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COMPONENT MAINTENANCE MANUAL

AVIATION RECORDERS

FA2100CVR

Rev. 15 Page 23

Apr. 14/16

Description and Operation

23–70–04

Use or disclosure of information on this sheet is subject

to the restrictions on the cover page of this document.

In summary each processor, RAM and programmable memory device in the FA2100
is monitored by BIT. They are checked at power

−

up and continuously monitored

during operation of the recorder. Failures are reported using the FAULT output sig-
nals.

4.

FA2100 CVR SPECIFICATIONS

Specifications for the Model FA2100CVR have been developed in close coordination with
Aerospace Industry regulatory agencies. As such, the FA2100CVR meets or exceeds the
requirements of technical standard order TSO–C123a, TSO–C123b, EUROCAE ED–55,
EUROCAE ED–56A, and EUROCAE ED

−

112.

A.

Applicable Documents

The following documents form a part of, or are referenced, within this CMM:

(1)

TSO–C123a

Federal Aviation Agency
Technical Standard Order TSO–C123a Techni-
cal Standard Order for Cockpit Voice
Recorder Systems.

(1)

TSO–C123b

Federal Aviation Agency
Technical Standard Order TSO–C123b Techni-
cal Standard Order for Cockpit Voice
Recorder Equipment.

(2)

EUROCAE MOPS ED–55

European Organization for Civil Aviation
Electronics Minimum Operational Performance
Specification for Flight Data Recorder Systems

(3)

EUROCAE MOPS ED–56A

European Organization for Civil Aviation
Electronics Minimum Operational Performance
Specification for CVR Systems, December
1993

(4)

EUROCAE MOPS ED–112

European Organization for Civil Aviation
Electronics Minimum Operational Performance
Specification for Crash Protected Airborne Re-
corder Systems, March 2003

(5)

ARINC 404A

Air Transport Equipment Cases and Racking
Characteristic

(6)

ARINC Report 604–1

Guidance for Design and Use of
Built-In-Test-Equipment

(7)

ARINC Report 624

Design Guidance for On-board Maintenance
System

(8)

ARINC Characteristic 557

Cockpit Voice Recorder

(9)

ARINC Characteristic 757

Cockpit Voice Recorder

(10) ARINC Characteristic 757A

Cockpit Voice Recorder

(11) ARINC Characteristic 777

−

1

Recorder Independent Power Supply (RIPS)

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

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Summary of Contents for FA2100 CVR

Page 1: ...91 93 Contact L 3AR Product Support WARNING THIS TECHNICAL DATA IS CONTROLLED UNDER THE EXPORT ADMINISTRATION REGULATIONS EAR ECCN 7E994 AND MAY NOT BE EXPORTED TO A FOREIGN PERSON EITHER IN THE U S...

Page 2: ...rt of this manual may be repro duced or utilized in any form or by any means electronic or mechanical including photocopying recording or by in formation storage and retrieval system without permissio...

Page 3: ...sons working with static sensitive devices When handling or servicing equipment containing static sensitive devices adequate precautions must be taken to prevent device damage or destruction Only thos...

Page 4: ...tle 23 70 04 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 ple...

Page 5: ...version numbers updated Software checksums updated Model configuration tables added for clarity Au tomatic Test Section revised Revision 12 Jul 03 13 Corrected page number errors and updated the LOEP...

Page 6: ...rvice bulletins Updated the IPL to reflect p n 21001026 02 Revision 06 May 01 07 Added new Section 200 Automatic Testing for operational testing of CVR to include the ROC6 w CATS software Revised Disa...

Page 7: ...Underwater Locator Device Added new CVR label and change of location Added 2100 1020 90 version Revision 04 Jan 01 03 Revised Disassembly Assembly sections to in clude the moisture resistant seals in...

Page 8: ...losure of information on this sheet is subject to the restrictions on the cover page of this document Rev 15 Page viii Apr 14 16 THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online...

Page 9: ...ted unit weights Added obsolete notes Removed A860 Testing Fault Isolation All Page headers updated Removed A860 Updated Software tables Automatic Testing All Page headers updated Removed section Disa...

Page 10: ...footer Added 2100 1220 00 2100 1220 02 2100 1225 22 2100 1226 02 2100 1225 24 2100 1227 02 and 2100 1925 22 Added 90 Day ULB Description Operation All Updated to include legal reference in footer Adde...

Page 11: ...p ment All Updated to include legal reference in footer Illustrated Parts List and Schem atic Diagrams All Updated to include legal reference in footer Removed 2100 1020 91 2100 1020 93 and 2100 1020...

Page 12: ...ted ROSE version updat ed Model configuration tables added Testing Fault Isolation 105 142 145 147 150 ROSE version updated ADLP added Software and directory labels updated Updated setup diagram Softw...

Page 13: ...r revised are outlined below together with the highlights of Revision 12 dated July 3 2013 Section Page Description Front Matter LOEP TOC Changed the List of Effective Pages to reflect Revision 12 cha...

Page 14: ...30 34 35 36 43 48 56 64 67 Added part number 2100 1027 02 ARINC 757A compliant Added NAND memory to part number matrix Adds description of PI 2 Added description of acquisition processor 205E2502 34 R...

Page 15: ...highlights of Revision 10 dated Jun 15 2012 Section Page Description List of FSB s n a Front Matter xix xxxiv Changed the List of Effective Pages to reflect the Revision 10 changes Changed the Table...

Page 16: ...eflect the Revision 09 changes Introduction 2 5 6 Added Rose 4 0 Updated L 3 Address Updated shop verication dates Description Operation 9 19 21 45 54 66 Added note on test tones for P N 2100 1025 6 0...

Page 17: ...p with support equipment Updated Table 106 with new software P N s for the CVR P N 2100 1025 22 and 2100 1026 02 Added note for the CICC 3 Automatic Testing 201 203 207 212 213 216 218 219 221 Added C...

Page 18: ...Testing Fault Isolation 105 107 114 126 131 137 148 150 Added Beacon Test note added Acquisition Processor configuration added reference to ROC 6 Updated Software Checksums Added p n 2100 1026 02 Rem...

Page 19: ...mpressor and Crash Survivable Memory Unit CSMU p ns Changed 2100 1025 02 to 2100 1025 or XX Added EURO CAE ED 112 Revised text for Per and Post MOD DOT 7 configu rations of P N 2100 1020 XX Revised be...

Page 20: ...pdated Table 1 FA2100 Recording Specifications to include the 2100 1025 02 Added OMS and Data link information Added Control Unit information on the S161 1390 00 Updated Figure 8 Interwiring Diagram t...

Page 21: ...ary Disk information Modified Figure 910 CVR Menu Structures to include p n 2100 1025 02 Added Audio Data Link Player Software information Illustrated Parts List Schematic Diagrams 1004 1015 Updated t...

Page 22: ...informa tion for Uploading Software changes for 2100 1010 and added 2100 1020 90 along with new checksums in Table 105 for SW Rev 02 Per SB005 Disassembly 302 309 Corrected nomenclature inconsistancie...

Page 23: ...orporated new label and updated label position Incorporated all GACVR s are DC only Incorporated Software changes for 2100 1010 and added 2100 1020 90 along with new checksums in Table 105 Disassembly...

Page 24: ...nd manufacturer information Disassembly Section 302 303 306 307 Updated information for ULDs Updated the beacon removal proce dure Added IPL Tag for 205E1849 04 Audio Compressor PWA Cleaning Section 4...

Page 25: ...Testing Fault Isolation Section 101 140 Added the GACVR Fault Circuitry for Pin 23 Modified testing proce dure for GACVRs p ns 2100 1010 51 and 2100 1020 51 Updated the Acquisition Processor test poin...

Page 26: ...losure of information on this sheet is subject to the restrictions on the cover page of this document Rev 15 Page xxvi Apr 14 16 THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online...

Page 27: ...SIONS REV NO INSERTION DATE BY REV NO INSERTION DATE BY REV NO INSERTION DATE BY 15 Apr 14 16 JG 14 Jul 13 15 JG 13 Dec 09 13 JG 12 Jul 03 13 JG 11 May 21 13 DN 10 Jun 15 12 JM 09 Apr 30 10 GM 08 Jul...

Page 28: ...04 Rev 15 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: ...010 P N 2100 1020 Introduce Moisture Resistant Seals self sealing Chassis Cover CSMU screws to pro tect against excessive moisture intrusion MOD DOT 4 FA2100 CVR FSB005 23 70 04 05 Apr 16 02 P N 2100...

Page 30: ...0 1025 Factory modification to track internal produc tion processes for new recorders MOD DOT 8 FA2100 CVR FSB013 23 70 04 13 Dec 14 07 P N 2100 1010 5 P N 2100 1020 5 Introducing a replacement Acquis...

Page 31: ...CVR FSB019 23 70 04 19 Feb 13 13 NAND Memory change NAND Memory change Introduction of New Crash Survivable Memory Unit CSMU MOD DOT 14 FA2100 CVR FSB020 23 70 04 020 Jan 10 13 Released Intro of SW Re...

Page 32: ...e Bulletin 23 70 04 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 33: ...artment of Commerce HTSUS Sch B 4901 10 0040 4901 10 0000 LIMITED RIGHTS LEGEND Notice to persons receiving this document and or data This document and or data con tains information in which L 3 Commu...

Page 34: ...Serial Number Effectivity Part Number Beginning Serial Number New Software Version Audio Compressor PWA P N 2100 3083 00 000840345 and greater 840E2261 07 205E3977 19 2100 3083 10 000849079 and greate...

Page 35: ...al Operators are not required to apply for modifica tion approval for this change as it does not affect the form fit or function of the top level LRU nor the FA2100CVDR TSO G Manpower 3 0 hours with t...

Page 36: ...nto the CVDR Customers must specify their request for the new part number on the Repair Exchange order For the 2100 3083 50 the current 205E3997 22 Audio Compression Circuit Board must be sent to the...

Page 37: ...Exchange 30 Days For 2100 3083 50 Audio Compres sion Circuit Board 1 ea 205E3977 25 1 746 New 90 Days For 2100 3083 50 Audio Compres sion Circuit Board 1 ea 205E3977 25 1 222 Exchange 30 Days B Toolin...

Page 38: ...nd Availability Keyword Quantity Part Number Price U S D Delivery Read Out Center 7 ROC 7 1 ea 17TES0700 48 000 90 Days Read Out Center 6 ROC 6 1 ea 17TES0400 N A 90 Days CVDR Recorder Interface RI Ca...

Page 39: ...RI ADAPTER 17TES0076 FA2100 COMPUTER INTERFACE COMMUNICATIONS CABLE CICC 2 17TES0070 and 17TES0072 READ OUT CENTER 6 or 7 17TES0400 or 17TES0700 Power Input Select RECORDER SOFTWARE CDROM The 17TES005...

Page 40: ...he ROC 3 At the Windows desktop shut down the Recorder Interface RI by right clicking on the RI Icon in the Windows System Tray at the bottom right of the screen Select shutdown 4 To install the CICC...

Page 41: ...ble 2 CICC 2 Interface Cable P N 17TES0072 5 Apply power to the FA2100CVDR Recorder under test 6 Turn ON the power to the ROC 7 Shut down the Recorder Interface RI by right clicking on the RI Icon in...

Page 42: ...Loader Window 15 Remove power from the recorder and Exit the CICC Loader utility pro gram 16 Disconnect the Software Upload Cable 17TES0058 from the FA2100 front panel GSE connector and CICC Cable Ass...

Page 43: ...the Version Command from the list and left click the Send Command button Observe that a pop up window appears showing the recorder software Part Number and SMP FDP Checksums 7 Match the listed SW Par...

Page 44: ...555 07 250 30 Days CICC Loader Utility Software Ver 3 0 1 ea 883E1893 12 No Charge 30 Days CICC Interface Utility Software Ver 3 7 1 ea 883E1827 18 No Charge 30 Days For 2100 3083 00 10 Audio Com pres...

Page 45: ...artment of Commerce HTSUS Sch B 4901 10 0040 4901 10 0000 LIMITED RIGHTS LEGEND Notice to persons receiving this document and or data This document and or data con tains information in which L 3 Commu...

Page 46: ...conformal coating process on all configura tions of the Acquisition Processor Circuit Card Assemblies CCA s to improve their mois ture resistance and mitigate pending obsolescence of the incumbent coa...

Page 47: ...artment of Commerce HTSUS Sch B 4901 10 0040 4901 10 0000 LIMITED RIGHTS LEGEND Notice to persons receiving this document and or data This document and or data con tains information in which L 3 Commu...

Page 48: ...th recorders model number FA2100 FA2200 and FA2300 assembled with the NAND memory C Description L 3 Aviation Recorders is now manufacturing model FA2100 FA2200 and FA2300 products with NAND memory dev...

Page 49: ...PI Unit will be crr The file extension for non modified CVRs older units with NOR memory remains as cvr for all audio downloads Downloaded files with the crr extension may be converted into wav files...

Page 50: ...roduct Support Engineers or at the factory repair station The cost for the update is 435 00 USD G Tooling Not applicable H Weight and Balance Not affected I Reference Portable Interface PI Unit Operat...

Page 51: ...Interface Mod Dot 9 for 435 The Portable Interface PI Unit must be returned to the Aviation Recorder factory Repair Station for modification Shipping Address L 3 Communications Aviation Recorders 100...

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

Page 53: ...v 15 xxviii Apr 14 16 Service Bulletin List Rev 15 xxix Apr 14 16 Rev 15 xxx Apr 14 16 Rev 15 xxxi Apr 14 16 Rev 15 xxxii Apr 14 16 List of Effective Pages Rev 15 xxxiii Apr 14 16 Rev 15 xxxiv Apr 14...

Page 54: ...ev 15 42 Apr 14 16 Rev 15 43 Apr 14 16 Rev 15 44 Apr 14 16 Rev 15 45 Apr 14 16 Rev 15 46 Apr 14 16 Rev 15 47 Apr 14 16 Rev 15 48 Apr 14 16 Rev 15 49 Apr 14 16 Rev 15 50 Apr 14 16 Rev 15 51 Apr 14 16 R...

Page 55: ...6 Rev 15 144 Apr 14 16 Rev 15 145 Apr 14 16 Rev 15 146 Apr 14 16 Rev 15 147 Apr 14 16 Rev 15 148 Apr 14 16 Rev 15 149 Apr 14 16 Rev 15 150 Apr 14 16 Rev 15 151 Apr 14 16 Rev 15 152 Apr 14 16 Rev 15 15...

Page 56: ...706 Apr 14 16 Rev 15 707 Apr 14 16 Rev 15 708 Apr 14 16 Rev 15 709 Apr 14 16 Rev 15 710 Apr 14 16 Rev 15 711 Apr 14 16 Rev 15 712 Apr 14 16 Rev 15 713 Apr 14 16 Rev 15 714 Apr 14 16 Rev 15 715 Apr 14...

Page 57: ...16 Rev 15 1004 Apr 14 16 Rev 15 1005 Apr 14 16 Rev 15 1006 Apr 14 16 Rev 15 1007 Apr 14 16 Rev 15 1008 Apr 14 16 Rev 15 1009 Apr 14 16 Rev 15 1010 Apr 14 16 Rev 15 1011 Apr 14 16 Rev 15 1012 Apr 14 16...

Page 58: ...MATTER 3 B DESCRIPTION AND OPERATION 3 C TESTING AND TROUBLESHOOTING 4 D DISASSEMBLY 4 E CLEANING 4 F CHECK 4 G REPAIR 4 H ASSEMBLY 4 I SPECIAL TOOLS AND TEST FIXTURES 5 J ILLUSTRATED PARTS LIST 5 7 D...

Page 59: ...e 22 P BIT and Fault Detection 22 4 FA2100 CVR SPECIFICATIONS 23 A Applicable Documents 23 B Physical Characteristics 24 C Electrical Characteristics 24 D Environmental Characteristics 24 E Crash and...

Page 60: ...rd Maintenance System Interface 60 A Label 350 Status Word Output 61 B Label 354 LRU Identification Output 64 C Label 377 ARINC 429 Equipment Identification Word Output 67 D OMS Input 67 10 CVR DATALI...

Page 61: ...OUT CENTER 7 ROC 7 CATS Autotest 145 D READ OUT CENTER 7 ROC 7 Autotest Descriptions 162 7 READ OUT CENTER 7 ROC 7 AUDIO DOWNLOAD PLAYBACK 170 8 Underwater Locator Beacon Testing 171 9 MODEL FA2100CVR...

Page 62: ...ted Wiring Assembly Cleaning 402 B Connector Cleaning 402 C Underwater Locator Device Beacon Cleaning 402 CHECK 1 GENERAL 501 2 CHECKS 501 A Main Recorder Assembly 501 B Mechanical Inspection 501 C El...

Page 63: ...and IPL Figure 1 Item 80 721 4 STORAGE INSTRUCTIONS 723 A Storage in Original Containers 723 B Storage Without Original Containers 723 C Shipment Container Kit 723 FITS AND CLEARANCES 1 GENERAL 801 2...

Page 64: ...LE OF CONTENTS Cont ILLUSTRATED PARTS LIST 1 GENERAL 1001 2 PURPOSE 1001 3 ABBREVIATIONS 1001 4 EQUIPMENT DESIGNATOR INDEX 1001 5 NUMERICAL INDEX 1002 6 DETAIL PARTS LIST 1002 7 PART NUMBERING 1004 8...

Page 65: ...iagram Recorder FA2100 CVR 2100 1X27 XX 28 9 Interwiring Diagram Recorder FA2100 GACVR 2100 10X0 50 51 with Customer Furnished Control Panel 30 10 FA2100 CVR Overall Function Block Diagram 32 11 2 Hr...

Page 66: ...127 Audio Reference Level Utility Confirmation 129 128 Audio Reference Level Utility Warning Message 129 129 Audio Reference Level Utility Menu 130 130 Audio Reference Level Utility File Open Menu 13...

Page 67: ...d Faults and Log Successful 151 157 CATS CVDR Fault History Log 152 158 CATS Continue Test Confirmation 152 159 CATS Test Results Screen 153 160 CATS Connecting Pop Up 154 161 CATS Power Toggle 154 16...

Page 68: ...5 FA2100 GACVR Chassis RTV Installation 713 706 FA2100CVR Chassis Cover Installation 714 707 Crash Survivable Memory Unit CSMU Seal Application Pre MOD DOT 13 715 708 Crash Survivable Memory Unit CSMU...

Page 69: ...ion Software CATS FA2100CVR TEST SETUP 914 908 Recorder Interface Cable Assembly 17TES0416 915 909 AC 115 VAC 400Hz Power Input Cable Assembly P N 17TES0411 916 910 DC 28VDC Power Input Cable Assembly...

Page 70: ...ult Warning Failures 55 10 CVR RIPS Pin Assignment for P N 2100 1X25 22 24 2100 1X26 1X27 58 11 CVR OMS Output Words 60 12 CVR Pins Assigned to RIPS Status Monitoring 61 13 CVR Label 350 Output Format...

Page 71: ...04 Rev 15 Page li 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 72: ...minute and 2 hour memory storage versions of the FA2100CVR The FA2100CVR is designed as maintenance free recorder No periodic adjustments calibration or maintenance is required to maintain this unit...

Page 73: ...ent Maintenance Manual F Portable Interface Operator s Manual Part Number 165E1630 00 F Portable Interface 2 Operator s Manual Part Number 165E1630 01 F Installation and Operation Manual Cockpit Voice...

Page 74: ...hat one or more of these assemblies is faulty the assem bly ies should be removed and returned to L 3 Aviation Recorders for repair or replacement Attempts to repair any discrete components of these a...

Page 75: ...uit board assemblies The steps of each procedure are coordi nated with the TESTING AND TROUBLESHOOTING Section Access to subassem blies within the FA2100CVR is described such that there is minimal dis...

Page 76: ...p n 2100 1010 30 minute and p n 2100 102X 2 hour currently produced 7 DOCUMENT VERIFICATION All CMM drawings illustrations wiring diagrams and block diagrams were validated against existing engineerin...

Page 77: ...and product serial number Effectivity of the manual is identified by a list of effective pages in the front of the manual 9 PART NUMBER FORMATTING L 3AR does not delineate its part numbers by special...

Page 78: ...hat is used to date time stamp the downloaded voice or flight data files This is not a function of the readout time displayed for voice or data The GMT inputs are the true time of the recording Data c...

Page 79: ...ULD GSE CONNECTOR BEHIND DUST COVER HARDWARE AND SOFTWARE MODIFICATIONS Figure 1 Model FA2100 Cockpit Voice Recorder FA2100CVR 2 FA2100 CONFIGURATIONS The current configurations of the FA2100CVR s ar...

Page 80: ...1025 22 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY W RIPS 10 6 max Figure 1 2100 1025 24 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY W RIPS S W 10 6 max Figure 1 2100 1026 02 ARINC 757 2 HR...

Page 81: ...quisition Processor PWA and the Crash Survivable Memory Unit CSMU which contains the solid state flash memory used as the recording medium A Underwater Acoustic Beacon The Model FA2100 FDR has an unde...

Page 82: ...e grated into the FA2100CVR electronics The removable circuit boards include the Aircraft Interface PWA Audio Compressor PWA and Acquisition Processor PWA C Power Control and Monitor Signal Interface...

Page 83: ...ORY TO AIRCRAFT FAULT MONITORING SYSTEM GSE OUTPUT COCKPIT AREA MICROPHONE CAM STOP RECORDING AUDIO COMPRESSOR PWA FA2100 CVR CVR FAULT TO GROUND STATION TEST EQUIPMENT GMT_IN_B 429 GMT_IN_A 429 ROTOR...

Page 84: ...ED SOLID STATE MEMORY TO AIRCRAFT FAULT MONITORING SYSTEM GSE OUTPUT COCKPIT AREA MICROPHONE CAM 3 STOP RECORDING AUDIO COMPRESSOR PWA FA2100 GACVR CVR FAULT TO GROUND STATION TEST EQUIPMENT GMT_IN_B...

Page 85: ...panel of the control unit via a 600 ohm headset The monitor audio signal has a reference input level of 2 55 Vrms into 600 ohms applied to one input channel In the 2100 1010 30 minute recorders the m...

Page 86: ...400 Hz ERASE A C 3rd Crew Member Spare Audio Cockpit Area Mic CAM Audio CH 4 CH 2 HQ 150 3500 Hz CH 3 HQ 150 3500 Hz CH 4 HQ 150 6000 Hz ERASE TO CONTROL UNIT HEADSET JACK AUDIO OUT CH 2 CH 1 CH 3 CH...

Page 87: ...1 Control Units Refer to the Component Maintenance Manual ED 56A Control Units Preamplifier Microphone Modules ATA 23 70 05 Part Number 165E1747 00 The 18 Vdc is a short circuit protected 30 mA line A...

Page 88: ...s used in an ARINC 557 757A configuration with interface to the air craft provided through a 57 pin DPXB rear panel connector The Reference Signal as required by ED 56A ED 112 is defined as an input s...

Page 89: ...ial pulse code modulation ADPCM processor These four streams are recorded as high quality HQ audio for a 30 minute dura tion In the case of P N 2100 1X25 1X26 1X27 XX and 2100 1X20 XX MOD DOT 7 these...

Page 90: ...d 30 minutes GMT 2 Wds per 1 Sec 120 minutes RSE 2 Wds per 1 2 Sec 120 minutes 429 GMT Time Code Rotor Speed CSMU FLASH MEMORY CH 1 HQV 150 3500 Hz CH 2 HQV 150 3500 Hz CH 3 HQV 150 3500 Hz CH 4 HQC 1...

Page 91: ...150 3500 Hz CH 4 HQC 150 6000 Hz CSMU FLASH MEMORY CH 1 24 kbps CH 2 24 kbps CH 3 24 kbps CH 4 48 kbps OMS Data Link OMS 120 minutes Figure 5 Sheet 2 of 2 Model FA2100 CVR 30 Minute and 120 Minute Re...

Page 92: ...0 minutes 120 minutes 120 minutes 120 minutes Not available Not available NOTE All of the times indicated in the above chart are minimum recording times 2 GMT FSK Output Signals In addition to the voi...

Page 93: ...d to the rear connector pins 39 and 40 as a low speed ARINC 429 signal The OMS output signal is sent out on pins 50 and 51 as a high speed ARINC 429 signal along with the Data Link output signal The R...

Page 94: ...a security feature implemented to protect the rights of pilots and other flight crew members The Cockpit Area Microphone CAM pilot co pilot and spare audio can be moni tored during recording using a h...

Page 95: ...X27 model any one of the high quality audio channels or the cockpit area microphone channel The PI or PI 2 Unit also has the capability to search through the stored data using the fast forward and fas...

Page 96: ...orm a continuous test of all bits within the solid state memory located in the Crash Survivable Memory Unit CSMU An additional built in test is initiated by pressing a green TEST pushbutton located on...

Page 97: ...otection requirements of EUROCAE ED 56A ED 112 and TSO 123a M Control Unit Microphone Preamplifier Equipment Refer to Aviation Recorders ED 56A Compliant Control Unit Preamplifier and Micro phone CMM...

Page 98: ...ly with TSO C123a and EUROCAE ED 56A However because ARINC Characteristic 757 does not address microphone preamplifiers the Model S150 S160 Preamplifiers are not considered ARINC 557 757 compliant The...

Page 99: ...ely cleared by a properly operating Store Manager Processor SMP as the recorder powers up Next a watchdog circuit monitors the operation of the SMP and associated circuitry This assures that a fault i...

Page 100: ...corder Systems 1 TSO C123b Federal Aviation Agency Technical Standard Order TSO C123b Techni cal Standard Order for Cockpit Voice Recorder Equipment 2 EUROCAE MOPS ED 55 European Organization for Civi...

Page 101: ...ntal characteristics refer to Section 800 Fits and Clearances E Crash and Fire Protection For specific crash and fire protection specifications refer to Section 800 Fits and Clearances F CSMU Torque R...

Page 102: ...er module by means of the aircraft wiring Refer to Figure 7 and Figure 9 for the Standard ARINC 757 and GACVR Interface Wiring Diagrams used when installing the FA2100CVR into an aircraft The Con trol...

Page 103: ...8 Vdc 1 2 7 FROM CAPTAIN S CLOCK AREA MICROPHONE FROM ROTOR SPEED SENSOR TO PILOT MICROPHONE SPARE MICROPHONE TO 3RD CREW MEMBER OR PA SYSTEM TO CO PILOT MICROPHONE 4 7 3 9 11 9 11 8 STANDARD INTERWIR...

Page 104: ...PS Active function the CVR has a backup power source or RIPS available pins 10 29 38 and 42 will be used for the RIPS Status Monitoring 8 BITE status output ground no fault open fault or CVR not insta...

Page 105: ...NTROL UNIT TO AC COLD TO 115 VAC 400 HZ 1 AMP 2 8 3 4 3 3 7 8 6 9 10 10 11 10 11 OR 115 VAC POWER IN HOT 115 VAC POWER IN COLD PREAMP PWR OUT GND PREAMP PWR OUT HOT 18 VDC REG PUSH TO TEST PREAMP PWR...

Page 106: ...elds to be grounded at the airframe using short connections Tie shields to existing single point GND used for Pin 17 see Note 3 8 If the power source has battery back up a means for terminating record...

Page 107: ...CK TYPICAL AUDIO JACK LO AUDIO JACK HI ATTENUATION COMMON 6dB ATTENUATION 12dB ATTENUATION 24dB ATTENUATION 6 STOP RECORDING CVR FAULT 8 MICROPHONE CONTROL PANEL OPEN IN FLIGHT CLOSED WEIGHT ON WHEELS...

Page 108: ...t connec tions Tie shields to existing single point GND use for Pin 17 see Note 4 6 If the power source has battery back up a means for terminating recording after a crash should be included in the ai...

Page 109: ...C 557 757 757A Model FA2100CVR consists of four subassemblies the Aircraft Interface Printed Wiring Assembly PWA the Audio Compressor PWA the Acquisition Processor PWA and Crash Survivable Memory Unit...

Page 110: ...re Used Aircraft Interface PWA P N Model Effectivity Notes 205E250305 2100 1010 00 2100 1020 00 2100 1020 02 2100 1220 00 2100 1220 02 205E250301 2100 1025 02 2100 1025 12 2100 1025 22 2100 1025 24 21...

Page 111: ...ut power as defined in RTCA DO 160C Section 16 AUDIO OUT HI LO Combined high quality voice and CAM channels to provide au dio monitor output With the reference signal applied to one channel the output...

Page 112: ...e is greater than 10 kohms CHANNEL 4 AUDIO IN HI LO CAM audio input Reference signal is 1 kHz at 2 Vrms Input impedance is greater than 10 kohms ROTOR SPEED IN HI LO Rotor speed input data as defined...

Page 113: ...utput 5 V through 15 kohms when not asserted Ground through 10 kohms when asserted TEST L Conditioned PUSH TO TEST signal output 5 V through 10 kohms for not asserted Less than 0 4 V sinking 3 5 ma wh...

Page 114: ...is 2 volts Current requirement is less than 25 ma 15VDC 15 volt output made from Storage Supply input voltage Tracks the unregulated input below about 15 volts and then regulates at that lev el 18VDC...

Page 115: ...io Compressor are output to the Aircraft Interface for audio moni toring Power ground and a master reset for the Audio Compressor are derived from the Acquisition Processor PWA The Audio Compressor PW...

Page 116: ...inputs The ED 56A and ED 112 reference voltage input to the AC for Channels 1 3 is 2 0 Vrms into a 10 kohm load and a specified bandwidth of 150 3500 Hz Input Channel 4 cor responds to the Cockpit Are...

Page 117: ...r Interface The AC AP Interface includes the following signals a Serial TDM Bus signals TCLK TFRM TADD and TDAT b Master Clock Input F8 192 MHz c Master Reset AC RESET L d BIT Control Input TEST MODE...

Page 118: ...2 205E250238 2100 1010 50 2100 1010 51 2100 1020 50 2100 1020 51 Compatible with 3V Intel Memory The Acquisition Processor interfaces with three internal functional modules Aircraft Interface Audio Co...

Page 119: ...data messages to the AP only in response to commands issued by the AP Additionally 5 V and 12 V power for the CSMU and CSMU reset are routed through this interface 4 Ground Support Equipment Interface...

Page 120: ...audio data This software is self contained and runs separately from the system software As defined in RTCA DO 178B the Criticality Category of the Model FA2100CVR is classi fied as Minor Accordingly t...

Page 121: ...tate for recovery of recorded audio The CVR Executive processes the input digital audio channel data and man ages the actual record or playback operations The Flash Manager acts as a server task suppo...

Page 122: ...eams into a form ready for storage into the CSMU The complete sequential process is described in the steps be low a The TDM interrupt handler receives the audio data stream from the Audio Compressor h...

Page 123: ...SF SF SQV 2 36 Word Frames per 72 ms Superframe 1 36 Word Special Frame per 4 Superframes SQV SF SPCL X SF SF SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SF SQC SQC 2 36 Word Fram...

Page 124: ...as been completely processed through the CSMU While in the record state the Mode Executive monitors the delayed shutdown input to the CVR If asserted and held this will cause the Mode Executive to sta...

Page 125: ...a before the power fail re set occurs e After the NVRAM values have been updated the CVR executive enters an idle loop waiting for power to drop If the power fail indicator relents the CVR executive w...

Page 126: ...push to test state which is initiated and controlled by the push to test discrete input to the CVR Assertion of the push to test input usually by depressing a push button on the control unit in the co...

Page 127: ...many memory devices for 30 minutes of high quality recording as it does for 120 minutes of standard quality recording For 30 minute recorders the total amount of physical memory capacity is 24 megaby...

Page 128: ...malies This includes all messaging between tasks SMP to CSMU and SMP to GSE The digitized audio data input stream from the Audio Compressor board is also monitored for integrity The software also moni...

Page 129: ...n The type of event field categorizes the general nature of the fault conditions Reported categories include Table 8 Fault Processing Event Types and Descriptions Type of Event Description Internal Fa...

Page 130: ...of two DSPs One DSP called the Flight Data Processor FDP is responsible for the collection processing and forwarding of Data Link messages The other processor called the Storage Management Proc essor...

Page 131: ...26 1X27 only The CVR is identified as a BITE Standard A equipment so as to be portable to other AIRBUS programs The CVR interfaces with the OMS through a system BITE such that the CVR will pass fault...

Page 132: ...udio circuit Control Unit loads Its pow er supply below 15 5 Volts Failure of the recording medium Failure of the recording medium Failure of the recorder to store Information In the storage medium Fa...

Page 133: ...that the crew can re initiate the test after a fault is detected in the hope of recovering the re corder test is specified to act as a reset of the recorder F Bulk Erase As per ARINC 757A the CVR prov...

Page 134: ...event FSK or ARINC 429 time reference is not available Label 350 Bit 17 indicates the status of the clock as the following 0 ok and 1 fail ure H Data downloading P N 2100 1X25 1X26 1X27 only It is pos...

Page 135: ...the data will be able to be retrieved using the existing support equipment for analysis Table 10 CVR RIPS Pin Assignment for P N 2100 1X25 22 24 2100 1X26 1X27 Pin Number Pre RIPS Pin Assignment RIPS...

Page 136: ...tted in the Label 350 Label 351 and new Label 352 outputs as follows RIPS Mainten ance Status CVR Discrete in put Pin 38 SSCVR Label 350 and 352 Bit 20 SSCVR Label 351 Bit 19 No Mainten ance required...

Page 137: ...nformation on the RIPS see P N 165E4900 00 Installation and Operation Instruction Manual for Recorder Independent Power Supply RIPS 9 On board Maintenance System Interface The 2100 1025 22 24 CVR incl...

Page 138: ...equired 42 RIPS Present Pin Program Open No RIPS Installed Ground RIPS Present If the RIPS is not present then the CVR will not monitor the RIPS status inputs and they will not be reported default to...

Page 139: ...ble 14 CVR Fault Reporting Interactions L350 BIT N FUNCTION REPORTED WITH L350 BIT 11 REPORTED WITH PUSH TO TEST REPORTED WITH CVR FAULT DIS CRETE 11 CVR Status Audio Recording Failure YES YES YES 12...

Page 140: ...g Criteria L350 BIT N FUNCTION FAILURE CRITERIA 11 CVR Status Audio Record ing Failure Any internal CVR failure that prevents correct record ing of the audio inputs including CU failure and Push to Te...

Page 141: ...ppropriate ground support equipment for review and analysis B Label 354 LRU Identification Output The CVR LRU IDENTIFICATION consists of multiple ARINC 429 words for the trans mission of the CVR part...

Page 142: ...tus 1 8 Label 354 11101100 9 15 Sixth character of part number 16 Not used 0 17 23 Seventh character of part number 24 Not used 0 25 31 Eighth character of part number 32 Parity f Part Number continue...

Page 143: ...ial Number continued Bit No Function Status 1 8 Label 354 11101100 9 15 Fifth character of serial number 16 Not used 0 17 23 Sixth character of serial number 24 Not used 0 25 31 Seventh character of s...

Page 144: ...e CMS Bus OMS input status as failed in the Label 350 CVR Status Word output If the OMS input bus is not connected then the associated Label 350 Status Word bit 12 can be ignored 10 CVR DATALINK INPUT...

Page 145: ...ARINC 619 formatting which provides the Network layer interface However the FA2100CVR records data at the link layer in terface level and is unaffected by any link layer or above data content This me...

Page 146: ...C Length ASCII Message Area ARINC 623 ATIS Display Server Length 0 2 3 5 1 4 6 Figure 13 Generic DataLink Message Encapsulation Structure As indicated in Section 1 above the FA2100 DataLink CVR also...

Page 147: ...ntly support Williamsburg Version 1 protocol or a low speed ARINC 429 interface for input of DataLink informa tion However the CVR does support the Williamsburg ALOHA exchange even though it is not re...

Page 148: ...same way as audio data All or a portion of the DataLink recording can be downloaded from the CVR using Ground Support Equipment supplied by L 3 Aviation Recorders The Portable Interface can be used t...

Page 149: ...and Operation 23 70 04 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 150: ...0 1X27 XX require the ROC 7 and CATS 2 0 This section provides operational level testing procedures for the Model FA2100 Cockpit Voice Recorder when using the CVR Automated Test Station CATS software...

Page 151: ...surface mount technology SMT The repair of a PWA containing SMT de vices requires specialized training and factory equipment along with special trouble shooting and soldering techniques therefore L 3...

Page 152: ...uilt in test feature has been designed to perform a continuous test of all bits within the solid state memory located in the Crash Survivable Memory Unit CSMU Any faults with the unit are stored in no...

Page 153: ...into the microphone at a normal voice level You should be able to hear your words without any significant distortion Bulk erasure of the Model FA2100CVR storage medium is accomplished using the associ...

Page 154: ...ad Out Center 6 ROC 6 P N17TES0400 L 3AR Read Out Center 7 ROC 7 P N17TES0700 CVR Automated Test Station Software CATS P N 17TES0420 L 3AR Beacon Test Set P N 17TES0015 Dukane Beacon Test Set Dukane 4...

Page 155: ...ROC 6 Interconnects CAUTION Make certain that all power is turned off before attaching cables Failure to turn off power before attaching cables will result in immediate and serious damage to the unit...

Page 156: ...ND IN J3 cable to the Sound Card Line In or Microphone In which is the blue connector 6 Attach the RIU Sound Card Out SND OUT J5 cable to the Sound Card Line Out which is the green connector 7 Connect...

Page 157: ...UT SPKRS J9 RCDR AC PWR TEST RECORDER INTERFACE UNIT RIU 17TES0410 SND IN BLUE 17TES0413 SND OUT GREEN 17TES0413 J4 J2 J1 L SPKR R SPKR YELLOW AC RED DC AC 1A DC 5A USB Note Speakers are optional and...

Page 158: ...n follow this procedure 2 Click the Speaker button Volume Control to display the Playback Control menu 3 Click on the Options pull down and then click on Properties 4 Click the Recording radio button...

Page 159: ...this document Figure 104 Line In Input Level 9 Click on the Options pull down and then click on Properties 10 Select the Playback radio button 11 Select the following check boxes Play Control Wave an...

Page 160: ...page of this document 13 Move the Playback and the Wave Volume Controls to full volume and check the Mute box on the Line in Mute should not be checked for all others Figure 106 Playback Control Volum...

Page 161: ...U us ing the cable p n 17TES0416 for the recorder rear connector and cable p n 17TES0072 for the recorder front connector b Setup an in line RMS multimeter Set to DC amps c Apply power to the RIU usin...

Page 162: ...ge of this document l Read and click on Yes Figure 107 CVR Test Start Toggle m Read and click on OK Figure 108 CVR Test Warning Message n Remove front cable and click on OK Figure 109 CVR Test Instruc...

Page 163: ...n window and click on OK Figure 111 CVR Test Power Consumption Entry r Connect the recorder front cable and click on OK Figure 112 CVR Test Instruction Message s Verify that the DC LED on the front of...

Page 164: ...Ensure that the RIU has no power applied Power is removed Connect a CVR to the RIU using the 17TES0416 for the recorder rear connector and 17TES0072 for the recorder front connector b Setup an in lin...

Page 165: ...ce is checked k From the pull down menu click on Test Start Test l Follow the instructions below as it appears presented by the software m Read and click on Yes Figure 114 CVR Test Instruction Message...

Page 166: ...n window and click on OK Figure 118 CVR Test Power Consumption Entry s Connect the recorder front cable and click on OK Figure 119 CVR Test Instruction Message t Verify that the AC LED on the front of...

Page 167: ...the fault history log by the pull down menu click on Test Clear Fault History D READ OUT CENTER 6 ROC 6 Autotest Descriptions The following provides detailed descriptions of the test performed during...

Page 168: ...8 02 42 PASSED Bulk Erase 1 Expected 400 Hz Results 400 0 Hz 08 02 50 PASSED Bulk Erase 2 with active Rotor Speed Expected 400 Hz Results 123 0 Hz 08 02 58 PASSED Bulk Erase 3 with No Recording Expect...

Page 169: ...0 Hz 1 10 reference level data for each channel 1 2 3 and 4 and verify amplitude all within 3 dB Example report message s 08 04 52 PASSED Channel Bal 1000 Hz 0 5 ref All within 3 dB Results HQ1 5 2 HQ...

Page 170: ...and 3500 Hz Frequencies for HQCAM and SQCAM are 217 314 454 656 949 1372 1984 and 2869 Hz Frequencies for HQCAM only are 4148 and 6000 Hz Verify HQ 24 0 dB and SQ 20 0 dB Example report message s 08 0...

Page 171: ...simulated GMT 429 and calculate channel results minus channel balance results Verify difference is less than 34 dB Example report message s 08 43 07 PASSED Channel Bal 1000 Hz 1 0 ref All within 3 dB...

Page 172: ...2 SQV3 80 7 SQC 85 0 dB 14 Shutdown Part 1 enable delayed shutdown Part 2 verify shutdown is detected CVR fault set after 9 and 10 minutes Part 3 verify shutdown is terminated following a push to tes...

Page 173: ...gain with channel 3 output Verify 9 good FSK data patterns and a switch to 9 good GMT 429 data patterns for each channel 1 and channel 3 Example report message s 14 50 07 PASSED FSK Time HQ1 Playback...

Page 174: ...Setup Cable Assembly p n 17TES0417 refer to Figure 121 LOOP BACK CONNECTOR Figure 121 Audio Setup Cable Assembly 17TES0417 NOTE Selections on the toggle switches of the Audio Setup Cable Assembly pn 1...

Page 175: ...bserve the con necting to recorder status window appears g From the pull down menu click on Power DC Power On or AC Power On NOTE Observe the connecting to recorder status window appears h Verify that...

Page 176: ...erence Utility Select Setup_1000Hz wav and click on Open Figure 124 Audio Reference Level Utility File Open Menu d Ensure the MultiMeter is connected to the Audio Setup Loop back cable Set the toggle...

Page 177: ...h Set the toggle switches on the loop back connector to the following set tings Switch Settings Channel 4 and No Audio Out i At the Audio Reference Level menu ensure that the Channel 4 check box is se...

Page 178: ...dio Reference Level menu by selecting the Close button NOTE The Audio Reference Utility volume value is used to define the VOICE VOLUME for channels 1 2 3 and the CAM VOLUME for channel 4 for output t...

Page 179: ...e wav file by selecting File Open File on the Audio Reference Utility Select Setup_1000Hz wav and click on Open Figure 130 Audio Reference Level Utility File Open Menu e From the menu bar under Utilit...

Page 180: ...nput sound h From the Audio Reference Level menu select Sound Stop Record to stop recording i From the Audio Reference Level menu select Sound Stop Play to stop audio output from the sound card j From...

Page 181: ...o adjust the audio voltages read from the audio output of a 600 ohm recorder during CVR tests For example if 1 952 Volts RMS is read from the sound card then Correction Factor 2 45 VRMS 1 952 VRMS If...

Page 182: ...ing the CATS soft ware The FA2100CVRs that have Hardware MOD DOT 7 installed have full two hour High Quality for all four audio channels as does all 30 Minute FA2100CVRs 1 Click on the Copy button Set...

Page 183: ...3 Com 17TES0413 Cable RIU to Sound Card 2ea L 3 Com 17TES0415 Cable RIU to USB L 3 Com 17TES0416 Cable RIU to CVR L 3 Com 17TES0417 Cable Assembly Audio Setup L 3 Com 17TES0420 CATS Software FA2100 L...

Page 184: ...er connector J8 on the rear of the RIU to a DC power supply that can generate 28 Volts 1 Amp b For AC power connect the AC power cable 17TES0411 from the AC Power connector J7 into a watt meter that h...

Page 185: ...nect the DIN CABLE from the speakers to the middle Speaker Out SPKRS OUT J6 connector on the front panel of the RIU 8 After all connections are made to the RIU apply power to the RIU This can be eithe...

Page 186: ...CDR AC PWR TEST RECORDER INTERFACE UNIT RIU 17TES0710 SND IN BLUE 17TES0413 SND OUT GREEN 17TES0413 J4 J2 J1 L SPKR R SPKR YELLOW AC RED DC AC 1A DC 5A USB Note Speakers are optional for ROC 7 To orde...

Page 187: ...J9 RCDR AC PWR TEST RECORDER INTERFACE UNIT RIU 17TES0710 SND IN BLUE 17TES0413 SND OUT GREEN 17TES0413 J4 J2 J1 L SPKR R SPKR YELLOW AC RED DC AC 1A DC 5A USB Note Speakers are optional for ROC 7 To...

Page 188: ...OC to start the software The applic ation will launch with the Channels control screen displayed as illustrated in Figure 136 Figure 136 CATS Channels Control Screen 2 In the Channels control screen c...

Page 189: ...s on the cover page of this document Figure 137 Volume Control 4 Under Applications click Sound Systems then click the Recording tab This will display the Sound control window illustrated on the follo...

Page 190: ...trictions on the cover page of this document 6 Highlight and select Line in 7 Click on Properties Figure 139 Line In Properties Line In Level 8 Select the Levels tab 9 Make sure that the Line In level...

Page 191: ...sure of information on this sheet is subject to the restrictions on the cover page of this document Figure 140 Sound Playback Devices 10 Click on the Playback tab 11 Highlight Speakers 12 Click on Pro...

Page 192: ...s Levels 13 Select the Levels tab 14 Make sure Playback Control is set at 100 move the Playback Control slider to its maximum setting 15 Make sure that the four remaining controls Microphone Line In A...

Page 193: ...ormation on this sheet is subject to the restrictions on the cover page of this document Figure 142 Volume Mixer Speaker Levels 17 In the Volume Mixer make sure both sliders are all the way up 18 Clos...

Page 194: ...C 2 When autotesting using both DC and AC power to CATS Autotest using AC and DC power paragraph C 2 1 ROC 7 CATS Autotest using DC power To perform the CATS Autotest using DC power only follow the pr...

Page 195: ...ecting Pop Up g On the tool bar select Power Figure 144 CATS Power Toggle NOTE When DC power is applied verify the appropriate LED is lit up on the RIU h Click on the Information tab in the Test secti...

Page 196: ...In the Test Mode and Options dialog box select either Return to Ser vice or Selectable Test Options then click on OK Figure 146 CATS Test Mode and Options Screen NOTE If a full return to service test...

Page 197: ...Figure 147 is only displayed if Selectable Test Option is cho sen from the CATS Test Mode and Options Screen Figure 147 CATS CVDR Test Confirmation NOTE Follow the instructions displayed in the confi...

Page 198: ...eter on the power supply or from the inline RMS multimeter And enter in the value in amps in window and click on OK Figure 150 CATS Power Test Input o Read the current DC amps value from the built in...

Page 199: ...over page of this document Figure 152 CATS CVDR Instruction Window q Observe the Fault History Log window appears Select Print if you want to save the fault history or Close to continue Figure 153 CAT...

Page 200: ...irmation s Click on Yes on the dialog box to clear the latched faults and fault history log Figure 155 CATS CVDR Clear Latched Faults and Log Confirmation t Click on Ok Figure 156 CATS CVDR Clear Latc...

Page 201: ...onfirmation w 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 provided...

Page 202: ...otest using AC power To perform the CATS Autotest using AC power only follow the procedures below a Ensure that the RIU has no power applied power is removed If not al ready done Connect a CVR to the...

Page 203: ...menu bar select Power Recorder Interface Reset NOTE This will load the Altera chip in the RIU unit Observe the con necting to the recorder status window appears h On the tool bar select Power Figure 1...

Page 204: ...appropriate information into Department Part Number and Serial Number fields k On the tool bar select Start Test Figure 162 CATS Start Test Toggle l In the Test Mode and Options dialog box select eit...

Page 205: ...e Test Options radio button and choose the test options desired NOTE Figure 164 is only displayed if you select Selectable Test Op tion from the CATS Test Mode and Options Screen Figure 164 CATS CVDR...

Page 206: ...eter on the power supply or from the inline RMS multimeter And enter in the value in amps in window and click on OK Figure 167 CATS Power Test Input p Read the current AC amps value from the built in...

Page 207: ...over page of this document Figure 169 CATS CVDR Instruction Window r Observe the Fault History Log window appears Select Print if you want to save the fault history or Close to continue Figure 170 CAT...

Page 208: ...og Confirmation t Click on Yes on the dialog box to clear the latched faults and fault history log Figure 172 CATS CVDR Clear Fault Log Confirmation u Click on Ok Figure 173 CATS CVDR Clear Latched Fa...

Page 209: ...onfirmation x 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 provided...

Page 210: ...ult Isolation 23 70 04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document Figure 176 CATS Test Results Screen The document reference is on...

Page 211: ...sults 12 watts 4 watts 8 watts 08 02 23 PASSED Power DC Expected 11 watts Results 12 375 watts 2 2 watts 10 175 watts 2 Fault Log Displays the current recorder fault log for user review and prompts th...

Page 212: ...ts 10 good patterns 6 Rotor Speed Part 1 Record simulated 6000 Hz rotor speed data and verify data is within 2 of sent frequency Part 2 Record simulated 7 Hz rotor speed data and verify data is within...

Page 213: ...1 4 SQV1 3 9 SQV2 3 9 SQV3 3 9 SQC 3 9 dBV 08 07 15 Frequency Resp 1000 Hz 0 5 ref Results HQ1 5 2 HQ2 5 3 HQ3 5 1 HQC 5 1 SQV1 5 4 SQV2 5 4 SQV3 5 4 SQC 5 4 dBV 08 08 02 Frequency Resp 3500 Hz 0 5 r...

Page 214: ...0 ref Expected HQC 24 0 dB Results HQC 30 6 dB 11 31 07 PASSED SN D 6000 Hz 1 0 ref Expected HQC 24 0 dB Results HQC 27 7 dB NOTE Running the Signal to Noise and Distortion test in the Selectable Tes...

Page 215: ...dB Results HQ1 11 2 HQ2 11 2 HQ3 11 0 HQC 11 1 SQV1 11 0 SQV2 11 3 SQV3 11 4 SQC 11 5 dBV 08 43 23 PASSED Crosstalk Data 6000 Hz 1 0 ref Expected Crosstalk Channel Bal 34 dB Results HQ1 304 9 HQ2 125...

Page 216: ...an 48 dB Example report message s 08 47 12 PASSED Sig To No Sig 0 Hz 1 0 ref Expected HQ 48 dB SQ 40 dB Results HQ1 304 9 HQ2 122 6 HQ3 108 4 HQC 115 4 SQV1 82 7 SQV2 82 2 SQV3 80 7 SQC 85 0 dB 15 Shu...

Page 217: ...mulated data link messages 18 OMS Read the OMS status words and verify CVR fault status and CVR part number and serial number Example report message s 08 59 00 PASSED OMS Part 1 Expected OMS Status to...

Page 218: ...the FA2100 fault log and existing faults that might prevent FDR test success Record simulated flight data and verify good flight data was recorded Example report message s 09 11 00 PASSED FDR Test Re...

Page 219: ...erted using the CATS soft ware The FA2100CVRs that have Hardware MOD DOT 7 installed have full two hour High Quality for all four audio channels as does all 30 Minute FA2100CVRs 1 Click on the Copy bu...

Page 220: ...57 Cable Assembly CVDR Interface L 3 Com 17TES0071 Cable Assembly F1000 CICC 2 L 3 Com 17TES0321 Read Out System Equipment Software ROSE 4 5 L 3 Com 17TES0058 FA2100 Software Upload Cable Assembly L 3...

Page 221: ...act with the metal pad at the center of the water switch 4 Read the battery voltage from the test set display If the battery voltage is at or above 2 97 volts the battery is operable If the battery vo...

Page 222: ...acon turn on the test set by rotating the front panel GAIN control clockwise until it clicks 4 On the front panel of the test set set the INT EXT switch to INT 5 Rotate TUNING control to a setting bet...

Page 223: ...rrective Actions Fault Code Failure Mode Corrective Action cde0 An invalid partition map was found 1 Remove Memory 09d7 The SMP Check timed out waiting for audio channelizer to shutdown 1 ck cables 2...

Page 224: ...f fault codes still present in status report then return the recorder to factory for repair 59db System Error CVR test failed Test tone failed 1 Remove and replace Audio Compressor PWA PN 205E3977 2 R...

Page 225: ...r PWA p n 205E2502 XX 2 Run autotest recheck recorder status 3 If fault codes still present in status report then return the recorder to factory for repair 89d1 The non volatile memory on the CVR has...

Page 226: ...77 XX 2 Run autotest recheck recorder status 3 If fault codes still present in status report then return the recorder to factory for repair 8453 Read After Write Errors Too Long Erase Event and Error...

Page 227: ...ludes the Computer Interface Communications Cable 2 p n 17TES0070 and the FA2100 to CICC 2 cable p n 17TES0072 The software upload procedure is also necessary when replacing a faulty Turbo Acquisi tio...

Page 228: ...tributed with ROSE 3 1 or lower will not work with the updated CICC 2 Interface Newer versions of the software are back ward compatible and will work with the original CICC Inter face 5 To load the In...

Page 229: ...Note Firmware Distribution Diskette P N will match the FA2100 Software Part Number located on the recorder s Name Plate Label TO ENHANCED PARALLEL PORT EPP FA2100 SOFTWARE UPLOAD BOOTLOAD CABLE ASSEMB...

Page 230: ...using the CICC 2 2 At the FA2100 J1A connector use the Recorder Interface RI Cable Assy P N 17TES0057 to connect either 115 Vac 400 Hz or 28 Vdc to the pig tail con nectors Alternatively 28Vdc power m...

Page 231: ...ecified in the CICCLDR ini file matches the ad dress of the parallel port connected to the CICC 14 Turn off power from the recorder and Exit the CICC Loader utility program 15 Disconnect the 17TES0058...

Page 232: ...s listed in Section 100 of this manual Table 106 FA2100CVR Software SMP Checksums Software P N Recorder P N SMP Checksum SMP Ver 840 E1657 01 2100 1020 00 2100 1020 02 0X5609 6 1 840 E1657 03 2100 102...

Page 233: ...0 51 0X3152 7 5 840 E1664 05 2100 1020 50 2100 1020 51 0XADB6 7 9 840 E1664 06 2100 1020 50 2100 1020 51 0X8A62 8 7 840 E1664 09 2100 1020 50 2100 1020 51 840 E3408 04 2100 1025 12 0XD857 8 1 840 E340...

Page 234: ...100 1025 02 2100 1025 12 0X44A9 1 8 840 E3408 05 2100 1025 02 2100 1025 12 0X44A9 1 8 840 E4568 06 2100 1025 22 2100 1125 02 0X486D 2 1 840 E4568 09 2100 1025 22 2100 1125 02 0X5E5E 2 3 840 E4568 11 2...

Page 235: ...lt Isolation 23 70 04 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 236: ...r disclosure of information on this sheet is subject to the restrictions on the cover page of this document AUTOMATIC TESTING 1 GENERAL There are no Automatic Test Procedures for the FA2100 CVR The do...

Page 237: ...c Testing 23 70 04 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 238: ...SURE PROPER PERSONNEL GROUND ING TECHNIQUES ARE USED ALSO ENSURE THAT ALL CIRCUIT BOARDS ARE PLACED INTO STATIC SHIELDING CONDUCTIVE BAGS WHEN HANDLING OR STORING SYMBOL FOR ESD GROUND CONNECTING O ES...

Page 239: ...tification 30 Day ULB s already in service may still be used and a ULB Battery Kit p n 147E0305 00 is available for battery replacement The 30 Day ULB p n 266E0305 00 is no longer manufactured due to...

Page 240: ...e CSMU 2 Loosen the lower right hex cap screw 1 75 which secures the right Beacon Mount Bracket to the CSMU and holds the beacon in the bracket 3 The beacon can now be removed from the Beacon Mount Br...

Page 241: ...y for repair If replacement of the CSMU is required proceed with the fol lowing procedure CSMU REMOVAL PROCEDURE 1 Remove the Underwater Acoustic Beacon 1 80 as described in paragraph A above 2 Remove...

Page 242: ...Acquisition Processor PWA Note the pins of J1 can be easily dam aged if handled incorrectly Memory Interface Cable Assembly P1 J1 Acquisition Processor PWA AP CSMU Memory Assembly 1 185 1 175 Recorde...

Page 243: ...emory Assembly Removal Diagram POST MOD DOT 6 PRE MOD DOT 13 c For Post MOD DOT 13 units only carefully lift the CSMU memory assem bly directly up without pulling the memory interface cable to gain ac...

Page 244: ...own ori ented so that this circuitry is not underneath the CSMU Failure to do this will result in damage to the CSMU Memory Assembly 6 Package CSMU memory assembly and return to L 3 Aviation Recorders...

Page 245: ...t the Audio Compressor PWA interconnection cable assembly W003 1 165 from J4 on the Acquisition Processor PWA 5 Remove 8 flat head screws 1 95 that secure the rear panel assembly 1 90 with attached Ai...

Page 246: ...1 1 170 Rear Panel Assy 1 90 J5 Figure 306 Acquisition Processor PWA Removal Diagram D Audio Compressor PWA AC Removal See Figure 307 or IPL Figure 1 Item 155 The Model FA2100 s Audio Compressor PWA i...

Page 247: ...ve 8 flat head screws 1 95 that secure the rear panel assembly 1 90 with attached Aircraft Interface PWA and Audio Compressor PWA into the recorder Chassis 1 5 NOTE Flat head screws 1 95 are one time...

Page 248: ...essor PWA AP 1 175 1 95 Qty 8 1 90 1 20 1 25 Qty 10 1 110 Qty 2 1 115 1 125 Qty 3 A 1 125 Aircraft Interface PWA AI 1 105 Audio Compressor PWA AC 1 155 1 120 Qty 4 W001 1 170 W002 1 165 J3 1 135 W003...

Page 249: ...A 1 155 from the rear panel assembly as de tailed in Para D above 2 Disconnect the interconnection cable assembly W001 1 165 from J2 and W002 1 170 from J3 on the Aircraft Interface PWA Keep these cab...

Page 250: ...andoffs 1 120 on the Aircraft Interface PWA 12 Remove the remaining single pan head screw 1 125 which attaches the center standoff 1 115 to the Aircraft Interface PWA 13 Using a 3 16 hex wrench unscre...

Page 251: ...sembly 23 70 04 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 252: ...nt 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 commercia...

Page 253: ...iring Assembly Cleaning 1 Remove dust dirt and foreign matter from all surfaces using soft bristle brush 2 Wipe finished surfaces and contacts using a cloth moistened in solvent B Connector Cleaning 1...

Page 254: ...CKS A Main Recorder Assembly 1 Check the general physical integrity of the recorder i e front panel ATE connector pins Underwater Locator Device acoustic beacon and J1A rear panel connector pins 2 Che...

Page 255: ...te for legibility 9 Reassemble recorder in accordance with the steps of procedure outlined in Section 700 Assembly C Electrical Inspection Perform all test set up and testing per instructions given in...

Page 256: ...FA2100CVR to component level in accordance with L 3AR Factory test calibration and repair speci fications As a result the Model FA2100CVR s maintenance philosophy is replacement of failed as semblies...

Page 257: ...pair 23 70 04 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 258: ...e common assembly materials used with the FA2100 Cock pit Voice Recorder Table 701 Required Assembly Materials Item Manufacturing and Specification Use 1 Adhesive Loctite Grade E Purple No 222 Lock se...

Page 259: ...or the FA2100 CVR a known defective circuit board assembly shall be returned to the factory for repair or replacement NOTE Numbers shown in parentheses in the following text are the Illustrated Parts...

Page 260: ...5 W001 1 170 Rear Panel Assy 1 90 J5 Figure 701 Acquisition Processor AP Installation Diagram The Acquisition Processor PWA provides an interface between the Aircraft Interface PWA through W001 Cable...

Page 261: ...n Processor requires specifically configured software to oper ate refer to the Test and Troubleshooting Section 100 for detailed procedures on loading the recorder software through the front panel GSE...

Page 262: ...of 5 6 in lbs 6 Position the Aircraft Interface PWA into the rear panel assembly such that the J1A mounting holes and upper standoffs are aligned properly 7 While holding the J1 connector flush with t...

Page 263: ...nsure that the Aircraft Interface PWA 1 105 is installed into rear panel assembly 1 90 as described in paragraph C above 2 Lay the rear panel assembly on its back with the Aircraft Interface PWA facin...

Page 264: ...20 1 25 Qty 10 1 110 Qty 2 1 115 1 125 Qty 3 A 1 125 Aircraft Interface PWA AI 1 105 Audio Compressor PWA AC 1 155 1 120 Qty 4 W001 1 170 W002 1 165 W003 1 165 J1 J3 1 130 Qty 4 1 160 Qty 4 1 125 Qty...

Page 265: ...8 1 90 1 20 1 25 Qty 10 1 110 Qty 2 1 115 1 125 Qty 3 A 1 125 Aircraft Interface PWA AI 1 105 Audio Compressor PWA AC 1 155 1 120 Qty 4 W001 1 170 W002 1 165 J3 1 135 W003 1 165 J1 J3 1 130 Qty 4 1 16...

Page 266: ...own in Figure 703 13 Turn the chassis over to the opposite side and tighten the remaining three screws to 9 10 in lbs in the same pattern as shown in Figure 703 14 Connect the Aircraft Interface PWA W...

Page 267: ...the seal screw holes line up with the chassis cover screw holes 9 Replace the chassis cover 1 20 by inserting the front end of the cover into the alignment grove and inserting ten attaching pan head s...

Page 268: ...1 20B meets the chassis 1 5 as indicated in Note 2 Figure 705 15 For GACVR p ns 2100 1010 5X and 2100 1020 5X apply RTV Table 701 Item 3 around the connector including the three keying holes and the s...

Page 269: ...CHASSIS COVER OVER SEAL PRESS IN PLACE ALIGN SEAL OVER FIXTURE HOLES REMOVE SEAL BACKING AND SMOOTH OUT 1 2 PUSH TOOL FIRMLY TO AFFIX SEAL TO SIDE 3 4 DO NOT STRETCH SEAL MATERIAL HOLES IN SEAL SHOULD...

Page 270: ...4 Apply RTV to entire seam where Chassis Cover meets the Chassis after the CSMU is installed and tight ened Note 2 Apply RTV to Two Front Screw Heads and the front seam where the Chassis Cover meets t...

Page 271: ...85 The Model FA2100 s Crash Survivable Memory Unit CSMU is a sealed unit and must not be opened in the field CSMU is mounted to the top of the recorder chas sis by 4 pan head srews The CSMU interfaces...

Page 272: ...on the CSMU memory assembly 1 185 with the sticky side against the CSMU cover See Figure 707 d Smooth the seal down onto the CSMU memory assembly such that the application is toward the memory interf...

Page 273: ...affixed to the bottom of the CSMU d Ensure that the flat underside surface of the CSMU is clean CSMU Cover Seal Apply RTV to seal Memory Cable Slit Figure 709 Crash Survivable Memory Unit CSMU Seal A...

Page 274: ...ould be con nected to J5 on the Acquisition Processor PWA 4 Apply Locktite 222 to the four pan head sealing screws 1 190 and insert them into the CSMU cover 1 185 NOTE Pan head sealing screws 1 190 ar...

Page 275: ...Assembly P1 J1 Acquisition Processor PWA AP Crash Survivable Memory Unit CSMU 1 185 1 175 Recorder Chassis Assembly 1 5 CSMU Mounting Seal Screws 1 190B Qty 4 Torque Sequence 75 in lb 1 2 3 4 After at...

Page 276: ...P1 J1 Acquisition Processor PWA AP Crash Survivable Memory Unit CSMU 1 185 1 175 Recorder Chassis Assembly 1 5 CSMU Mounting Seal Screws 1 190B Qty 4 Torque Sequence 75 in lb 1 2 3 4 After attached ap...

Page 277: ...sembly P1 J1 Acquisition Processor PWA AP Crash Survivable Memory Unit CSMU 1 185 1 175 Recorder Chassis Assembly 1 5 CSMU Mounting Seal Screws 1 190B Qty 4 Torque Sequence 75 in lb 1 2 3 4 After atta...

Page 278: ...r more details NOTE Once a unit has been changed to a 90 Day ULB it can not revert to a 30 Day ULB due to the Hardware MOD DOT marking NOTE Refer to the IPL effectivity column as some specific FA2100C...

Page 279: ...et 1 70 Underwater Acoustic Beacon 1 80 1 4 Hex Screw 1 75 Crash Survivable Memory Unit CSMU 1 185 Water Switch 1 4 2 3 Cross Pattern Torquing Sequence 75 in lbs Note Must use the L 3AR Conversion Kit...

Page 280: ...ainer s are not available perform the following procedures to wrap the FA2100CVR system equipment for storage 1 Wrap the recorder unit in plain wrapping paper or newspaper of sufficient thick ness to...

Page 281: ...ESSION SET OF 95 MATERIAL PACKING FOAM 2 00 IN THICK 1 2 LBS CUBIC FOOT WITH A COMPRESSION SET OF 40 FOAM TO BE BONDED TO CARDBOARD FLUTED SINGLE WALL 200 LBS CONSTRUCTION FOAM BONDED TO INSIDE FLAPS...

Page 282: ...5 and 7 ED 112 chapter 2 and Part I while conforming to the input interface required in ARINC 557 757 When the software detects a fault an CVR FAULT will be as serted immediately with no artificial d...

Page 283: ...D Crash and Fire Protection The Crash Survivable Memory Unit CSMU is designed to fully meet the 5 000 pounds crush test requirement of TSO 123a and provides impact protection for up to 3400 g s for 6...

Page 284: ...gh Temperature Short time Operating High Temperature Altitude Decompression Overpressure 4 0 4 5 1 4 5 2 4 5 1 4 5 2 4 5 3 4 6 1 4 6 2 4 6 3 Categories A2 F2 55_C 85_C 55_C 70_C 70_C 55 000 ft 55 000...

Page 285: ...ARE NOMINAL WITH 5 LBS TOLERANCE 4 OVERALL EQUIPMENT SIZE AND MOUNTING SCHEME COMPLY WITH ARINC 404 AND 404A REAR PANEL CONTAINS HOLES TO MATE WITH GUIDE PINS IN ARINC 404 MOUNTING TRAYS 5 A A 1 RECOR...

Page 286: ...NECTOR PART NUMBERS PN 063 E1072 00 CANNON DPBX 36571 59 MATING CONNECTORS CRIMP PN 063 98 01474 CANNON DPXBMA 57 33S 0001 SOLDER PN 9300 435 CANNON DPXB 57 33S 0001 4 88 04 5 5 2 4 12 4 98 04 CRASH S...

Page 287: ...Clearances 23 70 04 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 288: ...ule Obsolete L 3 Com 17TES0054 PI Memory Card Module L 3 Com 17TES0051 PI Audio Readout Cable L 3 Com 17TES0052 PI Aux Readout Cable L 3 Com Portable Interface 2 PI 2 Part Number Description Mfg 17TES...

Page 289: ...ndblaster Audigy L 3 Com 17TES0425 Speakers 110V Optional 17TES0426 Speakers 220V Optional FA2100 Software Upload Test Equipment Cable Assemblies Software ROC 7 Part Number Description Mfg 17TES0700 R...

Page 290: ...7 Recorder Interface Cable Assembly L 3 Com 17TES0058 FA2100 Software Upload Cable Assembly L 3 Com 883E4557 00 CD Soundblaster Audigy L 3 Com 17TES0426 Speakers 110V Optional 17TES0426 Speakers 220V...

Page 291: ...k L 3 Com 840E3408 04 FA2100CVR p n 2100 1025 12 CVR 120 Min Data Link Cyrillic Russian Text L 3 Com 840E4568 09 FA2100CVR p n 2100 1025 22 CVR 120 Min OMS Data Link L 3 Com 804E4568 06 FA2100CVR p n...

Page 292: ...Assembly Distribution Diskettes In the event that the Acquisition Processor PWA p n 205E1591 00 p n 205E1931 00 or p n 205E2502 10 11 requires replacement the FA2100CVR pro gram software must be loade...

Page 293: ...age of this document CVR MONITOR PLAYBACK STATUS CONTROL SPECIAL FUNCTIONS SELECT DELETE MENU AUDIO GMT ROTOR FSK PI AUX READOUT CABLE 17TES0052 TO RECORDER GSE CONNECTOR PI AUDIO READOUT CABLE 17TES0...

Page 294: ...ENU CLEAR LATCHED FAULT CLEAR FAULT LOG RELEASE FAULT GSE ON FAULT GSE OFF FAULT GSE CVR CVR CVR PLAYBACK CONTROL MENU HQ VOICE CH 1 OFF ON CH 2 OFF ON CH 3 OFF ON HQ CAM CH 4 OFF ON SQ VOICE CH 1 3 O...

Page 295: ...X XX PLAY STOP FFWD RWD END BEGIN XXXX XXXX CVR F PLAY CTRL MENU KEYPAD DUMPING FAULT LOG TO XXXX FLT This halts recording DUMPING TRACE LOG TO Note Data enclosed in parentheses does not appear on the...

Page 296: ...DISTRIBUTION DISK 840 EXXX XX Note Firmware Distribution Diskette P N will match the FA2100 Software Part Number located on the recorder s Name Plate Label TO ENHANCED PARALLEL PORT LPT 1 EPP FA2100 S...

Page 297: ...23 P1 115VAC HOT 115VAC COLD 28VDC FDR DATA IN LO 22 19 12 13 14 15 2 1 16 17 P2 GND FDR DATA OUT HI FDR DATA OUT LO ACID 7 ACID 6 MONITOR WIRE A MONITOR WIRE B P2 28VDC 115VAC P1A FDR DATA IN HI 24 T...

Page 298: ...ctions on the cover page of this document PNR 17 TES0070 SER XXXXXXXXX CICC 2 DMF MMYYYY MFR 06141 3 3 2 4 4 2 3 fT 2 IN 1 4 2 NOTE MUST BE USED WITH VER ROSE 3 2 RI 2 0 OR HIGHER SOFTWARE Figure 905...

Page 299: ...46 4 15 16 19 20 9 10 3 13 14 21 47 48 49 SER_B0_RX_HI SER_B0_RX_LO SER_A0_I0_HI SER_A0_I0_LO SER_B1_RX_HI SER_B1_RX_LO SER_C1_I0_HI SER_C1_I0_LO SER_B0_TX_HI SER_B0_TX_LO SER_B1_TX_HI SER_B1_TX_LO SE...

Page 300: ..._HI TDM_FRM_LO TDM_ADD_HI TDM_ADD_LO GND SER_FS_AP_HI SER_FS_AP_LO PRGM_VPP_SW PRGM_REC_L SER_CLK_HI SER_CLK_LO SER_DAT_AP_HI SER_DAT_AP_LO TDM_DAT_HI TDM_DAT_LO SER_DAT_PI_HI SER_DAT_PI_LO SEL_SMP FD...

Page 301: ...OUTPUT SPKRS J9 RCDR AC PWR TEST RECORDER INTERFACE UNIT RIU 17TES0410 SND IN BLUE 17TES0413 SND OUT GREEN 17TES0413 J4 J2 J1 L SPKR R SPKR YELLOW AC RED DC AC 1A DC 5A USB Note Speakers are optional...

Page 302: ...NLY P1 40 P2 34 PREAMP PWR OUT GND P1 13 P2 13 CHANNEL 3 AUDIO IN LO P1 41 P2 41 PREAMP PWR OUT HOT P1 14 P2 14 CVR IDENT PIN P1 43 P2 4 RESERVERED TEST IND P1 15 P2 15 CHANNEL 3 AUDIO IN HI P1 43 P2...

Page 303: ...wer Input Cable Assembly P N 17TES0411 144 0 1 0 IN 2X 1 00 13 I Strip and Tin 2X 2 00 13 IN 1 2 3 4 WIRE CHART BLACK OUTER WHITE INNER 5 See Note Note TRIM SHIELD EVEN WITH OUTER JACKET APPLY SLEEVIN...

Page 304: ...SWITCH 42A12 ULTRASONIC TEST SET UNDERWATER LOCATOR DEVICE MODEL 42A12 Figure 912 ULD Test Set Up C Audio Data Link Player Software The FA2100CVR Audio Data Link Player ADLP software provides a user...

Page 305: ...able Dual core CPU 2 5 GHz or greater Motherboard with EPP support compatible with PCMCIA reader below Four USB 2 0 connections 4 GB or greater memory 17 SVGA Color LCD Monitor and Graphics Adapter Mu...

Page 306: ...Ifc utility software in conjunction with the CICC 2 Interface Cable assembly p n 17TES0070 17TES0072 b Using the Portable Interface PI Unit p n 17TES0043 with Mod Dot 6 This device is used to download...

Page 307: ...P1 FA2100 CVR J1 CVR TRAY 115 VAC HOT AC COMMON COLD 27 5 VDC INPUT CHASSIS GND 115 VAC HOT AC COMMON COLD 27 5 VDC INPUT CHASSIS GND 2 3 5 6 7 8 9 12 13 14 15 16 17 2 3 5 6 7 8 9 10 12 13 14 15 16 1...

Page 308: ...ufacturing part numbers 2 PURPOSE The purpose of this Illustrated Parts List is to assist maintenance and supply personnel in requisitioning storing issuing and identifying parts to maintain the FA210...

Page 309: ...mbled or replaced Items that are riveted welded or spun over are not listed Parts made of bulk stock such as wire tape or bonding braid are also not listed Illustra tions are each assigned a figure nu...

Page 310: ...IG FOR NHA If the vendor is not L 3 Aviation Recorders the manufacturer s vendor code may be in cluded in parentheses in this column The indenture system provided by the numbers 1 through 6 in the hea...

Page 311: ...k H4 H8 Commercial and Government Entity CAGE codes formerly FSCM and or the NATO Code as applicable Ref ATA Spec 200 is listed below The CAGE code is the vendor V code listed in parentheses in the NO...

Page 312: ...on and the FAA Manufacturing Inspection District Office MIDO approved installation and assembly of all L 3AR Recorder models it is required that only the L 3AR ULB Conversion Kit p n 068E5542 00 be us...

Page 313: ...2 HR GA CVR 1 2 ATR SHORT TITANIUM CSMU W RTV 28 VDC ONLY 2100 1025 02 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY 2100 1025 12 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY CYRILLIC 2100 1025...

Page 314: ...93 C6 1 141A 2 MS24693 C7 1 141B 2 MS51957 14 1 160 4 MS51957 14 1 180 10 MS51957 14 1 125A 6 MS51957 14 1 125B 7 MS51957 28 1 25A 10 MS51957 45 1 60 4 279800024 1 225 1 2290200365 1 127 1 2529800107...

Page 315: ...191E1603 01 1 90B 1 192E1599 00 1 30 1 197E1746 00 1 220 1 205E1591 00 1 175A 1 205E1593 00 1 105A 1 205E1596 00 1 155A 1 205E1763 00 1 105B 1 205E1763 01 1 105C 1 205E1763 11 1 105F 1 205E1849 00 1...

Page 316: ...977 24 DEL 1 155U 1 205E3977 29 1 155V 1 205E3977 37 1 155W 1 2100 1010 00 1 1A 1 2100 1010 50 1 1E 1 2100 1010 51 1 1F 1 2100 1020 00 1 1B 1 2100 1020 02 1 1C 1 2100 1020 50 1 1G 1 2100 1020 51 1 1H...

Page 317: ...253E1568 07 1 185D 1 253E1568 33 1 185E 1 253E1568 38 1 185F 1 253E1568 39 1 185G 1 253E1568 40 1 185H 1 253E1568 41 1 185J 1 253E4427 33 1 185K 1 253E5675 00 1 185L 1 253E5675 11 1 185M 1 253E5675 20...

Page 318: ...n the cover page of this document B B 20 A A B B C C 190 80A 25 80B 5 10 105 110 125 155 135 141 146 175 165 15 farside 160 120 170 180 115 165 160 120 W2 W1 W3 151 A A 205 200 185 185 80C 80D Figure...

Page 319: ...e restrictions on the cover page of this document A A 50 40 45 55 60 30 70 80A B C 75 85 90 95 130 B B View View REPLACEMENT DATE 125 C C View REFERENCE ONLY 141 151 141 141 146 Figure 1 Sheet 2 of 2...

Page 320: ...PIT VOICE RECORDER FA2100 CVR ARINC 757 30 MIN GA CVR 1 2 ATR SHORT 28 VDC ONLY OBSOLETE E RF 1F 2100 1010 51 COCKPIT VOICE RECORDER FA2100 CVR ARINC 757 30 MIN GA CVR 1 2 ATR SHORT 28 VDC ONLY TITANI...

Page 321: ...S T RF 1U 2100 1220 00 COCKPIT VOICE RECORDER FA2100 CVR ARINC 757 2 HR CVR 1 2 ATR SHORT 90 DAY BEACON U RF 1V 2100 1220 02 COCKPIT VOICE RECORDER FA2100 CVR ARINC 757 2 HR CVR W FSK 1 2 ATR SHORT 90...

Page 322: ...4 00 TAPE REFLECTIVE ENGLISH FLIGHT RECORDER DO NOT OPEN 1 15 166E1595 00 TAPE REFLECTIVE FRENCH ENREGISTREUR DE VOL NE PAS OUVRIR 1 20A 075E1598 00 COVER CHASSIS SHORT A B C L M N P R T U V W Y AA AB...

Page 323: ...ETED 1 50 166E1647 00 LABEL IDENT COCKPIT VOICE RECORDER 55 111 98 00097 FASTENER HOOK NAS622 V94867 MFG NO HDH 4 2 ATTACHING PARTS 60 MS51957 45 SCREW PAN HEAD 8 32 X 1 2 V06141 2290200102 4 65 166 9...

Page 324: ...ACON ACOUSTIC UNDERWATER SUPSD BY 80D PER SB022 DUKANE V94970 ELP 362D FOR BATTERY REPLACEMENT ORDER 30 DAY BATTERY KIT 147E0305 00 A B C E F G H L M N P R T 1 80D 266E5542 00 BEACON LOCATOR UNDERWATE...

Page 325: ...05B PER ECO 9432 SUPSD BY 105F PER SB015 E F G H 1 105D 205E2503 01 PWA AIRCRAFT INTERFACE ARINC 757 4 L M N P R W Y AA AC 1 105E 205E2503 05 PWA AIRCRAFT INTERFACE ARINC 757 4 SUPSDS ITEM 105A PER SB...

Page 326: ...2290200365 SCR FLH 8 32 X1 4 T AB 1 130 MS24693 C4 SCREW FLAT HEAD 4 40 X 3 8 V06141 2290200356 4 135A 742E1619 00 CAPACITOR ASSEMBLY STORAGE SUPSD BY 135B PER SB017 1 135B 742E1619 03 CAPACITOR ASSEM...

Page 327: ...W Y AA AC 1 146B 016E5352 00 BRACKET PLASTIC CAPACITOR T AB 1 150 MS21044C04 NUT HEX SELF LOCKING 4 40 V06141 2870200019 SUPSD BY 151 PER SB016 2 151 140E4207 00 INSULATOR LATCH FC SUPSDS ITEM 150 PE...

Page 328: ...FSK SUPSDS 155C SN377 PER ECO 10365 SUPSD BY 155M PER SB009 C 1 155H 205E1849 14 Deleted 155J 205E1849 17 PWA AUDIO COMPRESSOR HIGH QUALITY ONLY SUPSD BY 155P PER SB009 L 1 155K 205E3977 10 PWA AUDIO...

Page 329: ...205E3977 37 PWA AUDIO COMPRESSOR HIGH QUALITY ONLY T AB 1 160 MS51957 14 SCREW PAN HEAD 4 40 X 5 16 V06141 2290200074 4 165A 024E1620 00 CABLE ASSEMBLY FA2100 W001 W003 SUPSD BY ITEM 165B for W001 an...

Page 330: ...PER SB006 A B C E F G H 1 175D 205E2502 11 PWA ACQUISITION PROCESSOR SUPSDS 175B 175C PER SB006 CONFIGS E F G H SUPSD BY ITEM 175F PER SB013 CONFIGS A B C SUPSD BY ITEM 175G PER SB015 A B C E F G H 1...

Page 331: ...185C 253E1568 06 MEMORY CSMU ASSEMBLY 7X32 MEG TITANIUM SUPSD BY 185H PER SB008 F 1 185D 253E1568 07 MEMORY CSMU ASSEMBLY 15X32 MEG TITANIUM SUPSD BY 185J PER SB008 H 1 185E 253E1568 33 MEMORY CSMU A...

Page 332: ...ER SB019 SUPSD BY 185P FOR B C N U V W AA AC PER SB023 A B C E G L N P R T U V W Y AA AB AC 1 185M 253E5675 11 MEMORY CSMU ASSEMBLY 2 GB NAND MEMORY MODULE TITANIUM SUPSDS 185H 185J PER SB019 SUPSD BY...

Page 333: ...MU COVER SHORT BOX SUPSDS 200A PER SB019 1 205 9030100047 LABEL ESD 1 210 147E1679 00 SHIPPING PACKAGE KIT 1 220 197E1746 00 CONTAINER SHIPPING SHORT 1 225 0279800024 CAP DUST DPX SERIES CONN 1 1 235...

Page 334: ...The document reference is online please check the correspondence between the online documentation and the printed version...

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