-C0085-0() |
|||
ETSO-C9c |
|
006-B0544-B() |
|
||||
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All |
||||||
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|
||||||
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|
except |
||||
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|
006-C0039-0() |
||||
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006-B0544-BA |
||||
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except |
||||
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through |
||||
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006-C0039-00 |
||||
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006-B0544-BB |
||||
|
|
|
through |
||||
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|
|
|
||
|
|
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|
|
|
006-C0039-02 |
|
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All |
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|
All |
|
|
006-C0084-0() |
|
|
|
|
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|
except |
||
|
|
|
006-B0544-1() |
|
|
||
|
|
|
|
|
006-C0084-00 |
||
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|
through |
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All |
||
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|
006-C0072-0() |
|||
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|
|
006-B0544-3() |
|
006-B0083-0() |
||
Glideslope |
TSO-C34e |
|
and all |
|
except |
006-C0085-0() |
|
Receiver |
ETSO-2C34f |
|
006-B0544-B() |
|
006-B0083-00 |
|
|
|
All |
||||||
|
|
|
except |
|
through |
||
|
|
|
|
006-C0039-0() |
|||
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|
|
006-B0544-BA |
|
006-B0083-01 |
||
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|
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|
except |
|||
|
|
|
through |
|
|
||
|
|
|
|
|
006-C0039-00 |
||
|
|
|
006-B0544-BB |
|
|
||
|
|
|
|
|
through |
||
|
|
|
|
|
|
||
|
|
|
|
|
|
006-C0039-02 |
|
|
|
|
|
|
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All |
|
|
|
|
|
|
|
006-C0084-0() |
|
|
|
|
|
|
|
except |
|
|
|
|
All |
|
|
006-C0084-00 |
|
|
|
|
|
|
006-C0072-0() |
||
|
|
|
006-B0544-1() |
|
|
||
|
|
|
through |
|
All |
006-C0085-0() |
|
|
|
|
006-B0544-3() |
|
006-B0082-0() |
|
|
|
|
|
|
All |
|||
|
TSO-C36e |
|
and all |
|
except |
||
Localizer Receiver |
Class A |
|
006-C0039-0() |
||||
ETSO-2C36f |
006-B0544-B() |
|
006-B0082-00 |
||||
|
|
|
except |
||||
|
|
|
except |
|
through |
||
|
|
|
|
006-C0039-00 |
|||
|
|
|
006-B0544-BA |
|
006-B0082-02 |
||
|
|
|
|
through |
|||
|
|
|
through |
|
|
||
|
|
|
|
|
006-C0039-02 |
||
|
|
|
006-B0544-BB |
|
|
||
|
|
|
|
|
All |
||
|
|
|
|
|
|
||
|
|
|
|
|
|
006-C0053-0() |
|
|
|
|
|
|
|
except |
|
|
|
|
|
|
|
006-C0053-00 |
|
Page 1-14 |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
|
GIA 63W TSO/ETSO Compliance, Continued |
|
|||||
Function |
TSO/ETSO |
Category |
Applicable LRU SW Part |
Applicable CLD Part |
|||
Numbers |
Numbers |
||||||
|
|
|
|||||
|
|
|
|
|
|
All |
|
|
|
|
|
|
|
006-C0084-0() |
|
|
|
|
|
|
|
except |
|
|
|
|
All |
|
|
006-C0084-00 |
|
|
|
|
|
|
006-C0072-0() |
||
|
|
|
006-B0544-1() |
|
|
||
|
|
|
through |
|
All |
006-C0085-0() |
|
|
|
|
006-B0544-3() |
|
006-B0082-0() |
|
|
|
|
|
All |
||||
|
TSO-C40c |
|
and all |
|
except |
||
VOR Receiver |
|
|
006-C0039-0() |
||||
ETSO-2C40c |
|
006-B0544-B() |
|
006-B0082-00 |
|||
|
|
|
except |
||||
|
|
|
except |
|
through |
||
|
|
|
|
006-C0039-00 |
|||
|
|
|
006-B0544-BA |
|
006-B0082-02 |
||
|
|
|
|
through |
|||
|
|
|
through |
|
|
||
|
|
|
|
|
006-C0039-02 |
||
|
|
|
006-B0544-BB |
|
|
||
|
|
|
|
|
All |
||
|
|
|
|
|
|
||
|
|
|
|
|
|
006-C0053-0() |
|
|
|
|
|
|
|
except |
|
|
|
|
|
|
|
006-C0053-00 |
|
|
|
|
|
|
|
All |
|
|
|
|
|
All |
006-C0084-0() |
||
|
|
|
|
except |
|||
|
|
|
006-B0544-1() |
||||
|
|
|
006-C0084-00 |
||||
|
|
|
through |
||||
|
|
|
006-C0072-0() |
||||
|
|
|
006-B0544-3() |
||||
Flight Director |
TSO-C52b |
|
and all |
006-C0085-0() |
|||
Equipment |
ETSO-C52b |
|
006-B0544-B() |
|
|||
|
All |
||||||
|
|
|
except |
||||
|
|
|
006-C0039-0() |
||||
|
|
|
006-B0544-BA |
||||
|
|
|
except |
||||
|
|
|
through |
||||
|
|
|
006-C0039-00 |
||||
|
|
|
006-B0544-BB |
||||
|
|
|
through |
||||
|
|
|
|
|
|
||
|
|
|
|
|
|
006-C0039-02 |
|
|
|
|
|
|
|
All |
|
|
|
|
|
All |
006-C0084-0() |
||
|
|
|
|
except |
|||
|
|
|
006-B0544-1() |
||||
|
|
|
006-C0084-00 |
||||
Ground Proximity |
|
|
through |
||||
|
|
006-C0072-0() |
|||||
|
|
006-B0544-3() |
|||||
Warning – Glide |
|
|
and all |
|
|||
|
|
006-C0085-0() |
|||||
Slope Deviation |
TSO-C92c |
|
|||||
|
006-B0544-B() |
||||||
Alerting |
|
|
All |
||||
|
|
except |
|||||
Equipment |
|
|
006-C0039-0() |
||||
|
|
006-B0544-BA |
|||||
|
|
|
except |
||||
|
|
|
through |
||||
|
|
|
006-C0039-00 |
||||
|
|
|
006-B0544-BB |
||||
|
|
|
through |
||||
|
|
|
|
|
|
||
|
|
|
|
|
|
006-C0039-02 |
|
Airborne |
|
|
All |
|
|
All |
|
|
|
006-B0544-1() |
|
|
006-C0084-0() |
||
Navigation |
|
|
|
All |
|||
|
|
through |
|
except |
|||
Sensors Using the |
|
|
|
||||
|
|
006-B0544-3() |
|
006-B0339-0() |
006-C0084-00 |
||
Global Positioning |
|
|
|
||||
TSO-C145a |
|
and all |
|
except |
|
||
|
|
006-C0072-0() |
|||||
System |
Class 3 |
|
|||||
ETSO-C145 |
006-B0544-B() |
|
006-B0339-00 |
||||
Augmented by the |
|
|
|
||||
|
|
|
|||||
|
|
except |
|
through |
|
||
Wide Area |
|
|
|
|
|||
|
|
006-B0544-BA |
|
006-B0339-03 |
006-C0085-0() |
||
Augmentation |
|
|
|
||||
|
|
through |
|
|
|||
System* |
|
|
|
|
|
||
|
|
006-B0544-BB |
|
|
|
||
|
|
|
|
|
|
||
GIA 63/GIA 63W Installation Manual |
Page 1-15 |
190-00303-05 |
Revision S |
|
GIA 63W TSO/ETSO Compliance, Continued |
|
|||||
Function |
TSO/ETSO |
Category |
Applicable LRU SW Part |
Applicable CLD Part |
|||
Numbers |
Numbers |
||||||
|
|
|
|||||
|
|
|
|
|
|
All |
|
|
TSO-C151b |
Class A |
|
All |
006-C0084-0() |
||
|
|
except |
|||||
|
|
and B |
006-B0544-1() |
006-C0084-00 |
|||
|
|
|
through |
|
|||
|
|
|
006-C0072-0() |
||||
|
|
|
006-B0544-3() |
||||
|
|
|
006-C0085-0() |
||||
TAWS |
|
|
and all |
||||
|
|
006-B0544-B() |
All |
||||
|
|
|
|||||
|
|
|
except |
||||
|
|
|
006-C0039-0() |
||||
|
ETSO-C151a |
Class B |
006-B0544-BA |
||||
|
except |
||||||
|
|
|
through |
006-C0039-00 |
|||
|
|
|
006-B0544-BB |
||||
|
|
|
through |
||||
|
|
|
|
|
|
||
|
|
|
|
|
|
006-C0039-02 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
All |
|
|
|
|
All |
|
|
006-C0084-0() |
|
|
|
|
|
|
except |
||
|
|
|
006-B0544-1() |
|
|
||
|
|
|
|
|
006-C0084-00 |
||
|
TSO-C169 |
Class 3 and |
through |
|
All |
||
|
|
006-C0072-0() |
|||||
VHF Radio |
5 |
006-B0544-3() |
|
006-B0081-0() |
|||
Equivalent to |
|
|
|||||
Communications – |
(transmitter) |
and all |
|
except |
006-C0085-0() |
||
ETSO-2C37e |
|
||||||
Transceiver |
Class C and |
006-B0544-B() |
|
006-B0081-00 |
|
||
|
All |
||||||
& |
|
||||||
Equipment |
E |
except |
|
through |
|||
ETSO-2C38e |
|
006-C0039-0() |
|||||
|
(receiver) |
006-B0544-BA |
|
006-B0081-04 |
|||
|
|
|
except |
||||
|
|
|
through |
|
|
||
|
|
|
|
|
006-C0039-00 |
||
|
|
|
006-B0544-BB |
|
|
||
|
|
|
|
|
through |
||
|
|
|
|
|
|
||
|
|
|
|
|
|
006-C0039-02 |
|
|
|
|
|
|
|
|
|
* GIA63W ARINC output labels 310 and 311 are not to be used as navigation data per RTCA/DO-229c.
Page 1-16 |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
1.6.4 GIA 63W TSO/ETSO Deviations
TSO/ETSO |
|
Deviation |
TSO-C9c |
1. Garmin was granted a deviation from TSO-C9c to use SAE AS 402B instead of AS- |
|
|
402A. |
|
|
|
|
|
2. |
Garmin was granted a deviation from TSO-C9c to use DO-160E instead of specified |
|
environmental tests. |
|
|
3. |
Garmin was granted a deviation from TSO-C9c subpart A (c), which requires marking |
|
the weight of the unit on the unit. Garmin will provide this information in the installation |
|
|
manual in lieu of marking on the serial tag. Garmin does not currently list the weight on |
|
|
other avionics units. |
|
|
4. |
Garmin was granted a deviation from SAE AS 402B paragraph 4.4.1 to limit autopilot |
|
engagement to attitudes considered safe for the certified aircraft. |
|
|
5. |
Garmin was granted a deviation from SAE AS 402B paragraph 4.3.2 to not provide |
|
servo effort indications when the automatic pilot is not engaged. |
|
ETSO-C9c |
1. Garmin was granted a deviation from ETSO-C9c to use SAE AS-402B instead of AS- |
|
|
402A. |
|
|
2. |
Garmin was granted a deviation from ETSO-C9c to use DO-160E instead of the |
|
specified environmental tests. |
|
|
3. |
Garmin was granted a deviation from AS-402B paragraph 4.3.2 to not provide servo |
|
effort indications when the automatic pilot is not engaged. |
|
|
4. |
Garmin was granted a deviation from AS-402B paragraph 4.4.1 to limit autopilot |
|
engagement to attitudes considered safe for the certified aircraft. |
|
TSO-C34e |
1. Garmin was granted a deviation from TSO-C34e to use DO-160E instead of DO-160B, |
|
|
and DO-178B instead of DO-178A. |
|
ETSO-2C34f |
1. Garmin was granted a deviation from ETSO-2C34f to use DO-160E instead of DO- |
|
|
160D. |
|
TSO-C36e |
1. Garmin was granted a deviation from TSO-C36e to use DO-160E instead of DO-160B, |
|
|
and DO-178B instead of DO-178A. |
|
GIA 63/GIA 63W Installation Manual |
Page 1-17 |
190-00303-05 |
Revision S |
|
|
TSO/ETSO Deviations, continued |
TSO/ETSO |
|
Deviation |
ETSO-2C36f |
1. |
Garmin was granted a deviation from ETSO-2C36f to use DO-160E instead of DO-160D |
|
2. |
Garmin was granted a deviation from ETSO-2C36f to use ED-46B amendment 2 in |
|
addition to ED 46B |
|
ETSO-2C37e |
1. |
Garmin was granted a deviation from ETSO-2C37e to use DO-160E instead of DO- |
|
160D. |
|
|
2. |
Garmin was granted a deviation from ETSO-2C37e to use ED-23B amendment 3 in |
|
addition to ED-23B. |
|
ETSO-2C38e |
1. |
Garmin was granted a deviation from ETSO-2C38e to use DO-160E instead of DO- |
|
160D. |
|
|
2. |
Garmin was granted a deviation from ETSO-2C38e to use ED-23B amendment 3 in |
|
addition to ED-23B. |
|
TSO-C40c |
1. |
Garmin was granted a deviation from TSO-C40c to use DO-160E instead of DO-160B, |
|
and DO-178B instead of DO-178A. |
|
|
|
|
ETSO-2C40c |
1. |
Garmin was granted a deviation from ETSO-2C40c to use DO-160E instead of DO- |
|
160D. |
|
TSO-C52b |
1. |
Garmin was granted a deviation from SAE AS 8008 paragraph 3.6 to limit flight director |
|
operation to attitudes considered safe for the certified aircraft. |
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2. |
Garmin was granted a deviation from TSO-C52b to use DO-160E instead of DO-160C. |
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The justification for this deviation is to use the latest accepted environmental standards. |
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ETSO-C52b |
1. |
Garmin was granted a deviation from ETSO-C52b to use DO-160E instead of DO-160D. |
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2. |
Garmin was granted a deviation from AS-8008 paragraph 3.6 to limit flight director |
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operation to attitudes considered safe for the certified aircraft. |
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TSO-C92c |
1. |
Garmin was granted a deviation from TSO-C92c to use DO-160E instead of DO-160C. |
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2. |
Garmin was granted a deviation from TSO-C92c to not include the version and levels of |
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software or the modification status of hardware in the appliance number. |
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Page 1-18 |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
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TSO/ETSO Deviations, continued |
TSO/ETSO |
Deviation |
TSO-C145a 1. Garmin was granted a deviation from TSO-C145a to use DO-160E instead of DO-160D.
2.Garmin was granted a deviation from RTCA/DO-229C paragraphs 2.1.1.10, 2.1.1.7, 2.1.1.8.1, 2.1.1.8.2, 2.1.1.9, 2.1.2.1, 2.1.3.1, 2.1.4.1.4, 2.1.4.1.5 and 2.1.5.1 in the form of an operational limitation to achieve an equivalent level of safety. This operational limitation applies to the GIA63W with GPS software version 2.40 or earlier, or GIA63W installations with certain models of GPS/WAAS antennas identified in Section 2.1.3.2. The operational limitation is based on:
1.The ability to use antennas that may not meet the minimum gain performance requirements of DO-228.
2.The ability to mitigate the effects of the different gain characteristics of those antennas by increasing the effective mask angle through operational limitations.
3.The ability to further increase the effective mask angle, through operational limitations, to a level commensurate with test conditions used in the original TSO qualification tests.
4.The ability to use -128 dBmic as the minimum GPS satellite signal-in-space for the purpose of assessing the operational limitation.
5.The ability to use -128 dBmic as the minimum SBAS satellite signal-in-space for the purpose of assessing the operational limitation.
3.Garmin was granted a deviation from RTCA/DO-229C paragraph 2.1.1.9 to use a 20 second satellite reacquisition time instead of a 10-second reacquisition time.
ETSO-C145 1. Garmin was granted a deviation from ETSO-C145 to use DO-160E instead of DO-160D
2.Garmin was granted a deviation from ETSO-C145 to use DO-229C instead of DO-229A
3.Garmin was granted a deviation from DO-229C paragraphs 2.1.1.10, 2.1.1.7, 2.1.1.8.1, 2.1.1.8.2, 2.1.1.9, 2.1.2.1, 2.1.3.1, 2.1.4.1.4, 2.1.4.1.5 and 2.1.5.1 in the form of an operational limitation to achieve an equivalent level of safety. This operational limitation applies to the GIA63W with GPS software version 2.40 or earlier, or GIA63W installations with certain models of GPS/WAAS antennas identified in Section 2.1.3.2. The operational limitation is based on:
1.The ability to use antennas that may not meet the minimum gain performance requirements of DO-228.
2.The ability to mitigate the effects of the different gain characteristics of those antennas by increasing the effective mask angle through operational limitations.
3.The ability to further increase the effective mask angle, through operational limitations, to a level commensurate with test conditions used in the original TSO qualification tests.
4.The ability to use -128 dBmic as the minimum GPS satellite signal-in-space for the purpose of assessing the operational limitation.
5.The ability to use -128 dBmic as the minimum SBAS satellite signal-in-space for the purpose of assessing the operational limitation.
4.Garmin was granted a deviation from RTCA/DO-229C paragraph 2.1.1.9 to use a 20 second satellite reacquisition time instead of a 10-second reacquisition time.
TSO-C151b 1. Garmin was granted a deviation from TSO-C151b to use DO-160E instead of DO-160D. 2. Garmin was granted a deviation from TSO-C151b 4.a. to mark the unit with the serial number instead of the date of manufacture.
GIA 63/GIA 63W Installation Manual |
Page 1-19 |
190-00303-05 |
Revision S |
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TSO/ETSO Deviations, continued |
TSO/ETSO |
Deviation |
ETSO-C151a 1. Garmin was granted a deviation from ETSO-C151a to use DO-160E instead of DO160D.
TSO-C169 1. Garmin was granted a deviation from TSO-C169 to use DO-160E instead of DO-160D.
2.Garmin was granted a deviation to TSO-C169, paragraph 4.d requirement to mark the installation procedures drawing number on the equipment. Garmin will mark as follows, which Garmin believes meets the intent of the requirement. The Install Manual is part of the furnished data package.
TSO-C145a
See Install Manual for additional appliance approvals
3.Garmin was granted a deviation to TSO-C169, paragraph 4.e requirement to mark (DEV) after the TSO number on the equipment. Garmin will mark as follows, as TSOC169 is not the primary TSO and the Install Manual contains all of the TSO-C169 information including deviations.
TSO-C145a
See Install Manual for additional appliance approvals
4.Garmin was granted to deviate from TSO-C169 by allowing a 6dB reduction of transmitter power during the Normal Operating Conditions – Emergency Operation Voltage as described in RTCA document DO-186a paragraph 2.5.13.1 and RTCA document DO160E paragraph 16.6.1.1.
Page 1-20 |
GIA 63/GIA 63W Installation Manual |
Revision S |
190-00303-05 |
1.6.5 GIA 63W Updated NAV/COM TSO/ETSO Compliance
Function |
TSO/ETSO |
Category |
Applicable LRU SW Part |
Applicable CLD Part |
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Numbers |
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Numbers |
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All |
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006-C0084-0() |
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006-B0544-3() |
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except |
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except |
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006-C0084-00 |
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006-B0544-30 |
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006-C0072-0() |
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through |
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Automatic Pilots |
TSO-C9c |
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006-B0544-34 |
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and all |
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006-B0544-B() |
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006-C0085-0() |
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006-B0544-BA |
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through |
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006-B0544-BD |
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All |
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All |
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006-C0084-0() |
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006-B0544-3() |
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except |
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except |
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006-C0084-00 |
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006-B0544-30 |
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006-C0072-0() |
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through |
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All |
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Glideslope |
TSO-C34e |
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006-B0544-34 |
006-B0082-1() |
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Receiver |
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and all |
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except |
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006-B0544-B() |
006-B0082-10 |
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except |
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006-C0085-0() |
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006-B0544-BA |
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through |
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006-B0544-BD |
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All |
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All |
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006-B0544-3() |
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006-C0084-0() |
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except |
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except |
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006-B0544-30 |
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All |
006-C0084-00 |
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through |
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006-C0072-0() |
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Localizer Receiver |
TSO-C36e |
Class A |
006-B0544-34 |
006-B0082-1() |
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006-C0085-0() |
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and all |
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except |
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006-B0544-B() |
006-B0082-10 |
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except |
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006-C0124-0() |
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006-B0544-BA |
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through |
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006-B0544-BD |
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GIA 63/GIA 63W Installation Manual |
Page 1-21 |
190-00303-05 |
Revision S |
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