Thales 82166 Series Installation And Maintenance Manual
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Thales 82166 Series Installation And Maintenance Manual

Thales 82166 Series Installation And Maintenance Manual

Flange mounted high power amplifier
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INSTALLATION AND MAINTENANCE

Flange Mounted High Power Amplifier
Revision No. 00
First Issue: Jul 2008
©
THALES AVIONICS Ltd. This document and any
information included are the property of Thales Avionics.
They cannot be reproduced, disclosed or utilized without the
company's prior written approval
86, Bushey Road
Raynes Park, London
SW20 0JW
Tel: +44 (0)20 8946 8011
Fax: +44 (0)20 8946 7530
MANUAL
(FMHPA)
82166 Series
1
Jul 2008

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  • Page 1: Installation And Maintenance

    82166 Series Revision No. 00 First Issue: Jul 2008 © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 2 Installation Maintenance Manual FMHPA 82166A30 THIS PAGE INTENTIONALLY BLANK © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 3: Table Of Contents

    Bonding Requirements ......... . . 3-3 © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the...
  • Page 4 Instructions for Continued Airworthiness ......6-5 © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the...
  • Page 5 Revision Date Revision Revision Date Date Inserted Date Inserted © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 6 Installation Maintenance Manual FMHPA 82166 THIS PAGE INTENTIONALLY BLANK © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 7: Purpose Of Manual

    INTRODUCTION 10000 1.1. PURPOSE OF MANUAL This manual sets forth installation and maintenance guidelines for the THALES TopFlight Satcom (TFS) Flange-mounted High Power Amplifier (FMHPA). The FMHPA installation specific and general guidelines contained within this manual are supported by mechanical and electrical interconnection drawings. Drawings should be reviewed by the installation organisation, and any requirements specific to a particular airframe should be assessed before installation is commenced.

  • Page 8: Scope Of Manual

    Fax. +44 (0)20 8946 7530 1.2. SCOPE OF MANUAL The Thales FMHPA comply with the design requirements set forward in the ARINC 781 Characteristic. An ARINC 781 compliant system is intended to support one or more of the Inmarsat aeronautical services known as ‘Classic-Aero’, ‘Swift 64’, and ‘SwiftBroadband’.

  • Page 9: European Aviation Safety Agency

    EASA/FAR 25.1431 Electronic equipment • EASA 25.561 Emergency Landing. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 10 Installation Maintenance Manual FMHPA 82166 THIS PAGE INTENTIONALLY BLANK © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 11: Description

    Internal connectors, connecting the RF SRU to the Logic SRU: • Power Supplies • Communication signal. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 12: Logic Sru

    There is no software in the FMHPA. All FMHPA functions shall be allocated to hardware. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 13: General Operation

    FMHPA is reduced to the minimum possible to permit temperature monitoring and © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 14: Hpa Module

    The PSM and CM SRU module contains two modules in the same housing: • Power Supply Module • Communication Module. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 15: Psm

    Its function is to manage the interface with the ARINC 429, to send control signals to the HPA and the PSM and report FMHPA status. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 16: Operating Environment

    265 W (assuming 100% duty cycles with HPA operating at 35 W output). © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the...

  • Page 17: Environment Conditions

    (metric: mm) values. Maximum Weight: 8.9 kg (19.8 lb) © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 18 Installation Maintenance Manual FMHPA 82166 THIS PAGE INTENTIONALLY BLANK © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 19 NOTE: MAXIMUM PERMISSIBLE TIGHTENING TORQUE OF ATTACHMENT SCREWS = 5.3 N.m (3.9 lbf.ft) POWER SUPPLY Figure 2.1 FMHPA Overall Dimensions © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 20 Installation Maintenance Manual FMHPA 82166 THIS PAGE INTENTIONALLY BLANK © THALES AVIONICS Ltd. This document and any 2-10 information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 21: Fmhpa Performances

    Circuit Breaker Return Figure 2.5 FMHPA Power Distribution Diagram © THALES AVIONICS Ltd. This document and any 2-11 information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 22: Communication Interface

    Connection between PSM and HPA Connection between the PSM (EMC filter) and © THALES AVIONICS Ltd. This document and any 2-12 information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 23: Connector Designation

    Discrete BITE #2 - Not Used Discrete BITE #2 - Not Used © THALES AVIONICS Ltd. This document and any 2-13 information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 24 ATE Pin - Not Used Manufacturer specific SPARE SPARE © THALES AVIONICS Ltd. This document and any 2-14 information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 25 Config Pin 2 Tav_e_0000765_00 Figure 2.4 FMHPA Interconnection Block Diagram © THALES AVIONICS Ltd. This document and any 2-15 information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 26 Installation Maintenance Manual FMHPA 82166 THIS PAGE INTENTIONALLY BLANK © THALES AVIONICS Ltd. This document and any 2-16 information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 27: Installation Guidelines

    Before installing any components or cabling, read all notes contained within drawings. 3.2. INTERCHANGEABILITY The FMHPA will only operate when installed with a Thales SDU. Therefore, the FMHPA are interchangeable only with identical system components as covered in this manual.

  • Page 28: Cooling

    Figure 2.5: Aircraft Power Distribution Figures 2.6: FMHPA Interconnection Diagram. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 29: Bonding Requirements

    20 milliohms. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 30 Installation Maintenance Manual FMHPA 82166 THIS PAGE INTENTIONALLY BLANK © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 31: Inspection And System Checkout

    Check that the correct air cooling and air flow is provided to the FMHPA. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 32: System Checkout

    DOWN LRU. CAUTION: NEVER DISCONNECT CABLES WHEN SYSTEM OPERATING. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 33: System Operations

    Refer to the Testing and Fault Isolation section for information on the FMHPA fault detection capabilities. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 34 Installation Maintenance Manual FMHPA 82166 THIS PAGE INTENTIONALLY BLANK © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 35: Fault Isolation

    SDU via the ARINC 429 interface. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 36: Health Monitor

    The FMHPA also displays serviceabilty via the SDU front panel Ext HPA LED (refer to the SDU/SCM IMM). © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 37: General

    MANUFACTURERS‚ MATERIAL SAFETY DATA SHEETS FOR SAFETY INFORMATION. SOME MATERIALS DANGEROUS. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 38: Procedure For The Fmhpa

    Un-stow and remove the bags from the cables as required. Remove ESD protective caps from the FMHPA connectors. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 39 Connect forced drawn air cooling pipe to rear of (1) FMHPA and secure. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the...

  • Page 40: Adjustment Procedure

    Do the Post-Installation Test Procedures referenced in the Inspection and System Checkout Section of this manual. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

  • Page 41: Cleaning Of Mechanical Parts

    Maintenance information for FMHPA, TFS LRU (system description, removal, installation, testing, etc.). © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...
  • Page 42 FAR Part 145 Section 43.9. © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. Jul 2008 They cannot be reproduced, disclosed or utilized without the company’s prior written approval...

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