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 38
Testing was performed to DO-160F, MIL-STD-810, EN-60068, ISO-2669, and the applicable
ABDs unless otherwise noted.
Temperature: -55° C (-67° F); to +85° C (+185° F)
Altitude: -100 to +55,000 FT
Vibration: 10 G’s (DO-160D/E F2-AB)
Electrical Specifications
Frequency: 1616.0 – 1625.5 MHz
VSWR: ≤ 1.5:1
Impedance: 50-Ohms
Polarization: RHCP
Axial Ratio: ≤ 3.0 db @ zenith
Power Handling: 60 Watts CW
Figure 4-2 - Iridium Antenna, Outline and Dimensions