L3 FA5000 Component Maintenance Manual With Illustrated Parts List Download Page 36

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COMPONENT MAINTENANCE MANUAL

AVIATION RECORDERS

Model FA5000

Initial Issue Page 2

Sep. 30/11

Introduction

−

70–40

Use or disclosure of information on this sheet is subject to

the restrictions on the cover page of this document.

CVDR

Cockpit Voice Data Recorder

Direct Current

EEPROM

Electrically Erasable Programmable Read Only Memory

EUROCAE

European Organization for Civil Aviation Equipment

FAA

Federal Aviation Administration

FDAU

Flight Data Acquisition Unit

CVDR

Flight Data Recorder

FPGA

Field-Programmable Gate Array

FTP

File Transfer Protocol

General Aviation

GMT

Greenwich Mean Time

GND

ground

GSE

Ground Support Equipment

HTTP

HyperText Transfer Protocol

Internet Protocol

IPL

Illustrated Parts List

LRU

Line Replaceable Unit

MHz

Megahertz

MTBF

Mean Time Between Failures

NVRAM

Non-Volatile Random Access Memory

OMS

Onboard Maintenance System

Personal Computer

PCMCIA

Personal Computer Memory Card International Association (now
known as PC Card)

PI/2

Portable Interface/2

PPI

Parallel Peripheral Interface

PWA

printed wiring assembly

PWR

power

REC LVL

Record Level

RIU

Recorder Interface Unit

ROC

Read

−

Out Center

ROSE

Read Out Support Equipment

RSE

Rotor Speed Encoder

RTCA

Radio Technical Commission for Aeronautics

RTMS

Requirements Traceability Management System

SMT

Surface Mount Technology

TDM

Time Division Multiplex

TSO

Technical Standard Order

ULB

Underwater Locator Beacon

UTC

Universal Time Coordinated

WPS

Words Per Second

VDK

Analog Devices RTOS

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

Summary of Contents for FA5000

Page 1: ...NT This document contains L 3 Aviation Recorders privileged information and must not without prior written consent of L 3 Aviation Recorders be used or reproduced in whole or in part or communicated t...

Page 2: ...pyright 2016 by L 3 Communications Cor poration Aviation Recorders End User Statement This manual is intended for aircraft owners and their designated agents for installation of this product No distri...

Page 3: ...motions of persons working with static sensitive devices When handling or servicing equipment containing static sensitive devices adequate precautions must be taken to prevent device damage or destru...

Page 4: ...itle 23 70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online pl...

Page 5: ...ges to Rev 06 Introduction Description Operation CVR Testing Troubleshoot 104 Replaced ULB testing procedure with Test Set P N 17TES0015 FDR Testing Troubleshoot Updated recommended test equipment Dis...

Page 6: ...xx xiv Revised pages to Rev 05 Introduction Description Operation CVR Testing Troubleshoot 104 Revised CATS software to V 2 1 and ROSE software to V 4 7 FDR Testing Troubleshoot Disassembly 301 302 Ad...

Page 7: ...100 140 Revised CATS software using ROC 7 procedure FDR Testing Troubleshoot 209 217 235 Revised Table 202 Check Sums Added Tables 203 204 and 205 Aircraft Interface Main Processor and CSMU troublesho...

Page 8: ...ting Fault Isolation 103 Changed part number 17TES0416 to read 17TES0418 with ad apter Automatic Testing Disassembly Assembly Fit and Clear ances 804 Replaced Environmental Qualification Form EQF Spec...

Page 9: ...Revision 02 Section Page Description Title List of FSB s Front Matter Introduction Description Operation Add sentence To be compliant with TSO C155a RIPS must be in stalled on CVDR Testing Fault Isol...

Page 10: ...on 01 Section Page Description Title List of FSB s Front Matter Introduction Description Operation 16 Add sentence To be compliant with TSO C155a RIPS must be in stalled on CVDR Testing Fault Isolatio...

Page 11: ...ormat Rev 01 Oct 06 11 Add statement on TSO C155a Compliance Rev 02 Jul 17 12 Added P Ns 5001 6103 10 and 5003 6103 11 Rev 03 Feb 27 13 Replaced Environmental Qualification Form EQF Rev 04 Feb 27 14 R...

Page 12: ...ge xii May 06 14 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online...

Page 13: ...tions on the cover page of this document RECORD OF REVISIONS REV NO INSERTION DATE BY REV NO INSERTION DATE BY REV NO INSERTION DATE BY 01 Oct 06 11 G M 02 Jul 17 12 G M 03 Feb 27 13 M R 04 Mar 21 14...

Page 14: ...70 40 Rev 05 Page xiv Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is o...

Page 15: ...D DOT 02 Improved Main Processor which improves CAM audio channel per formance FA5001 CVDR FSB002 23 70 40 002 May 20 14 5001 6103 11 5001 6133 11 INTRODUCTION OF SOFTWARE REVI SION 06 Push to test fi...

Page 16: ...e Bulletin 23 70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is onl...

Page 17: ...xx May 06 14 Table of Contents Rev 06 xxi Mar 16 16 Rev 06 xxii Mar 16 16 Rev 06 xxiii Mar 16 16 Rev 06 xxiv Mar 16 16 Rev 06 xxv Mar 16 16 Rev 06 xxvi Mar 16 16 Rev 06 xxvii Mar 16 16 Rev 06 xxviii...

Page 18: ...7 14 Rev 04 126 Feb 27 14 Rev 04 127 Feb 27 14 Rev 04 128 Feb 27 14 Rev 06 129 Mar 16 16 Rev 04 130 Feb 27 14 FDR Testing and Troubleshooting Rev 06 201 Mar 16 16 Rev 03 202 Feb 27 13 Rev 03 203 Feb 2...

Page 19: ...Sep 30 11 707 Sep 30 11 708 Sep 30 11 709 Sep 30 11 710 Sep 30 11 Rev 06 711 Mar 16 16 Rev 06 712 Mar 16 16 713 Sep 30 11 Rev 05 714 May 06 14 715 Sep 30 11 Rev 06 716 Mar 16 16 Fits and Clearances Re...

Page 20: ...fective Pages Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document 23 70 40 THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is...

Page 21: ...AND OPERATION 4 C TESTING AND TROUBLESHOOTING 4 D DISASSEMBLY 4 E CLEANING 5 F CHECK 5 G REPAIR 5 H ASSEMBLY 5 I SPECIAL TOOLS AND TEST FIXTURES 5 J ILLUSTRATED PARTS LIST 5 6 DOCUMENT VERIFICATION 6...

Page 22: ...NCE PHILOSOPHY 101 A Model FA5000CVDR 101 3 MODEL FA5000CVDR RECORDER IN SERVICE CHECKOUT 102 4 RECORDER INTERFACE UNIT RIU 102 A READ OUT CENTER 7 ROC 7 Interconnects 102 B READ OUT CENTER 7 ROC 7 So...

Page 23: ...hutdown 126 16 Capacitor 126 17 Data Link 126 18 OMS 127 19 RIPS 127 20 FRED 127 21 FDR 127 E READ OUT CENTER 7 ROC 7 RIU Audio Setup Procedure 128 5 READ OUT CENTER 7 ROC 7 AUDIO DOWNLOAD PLAYBACK 12...

Page 24: ...3 TEST THE UNDERWATER LOCATOR BEACON ULB 215 DISASSEMBLY 1 GENERAL 301 2 MODEL 500 RECORDER INDEPENDENT POWER SUPPLY RIPS REMOVAL INSTRUCTIONS 301 3 MODEL FA5000 DISASSEMBLY INSTRUCTIONS 302 A Remove...

Page 25: ...e CLEANING 1 GENERAL 401 2 MATERIALS REQUIRED 401 3 CLEANING PROCEDURES 401 A Printed Wiring Assembly Cleaning 402 B Connector Cleaning 402 C Underwater Locator Beacon Cleaning 402 CHECK 1 GENERAL 501...

Page 26: ...703 D Aircraft Interface PWA AI Installation See Figure 703 or IPL Figure 1 Item 30 705 E Rear Cover Installation See 704 or IPL Figure 1 Item 10 707 F Crash Survivable Memory Unit CSMU Installation...

Page 27: ...ES AND EQUIPMENT 1 GENERAL 901 2 GROUND SUPPORT EQUIPMENT GSE DESCRIPTIONS 904 A Audio Data Link Player Software 905 1 Hardware Requirements for Audio Data Link Player Software 905 2 Hardware Requirem...

Page 28: ...40 Rev 06 Page xxviii Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is o...

Page 29: ...e 105 Line In Properties Line In Level 108 Figure 106 Sound Playback Devices 109 Figure 107 Speaker Properties Levels 110 Figure 108 Volume Mixer Speaker Levels 111 Figure 109 CATS Connecting Pop Up 1...

Page 30: ...Rear Cover Removal Diagram 309 Figure 305 Aircraft Interface AI PWA Removal Diagram 310 Figure 306 Main Processor MP PWA Removal Diagram 312 Figure 307 Main Processor MP PWA Removal Diagram 313 Figure...

Page 31: ...T OF FIGURES Continued FIGURE TITLE Page Figure 901 ROC 7 w CVDR Automated Test Station Software CATS FA5000CVDR TEST SETUP 904 Figure 1000 Sheet 1 of 2 Model FA5001 CVDR Recorders 1007 Figure 1000 Sh...

Page 32: ...40 Rev 06 Page xxxii Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is o...

Page 33: ...61XX 11 Pin Outs and Signal Descriptions 17 Table 101 17TES0700 READOUT CENTER 7 ROC 7 104 Table 102 Underwater Locator Beacon Test Using L 3AR Test Set P N 17TES0015 129 Table 201 Recommended Test E...

Page 34: ...40 Rev 06 Page xxxiv Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is o...

Page 35: ...00CVDR that are equipped with a Video Expansion Card gets digital video in ITU656 digital frame format and compresses it using Motion JPEG compression every 200 milliseconds 5 frames per second It the...

Page 36: ...strated Parts List LRU Line Replaceable Unit MHz Megahertz MTBF Mean Time Between Failures NVRAM Non Volatile Random Access Memory OMS Onboard Maintenance System PC Personal Computer PCMCIA Personal C...

Page 37: ...Locator Beacon ULB Tester Part Number 17TES0015 if functional testing of ULB is required F L 3AR Underwater Locator Beacon CMM Part Number 165E5542 00 4 MAINTENANCE PHILOSOPHY The Model FA5000 Solid...

Page 38: ...peration C TESTING AND TROUBLESHOOTING Sections 100 contains specific checks and tests required to determine the operation al condition of a unit that has been removed from service Also included in th...

Page 39: ...step by step procedures describing the complete as sembly of the Model FA5000 Solid State Cockpit Voice Data Recorder Each major assembly procedure is accompanied with a line art exploded view of the...

Page 40: ...ty Assurance Engineer ap proval signature is kept on file with the CMM sign off release form For a copy of the Component Maintenance Manual Verification Report for this version of the CMM please addre...

Page 41: ...special characters to be the same for example there is no difference between part number 266 E0305 00 266E0305 00 or 266E030500 To be in compliance with ARINC Specifications 100 and 200 the part numbe...

Page 42: ...23 70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK Rev 06 Page 8 Mar 16 16 The document ref...

Page 43: ...112 The Model FA5000 recorder is designed as a maintenance free recorder There is no periodic or scheduled maintenance required for this recorder It is considered an on condition LRU The FA5000 Record...

Page 44: ...document 2 FA5000 CONFIGURATIONS The current configurations of the FA5000s are listed with its specific part number in the IPL Section Figure 2 The specific configuration FA5000 part number is constr...

Page 45: ...provides the flexibility to be factory configured into a crash survivable combina tion cockpit voice recorder flight data recorder CVDR This unit converts analog cockpit audio signals to digital form...

Page 46: ...trictions on the cover page of this document ARINC 429 UTC Rotor Speed Discretes Bulk Erase Push to Test Record On Stop Record CVR Ident FDR Inhibit FDR Rate DataLink Valid System Outputs Audio Monito...

Page 47: ...EL 3 INPUT CHANNEL 2 INPUT CHANNEL 1 INPUT AREA MICROPHONE CAM INPUT ATTENUATION FDR MAINTENANCE FAULT FDR STATUS CVR MAINTENANCE FAULT AUDIO OUTPUT MONITOR PUSH TO TEST ERASE CVR INPUT 28 VDC PRIMARY...

Page 48: ...ormation The user can interface to the Model FA5000 in several different ways All of the interfaces use an Ethernet network as the means for transferring data The most common interface will be to a we...

Page 49: ...rophone Pre Amplifier Input Attenuation Decode J1 Pin50 n24dB_CAM_INPUT J1 Pin49 n12dB_CAM_IN PUT J1 Pin48 n6dB_CAM_IN PUT ATTENUATION 1dB GdB GND GND GND 42 GND GND OPEN 36 GND OPEN GND 30 GND OPEN O...

Page 50: ...I PWA Floating input configuration is accommodated by soft ware programmed tri state capability within the Audio CODEC D2 Analog_Audio_Return4 Unused Differential analog input line low Referenced to t...

Page 51: ...INC 429 differential input B side Reserved possible assignment as GMT input Referenced to the Signal Ground D10 ARINC429_RCV_A4 I Standard ARINC 429 differential input A side Referenced to the Signal...

Page 52: ...FDR INPUT DATA RATE PROGRAM PIN A shunt discrete input to the 12 bit ADC converter The discrete state is determined as high or low by comparison to internally programmed thresholds Referenced to the S...

Page 53: ...as high or low by comparison to internally pro grammed thresholds Referenced to the Signal Ground E5 Discrete_Input10 I Not Used Conditioned shunt discrete input to the 12 bit ADC converter The discr...

Page 54: ...nput Referenced to the Signal Ground B3 FDR_DATA_IN_LO I Standard ARINC 573 717 747 FDR Data low input Referenced to the Signal Ground A4 FDR_DATA_OUT_HI O Standard ARINC 573 717 747 FDR Data high out...

Page 55: ...FDRMaintenanceRe lay_Feedback I Open Ground input pulled high to 3 3 volts by default to be used as an optional feedback to alert the processor of the relay s contact closure Referenced to the Signal...

Page 56: ...input to indicate overvoltage on either 28VDC Input Primary or 28VDC Input Secondary aircraft power Overvoltage threshold is set to 34 08VDC and excludes the 0 75VDC forward voltage drop of the input...

Page 57: ...ONN PIN SIGNAL NAME AI PWA I O 1 2 HoldUPCap_Voltage Out 40 volts DC output to recorder hold up capacitor Connector Amphenol 62650 1 Mate Table 4 Hold Up Capacitor Voltage Return to CPU PWA J7 CONN PI...

Page 58: ...Order for Cockpit Voice Recorder Equipment 1 TSO C155a Federal Aviation Agency Technical Standard Order TSO C155a Techni cal Standard Order for Recorder Independent Power Supply 1 TSO C177 Federal Avi...

Page 59: ...d Clearances 6 INSTALLATION The information provided in this section is for general knowledge use only For authorized detailed installation instructions refer to the Model FA5000CVDR Installation and...

Page 60: ...SE CVR INPUT A IN Bulk erase signal from the flight deck push to erase switch Bulk Erase initiates when VOICE_ERASE_A is connected to VOICE_ERASE_C for 2 seconds and interlock circuits are closed ARIN...

Page 61: ...maximum Im pedance 5K ohm minimum 17 CVR MAINTENANCE FAULT OUT BITE status output of the voice recording section Shunt discrete output at standard ground indicates correct CVR operational status Func...

Page 62: ...described in ARINC 604 and 624 Also used for data link recorder handshaking using the ARINC 429 Williamsburg V1 file data transfer protocol Supports either low speed or high speed bit rates 29 FDR IN...

Page 63: ...R OUT 18 2 VDC output for Area Microphone bias Maximum operating current is 25 milliamps Short circuit limited at approximately 30 milliamps 38 AREA MICROPHONE SIGNAL LOW IN Area Microphone signal ret...

Page 64: ...l microphone preamplifier gain selec tion Jumper Common Pin 54 to pins 48 49 50 individually or combined to hardware decode one of eight possible attenuations See Table A2 be low 50 24dB CAM INPUT ATT...

Page 65: ...N COMMON GND IN Signal ground reference output for the grounding of pins 48 49 50 individually or combined to set the microphone gain selection in voice recorders having an internal microphone preampl...

Page 66: ...tion and Operation 23 70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document referenc...

Page 67: ...INTED CIRCUIT BOARD SHOULD COMPLY WITH PROPER ESD HANDLING PROCEDURES FAILURE TO DO SO MAY RESULT IN DAM AGE TO THE ESD SENSITIVE DEVICES RENDERING THE PRINTED CIRCUIT BOARD USELESS PRIOR TO HANDLING...

Page 68: ...A5000CVDR and is activated using front panel controls on its associated control unit Bulk erasure of the Model FA5000CVDR storage medium is accomplished using the associated control unit red ERASE pus...

Page 69: ...the ROC 7 port 4 Connect the USB Interface cable 17TES0415 between the RIU rear panel connector J4 and a USB connector on the ROC 7 NOTE Note Make the following audio connections from the RIU to Soun...

Page 70: ...TES0420 CATS Software FA2100 V 2 1 17TES0070 CICC 2 Assembly 17TES0072 Cable Assembly FA2100 CICC 2 2 ea 17TES0042 Cable Assembly Recorder Interface 17TES0057 Cable Assembly CVDR Interface 17TES0071 C...

Page 71: ...RIU AUDIO OUTPUT SPKRS J9 RCDR AC PWR TEST RECORDER INTERFACE UNIT RIU 17TES0710 SND OUT GREEN 17TES0413 J4 J2 J1 L SPKR R SPKR YELLOW AC RED DC AC 1A DC 5A USB BLUE GREEN SND IN SND OUT SPKRS OUT GS...

Page 72: ...ROC to start the software The applic ation will launch with the Channels control screen displayed as illustrated in Figure 102 Figure 102 CATS Channels Control Screen 2 In the Channels control screen...

Page 73: ...to the restrictions on the cover page of this document Figure 103 Volume Control 4 Under Applications click Sound Systems then click the Recording tab This will display the Sound control window illus...

Page 74: ...the cover page of this document 5 Highlight and select Line in 6 Click on Properties 7 Select the Levels tab Figure 105 Line In Properties Line In Level 8 Make sure that the Line In level is set at 10...

Page 75: ...sclosure of information on this sheet is subject to the restrictions on the cover page of this document Figure 106 Sound Playback Devices 10 Highlight Speakers 11 Click on Properties 12 Select the Lev...

Page 76: ...Levels 13 Make sure Playback Control is set at 100 move the Playback Control slider to its maximum setting 14 Make sure that the four remainingVolume slider levels do not need modification since these...

Page 77: ...nformation on this sheet is subject to the restrictions on the cover page of this document Figure 108 Volume Mixer Speaker Levels 17 In the Volume Mixer make sure both sliders are all the way up 18 Cl...

Page 78: ...CATS Autotest using DC power only follow the procedures below a Ensure that the recorder has no power applied power is removed if not already done Connect a CVR to the RIU using the cable p n 17TES04...

Page 79: ...necting to the recorder status window appears Observe Figure 109 CATS Connecting Pop Up g On the tool bar select Power ON Figure 110 CATS Power Toggle NOTE When DC power is applied verify the appropr...

Page 80: ...Start Test Toggle k In the Test Mode and Options dialog box select either Return to Ser vice or Selectable Test Options then click on OK Figure 112 CATS Test Mode and Options Screen NOTE If a full ret...

Page 81: ...from the CATS Test Mode and Options Screen Figure 113 CATS CVDR Test Confirmation NOTE Follow the instructions displayed in the confirmation window l Read and click on Yes Figure 114 CATS CVDR Warning...

Page 82: ...Input n Read the current DC amps value from the built in multimeter on the power supply or from the inline RMS multimeter And enter in the value in amps in window and click on OK Figure 116 CATS CVDR...

Page 83: ...page of this document Figure 117 CATS CVDR Fault History Log p Click on Yes on the dialog box to clear the fault logs Figure 118 CATS CVDR Clear Fault Log Confirmation q Observe the Fault History Log...

Page 84: ...Confirmation s At the end of the test save the report by selecting File Test Report Save Report NOTE The test report is named with the part number of the Unit Under Test and the serial number provide...

Page 85: ...page of this document Figure 121 CATS Test Results Screen u If the autotest is successful power off the recorder from the CATS menu bar v Turn 28VDC power off and remove the crossover and RIU cables f...

Page 86: ...enter the DC power consumption in amps or watts Please enter the DC power consumption in amps or watts Please connect the recorder front panel cable and press the OK button Example report message s 0...

Page 87: ...Expected 400 Hz Results 3334 6 Hz 4 Test Tone Enable push to test and verify push to test indicator is set Example report message s 08 03 06 PASSED Test Tone Expected Push To Test indicator Results P...

Page 88: ...QV2 5 4 SQV3 5 4 SQC 56 6 dBV 08 05 40 PASSED Channel Bal 1000 Hz 0 1 ref All within 3 dB except HQC Results HQ1 8 3 HQ2 8 2 HQ3 8 4 HQC 9 4 SQV1 8 0 SQV2 8 1 SQV3 8 1 SQC 293 8 dBV 8 Frequency Respon...

Page 89: ...1600 2000 2500 and 3500 Hz Frequencies for HQCAM and SQCAM only is 3150 Hz Frequencies for HQCAM only are 4148 and 6000 Hz Example Return to Service report message s 11 24 20 PASSED SN D 150 Hz 1 0 r...

Page 90: ...2 127 4 HQ3 11 1 HQC 104 4 SQV 11 4 SQC 72 0 dBV 08 42 19 PASSED Crosstalk Audio 1000 Hz 1 0 ref Expected Driven Non Driven 40 dB Results HQ1 304 9 HQ2 304 9 HQ3 111 7 HQC 11 1 SQV 72 4 SQC 11 4 dBV 1...

Page 91: ...HQ3 Playback Expected 9 patterns Results 9 good patterns 14 50 53 PASSED FSK Time HQ3 GMT Switch Expected 9 patterns Results 9 good patterns 13 Audio Out Monitor Record simulated 1000 Hz data for eac...

Page 92: ...D Shutdown CVDR Fault Expected CVDR fault to occur Res ult CVDR Fault 08 56 27 PASSED Shutdown Push to Test Expected 1000 Hz frequency Results 999 9 Hz 16 Capacitor Power off recorder and verify recor...

Page 93: ...ver 9 minutes after power is removed Example report message s 09 00 02 RIPS Initialization Power has been removed Please wait 9 minutes 09 09 15 PASSED RIPS Expected no CVR Fault for over 9 minutes Re...

Page 94: ...ult file name with the part number of the recorder and serial number that was entered in the information fields of the test section 2 Click on the Save button 3 Select either Full Audio Data Download...

Page 95: ...below the level required for operation and the 9 Volt battery should be replaced 3 To test the Beacon battery voltage attach the test probe clip to the Beacon case The clip has a spring action that wi...

Page 96: ...ault Isolation 23 70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is...

Page 97: ...ding the operation and application of indicated changes will be provided in the ROSE Software Operators manu al for Version 4 7 p n 165 E1696 03 A Recommended Test Equipment Maintenance procedures for...

Page 98: ...rting in paragraph 2 B 1 FA5000CVDR Operating Mode States The following operating states and time limits exist within the FA5000CVDR a Initialization State When power is applied to the FA5000CVDR with...

Page 99: ...lated data first prior to entering the record mode c Data Retrieval State When the CICC cable assembly attached to the front panel GSE connec tor and a data copy request from the GSE is received the r...

Page 100: ...data set in the initial Header Word of the 32K Word Erase Block This may not initial ly match the type set by the ROSE until the dump extends into the next 32K Word Erase Block 2 FA5000CVDR BENCH TES...

Page 101: ...7TES0076 READ OUT CENTER 7 P N 17TES0700 ROSE RI SOFTWARE 17TES0321 CDROM Power Input Select FA5001 ADAPTER CABLE ASSY 17TES0711 ETHERNET CROSS OVER CABLE ASSY P N 0249800386 Figure 201 ROSE RI Setup...

Page 102: ...re run the test Test the recorder again after each corrective action taken If the recorder fault is still present display and print the Fault History Log as described steps 1 14 in the initialization...

Page 103: ...ing functions on ROSE The default password is Rose if it has been reset see your administrator Click the OK button Figure 202 RI Recorder Status Window Indications 6 Ensure that the RI Icon is display...

Page 104: ...atched fault condition does not clear then terminate this test disconnect the test equipment and return to the recorder L 3 Communications Aviation Recorders Repair Depot for further testing and repai...

Page 105: ...e Simulated Data block select the radial button for Fixed Data pattern and click the Start Data button 2 At the Recording block click the Start Recording button 3 Observe a Record Data pop up warning...

Page 106: ...ator Stopped FDR Fault Fault J1A 18 Open NOTE FDR Non Latched Fault entry is normal because the data has stopped and the recorder is still in the RE CORD mode of operation 10 Restart data by clicking...

Page 107: ...Type to 717 and Words per Frame to 128 wps Click the OK but ton 2 Observe a Rose pop up status window states Set Data Type Rate command was successful Click the OK button 3 At the Recorder Test block...

Page 108: ...e test pass Single Pass Test for XX hours and XX minutes monitor data will be quickly verified then data will be recorded for the specified number of hours and minutes and then dumped and verified Ful...

Page 109: ...test results to the return to service paperwork as needed 13 If the recorder passes the Autotest this qualifies the FA5000CVDR recorder FDR function for a Return To Service condition NOTE In order fo...

Page 110: ...the small box matches the Memory Marker number set previously in step 6 13 Click the Close button to exit the Flight Data File Control menu and return to the ROSE Main menu screen Press Test Flight Re...

Page 111: ...fallen below the level required for operation and the 9 Volt battery should be replaced 3 To test the Beacon battery voltage attach the test probe clip to the Beacon case The clip has a spring action...

Page 112: ...shorted No audio voice is present Unable to monitor au dio 05 Discrete Erase CVR Input A The signal path is open Loss of ability to erase recorded audio The recorder does not erase recorded audio 05...

Page 113: ...ect No Effect 14 N A Spare The signal path is shorted No Effect No Effect 15 Differential Audio Channel 2 Low Input The signal path is open Degraded Audio Chan nel 2 Low Signal Fails to record no au d...

Page 114: ...A Spare The signal path is shorted No Effect No Effect 23 Differential Audio Channel 3 Low Input The signal path is open Degraded Audio Chan nel 3 Low Signal Fails to record no au dio is recorded 23...

Page 115: ...ocessor may generate an FDR fault depending upon the rate 30 Discrete FDR Input Data Rate Program B The signal path is shorted Only 128 and 512 Wps rates are available The Main Processor may generate...

Page 116: ...ophone Loss of Area Micro phone functionality 37 Power Area Microphone 18V Power The signal path is shorted Loss of bias to Area Mi crophone Loss of Area Micro phone functionality 38 Differential Audi...

Page 117: ...l path is open Loss of Area Micro phone Power Return Fails to record no au dio is recorded 45 Power Rtn Res Area Microphone Power Return The signal path is shorted Area Microphone Power Return is de g...

Page 118: ...to record Rotor Speed 52 Differential Analog Rotor Speed High The signal path is open Rotor Speed High sig nal data is disrupted Unable to record Rotor Speed 52 Differential Analog Rotor Speed High Th...

Page 119: ...MP PWA fails to operate The CVDR fails to operate Watch Dog Timer ARINC 429 RX TX Dis crete I Ps and O Ps FDR Data Frequency Counter CSMU Inter face Power Supply Status Single Event Upset SEU The DSP...

Page 120: ...om municate with the CSMU The MP PWA fails to operate The CVDR fails to operate Watch Dog Timer ARINC 429 RX TX Dis crete I Ps and O Ps FDR Data Frequency Counter CSMU Inter face Power Supply Status A...

Page 121: ...data A005 Flash Memor y Non Volatile Memory Loss of Power The Flash Memory fails Unable to store data and the SDRAM is unable to copy data The MP PWA fails to operate The CVDR PWA fails to oper ate No...

Page 122: ...ctrical In terference Software glitch flips data bits causing data corruption such as lost missing or scrambled data The MP PWA does not oper ate properly and may have corrupted data The CVDR does not...

Page 123: ...I P Audio I P Ch 3 is shorted No Audio to Ch 3 Ch 3 is unable to record audio Ch 3 is unable to record audio B012 Ana log Audio Input 4 Audio I P Audio I P Ch 4 is open No Audio to Ch 4 Ch 4 is unable...

Page 124: ...Chan nel 4 Audio Mi crophone HI in put Loss of Channel 4 Audio Mi crophone HI Audio I P HI Analog Area MIC I P HI is shorted Inputs Channel 4 and the Area Microphone Channel HI do not get pro cessed...

Page 125: ...formed No Effect Audio I P Audio I P Tone Test 2 is shorted Audio CODEC receives re cords either no audio tone test or a continu ous tone test from the DSP No audio tone test or a con tinuous tone tes...

Page 126: ...put is not scaled up by the output stage and does not pass through the output trans former The Analog Audio Monitor Output Chan nel HI does not function Loss of the Analog Audio Mon itor Output Chann...

Page 127: ...tion between the UART1 and the front panel RJ 45 GSE port The MP PWA has no GSE capability Communication is disrupted with the GSE UART1 RxD The UART1 RxD GSE is shorted There is no communication betw...

Page 128: ...odes The CVDR is unable to per form normally but still oper ates The CVDR is unable to per form normally but still operates Ethernet The Ethernet Interface is shorted The ethernet MAC port fails to op...

Page 129: ...PWA K032 FDR Data Out LO Differential ARINC757 Data 0 P LO is open Disrupted FDR Data Output ARINC 717 Low echoed back to the AI PWA Disrupted FDR Data Output ARINC 717 Low echoed back to the AI PWA...

Page 130: ...e FPGA initially does not operate It is in an undeter mined condition The MP PWA initially does not operate The CVDR initially does not operate Some data may be corrupt lost and or may not be recorded...

Page 131: ...emory Electrical In terference Software glitch flips data bits causing data corruption such as lost missing or scrambled data The CSMU does not oper ate properly Some data may be corrupt and may not b...

Page 132: ...olation 23 70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK Rev 06 Page 236 Mar 16 16 The do...

Page 133: ...DEVICES RENDERING THE PRINTED CIRCUIT BOARD USELESS PRIOR TO HANDLING A PRINTED CIRCUIT BOARD ENSURE PROPER PERSONNEL GROUND ING TECHNIQUES ARE USED ALSO ENSURE THAT ALL CIRCUIT BOARDS ARE PLACED INT...

Page 134: ...number followed by the IPL item number for a particular part e g 1 100 for IPL Figure 1 Item 100 For items listed in the parts list but not illustrated the item number is preceded by a In addition to...

Page 135: ...is equipped with a battery having a life expectancy same as the replacement date on the beacon A new replacement beacon may be ordered if needed directly from Aviation Recorders The beacon is recomme...

Page 136: ...P N 2290200424 are used to ensure a secure connection to the CSMU When replacing the 90 day ULB it is REQUIRED that four new mounting hex screws MS 16995 54 L 3AR P N 2290200424 are used to secure th...

Page 137: ...Model FA5000 s CSMU is mounted to the top of the recorder chassis by 6 Flat head screws It interfaces to the Main Processor MP PWA through the Memory In terface Cable assembly attached to the J 3 con...

Page 138: ...ble 1 120 connect or to the MP PWA 1 50 and remove CSMU cable connector and the seal pad 1 140 NOTE Ensure that the CSMU is support before proceeding 3 Remove the the six screws 1 125 and washers 1 13...

Page 139: ...on the cover page of this document VIEW A A A 1 120 1 100 1 140 1 115 1 110 1 135 1 125 1 130 1 50 QTY 6 QTY 6 QTY 2 QTY 2 1 125 REF 1 115 REF 1 110 REF 1 135 REF 1 120 REF Some parts are removed for...

Page 140: ...screws 1 20 used to secure the four corners of rear cover 1 10 to the rear part of the Shielded Housing 1 5 Remove the two screws 1 20 used to secure the middle of rear cover 1 10 to the rear part of...

Page 141: ...or 1 100 Qty 4 Figure 304 Rear Cover Removal Diagram D Aircraft Interface AI PWA Removal See Figure 305 or IPL Figure 1 Item 30 AIRCRAFT INTERFACE PWA REMOVAL PROCEDURE 1 Remove the rear cover as desc...

Page 142: ...1 10 as described in Paragraph C Rear Cover Re moval 2 Disconnect the hold up capacitor cables at J 6 and J 7 and on the MP PWA 1 50 3 Disconnect the RIPS cable 1 85 at P 5 on the MP PWA 1 50 4 Remove...

Page 143: ...secure the lower half Ethernet connector J 2 to the front part of the Shielded Housing 1 5 8 Remove the lower one screw 1 55 used to secure the front end of the MP PWA 1 45 to front part of the Shiel...

Page 144: ...page of this document DETAIL A 1 65 1 70 1 75 1 60 1 120 1 55 1 50 1 85 QTY 2 QTY 2 SEE DETAIL A P 5 Connector 1 110 1 115 QTY 2 1 135 1 100 J 2 Connector Some parts are removed for clarity purposes N...

Page 145: ...escribed in Paragraph E Main Processor PWA Removal 2 Remove the eight screws 1 180 and three stand off 1 185 used to secure the Video Card PWA 1 175 to the MP PWA 1 50 3 Remove the Video Card PWA 1 17...

Page 146: ...3 70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK Rev 06 Page 314 Mar 16 16 The document re...

Page 147: ...cification MIL PRF 680 Soft Bristle Brush Cotton Swabs Lint Free Cotton Cloth NOTE Equivalent substitutes may be used for all cleaning materials All ma terials and chemicals may be obtained from any c...

Page 148: ...of clean ing the center contact of the beacon water switch at least once every 24 months more frequently under high humidity conditions Make sure the beacon case and water switch are free of dirt and...

Page 149: ...ument Left Beacon Mount Bracket 1 145 Right Beacon Mount Bracket 1 145 Underwater Locator Beacon 1 155A or 155B 1 4 Hex Screw 1 150 Crash Survivable Memory Unit CSMU 1 120 Water Switch 1 4 2 3 Cross P...

Page 150: ...1 Cleaning 23 70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is onl...

Page 151: ...e general physical integrity of the recorder i e J2 Ethernet GSE connector Underwater Locator Beacon and J1 rear panel connector pins 2 Check that dust cover is serviceable exhibiting no undue deterio...

Page 152: ...mponent Maintenance Manual D Underwater Locator Beacon ULB The ULB beacon used in the Model FA5000 is equipped with a battery which sup plies the power when activated The beacon is recommended to be t...

Page 153: ...omponent level in accordance with L 3AR Factory test calibration and repair specifications As a result the Model FA5000 s maintenance philosophy is replacement of failed assem blies In the case of the...

Page 154: ...11 Repair 23 70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is onli...

Page 155: ...t required for testing and assembly of the recorder can be found in Table 901 of the Special Tools Fixtures and Equipment Section 900 of this CMM Table 701 provides a list of the common assembly mater...

Page 156: ...he accepted Level 2 repair philosophy for the FA5000 CVDR a known defective circuit board assembly shall be returned to the factory for repair or replacement NOTE Numbers shown in parentheses in the f...

Page 157: ...WA Installation See Figure 702 or IPL Figure 1 Item 50 MAIN PROCESSOR INSTALLATION PROCEDURE 1 Slide straight in and forward on the MP PWA 1 50 using the guides in the Shielded Housing 1 5 to ensure n...

Page 158: ...lbs 5 Install the two screws 1 135 used to secure the Seal Pad 1 140 and the CSMU cable 1 120 connector to the MP PWA 1 50 Tighten screws to a torque value of 5 6 in lbs 6 Install CSMU cable cover pla...

Page 159: ...J2 Connector Some parts are removed for clarity purposes NOTE 1 5 REF QTY 2 J 7 J 6 RED BLACK 1 140 Torque 5 6 in lbs Torque 5 6 in lbs Torque 2 3 in lbs Torque2 3 in lbs Figure 702 Main Processor MP...

Page 160: ...n screws to a torque value of 9 10 in lbs 3 install the four screws 1 40 used to secure the Rear Connector J1 to the back of the rear cover 1 10 Tighten screws to a torque value of 5 6 in lbs 4 Instal...

Page 161: ...aptive screws 1 20 on the inside corners of the rear cover 1 10 3 Align the guide on the AI PWA 1 30 attached to the Rear Cover 1 10 with the receptacle on the MP PWA 1 50 4 Slide rear cover 1 10 stra...

Page 162: ...9 10in lbs Qty 4 1 100 Figure 704 Rear Cover Installation Diagram F Crash Survivable Memory Unit CSMU Installation See Figure 705 or IPL Figure 1 Item 120 CSMU INSTALLATION PROCEDURE CAUTION The foll...

Page 163: ...and align with mounting screw holes 4 Install the six screws 1 125 used to secure the CSMU 1 120 to the mount ing chassis 1 100 Tighten screws to a torque value of 31 in lbs 5 Install Seal Pad 1 140 a...

Page 164: ...he cover page of this document VIEW A A A 1 120 1 100 1 140 1 115 1 110 1 135 1 125 1 130 1 50 QTY 6 QTY 6 QTY 2 QTY 2 1 125 REF 1 115 REF 1 110 REF 1 135 REF 1 120 REF Some parts are removed for clar...

Page 165: ...OTE When replacing the 30 day ULB it is recommended that new mounting hex screws 1 150 MS 16995 54 L 3AR P N 2290200424 are used to ensure a secure connection to the CSMU When replacing the 90 day ULB...

Page 166: ...5 in lbs 4 Perform the ULB operation test using P N 17TES0015 as described in Section 100 of this CMM Left Beacon Mount Bracket 1 145 Right Beacon Mount Bracket 1 145 Underwater Locator Beacon 1 155A...

Page 167: ...nector 4 Line up the Rips in the most rearward position while aligning the RIPS in the guide slots of the CVDR 5 Slide the rips forward within the guides until the connectors engage and the RIPS face...

Page 168: ...st is recommended after storage of more than one year Refer to Testing Troubleshooting Section 100 for specific test and check out procedures A Storage in Original Containers When possible the FA5000...

Page 169: ...icient thick ness to thoroughly cover all sharp corners and protrusions 2 Enclose the unit in a polyethylene bag 3 mils thick min seal the bag 3 Place the recorder unit in a suitably sized heavy const...

Page 170: ...70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK Rev 06 Page 716 Mar 16 16 The document ref...

Page 171: ...hile conforming to the input interface required in ARINC 757 757A 3 Physical Characteristics The Model FA5000 fit within the envelope of a trayless short case Refer to Figure 801 for outline and dimen...

Page 172: ...rophone 150 6000 Hz band width Audio Input Level 50 mVrms to 3 Vrms Audio Quality Meets ED112 specifications Signal to noise plus distortion ratio SINAD of the signal when repro duced 24 dB 6 distorti...

Page 173: ...nts The following assembly items have the specified torque requirements CSMU screws 31 in lbs Beacon Bracket mounting screws 75 in lbs Rear Cover screws Aircraft Interface PWA 9 10 in lbs J1 Connector...

Page 174: ...ction 4 5 3 45_C 45_C 85_C 85_C Altitude Decompression Overpressure 4 6 1 4 6 2 4 6 3 SPX902A0002E01 25 000 feet 8 000 to 25 000 feet 170kPa Section 4 1 Temperature Variation 5 0 DO 160F Equipment tes...

Page 175: ...and Dust 12 0 DO 160F Equipment tested to Category D By Similarity to ENV227 Fungus Resistance 13 0 DO 160F Equipment tested to Category F By Similarity to ENV227 Salt Fog 14 0 DO 160F Equipment teste...

Page 176: ...Hz was 55V m Radio Frequency Emissions Interference Voltages Conducted Radiated 21 0 DO 160F 21 4 21 5 Equipment was tested to Category M exten ded Equipment was tested to Category M exten ded Lightni...

Page 177: ...ions on the cover page of this document 96 5 21 3 6 1 137 2 303 3 2x 2x 3 6 2 3 80 84 24 5 40 6X 0 22 96 5 2x 3 80 251 3 9 89 91 4 5 0 11 94 Figure 801 Sheet 1 of 2 Outline Dimension Drawing Model FA5...

Page 178: ...strictions on the cover page of this document 71 1 5 0 2 3 2 149 4 5 88 123 8 10 4 88 04 167 1 6 58 38999 I O CONNECTOR 2 8 2 58 4 5 0 Figure 801 Sheet 2 of 2 Outline Dimension Drawing Model FA5000 Co...

Page 179: ...IXTURES AND EQUIPMENT 1 GENERAL This section provides a listing of all required tools fixtures and equipment which are not common maintenance tools Refer to Table 901 for a table listing required FA50...

Page 180: ...ssembly 17TES0072 Cable Assembly FA2100 CICC 2 2 ea 17TES0042 Cable Assembly Recorder Interface 17TES0057 Cable Assembly CVDR Interface 17TES0071 Cable Assembly F1000 CICC 2 17TES0321 Read Out System...

Page 181: ...ument FA5001 CDVR Software Library Disk Part Number Description 840E5490 06 FA5001CVR p n 5001 6103 11 and 5003 6103 11 Program Software 840E5497 03 FA5001CVR p n 5001 6133 11 Program Software Audio D...

Page 182: ...T 17TES0411 AC J7 J6 RIU AUDIO OUTPUT SPKRS J9 RCDR AC PWR TEST RECORDER INTERFACE UNIT RIU 17TES0710 SND OUT GREEN 17TES0413 J4 J2 J1 L SPKR R SPKR YELLOW AC RED DC AC 1A DC 5A USB BLUE GREEN SND IN...

Page 183: ...required hardware running under the Windows 98t or Windows XPt operating software with Microsoft Direct X ver sion 8 0 or higher The minimum recommended hardware specifications for a PC running ADLP...

Page 184: ...he Portable Interface 2 PI 2 Unit p n 17TES0062 with Mod Dot 1 This device is used to download the FA5001CVR voice and data link information to a SD CF memory card or USB Flash Drive which then can be...

Page 185: ...ols and Test Equipment 23 70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document refe...

Page 186: ...requisitioning storing issuing and identifying parts to maintain the FA5001 Cockpit Voice Recorder Flight Data Recorder This Illustrated Parts List is not to be taken as the author ity for the proced...

Page 187: ...l lustration in which the item is shown and the item number listed on the illustration Figure numbers are shown for the first entry of each figure and at the top of each subsequent column When there i...

Page 188: ...tes the end of attaching parts The EFFECTIVITY CODE column establishes parts relationship with units or assemblies which are essentially the same but have variations These units or assemblies are the...

Page 189: ...e Memory Units CSMU for all Models of recorders using the L 3AR 90 Day Underwater Locator Beacon PN 266E5542 00 brackets and mounting screws that make up the ULB Conversion Kit p n 068E5542 00 These t...

Page 190: ...6133 11 CVDR TRAYLESS INTERNAL RIPS Data link OMS Video 5003 6103 11 CVDR TRAYLESS INTERNAL RIPS Data link OMS 2GB Memory NUMERICAL INDEX PART NUMBER AIRLINE PART NO FIG ITEM TTL REQ BB1P041H05 1 55...

Page 191: ...TL REQ ITEM FIG AIRLINE PART NO 205E5163 00 1 160 1 229E5452 00 1 30 1 229E5459 00 1 175 1 2299800577 1 65 1 230E5488 00 1 45 1 230E5490 00 1 95 1 253E5279 00 1 120a 1 253E5279 03 1 120b 1 266E0305 00...

Page 192: ...trictions on the cover page of this document 100 50 120 10 125 130 110 115 135 QTY 6 QTY 2 QTY 2 5 85 95 90 55 QTY 2 QTY 2 60 65 70 80 75 QTY 2 A A B B QTY 2 15 140 QTY 6 160 165 170 QTY 2 175 160 180...

Page 193: ...eet is subject to the restrictions on the cover page of this document 155A QTY 6 20 145 10 QTY 6 QTY 4 25 40 45 150 QTY 2 QTY 4 REF QTY 4 30 35 View A QTY 2 View B 155B Figure 1000 Sheet 2 of 2 Model...

Page 194: ...Y B RF 1C 5001 6103 10 Deleted C RF 1D 5003 6103 11 COCKPIT VOICE DATA RECORDER FA5001 CVDR DATALINK 28 VDC ONLY 2 GB MEMORY D RF 1E 5011 6103 11 COCKPIT VOICE DATA RECORDER FA5001 CVDR DATALINK 28 VD...

Page 195: ...01 1 ATTACHING PARTS 55 BB1P041H05 SCR PNH 4 40X5 16 SEALING V06141 2299800500 2 60 075E5352 00 COVER RJ45 EMI 1 65 2299800577 SCREW 4 40X5 8 TRUSS HD 1 70 1110 4 AL 9 SPACER 3 16OD 115ID 5 16 V55582...

Page 196: ...A B 1 120b 253E5279 01 CRASH SURVIVABLE MEMORY D 1 ATTACHING PARTS 125 MS24693 C48 SCR PNH 8 32X3 8 V06141 2290200366 6 130 MS35333 73 WASHER 10 INT TOOTH V06141 2730200028 6 135 MS51957 12 SCR PNH 4...

Page 197: ...ONLY UN3091 WITH BEACON FOR BATTERY REPLACEMENT ORDER 90 DAY BATTERY KIT 147E5542 00 1 160 205E5163 00 PWA HOLD UP CAP FA5000 1 165 MS51957 12 SCR PNH 4 40 X3 16 V06141 2290200072 2 170 MS51957 28 SC...

Page 198: ...Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document 1 Figure 1001 Model 500 Recorder Independent Power Supply RIPS Rev 01 Page 1013 Oct 06...

Page 199: ...List 23 70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK Rev 06 Page 1014 Mar 16 16 The docu...

Page 200: ...is sheet is subject to the restrictions on the cover page of this document FIG ITEM PART NUMBER AIRLINE PART NO NOMENCLATURE 1234567 EFF CODE UNITS PER ASSY 1 1 500 4030 000 Recorder Independent Power...

Page 201: ...List 23 70 40 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK Rev 06 Page 1016 Mar 16 16 The docu...

Page 202: ...The document reference is online please check the correspondence between the online documentation and the printed version...

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