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Thales NSS 100S-1 Component Maintenance Manual With Illustrated Parts List
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Thales NSS 100S-1 Component Maintenance Manual With Illustrated Parts List

Thales NSS 100S-1 Component Maintenance Manual With Illustrated Parts List

Gps receiver processor unit
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GPS RECEIVER PROCESSOR UNIT
COMPONENT MAINTENANCE MANUAL
DAH/DTV/95/1018
First issue: MAY 95
Update: MAY 30/03
The document reference is online, please check the correspondence between the online documentation and the printed version.
F9111
NSS 100S-1
P/N: C17004DA02
C17004DA04
C17004HA02
C17004HA04
C17004PA01
C17004PA03
WITH
ILLUSTRATED PARTS LIST
34-57-96

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Summary of Contents for Thales NSS 100S-1

  • Page 1 F9111 GPS RECEIVER PROCESSOR UNIT NSS 100S-1 P/N: C17004DA02 C17004DA04 C17004HA02 C17004HA04 C17004PA01 C17004PA03 COMPONENT MAINTENANCE MANUAL WITH ILLUSTRATED PARTS LIST 34-57-96 DAH/DTV/95/1018 First issue: MAY 95 Update: MAY 30/03 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 2 This document is the property of THALES AVIONICS and contains proprietary and confidential information which shall neither be duplicated nor disclosed to others without the prior written consent of THALES AVIONICS. The recipient shall not use this document for any purpose other than the installation or maintenance of relevant equipment and shall return it promptly to THALES AVIONICS upon its request.

  • Page 3: Table Of Contents

    This document and any data included are the property MAY 30/03 MAY 30/95 of THALES AVIONICS. They may not be reproduced, disclosed or utilized without the company's prior written approval. The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 4 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 5 COMPONENT MAINTENANCE MANUAL C17004 RECORD OF TEMPORARY REVISIONS TEMPORARY INCORPORATED CANCELLED REVISION PAGE No DATE REVISION No 34-57-96 RTR Page 1 MAY 30/95 COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 6 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 7 This document and any data included are the property MAY 30/03 of THALES AVIONICS. They may not be reproduced, disclosed or utilized without the company's prior written approval. The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 8 This document and any data included are the property MAY 30/03 of THALES AVIONICS. They may not be reproduced, disclosed or utilized without the company's prior written approval. The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 9 COMPONENT MAINTENANCE MANUAL C17004 RECORD OF VALIDITY TEMPORARY REVISIONS REMOVED BY REVISION DATE OF ISSUE OBSERVATIONS DATE 34-57-96 RVTR Page 1 MAY 30/95 COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 10 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 11 COMPONENT MAINTENANCE MANUAL C17004 SERVICE BULLETIN LIST SERVICE DATE INCORPORATED SUBJECT BULLETIN 34-57-96 SBL Page 1 MAY 30/95 COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 12 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 13 PCB Z3 E17006MA01 16181AC of Z3 PCB (CPU) becomes E17006MA03 RPU P/N C17004PA01 becomes C17004PA03 34-57-96 EEL Page 1 © THALES AVIONICS OCT 15/01 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 14 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 15 COMPONENT MAINTENANCE MANUAL C17004 TABLE OF CONTENTS PAGE INTRODUCTION INTRO 1 DESCRIPTION AND OPERATION TESTING AND TROUBLESHOOTING DISASSEMBLY CLEANING CHECK Not applicable REPAIRS Not applicable ASSEMBLY AND STORAGE FITS AND CLEARANCES Not applicable SPECIAL TOOLS FIXTURES AND EQUIPMENT LIST OF SPECIAL MATERIALS ILLUSTRATED PARTS LIST 1001 34-57-96...
  • Page 16 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 17 Schematic Diagram of power supply PCB, Z1 47/48 Figure 701: Sub-units interconnection Figure 1: NSS100S-1 1014 34-57-96 TC Page 2 © THALES AVIONICS OCT 15/01 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 18 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 19 COMPONENT MAINTENANCE MANUAL C17004 INTRODUCTION 1. General A. This maintenance manual has been prepared in accordance with standard N 100 of the AIR TRANSPORT ASSOCIATION OF AMERICA (Standard ATA 100). B. This manual gives all necessary information for repairs and general overhaul of the aircraft.
  • Page 20 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 21 COMPONENT MAINTENANCE MANUAL C17004 LIST OF ABBREVIATIONS Antenna Coupler Unit Automatic Gain Control A.S. Anti-Spoofing COMA Arinc Communication coprocessor Central Processing Unit Dead Reckoning General Logic Unit Global Positioning System Hectopascal Intermediate Frequency Navstar Sensor System Precise code (precise acquisition code) PreAmplifier Unit Precise Positioning Service (precise position determination service for authorized users)
  • Page 22 The document reference is online, please check the correspondence between the online documentation and the printed version.

  • Page 23: Oct 16/95

    COMPONENT MAINTENANCE MANUAL C17004 DESCRIPTION AND OPERATION 1. General A. Presentation The Receiver Processor Unit (RPU) is built into the GPS (Global Positioning System) navigation system NSS100S-1 (Navstar Sensor System type 100-1 SPS). It can operate with an active or passive antenna (ACU), and with a preampli- fier (PAU);...

  • Page 24: Oct 15/01

    Y code PTTI µp clock 20 MHz 20 MHz 25 MHz 34-57-96 Page 2 OCT 15/01 © THALES AVIONICS COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 25 COMPONENT MAINTENANCE MANUAL C17004 D. General Characteristics (1) Physical characteristics - Length: 241 mm - Width: 161 mm - Height: 81 mm - Weight: 2.5 kg max. (2) Electrical characteristics - 28 V DC power supply through the aircraft mains (as per AIR standard 2021E);...
  • Page 26 COMPONENT MAINTENANCE MANUAL C17004 (d) Performance Note: Performance complies with STANAG document 4294-1. 1 Acceptable level of satellite signals (frequency L1, C/A code): - Minimum acquisition level: -164 dBW - Minimum level of tracking (code and carrier frequency): -169 dBW - Maximum acquisition level: -150 dBW - Maximum power before destruction: 0 dbW - Note: dBW=decibels referenced to 1 W...
  • Page 27 (b) Input no. 2 (optional) - Mnemonic: A.REC.2L/A.REC.2H 34-57-96 Page 5 OCT 15/01 © THALES AVIONICS COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 28 COMPONENT MAINTENANCE MANUAL C17004 (c) Double output no. 1 and 2 - Mnemonics: A.EM.1L/A.EM.1H and A.EM.2L/A.EM.2H, - Type: ARINC 429 HS (100 KHz), - Functions: transmission of position-fixing information: . Positions (latitude, longitude, altitude) . Speeds (North/South, East/West, Altitude), . Speed and position standard deviation .

  • Page 29: May 30/95

    COMPONENT MAINTENANCE MANUAL C17004 (c) 250 Hz time base output - Mnemonic: BT250 - Function: maintenance (d) Reset output - Mnemonic: M.RST - Function: maintenance (6) List of Inputs/Outputs (connector J1) Signal name Function A.REC.1H Arinc 429 LS no.1 input high BL.AR1 Arinc no.1 digital shielding A.EM.1H...

  • Page 30: Oct 15/01

    RS422 input low (optional) TMP1.IH TMP no. 1 input high (optional) BL.TMP2 TMP2 Shielding 34-57-96 Page 8 OCT 15/01 © THALES AVIONICS COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 31 COMPONENT MAINTENANCE MANUAL C17004 ANTENNA COUPLER UNIT (ACU) PRE-AMPLIFIER UNIT (PAU) RF SIGNAL A.REC.1 ARINC 429 LS A.REC.2 ARINC 429 HS (Optional) A.EM.1 ARINC 429 HS A.EM.2 PP1 to PP5 (Optional) ELITE.I RECEIVER-PROCESSOR UNIT RS422 ELITE.O (RPU) RSOPT.I RS422 RSOPT.O (Optional) TMP1.0 BT250...

  • Page 32: May 30/95

    COMPONENT MAINTENANCE MANUAL C17004 34-57-96 Outside Description Page 10 Figure 2 MAY 30/95 COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 33 COMPONENT MAINTENANCE MANUAL C17004 2. Description A. Outside Description (see Figure 2) The Receiver Processor Unit comes in the form of a parallelepiped case made up of two parts assembled using 8 screws (9): - The lower part, known as the HF frame (8), - The upper part, known as the CPU/filter frame (7) The RPU is secured to the aircraft using four M6 screws (not supplied), which cross the 4 flanges (10), located symmetrically on each side of the lower...
  • Page 34 COMPONENT MAINTENANCE MANUAL C17004 34-57-96 Inside Description Page 12 Figure 3 MAY 30/95 COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 35 COMPONENT MAINTENANCE MANUAL C17004 B. Inside Description (see Figure 3) Disassembling the battery cover (2) provides access to the two batteries (3) and (4). Disassembling cover (1) provides access to: - Power supply PCB Z1 (5), secured directly under the cover (1); - Filter PCB Z2 (16), and its connections: flexible circuit (15), connected to the circuit (14), soldered to functional connector J1 (13).
  • Page 36 COMPONENT MAINTENANCE MANUAL C17004 3. Operation A. Principle of the GPS System The GPS system is divided into 3 segments: - The space segment (the satellites) - The ground segment (the control stations) - The user segment (the Receiver Processor Unit, the Antenna Coupler Unit and, in some cases, the PreAmplifier Unit).
  • Page 37 COMPONENT MAINTENANCE MANUAL C17004 B. General RPU Operation (see Figure 4) (1) Composition The Receiver Processor Unit RPU comprises the following interchangeable subassemblies: (a) Power supply PCB, Z1 which supplies the voltages required for operating the various subassemblies as well as the monitoring and power-on signals.
  • Page 38 COMPONENT MAINTENANCE MANUAL C17004 - Fixing aircraft position: . computation, filtering, and maintenance of aircraft position and speed . computation of GPS and UTC time, . management of navigation modes. - Input/output management: . ARINC 429 . RS 422, . program pin .
  • Page 39 COMPONENT MAINTENANCE MANUAL C17004 34-57-96 RPU Block Diagram Pages 17/18 Figure 4 OCT 16/95 COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 40 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 41 The amplified IF signal is transformed into a digital signal by the A/D converter before being processed digitally. 34-57-96 Page 19 OCT 15/01 © THALES AVIONICS COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 42 COMPONENT MAINTENANCE MANUAL C17004 (b) Signal processing This function is designed to make the signals received usable by the central processing unit. The signal is processed on PCBs Z3 and Z4. The HF PCB, Z4, pre-processes the signal. The CPU PCB, Z3, processes the signal. On the Z4 PCB, the Asic T100 performs common pre-processing of the GPS signals.
  • Page 43 COMPONENT MAINTENANCE MANUAL C17004 (3) Operating modes The RPU has various operating modes, the procedure and sequencing of which are defined by the software program, according to the state of the RPU, the number of satellites received, the presence (or absence) and the state of certain parameters.
  • Page 44 COMPONENT MAINTENANCE MANUAL C17004 (d) Clock warm-up mode If thermal stabilization of the RPU internal clock has not been at- tained by the end of the Initialization mode (acquisition is not yet possible), the RPU is set to the clock warm-up mode; the position, speed and the time are maintained by available external aids.
  • Page 45 COMPONENT MAINTENANCE MANUAL C17004 1 3D+T mode (5 to 8 satellites usable) This mode (3 dimensions with time) is the preferred operating mode of the RPU. It provides the functions generally available in the 3D+T mode; moreover, the use of a fifth satellite adds dual redundancy to PVT (speed time position) processing, which makes it possible to check measurement consistency.
  • Page 46 COMPONENT MAINTENANCE MANUAL C17004 4 2D+T mode ( 3 satellites usable in the medium and short term). This mode is used if the 3D+T (5 satellites), 3D+T or 3D modes cannot be activated, under the following conditions: - Geometry of these satellites enabling activation of the 2D+T mode (specific geometric criteria of the mode), - Availability of an altitude and altitude rate aid (if these con- ditions are satisfied, the RPU goes into the DR mode).
  • Page 47 (10 MHz) is applied to the V input of the phase/frequency phase comparator. 34-57-96 Page 25 OCT 15/01 © THALES AVIONICS COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 48 OVFL overflow bit are transmitted to the T100 circuit. 34-57-96 Page 26 OCT 15/01 © THALES AVIONICS COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 49 COMPONENT MAINTENANCE MANUAL C17004 (7) AGC Loop The automatic gain control (AGC) is designed to slave the amplitude of the A/D converter input signal to a programmable instruction. An AGC (DAC 0/11) digital signal is generated by the Asic T100 circuit. It is applied to the input of a digital/analog converter;...
  • Page 50 COMPONENT MAINTENANCE MANUAL C17004 (b) Clock reception and generation The Asic T100 receives: - The HT100 clock (100 MHz), generated from the PLL1 circuit, - The BT time base signal generated by the CPU PCB Z3 Based on these clocks, the Asic T100 generates the following clock signals: - H25T100 (25 MHz), by 4 way division of HT100, - H2OT100 (20 MHz) by 5 way division of HT100...
  • Page 51 COMPONENT MAINTENANCE MANUAL C17004 (9) Power supplies provided by the HF PCB Starting with the following voltages: +5VHF, +15 VHF, delivered by power supply PCB Z1, the HF PCB provides the following voltages: (a) Internal voltages +1.6 VDC, obtained after filtering the +5VHF +10VANA, + 10VHF, obtained after filtering the +15VHF External voltages -15VPILOTE, after filtering the - 15VHF, is used by the Z5 clock PCB.
  • Page 52 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 53 COMPONENT MAINTENANCE MANUAL C17004 Schematic Diagram of single-HF PCB, Z4 34-57-96 (RPU P/N C17004HA02, C17004HA04) Figure 5 Pages 29/30 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 54 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 55 C17004 Schematic Diagram of double-HF PCB, Z4 34-57-96 (RPU P/N C17004DA02, C17004DA04, C17004PA01, C17004PA03) Pages 29a/30a Figure 5a OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 56 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 57 COMPONENT MAINTENANCE MANUAL C17004 D. Operation of sub-unit CPU PCB Z3 (see Figure 6) (1) Composition The CPU PCB includes - A microprocessor (µp) 68020, - A coprocessor (cp) 68882, - An un-backed RAM memory, - An backed RAM memory, - An EEPROM memory, - An Asic GLU circuit, - An Asic COMA circuit,...
  • Page 58 COMPONENT MAINTENANCE MANUAL C17004 (b) µp bus interface This interface is used to: - Create selection read and write orders for the various TS25 pro- grammable functions, upon command from the 68020 µp, - Manage interrupt logic, - Perform discrete management of outputs P104 and P106, The µp bus interface is connected to the data bus (D 16/31), address bus (A1/9), SB service bus that also includes the signals for "chips select"...
  • Page 59 COMPONENT MAINTENANCE MANUAL C17004 (e) Acquisition function The acquisition function receives the following signals: - Satellite signal (ACQ 0/15), pre-processed in the HF PCB, Z4, -The code signals, generated by the TS25 code function. This function performs the following operations: - Correlation of the coded signal (during transmission) and of the code, on two channels (either delay advance or delta point) in or- der to find the non coded signal.
  • Page 60 COMPONENT MAINTENANCE MANUAL C17004 This memory comprises 2 circuits of 8 K x 8 bits that create as a whole, a capacity of 8 Kwords of 16 bits; these 2 circuits are connected to the 16 most significant bits (D16 to D31); They are powered by a backed-up 5 V supply (5VSPIL) which enables memo- ryzed data saveguard, while the RPU is switched off.
  • Page 61 COMPONENT MAINTENANCE MANUAL C17004 (9) Asic COMA This circuit receives, transmits and stores ARINC data. The COMA circuit is connected to: - Data bus D (0/31), - Address bus A (0/25), - Service bus SB. ARINC interface circuits The COMA circuit provides: - Access to the EEPROM and RAM memories, - ARINC communications management.
  • Page 62 COMPONENT MAINTENANCE MANUAL C17004 (12) Discrete signal input/output interface (a) Time Mark Pulse Inputs (optional) The two inputs, TMP1.1 and TMP2.1 are matched by a buffer circuit (EVTA and EVTB signals) and are applied to the EVT inputs of the 2 TS25 circuits.
  • Page 63 COMPONENT MAINTENANCE MANUAL C17004 34-57-96 Schematic Diagram of CPU PCB, Z3 Pages 37/38 Figure 6 (Sheet 1/2) OCT 16/95 COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 64 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 65 COMPONENT MAINTENANCE MANUAL C17004 34-57-96 Schematic Diagram of CPU PCB, Z3 Pages 39/40 Figure 6 (Sheet 2/2) MAY 30/95 COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 66 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 67 COMPONENT MAINTENANCE MANUAL C17004 E. Operation of sub-unit Filter PCB, Z2 (see Figure 7) The filters PCB is connected by a flexible circuit to functional connector This PCB manages: - the interface between J1 and the other RPU PCBs, - the interconnection between the Z1 power supply PCB and the CPU PCB Z3, using inter-PCB connectors.
  • Page 68 COMPONENT MAINTENANCE MANUAL C17004 FILTERS PCB +28VAvion +28VFILT (Z1) 0VAvion 0VFILT (Z1) Filtering circuits 34-57-96 Schematic Diagram of filters PCB, Z2 Page 42 Figure 7 OCT 16/95 COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 69 COMPONENT MAINTENANCE MANUAL C17004 F. Operation of sub-unit Clock PCB Z5 This PCB is designed to generate a reference clock: 10 MHz. This clock is generated by a thermostated oscillator Y1 (temperature adjust- ment at + 85°C); Y1 is powered by regulator Q1 which supplies - 12 V, from -15VPILOTE from HF PCB Z4.
  • Page 70 COMPONENT MAINTENANCE MANUAL C17004 G. Operation of sub-unit Power supply PCB Z1 (see Figure 8) (1) Functions Using +28VFILT (+28VAVION mains filtered on the Z2 filter PCB), PCB Z1 is designed to supply: - The voltage levels necessary for RPU operation: - +15VUC, -15VUC, +15VHF -15VHF, +5VUC, -5VUC, +5VSPIL (+5 V backed up by batteries), to guarantee that information remains stored during a mains failure.
  • Page 71 The ITCOUPAL signal (power supply cut-off interrupt) is generated for cut-offs > 1 ms. 34-57-96 Page 45 OCT 15/01 © THALES AVIONICS COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 72 COMPONENT MAINTENANCE MANUAL C17004 (9) Temperature monitoring This circuit comprises a TH1 thermostat, powered with +5VUC, which sup- plies a voltage that indicates equipment temperature: the STEMPE signal changes state whenever equipment temperature is higher than + 85°C. 34-57-96 Page 46 MAY 30/95 COPYRIGHT SEXTANT Avionique 1995...
  • Page 73 COMPONENT MAINTENANCE MANUAL C17004 34-57-96 Schematic Diagram of the power supply PCB, Z1 Pages 47/48 Figure 8 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 74 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 75 COMPONENT MAINTENANCE MANUAL C17004 TESTING AND TROUBLESHOOTING Not covered by this document. 34-57-96 Page 101 MAY 30/95 COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 76 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 77 - Remove the Z3 PCB (130) by disconnecting it from the filter PCB Z2 (150). - Place Z3 into an antistatic bag (145). 34-57-96 Page 301 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 78 (310); recuperate the four washers (290) and the insulation bush (300). - Unplug PCB Z5 and place it into an antistatic bag (295). 34-57-96 Page 302 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 79 COMPONENT MAINTENANCE MANUAL C17004 CLEANING 1. Materials Required - A clean, soft, lint-free cloth. - A compressed air blower.oft bristle brush for cleaning. - A soft, cleaning brush. 2. Ingredients - Denatured alcohol. 3. Method Remove dust from outer parts using the cloth. Clean the connectors using a soft brush dipped in denatured alcohol and then dry using the compressed air blower.
  • Page 80 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 81 (240) in place on PCB Z4. - Lock the 4 screws (280) in place on PCB Z5 (260) 34-57-96 Page 701 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 82 PCB Z1 support bracket. - Use the 6 loss proof screws (20) to attach the cover. 34-57-96 Page 702 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 83 After removal from storage and before use, install the batteries and check that the equipment works correctly. 34-57-96 Page 703 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 84 34-57-96 34-57-96 Sub-units Interconnection Page 704 Figure 701 Page 704 MaY 30/95 Figure 701 OCT 15/01 © THALES AVIONICS COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 85 COMPONENT MAINTENANCE MANUAL C17004 SPECIAL TOOLS, FIXTURES AND EQUIPMENT LIST OF SPECIAL MATERIALS 1. List tools and equipment Not applicable 2. List of special materials NOTE: Equivalent products can be used. UTILIZATION NAME CODE NAME AND ADDRESS OF PRODUCT OF SUPPLIER Denatured alcohol F0619 PROLABO...
  • Page 86 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 87 COMPONENT MAINTENANCE MANUAL C17004 ILLUSTRATED PARTS LIST INTRODUCTION A. General This ILLUSTRATED PARTS LIST (IPL) is prepared to ATA Specification 100. It is divided as follows: - INTRO: Introduction, - OPT: Otional Parts List, - VCL: Vendor Code List, - EDI: Equipment Designator Index, - NI: Numerical Index (in alphanumeric order), - Detailed Parts List.
  • Page 88 COMPONENT MAINTENANCE MANUAL C17004 (1) Figure and Item Number The figure number is given on the first line at the top of each page. Each item in the parts list which has a part number also has an item number. If there is a dash in front of an item number, the item is not shown on the figure.
  • Page 89 COMPONENT MAINTENANCE MANUAL C17004 (5) Effectivity Code The Effectivity Code is a letter which shows the interchangeability of the parts on a figure, as shown below: FIGURE PART NUMBER AIRLINE NOMENCLATURE EFF. ITEM STOCK NO. CODE ASSY B490AAM01 UNIT B490AAM02 UNIT B490AAM03 UNIT...
  • Page 90 COMPONENT MAINTENANCE MANUAL C17004 (6) Units per Assy The UNITS PER ASSY column shows the number of parts necessary for the next highter assembly. For some assemblies or parts, the number is replaced by the letters RF (for Reference) and AR (As Required). D.
  • Page 91 COMPONENT MAINTENANCE MANUAL C17004 OPTIONAL PARTS LIST MANUFACTURER‘S OPTIONAL MFR PART NUMBER CODE PART NUMBER CODE XUQ1ZH030APA F0110 E25401B30QZHAPA F0188 E25401B30QZHAPA F4796 E25401B30QZHAPA K5997 34-57-96 Page 1005 MAY 30/95 COPYRIGHT SEXTANT Avionique 1995 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 92 156 AVENUE DE METZ 93230 ROMAINVILLE FRANCE F8841 SJM EUROSTAT 45 ROUTED’ORGELET 39130 PONT DE POITTE FRANCE F9111 THALES AVIONICS SA AERODROME DE VILLACOUBLAY ZONE AERONAUTIQUE LOUIS BREGUET BP 200 78141 VELIZY CEDEX FRANCE 34-57-96 Page 1007 OCT 15/01 © THALES AVIONICS...
  • Page 93 DESIGNATION ITEM DESIGNATION ITEM DESIGNATION ITEM 150A 150B 130A 130B 130C 130D 230A 230B 260A 34-57-96 Page 1009 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 94 NYLON 2,2X5X0,3MM SAME AS A1229457 S1ZE025APA 290A UTQ1ZH025006APA 140A 160A 240A 270A UTQ1ZH025008APA 280A UTQ1ZH025016APA 34-57-96 Page 1011 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 95 145A 255A 20-803-0020 295A 79078538 330A 79106699 300A 79129947 320A 79136839 350A 79137486 340A 8500-5600 34-57-96 Page 1012 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 96 COMPONENT MAINTENANCE MANUAL C17004 NUMERICAL INDEX Page left blank intentionally 34-57-96 Page 1013 NOV 30/97 COPYRIGHT SEXTANT Avionique 1997 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 97 This document and any data included are the property MAY 30/03 of THALES AVIONICS. They may not be reproduced, disclosed or utilized without the company's prior written approval. The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 98 ORDER OVERLGTH MPN NYLON 2,2X5X0,3MM MADE BY VF9806 * * * - Item not illustrated 34-57-96 Page 1015 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 99 UTQ1ZH040020APA .SCREW F0110 CZX M4X20 SST PASS. (A1246562) * * * - Item not illustrated 34-57-96 Page 1016 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 100 ATTACHING PARTS 190A UTQ1ZH030006APA .SCREW F0110 CZX M3X6 SST PASS. (A1229703) - Item not illustrated 34-57-96 Page 1017 OCT 15/01 © THALES AVIONICS The document reference is online, please check the correspondence between the online documentation and the printed version.
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