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Thales C17004DA02, Component Maintenance Manual With Illustrated Parts List

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Pages 29a/30a

© THALES AVIONICS

OCT 15/01

COMPONENT MAINTENANCE MANUAL

C17004

Schematic Diagram of double-HF PCB, Z4

(RPU P/N C17004DA02, C17004DA04,

C17004PA01, C17004PA03)

Figure 5a

The document reference is online, please check the correspondence between the online documentation and the printed version.

Summary of Contents for C17004DA02

Page 1: ...VER PROCESSOR UNIT NSS 100S 1 P N C17004DA02 C17004DA04 C17004HA02 C17004HA04 C17004PA01 C17004PA03 COMPONENT MAINTENANCE MANUAL WITH ILLUSTRATED PARTS LIST The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 2: ...tenance of relevant equipment and shall return it promptly to THALES AVIONICS upon its request Users are kindly requested to notify THALES AVIONICS of any discrepancy omission or error found in this manual Please send your comments to THALES AVIONICS Documentation Department 25 Rue Jules Vedrines 26027 VALENCE Cedex FRANCE Tel 33 04 75 79 85 11 Telex 345824F Telefax 33 04 75 79 87 44 The document ...

Page 3: ...t be reproduced disclosed or utilized without the company s prior written approval MAY 30 95 RECORD OF REVISIONS REV No ISSUE DATE INSERTED REV No ISSUE DATE INSERTED DATE BY DATE BY 01 02 03 04 OCT 16 95 NOV 30 97 OCT 15 01 MAY 30 03 The document reference is online please check the correspondence between the online documentation and the printed version Oct 03 cc ...

Page 4: ...The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 5: ...Avionique 1995 c RECORD OF TEMPORARY REVISIONS TEMPORARY REVISION INCORPORATED CANCELLED No PAGE No DATE BY REVISION No BY RTR Page 1 MAY 30 95 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: ...Y 30 95 OCT 15 01 MAY 30 95 MAY 30 95 OCT 16 95 OCT 15 01 NOV 30 97 OCT 16 95 OCT 15 01 OCT 16 95 MAY 30 95 OCT 15 01 MAY 30 95 MAY 30 95 MAY 30 95 MAY 30 95 MAY 30 95 OCT 16 95 MAY 30 95 OCT 16 95 Testing and Troubleshooting Disassembly Cleaning Assembly and Storage 17 18 19 20 21 22 23 24 25 26 25a 26a 27 28 29 30 29a 30a 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 101 102 301 302 401 ...

Page 8: ...cial Tools Fixtures and Equipment List of Special Materials Illustrated Parts List 901 902 1001 1002 1003 1004 1005 1006 1007 1008 1009 1010 1011 1012 1013 1014 1015 1016 1017 1018 1019 1020 MAY 30 95 Blank MAY 30 95 MAY 30 95 MAY 30 95 MAY 30 95 MAY 30 95 Blank OCT 15 01 Blank OCT 15 01 Blank OCT 15 01 OCT 15 01 NOV 30 97 MAY 30 03 OCT 15 01 OCT 15 01 OCT 15 01 OCT 15 01 OCT 15 01 Blank The docum...

Page 9: ...ANT Avionique 1995 c RECORD OF VALIDITY TEMPORARY REVISIONS No DATE OF ISSUE REMOVED BY REVISION OBSERVATIONS No DATE RVTR Page 1 MAY 30 95 The document reference is online please check the correspondence between the online documentation and the printed version ...

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Page 11: ...6 COPYRIGHT SEXTANT Avionique 1995 c SERVICE BULLETIN LIST SERVICE BULLETIN DATE INCORPORATED SUBJECT SBL Page 1 MAY 30 95 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: ...7AA 16181AA 03 DA02 Software modification of Z3 PCB CPU PCB Z3 E17006AB03 becomes E17006AB05 RPU P N C17004DA02 becomes C17004DA04 16177AC 16181AB 03 HA02 Software modification of Z3 PCB CPU PCB Z3 P N E17006AB03 becomes E17006AB05 RPU P N C17004HA02 becomes C17004HA04 16177AD 16181AC 03 PA01 Software modification of Z3 PCB CPU PCB Z3 E17006MA01 becomes E17006MA03 RPU P N C17004PA01 becomes C17004...

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Page 15: ...ING 101 DISASSEMBLY 301 CLEANING 401 CHECK Not applicable REPAIRS Not applicable ASSEMBLY AND STORAGE 701 FITS AND CLEARANCES Not applicable SPECIAL TOOLS FIXTURES AND EQUIPMENT LIST OF SPECIAL MATERIALS 901 ILLUSTRATED PARTS LIST 1001 TC Page 1 MAY 30 95 The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 16: ...The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 17: ...ematic Diagram of double HF PCB Z4 29a 30a RPU P N C17004DA02 C17004DA04 C17004PA01 C17004PA03 Figure 6 Schematic Diagram of CPU PCB Z3 sheet 1 2 37 38 Figure 6 Schematic Diagram of CPU PCB Z3 sheet 2 2 39 40 Figure 7 Schematic Diagram of filter PCB Z2 42 Figure 8 Schematic Diagram of power supply PCB Z1 47 48 Figure 701 Sub units interconnection 704 IPL Figure 1 NSS100S 1 1014 TC Page 2 OCT 15 01...

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Page 19: ...bering is based on a section of numbers for each title 1 100 DESCRIPTION AND OPERATION 101 200 TESTING AND TROUBLESHOOTING 201 300 NOT ALLOCATED 301 400 DISASSEMBLY 401 500 CLEANING 501 600 CHECK 601 700 REPAIRS 701 800 ASSEMBLY AND STORAGE 801 900 FITS AND CLEARANCES 901 1000 SPECIAL TOOLS AND EQUIPMENT LIST OF SPECIAL MATERIALS 1001 1100 ILLUSTRATED PARTS LIST B Values are generally given in SI ...

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Page 21: ...AU PreAmplifier Unit PPS Precise Positioning Service precise position determination service for authorized users PT Precise Time PTTI Precise Time and Time Interval PVT Position Speed Time RPU Receiver Processor Unit SA Selective Availability SB Service Bus SPS Standard Positioning Service STANAG Standardization Agreement UTC Universal Time Coordinated 3D T three dimensional and time position solu...

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Page 23: ...s in the parallel mode over 8 channels using L1 L2 receive frequencies Measurement of pseudo distances and pseudo speeds that correspond to the satellites used Fixing and maintenance of aircraft position and geographic speed based on GPS measurements position determination is based on the SPS system Stan dard Positioning Service Determination of GPS and UTC Universal Time Coordinated Taking into a...

Page 24: ... frequency L1 L2 receiver No Yes Yes Differential GPS No No No Lightning protection No No No External clock No No No ARINC A REC 2 input No No No RS422 RS OPT Inputs Outputs No No No Program pin inputs No No No Bus coupler 1553 No No No P Y codes No No No Y code No No No PTTI No No No PPS No No No µp clock 20 MHz 20 MHz 25 MHz OCT 15 01 THALES AVIONICS The document reference is online please check...

Page 25: ...lectrically bonded and have the same potential as the antenna and the power supply grounds The RPU must be installed in such a way as to have sufficient clea rance for heat dissipation it is recommended to install it vertically so as to facilitate natural convection b Environment The environmental conditions comply with MIL STD 810D Operating temperature from 45 C to 70 C Storage temperature from ...

Page 26: ...m level of tracking code and carrier frequency 169 dBW Maximum acquisition level 150 dBW 3 Acceptable level of satellite signals frequency L2 P code optional processing Minimum acquisition level 169 dBW Minimum level of tracking code and carrier frequency 169 dBW Maximum acquisition level 150 dBW 4 Maximum power before destruction 0 dbW Note dBW decibels referenced to 1 W 5 Position fixing Precisi...

Page 27: ...ionosphere delay model parameters ephemerides all parameters that precisely define the orbit of received satellites 2 ARINC Inputs outputs a Input no 1 Mnemonic A REC 1L A REC 1H Type ARINC 429 LS 12 5 kHz Functions RPU initialization latitude longitude altitude time and date RPU programming in special configurations satellite deselection preferential choice of position fixing mode Reception using...

Page 28: ... IH and ELITE OL ELITE OH Functions used for integration and tests used to display the con tents of the entire memory and in particular the self test parameters b Optional input output Mnemonic RSOPT IL RSOPT 1H and RSOPT OL RSOPT OH 4 Program pin inputs optional Mnemonics PP1 PP2 PP3 PP4 PP5 5 Discrete inputs outputs a Time Mark Pulse Inputs optional Mnemonic TMP1 IL TMP1 IH and TMP2 IL TMP2 IH b...

Page 29: ...inc 429 LS no 1 input low 7 O A EM 1L Arinc 429 HS no 1 output low 8 Spare 9 Spare 10 I 0VAVION 0 V power supply input 11 I TMP2 IH Time Mark Pulse no 2 input high optional 12 I TMP2 IL Time Mark Pulse no 2 input low optional 13 O TMP1 OH Time Mark Pulse no 1 output high 14 Spare 15 Spare 16 Spare 17 O A EM 2H Arinc 429 HS no 2 output high 18 0VLOG Logic 0V 19 I PP1 Program pin no 1 input optional...

Page 30: ...tenance output 37 Spare 38 I ELITE IH Elite maintenance input high 39 I ELITE IL Elite maintenance input low 40 Spare 41 Spare 42 I PP4 Program pin no 3 input optional 43 O RSOPT OH RS422 output high optional 44 Spare 45 BL BF TMP1 TMP2 Shielding 46 Spare 47 BL AR2 Arinc no 2 digital shielding 48 I RSOPT IH RS422 input high optional 49 BL RSOPT RS OPT shielding 50 O RSOPT IL RS422 output low optio...

Page 31: ... J1 ARINC 429 LS A REC 1 A REC 2 A EM 1 A EM 2 PP1 to PP5 ELITE I ELITE O RSOPT I RSOPT O TMP1 0 BT250 M RST 28VAVION TMP1 I TMP2 I Optional ARINC 429 HS Optional ARINC 429 HS Optional RS422 RS422 Optional GPS System Inputs and Outputs Figure 1 MAY 30 95 The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 32: ...4 57 96 Page 10 COPYRIGHT SEXTANT Avionique 1995 c 1 2 3 4 5 6 7 8 9 10 11 12 Outside Description Figure 2 MAY 30 95 The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 33: ...crews not supplied which cross the 4 flanges 10 located symmetrically on each side of the lower part The upper part CPU filter frame is closed off by a cover 1 secured using 13 screws 2 a second cover 5 secured using six screws 6 provides direct access to the two batteries 3 and 4 Connection to the ACU antenna or the PAU preamplifier is made using connector J5 12 Connection to the aircraft mains a...

Page 34: ...96 Page 12 COPYRIGHT SEXTANT Avionique 1995 c 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 Inside Description Figure 3 MAY 30 95 The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 35: ...4 soldered to functional connector J1 13 After disassembly of the CPU filter frame 6 and the HF frame 9 it is possible to access The CPU PCB Z3 7 secured to the CPU filter frame 6 The HF PCB Z4 8 secured to the HF frame 9 the Z4 PCB is fitted with a bracket 12 for attaching connector J5 11 Clock PCB Z5 10 secured to the HF frame under the Z4 PCB 8 Interconnection between the various PCBs is provid...

Page 36: ...ast 4 satellites is possible anywhere in the world The earth revolution time of each satellite is 12 hours Each satellite calculates and maintains its position by means of the ground segment It transmits to the user segment its position the GPS time the date the ephemerides of its orbit and the GPS network 2 Ground segment This segment comprises a main station and various relay stations instal led...

Page 37: ...ain the time Supply power to the protected memory Z3 PCB b Filter PCB Z2 which provides Protection against power surges and filtering of the 28VAVION supply Filtering of all the input output information available on connec tor J1 c Central Processing Unit CPU PCB Z3 which provides the following functions Processing of signals transmitted by satellites on eight indepen dent receive channels namely ...

Page 38: ...ameters in the protected memory while the RPU is off d HF PCB Z4 This PCB provides the interface between the ACU antenna or the PAU preamplifier and the CPU PCB Z3 central processing unit Its main functions are as follows Analog filtering of the RF signal on each frequency L1 and L2 Conversion of the RF signal into an intermediate frequency signal IF Amplification of the IF signal Processing the 1...

Page 39: ...NUAL C17004 34 57 96 OCT 16 95 COPYRIGHT SEXTANT Avionique 1995 c RPU Block Diagram Figure 4 Pages 17 18 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: ...ite signal contains an identification code and navigation data Two types of HF PCB can be mounted which can process one or two frequency waves see versions chart The HF PCB also receives an signal OL generated by a local oscillator which is in turn controlled by a 10 MHz clock sent from PCB Z5 The intermediate frequency signal IF available at the output of the frequency converter is applied to the...

Page 42: ...it The fact that the TS25 circuits and the central processing unit are grouped together on the CPU PCB means that the signal is completely processed on this PCB c Central processing unit The central processing unit comprises a 68020 microprocessor and a 68822 coprocessor associated with the memory circuits The following buses are used for communication between the various Asic circuits the central...

Page 43: ...acs and ephemerides in the protected memory area before the RPU power is turned off Storage of the last position calculated b Self test mode As soon as the power is turned on the RPU performs self test se quences on each of its subassemblies Once these self tests have been completed the RPU goes to the next mode Note Cyclic self tests are then carried out as background tasks in all operating modes...

Page 44: ...R Dead Reckoning mode This mode is engaged if the number of satellites used for navigation available ephemerides satisfactory geometry is insufficient to activate the Position fixing mode In this mode the RPU performs the following functions Dead reckoning navigation according to the best external aids available inertial or pressure altitude data true air speed true heading magnetic heading altitu...

Page 45: ...ds when 4 satellites are available with a satisfactory geometry GDOP criteria and if the 3D T mode 5 satellites cannot be used The following functions are provided GPS position fixing 3 dimensions and readjusting the GPS time Checking the position fixing solution by checking consistency with the aids 3 3D mode 3 satellites usable in the short term This mode clock coasting is the preferred mode of ...

Page 46: ...eration of sub unit HF PCBs Z4 see Figures 5 and 5a 1 Versions Two types of HF PCBs can be mounted single high frequency PCB receiving L1 frequency double high frequency PCB which can receive L1 and L2 frequencies 2 Z4 PCB components The main elements of the Z4 PCB are Analog filtering and matching of GPS signals for one or two frequencies Filters switching only for double HF PCB A local oscillato...

Page 47: ...CB when the specific software is installed 4 Generation of the H1400 signal and HT100 HCAN clocks a Local oscillator This is a quartz oscillator which generates sinusoid signal H1400 F 1400 MHz used by the frequency converter this oscillator is controlled by frequency synthesis circuit PLL1 b PLL1 circuit This is an AsGa integrated circuit which includes the elements required for performing a phas...

Page 48: ...into a IF intermediate frequency signal It receives the filtered radio frequency signal 1575 42 MHz or 1227 60 MHz and the 1400 MHz frequency H1400 signal OL generated by the local oscillator The IF signal value is the difference between the two frequencies IF 1575 42 1400 175 42 MHz or IF 1400 1227 60 172 40 MHz 6 Filtering amplification and D A conversion of the IF signal The IF signal from the ...

Page 49: ...it its other functions are Clock reception and generation Overflow counter Programmable local oscillator µp bus interface AGC signal generation a Signal pre processing This function involves performing the following operations Reception of 4 bits CAN 0 3 from the A D converter Sampling of 4 bits and the OVLF overflow bit on the 100 MHz fre quency by the HT100 clock parallelization on 4 channels Tr...

Page 50: ...e d Programmable local oscillator This oscillator specific to the Asic T100 is used to pre process the signal before a frequency change The oscillator frequency is programmed using the µp bus interface with 5 KHz steps this makes it possible to perform an infradine or supradine demodulation de pending on the frequency sign e µp bus interface This interface enables the Asic T100 to communicate with...

Page 51: ...P after filtering of the 15VHF is used to power the optional preamplifier PAU it is transmitted by the same wire as the RF input signal 10 Monitoring and test signals The HF PCB transmits the following signals to the CPU on PCB Z3 PLL ASSER from PLL1 or logic from UP and DWN PRES ANT antenna presence CAGTST AGC test SURPILO monitoring of the Z5 clock PCB this signal is obtained from IPILOTE curren...

Page 52: ...The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 53: ... 15 01 COMPONENT MAINTENANCE MANUAL C17004 Schematic Diagram of single HF PCB Z4 RPU P N C17004HA02 C17004HA04 Figure 5 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: ...PONENT MAINTENANCE MANUAL C17004 Schematic Diagram of double HF PCB Z4 RPU P N C17004DA02 C17004DA04 C17004PA01 C17004PA03 Figure 5a 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: ...utput interface A program pin and discrete signal interface 2 Asic TS25 Circuits a Functions The 2 TS25 circuits process GPS signals on 2 X 5 identical channels 8 are used the 8 channels are independently read and write acces sible by the 68020 microprocessor data bus Each circuit performs the following functions Interface with the 68020 µp buses Code generation and checking Sequencing and time st...

Page 58: ... each channel 0 to 4 The following programmable parameters are transmitted to the TS25 acquisition blocks The pseudo distance The air speed code The choice of satellite The code word The delay advance step deviation of the codes from the so called normal code The type of correlation d Sequencer and Time Stamping Function This function is designed to generate The synchronization signals required by...

Page 59: ...ction based on instructions supplied by the data bus pro vides checking code outputs switching of the selected channel g Time function This function provides a time measurement of a GPS power supply cut during which the RPU is powered by the backed up power supply 5VSPIL The time function comprises A 40 bit asynchronous counter with self test by the 68020 µp A 32 kHz clock controlled by an externa...

Page 60: ...2 interface circuits This circuit performs the following functions Clock generation based on clocks CLK20 20 MHz and H50 50 MHz it generates the µp clock CLKMIC 20 or 25 MHz chip select generation Watch dog for monitoring bus exchanges and DMA sequences direct access memory Interrupt encoder Processing 2 RS422 lines the data transfers are carried out in the asynchronous mode 8 RS422 input output i...

Page 61: ...match 2 ARINC input lines A REC1 A REC 2 and 1 double ARINC output line A EM1 and A EM2 In order to test the ARINC lines wire is used to reloop the unused inputs on the Asic COMA The transmission speed of the ARINC lines is defined by program A REC1 and A REC2 12 5 KHz A EM1 and A EM2 100 KHz 11 Program pin input interface The CPU PCB has 5 optional program pin inputs PP1 to PP5 These inputs are m...

Page 62: ...utput is generated by one of the TS25 circuits after storage and matching by a buffer c BT250F The BT output of one of the TS25 is matched by a buffer and consti tutes the BT250 output reserved for maintenance d Internal discrete inputs Six signals internal to the RPU from PCBs Z1 and Z4 are applied to an A D converter then to a 3 state buffer circuit the outputs of which are connected to data bus...

Page 63: ...34 57 96 OCT 16 95 COPYRIGHT SEXTANT Avionique 1995 c Schematic Diagram of CPU PCB Z3 Figure 6 Sheet 1 2 Pages 37 38 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: ...34 57 96 MAY 30 95 COPYRIGHT SEXTANT Avionique 1995 c Schematic Diagram of CPU PCB Z3 Figure 6 Sheet 2 2 Pages 39 40 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: ...CPU PCB Z3 using inter PCB connectors 1 Filtering and protecting the 28VAVION The input 28VAVION OVAVION is protected against power surges by 2 tumble diodes electromagnetic disturbance by two LC filters 2 Filtering inputs and outputs All input output connections hot point and cold point are filtered by LRC low pass filtering cells the cut off frequency is defined in accor dance with the type of i...

Page 68: ...T Avionique 1995 c J1 28VAvion 0VAvion FILTERS PCB Z2 Filtering circuits 28VFILT Z1 0VFILT Z1 Schematic Diagram of filters PCB Z2 Figure 7 OCT 16 95 The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 69: ...from the analog ground due to a 0 5 ohm resistor installed on HF PCB Z4 thus enabling monitoring of IPI LOTE current discharged by Y1 the value of IPILOTE increased at start up is stabilized whenever the temperature of Y1 is adjusted IPILOTE is matched in Z4 informing the CPU that Y1 s temperature has been set which by extension means that the clock is stable HF PCB CLOCK PCB Z5 15VPILOTE 12V IPIL...

Page 70: ... threshold voltages Energy command threshold 17 V used to provide the Reserve com mand signal Anti feedback blockage threshold 20 V used to command transistor CMOS Q1 this transistor functions as an assisted diode when the 28VFILT is lower than 20 V transistor Q1 is blocked which insu lates the RPU from the aircraft mains 3 DC DC converter PS3 It is powered by the 28VFILT filtered once again in th...

Page 71: ...ors during power transients of less than 1 ms 7 Battery management circuit This circuit is designed to generate a backup voltage 5VSPIL which replaces 5VUC once it disappears It also delivers a monitoring signal SURPILE which is indicative of battery condition which is processed by the central processing unit The battery management circuit is connected to the two 3 5 V batteries BT1 and BT2 mounte...

Page 72: ...it 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 MAY 30 95 The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 73: ...AVIONICS OCT 15 01 COMPONENT MAINTENANCE MANUAL C17004 Schematic Diagram of the power supply PCB Z1 Figure 8 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: ... 57 96 Page 101 MAY 30 95 COPYRIGHT SEXTANT Avionique 1995 c TESTING AND TROUBLESHOOTING Not covered by this document 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: ...Z1 PCB connector If necessary remove the Z1 PCB 80 unscrew the 4 upper screws 100 mounting the Z1 PCB converter onto the cover 50 unscrew the 4 screws 90 attaching the Z1 PCB under the cover 50 remove the Z1 PCB 80 and plate it into an antistatic bag 105 C CPU Frame fitted filters unscrew the 8 screws 120 attaching the CPU filter frame 110 onto the HF frame 310 Remove the two frames from the box t...

Page 78: ...it Place Z2 into an antistatic bag 175 F HF PCB Z4 230 Unscrew the 18 screws that mount the Z4 PCB into the HF frame 310 Remove the Z4 PCB 230 by disconnecting it from clock PCB Z5 260 and place it into an antistatic bag 255 G Clock PCB Z5 260 Remove the 4 screws 270 and 280 attaching PCB Z5 onto the HF frame 310 recuperate the four washers 290 and the insulation bush 300 Unplug PCB Z5 and place i...

Page 79: ...ower 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 The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 80: ...The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 81: ... screwdriver C Clock PCB Z5 260 and HF PCB Z4 230 Place an insulating bush 300 on regulator Q1 on the Z5 PCB and install Z5 260 in the HF frame 310 Install PCB Z5 260 using the four screws 270 and 280 do not lock the screws temporarily Install PCB Z4 into the HF frame by plugging connector J22 into connector P22 on PCB Z5 make sure that PCB Z4 is correctly centered in the HF frame Attach the J5 co...

Page 82: ...s Z2 and Z3 on the HF frame equipped with PCBs Z4 and Z5 by plugging connectors J10 J12 J18 on PCB Z3 into connectors P10 P12 P18 on PCB Z4 Use the 8 screws 120 to mount the two frames F Power supply PCB Z1 80 and cover 50 Place PCB Z1 under the cover 50 and screw on without tightening the 4 screws 90 that attach the converter on PCB Z1 to the cover Screw and lock into place the 4 screws 90 that a...

Page 83: ...s or other items releasing toxic gases as this can damage the equipment B Long term storage 1 Remove the batteries 2 Carry out the operations listed above for short term storage 3 Wrap the package in a heat sealable canvas 4 Heat seal the canvas so that it may be unsealed and resealed at least three in the future without having to be replaced 5 Mark the package and protect the labels with transpar...

Page 84: ... J18 P10 P18 Z3 Z4 J5 J1 Z2 Z1 P19 J19 J12 P12 Z5 Sub units Interconnection Figure 701 34 57 96 Page 704 MaY 30 95 COPYRIGHT SEXTANT Avionique 1995 c Sub units Interconnection Figure 701 The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 85: ...products can be used NAME OF PRODUCT CODE NAME AND ADDRESS OF SUPPLIER UTILIZATION T E S T I N G D I S A S S E M B L Y C L E A N I N G C H E C K R E P A I R S A S S Y S T O R Denatured alcohol F0619 PROLABO 12 rue pelée 75011 PARIS FRANCE X LOCTITE 932 F0406 LOCTITE UK LTD Watchmead Wellwgn Garden city herts AL7 1JB ENGLAND X The document reference is online please check the correspondence between...

Page 86: ...The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 87: ...t give the figure and item number of the part in the Detailed Parts List 2 From the Equipment Designator Find the equipment designator of the part on the Electrical Diagram Then refer to the EDI to find the figure and item number of the part in the Detailed Parts List 3 If the Part Number or Equipment Designator of the Part are not known Look for the figure which shows the parts and its item numbe...

Page 88: ...ac turer s NATO code number 3 Airline Stock Number This column is for airline use 4 Nomenclature The NOMENCLATURE column gives the names of the assemblies and parts The indication ATTACHING PARTS shows the parts which attach an assembly or part These attaching parts are given directly below the assembly or part they attach The next line has three asterisks the first of which is directly below the ...

Page 89: ...an only be installed in the unit with item number 1A The detail part with item number 10B can only be installed in units 1A 1B an 1C The detail part with item number 10C can only be installed in unit 1D The subassembly with item number 20A can only be installed in unit 1A The subassembly with item number 20B can be installed in units 1A 1B and 1C The subassemblies with item numbers 20C and 20D and...

Page 90: ...d in the Detailed Parts List AR As Required DET Detail EFF Effectivity ESDS Electrostatic Discharge Sensitive LOC Location NHA Next Higher Assembly NP Not Procurable OPT Optional ORDER OVERLGTH MPN Order Overlength Manufacturer s Part Number POST SB Post Service Bulletin PRE SB Pre Service Bulletin R Revised Lines or pages revised RF For Reference SEL FROM Select From SUPSD BY Superseded By SUBSDS...

Page 91: ...T NUMBER CODE PART NUMBER CODE 34 57 96 Page 1005 MAY 30 95 COPYRIGHT SEXTANT Avionique 1995 c XUQ1ZH030APA F0110 E25401B30QZHAPA F0188 E25401B30QZHAPA F4796 E25401B30QZHAPA K5997 The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 92: ...SAINTE HONORINE FRANCE F6069 POPPELMANN FRANCE R PLASTIQUES SARL 3 RUE ROBERT SCHUMAN BP 87 68172 RIXHEIM CEDEX FRANCE F6177 SAFT DPT ACCUMULATEURS INDUSTRIELS 156 AVENUE DE METZ 93230 ROMAINVILLE FRANCE F8841 SJM EUROSTAT R 45 ROUTED ORGELET 39130 PONT DE POITTE FRANCE F9111 THALES AVIONICS SA R AERODROME DE VILLACOUBLAY ZONE AERONAUTIQUE LOUIS BREGUET BP 200 78141 VELIZY CEDEX FRANCE F9806 BULTE...

Page 93: ... ITEM DESIGNATION ITEM DESIGNATION ITEM 34 57 96 Page 1009 THALES AVIONICS OCT 15 01 Z1 1 80A Z1 1 80B Z1 1 80C Z2 1 150A Z2 1 150B Z3 1 130A Z3 1 130B Z3 1 130C R Z3 1 130D R Z4 1 230A Z4 1 230B Z5 1 260A The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 94: ...01 1 130B 1 E17006MA03 1 130D 1 R E17007CA 1 230B 1 E17007DA 1 230A 1 E17008AA 1 260A 1 E17009AA 1 150A 1 E17009BA 1 150B 1 F1280000 1 310A 1 F1280002 1 110A 1 F1280006 1 50A 1 F1280095 1 180A 1 F1280099 1 210A 2 F1280224 1 10A 1 F1280471 1 220A 2 F1280580 1 10B 1 F1280580 1 10C 1 R F2000175 1 360A 1 GPN200Z10X10 1 5A 1 R LS14500CODE04224X SAME AS A1231323 NYLON 2 2X5X0 3MM SAME AS A1229457 S1ZE02...

Page 95: ...030008APA 1 100A 4 1 170A 4 UTQ1ZH040020APA 1 120A 8 XUQ1ZH030APA 1 200A 2 20 801 0812 1 105A 1 R 1 175A 1 R 20 801 0816 1 145A 1 R 1 255A 1 R 20 803 0020 1 295A 1 R 79078538 1 330A 1 79106699 1 300A 1 79129947 1 320A 1 79136839 1 350A 1 79137486 1 340A 1 8500 5600 1 3A 1 R The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 96: ...04 NUMERICAL INDEX 34 57 96 Page 1013 NOV 30 97 COPYRIGHT SEXTANT Avionique 1997 c Page left blank intentionally The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 97: ...be reproduced disclosed or utilized without the company s prior written approval NSS100S 1 FIGURE 1 60 10 350 100 70 360 50 220 210 90 80 40 130 120 110 20 340 260 300 290 140 280 290 330 270 310 160 150 190 180 320 170 250 30 Z1 Z3 Z2 Z5 Z4 230 240 200 5 3 The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 98: ...DA04 NSS100S 1 RF R ESDS AMDMNT A SUPSDS ITEM 1B POST FEE 16181AA 1F C17004PA03 NSS100S 1 RF R ESDS SUPSDS ITEM 1C POST FEE 16181AC STORAGE PARTS 3A 8500 5600 CAP PROTECTIVE VF0225 1 R A1247178 5A GPN200Z10X10 CAP PROTECTIVE VF6069 1 R A1229222 10A F1280224 COVER ASSEMBLY 1A 1 R SUPSD BY ITEM 10B 10B F1280580 COVER ASSEMBLY 1A 1 R SUPSDS ITEM 10A 10C F1280580 COVER ASSEMBLY 1BCDEF 1 R ATTACHING PA...

Page 99: ...CARD PRINTED EQUIPPED NP 1AB 1 ESDS Z1 POWER SUPPLY PRE AMDMNT A 80B E17004AC CARD PRINTED EQUIPPED 1ABDE 1 R ESDS Z1 POWER SUPPLY POST AMDMNT A 80C E17004BB CARD PRINTED EQUIPPED 1CF 1 R ESDS Z1 POWER SUPPLY ATTACHING PARTS 90A UTQ1ZH025006APA SCREW F0110 4 CZX M2 5X6 SST PASS A1235914 100A UTQ1ZH030008APA SCREW F0110 4 CZX M3X8 SST PASS A1235998 STORAGE PARTS 105A 20 801 0812 BAG ANTISTATIC VF88...

Page 100: ...SCREW F0110 14 CZX M2 5X6 SST PASS A1235914 STORAGE PARTS 145A 20 801 0816 BAG ANTISTATIC VF8841 1 R A1170181 150A E17009AA CARD PRINTED EQUIPPED 1ABDE 1 R ESDS Z2 FILTERS 150B E17009BA CARD PRINTED EQUIPPED 1CF 1 R ESDS Z2 FILTERS ATTACHING PARTS 160A UTQ1ZH025006APA SCREW F0110 10 CZX M2 5X6 SST PASS A1235914 170A UTQ1ZH030008APA SCREW F0110 4 CZX M3X8 SST PASS A1235998 STORAGE PARTS 175A 20 801...

Page 101: ...ARTS 240A UTQ1ZH025006APA SCREW F0110 18 CZX M2 5X6 SST PASS A1235914 250A UTQ1ZH030006APA SCREW F0110 4 CZX M3X6 SST PASS A1229703 STORAGE PARTS 255A 20 801 0816 BAG ANTISTATIC VF8841 1 R A1170181 260A E17008AA CARD PRINTED EQUIPPED 1 ESDS Z5 CLOCK ATTACHING PARTS 270A UTQ1ZH025006APA SCREW F0110 3 CZX M2 5X6 SST PASS A1235914 280A UTQ1ZH025008APA SCREW F0110 1 CZX M2 5x8 SST PASS A1235915 290A S...

Page 102: ... illustrated 34 57 96 Page 1019 THALES AVIONICS OCT 15 01 1 300A 79106699 BUSH 1 310A F1280000 FRAME HF 1 320A 79129947 LABEL 1 330A 79078538 LABEL 1 340A 79137486 LABEL 1 350A 79136839 LABEL 1 360A F2000175 LABEL 1 R The document reference is online please check the correspondence between the online documentation and the printed version ...

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