Garmin GDR 66 Installatioin Manual

190-00303-24 January, 2012 Revision A
GDR 66
Transceiver Installation Manual
DRAFT
© Copyright 2011
DRAFT
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 Panel-Mount Technical Support Line (Toll Free) 1.888.606.5482
www.garmin.com
Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road
Hounsdown Business Park
Southampton, SO40 9RB U.K.
+44/ (0) 870.8501241
Garmin AT, Inc.
2345 Turner Rd., SE
Salem, OR 97302 USA
Telephone: 503.581.8101
RECORD OF REVISIONS
Revision Revision Date Description
A 01/17/2012 Initial Release
INFORMATION SUBJECT TO EXPORT CONTROL LAWS
DRAFT
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 of 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
CURRENT REVISION DESCRIPTION
.
Revision
A All All Initial release
Page
Number(s)
Section
Number
DOCUMENT PAGINATION
Section Page Range
Table of Contents i – vi
Section 1 1-1 – 1-8 Section 2 2-1 – 2-4 Section 3 3-1 – 3-4
Section 4 4-1 – 4-10 Appendix A A-1 – A-3 Appendix B B-1 – B-3
Description of Change
GDR 66 Installation Manual Page i 190-00303-24 Revision A
TABLE OF CONTENTS
DRAFT
PARAGRAPH PAGE
Section 1 GENERAL DESCRIPTION............................................................. 1-1
1.1 Introduction ..................................................................................................................... 1-1
1.2 Equipment Description................................................................................................... 1-1
1.3 Interface Summary .........................................................................................................1-1
1.4 Technical Specifications .................................................................................................1-2
1.4.1 Environmental Qualification Form..................................................................................... 1-2
1.4.2 Physical Characteristics ...................................................................................................... 1-2
1.4.3 General Specifications ........................................................................................................ 1-2
1.4.4 Power Requirements ........................................................................................................... 1-3
1.4.5 Transmitter Power Versus Aircraft Bus Voltage................................................................ 1-3
1.4.6 COM Transceiver Specifications........................................................................................ 1-4
1.4.7 Digital Transceiver Characteristics..................................................................................... 1-4
1.4.8 License Requirements......................................................................................................... 1-6
1.5 Certification..................................................................................................................... 1-6
1.5.1 TSO/ETSO Compliance......................................................................................................1-7
1.5.2 TSO/ETSO Deviations........................................................................................................ 1-7
1.6 Reference Documents .....................................................................................................1-7
1.7 Aviation Limited Warranty ............................................................................................. 1-8
Section 2 INSTALLATION OVERVIEW....................................................... 2-1
2.1 Introduction ..................................................................................................................... 2-1
2.2 Installation Materials....................................................................................................... 2-1
2.2.1 Equipment Available .......................................................................................................... 2-1
2.2.2 Additional Equipment Required ......................................................................................... 2-1
2.3 Installation Considerations.............................................................................................. 2-2
2.3.1 Antenna Considerations...................................................................................................... 2-2
2.3.2 Com Antenna Location....................................................................................................... 2-2
2.4 Cabling and Wiring .........................................................................................................2-3
2.5 Cooling Air...................................................................................................................... 2-3
2.6 Mounting Requirements.................................................................................................. 2-4
Section 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 ............................................................................................................3-3
3.5 Backshell Assembly ........................................................................................................3-4
3.6 Final Installation.............................................................................................................. 3-4
3.7 Post Installation Configuration & Checkout ...................................................................3-4
3.8 Continued Airworthiness ................................................................................................3-4
Page ii GDR 66 Installation Manual Revision A 190-00303-24
TABLE OF CONTENTS
DRAFT
PARAGRAPH PAGE
Section 4 SYSTEM INTERCONNECTS......................................................... 4-1
4.1 Pin Function List .............................................................................................................4-1
4.1.1 P661 (COM)........................................................................................................................ 4-1
4.1.2 P662 (Main) ........................................................................................................................ 4-2
4.2 Power Functions.............................................................................................................. 4-4
4.2.1 Aircraft Power..................................................................................................................... 4-4
4.2.2 Remote Power Off .............................................................................................................. 4-4
4.2.3 GDR System ID Program ................................................................................................... 4-4
4.3 Serial Data....................................................................................................................... 4-5
4.3.1 RS-422 ................................................................................................................................ 4-5
4.3.2 RS-232 ................................................................................................................................ 4-5
4.3.3 ARINC 429 ......................................................................................................................... 4-6
4.4 Discrete I/O ..................................................................................................................... 4-7
4.4.1 Active Low Discrete Inputs ................................................................................................ 4-7
4.4.2 Key Event Out..................................................................................................................... 4-7
4.5 Audio............................................................................................................................... 4-8
4.5.1 Analog Audio...................................................................................................................... 4-8
4.5.2 ACARS/SELCAL............................................................................................................... 4-9
Appendix A Outline and Installation Drawings............................................. A-1
Appendix B Interconnect Examples.................................................................B-1
GDR 66 Installation Manual Page iii 190-00303-24 Revision A
LIST OF FIGURES
DRAFT
FIGURE PAGE
Section 1 GENERAL DESCRIPTION............................................................. 1-1
Section 2 INSTALLATION OVERVIEW....................................................... 2-1
Figure 2-1: GDR 66 Standalone Rack ..................................................................................2-4
Section 3 INSTALLATION PROCEDURE .................................................... 3-1
Figure 3-1 TNC Connector Installation ................................................................................3-3
Section 4 SYSTEM INTERCONNECTS......................................................... 4-1
Figure 4-1 View of J661 connector, from back of unit......................................................... 4-1
Figure 4-2 View of J662 connector, from back of unit......................................................... 4-2
Appendix A Outline and Installation Drawings ............................................ A-1
Figure A-1 GDR 66 Outline Drawing.................................................................................. A-1
Figure A-2 GDR 66 Connector/Rack Assembly Drawing.................................................. A-2
Figure A-3 GDR 66 Minimum Installation/Removal Clearance ......................................... A-3
Appendix B Interconnect Examples ................................................................B-1
Figure B-1 GDR 66 Power and Antenna Interconnect Example ......................................... B-1
Figure B-2 GDR 66 VDL Mode 2 Interconnect Example ................................................... B-2
Figure B-3 GDR 66 Analog Voice Mode Interconnect Example ........................................ B-3
Page iv GDR 66 Installation Manual Revision A 190-00303-24
LIST OF TABLES
DRAFT
TABLE PAGE
Section 1 GENERAL DESCRIPTION .............................................................1-1
Table 1-1 Physical Characteristics........................................................................................ 1-2
Table 1-2 General Specifications.......................................................................................... 1-2
Table 1-3 Power Requirements............................................................................................. 1-3
Table 1-4 TX Power (into 50 load) vs Bus Voltage .......................................................... 1-3
Table 1-5 Transceiver Specifications ................................................................................... 1-4
Table 1-6 Digital Transceiver Characteristics ...................................................................... 1-4
Table 1-7 License Requirements .......................................................................................... 1-6
Table 1-8 TSO/ETSO Compliance ....................................................................................... 1-7
Table 1-9 TSO/ETSO Deviations ......................................................................................... 1-7
Table 1-10 Reference Documents......................................................................................... 1-7
Section 2 INSTALLATION OVERVIEW........................................................2-1
Table 2-1 Available Units..................................................................................................... 2-1
Table 2-2 Equipment Available............................................................................................ 2-1
Table 2-3 Additional Equipment Required........................................................................... 2-1
Section 3 INSTALLATION PROCEDURE.....................................................3-1
Table 3-1: Pin Contact Part Numbers ................................................................................... 3-1
Table 3-2 Recommended Crimp Tools................................................................................. 3-2
Section 4 SYSTEM INTERCONNECTS..........................................................4-1
Table 4-1 P661 Connector .................................................................................................... 4-1
Table 4-2 P662 Connector .................................................................................................... 4-2
Table 4-3 Aircraft Power ...................................................................................................... 4-4
Table 4-4 Remote Power Off................................................................................................ 4-4
Table 4-5 System ID Program .............................................................................................. 4-4
Table 4-6 Unit Number Configuration ................................................................................. 4-5
Table 4-7 RS-422.................................................................................................................. 4-5
Table 4-8 RS-232.................................................................................................................. 4-5
Table 4-9 ARINC 429........................................................................................................... 4-6
Table 4-10 Discrete Inputs.................................................................................................... 4-7
Table 4-11 Key Event Out .................................................................................................... 4-7
Table 4-12 Com Mic Audio.................................................................................................. 4-8
Table 4-13 Com Audio Out .................................................................................................. 4-8
Table 4-14 Com Mic Key ..................................................................................................... 4-8
Table 4-15 Com Remote Transfer ........................................................................................ 4-9
Table 4-16 SELCAL Audio and ACARS Data Out ............................................................. 4-9
GDR 66 Installation Manual Page v 190-00303-24 Revision A
Page vi GDR 66 Installation Manual
DRAFT
Revision A 190-00303-24
1 GENERAL DESCRIPTION
DRAFT
1.1 Introduction
This manual presents mechanical and electrical installation requirements for installing the GDR 66 as part of a Garmin Integrated Flight Deck. The GDR 66 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.
1.2 Equipment Description
The GDR 66 is a remote mounted digital communications transceiver. The GDR 66 operates in the following modes in the 118.000 to 137.000 MHz VHF aviation communications band:
Analog Voice Mode (ARINC 716 Voice): Voice communications using DSB-AM modulation with
8.33 and 25 kHz channel spacing.
VDL Mode 0/A (ARINC 716 Data): ACARS using DSB-AM modulation with a 2.4 kbps data rate and 25 kHz channel spacing.
VDL Mode 2 (ARINC 750 Data): Data link using D8PSK modulation with a 31.5 kbps data rate and 25 kHz channel spacing.
1.3 Interface Summary
The GDR 66 provides the following interfaces:
• 2 RS-422 inputs
• 2 RS-422 outputs
• 1 RS-232 input
• 1 RS-232 output
• 5 configurable ARINC 429 inputs
• 2 configurable ARINC 429 outputs
• 8 configurable active low discrete inputs
• 5 active low discrete inputs: COM MIC KEY*, COM REMOTE TRANSFER*, GDR SYSTEM ID PROGRAM* 1, GDR SYSTEM ID PROGRAM* 2, GDR SYSTEM ID PROGRAM* 3
• 1 active high discrete input: COM REMOTE POWER OFF
• 1 active low discrete outputs: KEY EVENT OUT*
• 1 analog microphone audio input
• 1 analog audio output
• 1 SELCAL audio/ACARS analog data output
• 2 aircraft power bus inputs
GDR 66 Installation Manual Page 1-1 190-00303-24 Revision A
1.4 Technical Specifications
DRAFT
1.4.1 Environmental Qualification Form
It is the responsibility of the installing agency to obtain the latest revision of the GDR 66 Environmental Qualification Form. This form is available directly from Garmin under the following part number:
GDR 66 Environmental Qualification Form, Garmin part number 005-00548-01
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
Table 1-1 list the physical characteristics for the GDR 66 unit, rack, and connectors. Please refer to Appendix A for additional information.
Table 1-1 Physical Characteristics
Characteristics Specifications
Width (w/out Rack) 2.06 inches (5.23 cm)
Height (w/out Rack) 6.46 inches (16.4 cm)
Depth (w/out Rack) 8.78 inches (22.3 cm)
Width (with Rack) 2.06 inches (5.23 cm)
Height (with Rack) 6.62 inches (16.8 cm)
Depth (with Rack & Connectors) 10.1 inches (25.8 cm)
Unit Weight 4.2 lbs. (1.9 kg)
Rack Weight 0.36 lbs. (0.16 kg)
Connector Weight 0.33 lbs. (0.15 kg)
1.4.3 General Specifications
For detailed specifications, see the Environmental Qualification Form.
Table 1-2 General Specifications
Characteristics Specifications
Operating Temperature Range -55°C to +70°C. For more details see Environmental Qualification Form.
Humidity 95% non-condensing
Altitude Range -1,500 ft to 55,000 ft
Software Compliance RTCA/DO-178B Level C, EUROCAE/ED-12B Level C
Environmental Conditions RTCA/DO-160E, EUROCAE/ED-14E
.
Page 1-2 GDR 66 Installation Manual Revision A 190-00303-24
1.4.4 Power Requirements
DRAFT
Table 1-3 Power Requirements
Characteristics Specifications
Input Voltage
14V
28V
1.4.5 Transmitter Power Versus Aircraft Bus Voltage
14/28 Vdc. See the Environmental Qualification Form for details on surge ratings and minimum/maximum operating voltages.
Receive (AM or VDL) Maximum 3.0A
Transmit (AM or VDL) Maximum 9.0A
Receive (AM or VDL) Maximum 1.5A
Transmit (AM or VDL) Maximum 8.0A
Table 1-4 TX Power (into 50 load) vs Bus Voltage
Aircraft Power Bus Voltage
(V)
V 22.0 V
22.0 > V ≥11.0
11.0 > V ≥10.25
GDR 66 does not claim Emergency Operation as defined by RTCA DO-160E, Section 16
Tx Power AM Mode Tx Power VDL Mode
16 W minimum 20 W Typical
8 W minimum 10 W Typical
4 W minimum 5 W Typical
NOTE
15 W minimum 20 W Typical
7.5 W minimum 10 W Typical
4 W minimum 5 W Typical
GDR 66 Installation Manual Page 1-3 190-00303-24 Revision A
1.4.6 COM Transceiver Specifications
DRAFT
The GDR 66 Transceiver minimally meets the requirements of DO-186B and ED-23B. Refer to Table 1-5 for detailed specifications.
Table 1-5 Transceiver Specifications
Characteristics Specifications
Audio Outputs
Audio Response
Audio Distortion
Receiver Dynamic Range -107 dBm to +10 dBm typical
Sensitivity
Squelch
Spurious Response
Multi-Carrier Operation
Transmitter Power See Section 1.4.5
Transmitter Duty Cycle 10% maximum, thermally limited, 30 second limit per transmission
Modulation Capability
Carrier Noise Level Shall be at least 45 dB (S+N)/N
Frequency Stability + / - 5ppm (-55ºC to +70ºC with a 5-minute warmup at -55ºC)
Demodulated Audio Distortion Less than 10% distortion when the transmitter is modulated at least 70%
Sidetone 1.4 Vrms into a 600 load
Transmit Modulation Fidelity
Microphone Sensitivity See Section 4.5.1.1
Spurious Emissions - Global Navigation Satellite System Band
Received Audio: 40 mW minimum into a 600 load SELCAL/Data: 10.4 mW minimum into a 600 load
Less than 6 dB of variation between 300 and 2500 Hz Greater than 40dB rejection above 3750 Hz
Not greater than 20.0% across the band from 300 Hz to 2500 Hz with a 90% modulated signal. No greater than 7.5% with a 30% modulated signal
(S+N)/N on all channels shall be greater than 6 dB when the RF level is -107dBm modulated 30% at 1000 Hz
Selectable between 0 to 20 dB SNR. Squelch hysteresis is selectable up to 15 dB
74 dB minimum (-33 dBm signal produces no more output than desired signal producing 6 dB (S+N)/N)
Meets multi-carrier sensitivity, distortion, and audio output level requirements of ED-23C for Class C and Class H2 reveivers.
The modulation shall not be less than 70% with a standard modulator signal applied to the transmitter
Shall be less than 6 dB when the audio input frequency is varied from 350 to 2500 Hz
Harmonic Emission products in the band extending from 1559 to 1610 Mhz shall be no greater than -60dBm
1.4.7 Digital Transceiver Characteristics
The GDR 66 Transceiver minimally meets the requirements of DO-281A. Refer to Table 1-6 for detailed specifications.
Table 1-6 Digital Transceiver Characteristics
Characteristics Specifications
Dynamic Range +10dBm to -98dBm typical
Sensitivity Uncorrected BER of no more than 0.001 at -98 dBm
Transmitter Power See Section 1.4.5
Transmitter Duty Cycle 20% maximum, thermally limited
Modulation Capability D8PSK
Frequency Stability + / - 5ppm (-55ºC to +70ºC with a 5-minute warmup at -55ºC)
Transmit Symbol Constellation Error EVM of less than 6%
Spurious Emissions - Global Navigation Satellite System Band
Page 1-4 GDR 66 Installation Manual Revision A 190-00303-24
Harmonic Emission products in the band extending from 1559 to 1610 Mhz shall be no greater than -60dBm
Loading...
+ 28 hidden pages