User's Manual
Table Of Contents
- Cover
- 1-Welcome Letter
- 2-Table of Contents
- 3-Contacts
- 4-Quick Start Guide Rev 2
- 5-SIM Registration
- 6-Installation and Operations Rev 2
- 7-Component Maintenance Manual Rev 1
- SERVICE BULLETIN LIST
- RECORD OF CHANGES
- RECORD OF REVISIONS
- LIST OF EFFECTIVE PAGES
- LIST OF EFFECTIVE PAGES
- INTRODUCTION
- DESCRIPTION AND OPERATION
- TESTING AND TROUBLESHOOTING
- DISASSEMBLY
- CLEANING
- CHECK
- REPAIR
- ASSEMBLY
- FITS AND CLEARANCES
- SPECIAL TOOLS, FIXTURES AND EQUIPMENT
- ILLUSTRATED PARTS LIST
Airbus Iridium SATCOM System
165E5733-00 L-3 Aviation Recorders Proprietary
Issue, Rev. 02
21 January 2014
Page 22
Mounting: ARINC 600 2MCU Mounting Tray
Rear Mating Connector: Size 2 ARINC 600 Receptacle
Radiall P/N: NSXN2P201S0004
Maintenance Connector: RJ45 (8P8C) Modular Connector Jack
Flash Card: CompactFlash
®
(Type I or Type II)
3.1.3 Environmental Specifications – Airbus Iridium SATCOM System
Refer to Appendix C – Environmental Qualification Forms for environmental testing conditions,
categories and descriptions of the conducted tests of the SDU.
Note:
DO-160G Categories for the Airbus Iridium SATCOM System are as specified by the design.
Qualification tests on the Airbus Iridium SATCOM System SDU have not been completed to date.
3.2 SDU Configuration Module (SCM)
This section describes the mechanical and environmental specifications of the components of the
SDU Configuration Module (SCM) – see Figure 3-3.
3.2.1 General
The SCM is housed in a small enclosure, which is designed to be mounted within 24” of the SDU rear
connector.
Figure 3-3 – Airbus Iridium SATCOM System SDU Configuration Module (SCM)