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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Model FA2100 CVR Rev. 15 Apr. 14/16 ECopyright 2016 by L-3 Communications. All rights reserved. No part of this manual may be repro- duced or utilized in any form or by any means, electronic or...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR GENERAL This product and related documentation must be reviewed for familiarization with safety markings and instructions before operation. This instrument was constructed in an ESD (electro–static discharge) protected environ- ment. This is because most of the semiconductor devices used in this instrument are susceptible to damage by static discharge.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–04 Use or disclosure of information on this sheet is subject Title to the restrictions on the cover page of this document. Rev. 15 Page iv Apr. 14/16 The document reference is online, please check the correspondence between the online documentation and the printed version.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR RECORD OF HIGHLIGHTS Issue Revision Date of Comments Change Revision Apr. 14/16 Page headers updated. Updated unit weights. Added obsolete unit notes. Removed A860, Cali- brated Sound Source, and ROC/5. Added PI/2. Removed Auto Test section. Updated Software tables.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR RECORD OF HIGHLIGHTS (Continued) Issue Revision Date of Comments Change Revision Dec. 01/08 Updated for Revision. Added SB011, SB012, SB013, SB014, SB015, SB 016. Changed the List of Effective Pages to reflect the Revision 07, added divider to Table of Contents.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR RECORD OF HIGHLIGHTS (Continued) Issue Revision Date of Comments Change Revision Oct. 01/04 Revised Disassembly & Assembly sections to in- clude p/n: 2100−1025−02 and associated parts. Added OMS and Data Link information in the De- scription Section for p/n: 2100−1025−02.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document. Highlights Rev. 15 Page viii Apr. 14/16 The document reference is online, please check the correspondence between the online documentation and the printed version.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HIGHLIGHTS REVISION 15 DATED Apr. 14, 2016 Pages which have been added or revised are outlined below, together with the highlights of Revision 15, dated Apr. 14, 2016. Section Page Description Title Page headers updated. List of FSB’s Page headers updated.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HIGHLIGHTS REVISION 14 DATED Jul. 13, 2015 Pages which have been added or revised are outlined below, together with the highlights of Revision 14, dated Jul. 14, 2015. Section Page Description Title Updated to include legal reference in footer. Moved legal statements from inside front cover to front cover.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Special Tools Updated to include legal reference in footer. and Test Equip- ment Illustrated Parts Updated include legal reference footer. Removed List and Schem- 2100−1020−91, 2100−1020−93, and 2100−1020−90. Added atic Diagrams 2100−1220−00, 2100−1220−02, 2100−1225−22, 2100−1226−02, 2100−1225−24, 2100−1227−02, and 2100−1925−22.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HIGHLIGHTS REVISION 13 DATED December 9, 2013 Pages which have been added or revised are outlined below, together with the highlights of Revision 13, dated December 9, 2013. Section Page Description Front Matter LOEP & TOC Changed the List of Effective Pages to reflect Revision 13 changes.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HIGHLIGHTS REVISION 12 DATED July 3, 2013 Pages which have been added or revised are outlined below, together with the highlights of Revision 12, dated July 3, 2013. Section Page Description Front Matter LOEP & Changed the List of Effective Pages to reflect Revision 12 changes.
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NAND memory to part number matrix. Adds description of PI/2. Added Section 13−16, 21, description of acquisition processor 205E2502−34. Removed descrip- 22, 23, 25, tion of FA2100 CVR p/n: S2100−1020−91 29, 30−34, 35, 36, 43, 48−56, 64, Testing & Fault...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HIGHLIGHTS REVISION 10 DATED Jun. 15, 2012 Pages which have been added or revised are outlined below, together with the highlights of Revision 10, dated Jun. 15, 2012. Section Page Description List of FSB’s xix −...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HIGHLIGHTS REVISION 09 DATED Apr. 30, 2010 Pages which have been added or revised are outlined below, together with the highlights of Revision 09, dated Apr. 30, 2010. Section Page Description i − ii Title Updated for Revision 9.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HIGHLIGHTS REVISION 08 DATED Jul. 30, 2009 Pages which have been added or revised are outlined below, together with the highlights of Revision 08, dated Jul. 30, 2009 Section Page Description i − ii Title Updated for Revision 8.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HIGHLIGHTS REVISION 07 DATED DECEMBER 01, 2008 Pages which have been added or revised are outlined below, together with the highlights of Revision 07, dated December 01, 2008 Section Page Description i − ii Title Updated for Revision.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HIGHLIGHTS REVISION 06 DATED May 01, 2007 Pages which have been added or revised are outlined below, together with the highlights of Revision 06, dated May 01/2007. Section Page Description i − ii Title Updated for Revision.
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101, 105, 112 Updated test section/procedure to include p/n: 2100−1025−02, Isolation 114−118, 122, 2−hour HQ only recorder. Updated FA2100 CVR test bench setup re- 124−127, quirements and Table 1. Recommeded Standard Test Equipment. 141−142 Added Data Link Check to Table 102. Operational Test Procedure.
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Updated the Configuration Matrix, Numerical Index, Figure 1., and List & the IPL to include p/n: 2100−1025−02 and associated parts. Added Schematic new Acquistion Processor board for the FA2100 CVR. Diagrams 23–70–04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HIGHLIGHTS REVISION 04 DATED JAN. 01, 2003 Pages which have been added or revised are outlined below, together with the highlights of Revision 04, dated Feb. 01/2003. Section Page Description 1 − 2 Title Updated for Revision.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HIGHLIGHTS REVISION 03 DATED MAR. 01, 2001 Pages which have been added or revised are outlined below, together with the highlights of Revision 03, dated Mar. 01/2001. Section Page Description Title 1−2 Updated for Revision. Front Matter LOEP &...
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Compressor PWA. Updated numerical index and part number list to Diagrams reflect shift in item numbers for all FA2100 CVR models. Updated nu- merical index to include ULDs. Updated item numbers for Audio Com- pressor PWA and ULDs. Updated include correct RTCA / DO−178B level.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HIGHLIGHTS REVISION 01 DATED FEB. 01, 2000 Pages which have been added or revised are outlined below, together with the highlights of Revision 01, dated Feb. 01/2000. Section Page Description Title 1−2 Updated for the Revision and the Copyright year. List of FSB’s Updated for FSB002 (23−70−04−02).
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document. Highlights Rev. 15 Page xxvi Apr. 14/16 The document reference is online, please check the correspondence between the online documentation and the printed version.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR RECORD OF REVISIONS REV. INSERTION REV. INSERTION REV. INSERTION DATE DATE DATE Apr. 14/16 Jul. 13/15 Dec. 09/13 Jul. 03/13 May 21/13 Jun. 15/12 Apr. 30/10 Jul. 30/09 Dec. 01/08 May 01/07 Oct. 01/04 Jan.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–04 Record of Revisions Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document. Rev. 15 Page xxviii Apr.
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COMPONENT MAINTENANCE MANUAL FA2100CVR SERVICE BULLETIN LIST SERVICE BULLETIN DATE EFFECTIVITY DESCRIPTION FA2100 CVR Sep. 08/98 P/N: 2100-1010-00 Modification of Aircraft Interface PWA, FSB001 P/N: 2100-1020-00 p/n: 205E1593-00 to prevent erroneous 23−70−04−01 test tone activation due excessive noise environment. MOD-DOT #1 FA2100 CVR Apr.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR SERVICE BULLETIN LIST FA2100 CVR Dec. 15/05 P/N: 2100-1020-( ) This modification includes replacing the exist- ing Audio Compressor PWA, p/n: FSB009 P/N: 2100-1020-( ) 205E1596−00, 205E1849−00, 205E1849−10, 23−70−04−09 205E1849−02, 205E1849−03, 205E1849−13, 205E1849−04 or 205E1849−14 with a re- placement Audio Compressor PWA, p/n: 205E3977−10, 205E3977−12, 205E3977−13...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–04 Service Bulletin Use or disclosure of information on this sheet is subject Rev. 15 Page xxxii to the restrictions on the cover page of this document. Apr. 14/16 The document reference is online, please check the correspondence between the online documentation and the printed version.
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AVIATION RECORDERS L–3 COMMUNICATIONS, AVIATION RECORDERS FIELD SERVICE BULLETIN / SERVICE INFORMATION LETTER EXPORT CONTROL STATEMENT The technical information about recorder products/software are being exported from the United States in accordance with the Export Administration Regulations ECCN 9E991, No License Required. Diversion contrary to U.S. law is prohibited. In accordance with U.S. Law (31 CFR Part 746, and Supplement No.1 to Part 774, and CFR Part 550) resale/re–ex- port or transfer to the countries identified therein is prohibited without the prior written con- sent of the U.S.
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AVIATION RECORDERS 100 Cattlemen Rd., Sarasota, FL 34232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN MODEL FA2100 COCKPIT VOICE AND DATA RECORDER INTRODUCTION OF SOFTWARE REVISION 07 & 08 Date: May 02, 2013 BULLETIN NO. FA2100CVDR SB017 R1 PLANNING INFORMATION Effectivity L−3 Communications, Aviation Recorders, Model FA2100 Cockpit Voice &...
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AVIATION RECORDERS 100 Cattlemen Rd., Sarasota, FL 24232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN FA2100CVDR BULLETIN NO. FA2100CVDR SB017 R1 Compliance This is a recommended modification for units in the field and may be incorpo- rated the next time the recorder is in the shop. Approval This service bulletin contains no modification information that revises the ap- proved configuration and therefore does not require governmental or other...
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AVIATION RECORDERS 100 Cattlemen Rd., Sarasota, FL 24232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN FA2100CVDR BULLETIN NO. FA2100CVDR SB017 R1 MATERIAL INFORMATION Material Price and Availability This modification can be completed in one of the following ways: 1) An L-3AR Product Support Engineer can provide on−site support; or 2) The FA2100CVDR may be shipped to the L-3AR repair station;...
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AVIATION RECORDERS 100 Cattlemen Rd., Sarasota, FL 24232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN FA2100CVDR BULLETIN NO. FA2100CVDR SB017 R1 Table 2. Material Information/Pricing List Keyword Quantity Part Price Delivery Number U.S.D. 2100-3083−00 Recorder Software 1 ea. 840E2261−07 30 Days 2100-3083−10 Recorder Software 1 ea.
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AVIATION RECORDERS 100 Cattlemen Rd., Sarasota, FL 24232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN FA2100CVDR BULLETIN NO. FA2100CVDR SB017 R1 Table 3. Required Tooling and Availability Keyword Quantity Part Number Price Delivery U.S.D. Read Out Center 7 (ROC/7) 1 ea. 17TES0700 48,000 90 Days...
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AVIATION RECORDERS 100 Cattlemen Rd., Sarasota, FL 24232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN FA2100CVDR BULLETIN NO. FA2100CVDR SB017 R1 III. ACCOMPLISHMENT INSTRUCTIONS CAUTION: ELECTROSTATIC DISCHARGE (ESD) WARNING: Since the FA2100CVDR contains electrostatic sensitive devices, it must be modified at a workstation equipped for such devices.
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AVIATION RECORDERS 100 Cattlemen Rd., Sarasota, FL 24232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN FA2100CVDR BULLETIN NO. FA2100CVDR SB017 R1 FA2100 Software Upload Procedure (1) Connect the J1A rear connector of the FA2100CVDR to the ROC/6 or ROC/7 using the Recorder Interface (RI) Cable Assy, P/N 17TES0057. (2) Connect either 115 Vac/400 Hz, or +28 Vdc to the pig−tail connections of the Recorder Interface (RI) Cable Assy.
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AVIATION RECORDERS 100 Cattlemen Rd., Sarasota, FL 24232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN FA2100CVDR BULLETIN NO. FA2100CVDR SB017 R1 (14) Observe the progress window and verify that a status pop−up window ap- pears stating that the FA2100 loaded successfully. Note: If the load procedure was unsuccessful, remove the CD from the D:\ drive, exit the CICC loader program, turn OFF power to the FA2100...
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AVIATION RECORDERS 100 Cattlemen Rd., Sarasota, FL 24232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN FA2100CVDR BULLETIN NO. FA2100CVDR SB017 R1 (3) At the Windows desktop, shut down the Recorder Interface (RI) if not already shutdown from previous steps by right clicking on the RI Icon in the Windows System Icon Tray at the bottom right of the screen.
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AVIATION RECORDERS 100 Cattlemen Rd., Sarasota, FL 24232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN FA2100CVDR BULLETIN NO. FA2100CVDR SB017 R1 Table 4. Software Revision Marking Recorder Software Revision 2100−3083−00 2100−3083−10 2100−3083−50 Material Information Table 5. Material Information/Pricing List Keyword Quantity Part Price Delivery...
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AVIATION RECORDERS L–3 COMMUNICATIONS, AVIATION RECORDERS FIELD SERVICE BULLETIN / SERVICE INFORMATION LETTER EXPORT CONTROL STATEMENT The technical information about recorder products/software are being exported from the United States in accordance with the Export Administration Regulations ECCN 9E991, No License Required. Diversion contrary to U.S. law is prohibited. In accordance with U.S. Law (31 CFR Part 746, and Supplement No.1 to Part 774, and CFR Part 550) resale/re–ex- port or transfer to the countries identified therein is prohibited without the prior written con- sent of the U.S.
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As this is a process change only, not affecting any form, fit or function aspects of the Model FA2100 CVR, no external modification identification will be implemented. However, through L-3 AR’s internal serialization and as built manufacturing system, we are tracking all Serial Numbers that have the new process CCA’s incorporated.
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AVIATION RECORDERS L–3 COMMUNICATIONS, AVIATION RECORDERS FIELD SERVICE BULLETIN / SERVICE INFORMATION LETTER EXPORT CONTROL STATEMENT The technical information about recorder products/software are being exported from the United States in accordance with the Export Administration Regulations ECCN 9E991, No License Required. Diversion contrary to U.S. law is prohibited. In accordance with U.S. Law (31 CFR Part 746, and Supplement No.1 to Part 774, and CFR Part 550) resale/re–ex- port or transfer to the countries identified therein is prohibited without the prior written con- sent of the U.S.
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AVIATION RECORDERS 100 Cattlemen Road, Sarasota, Florida 34232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN PORTABLE INTERFACE (PI) UNIT MOD DOT 9 REQUIRED FOR NAND RECORDERS Date: September 19, 2013 BULLETIN NO. PI SB005 Rev. 1 PLANNING INFORMATION Effectivity Portable Interface (PI) Unit, manufactured by L-3 Communications, part number 17TES0043.
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AVIATION RECORDERS 100 Cattlemen Road, Sarasota, Florida 34232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN PORTABLE INTERFACE (PI) UNIT MOD DOT 9 REQUIRED FOR NAND RECORDERS Date: September 19, 2013 BULLETIN NO. PI SB005 Rev. 1 Table 1. Recorder Mod Dot Status with NAND Memory Recorder Type Mod Dot Number Mod Dot 14...
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AVIATION RECORDERS 100 Cattlemen Road, Sarasota, Florida 34232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN PORTABLE INTERFACE (PI) UNIT MOD DOT 9 REQUIRED FOR NAND RECORDERS Date: September 4, 2013 BULLETIN NO. PI SB005 Manpower Not applicable. Material Cost and Availability Mod Dot 9 can be installed by L−3AR Product Support Engineers, or at the factory repair station.
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AVIATION RECORDERS 100 Cattlemen Road, Sarasota, Florida 34232 Telephone: 941-371-0811 Facsimile: 941-377-5591 SERVICE BULLETIN PORTABLE INTERFACE (PI) UNIT MOD DOT 9 REQUIRED FOR NAND RECORDERS Date: September 4, 2013 BULLETIN NO. PI SB005 III. MATERIAL INFORMATION L−3 Aviation Recorders will install this Service Bulletin (Portable Interface Mod.
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The document reference is online, please check the correspondence between the online documentation and the printed version.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR LIST OF EFFECTIVE PAGES Section Page Date Section Page Date Title Page Rev. 15 xxxiv Apr. 14/16 Rev. 15 xxxv Apr. 14/16 Rev. 15 Apr. 14/16 Rev. 15 xxxvi Apr. 14/16 Rev. 15 Apr. 14/16 Rev.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR TABLE OF CONTENTS (Cont.) Audio Compressor PWA (AC) Removal (See Figure 307 or IPL Figure 1, Item 155) ......Aircraft Interface PWA (AI) Removal (See Figure 307 or IPL Figure 1, Item 105) .
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR TABLE OF CONTENTS (Cont.) Audio Compressor PWA (AC) Installation (See Figure 703 or IPL Figure 1, Item 155) ......Chassis Cover Installation (See Figure 704 and Figure 706 or IPL Figure 1, Item 20A/B) .
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR TABLE OF CONTENTS (Cont.) ILLUSTRATED PARTS LIST GENERAL ..............1001 PURPOSE .
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR INTRODUCTION 1. GENERAL This Component Maintenance Manual (CMM) documents the operation of and suggested maintenance for the Model FA2100 Cockpit Voice Recorder, herein after referred to as the FA2100CVR. The FA2100CVR meets the performance requirements of ED-56A, while complying with the interface requirements of ARINC 557/757 cockpit voice input data including Rotor Speed and GMT interfaces.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Line Replaceable Unit MTBF Mean Time Between Failures Onboard Maintenance System Personal Computer PCMCIA Personal Computer Memory Card International Association (now known as PC Card) Portable Interface printed wiring assembly power REC LVL Record Level Recorder Interface Unit Read−Out Center ROSE...
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COMPONENT MAINTENANCE MANUAL FA2100CVR however only the FA2100CVR P/Ns:2100−1025/1026/1027−XX, supports OMS in soft- ware. Only FA2100 CVR P/N: 2100−1025/1026/1027−XX, supports RIPS Monitoring sta- tus and Datalink. 5. MAINTENANCE PHILOSOPHY The Model FA2100 Solid-State CVR Recorder is considered an “ON CONDITION LRU”...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR TESTING AND TROUBLESHOOTING Sections 100 and 200 contains specific checks and tests required to determine the operational condition of a unit that has been removed from service. Also included in the section are tables of required test equipment, test set-up data, procedures, and test parameters.
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Recorder Interface Unit (RIU) to test and download from the FA2100CVR. ILLUSTRATED PARTS LIST This section contains parts location diagrams and parts listings for all versions of the Model FA2100 CVR, 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 engineering source material.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Table 1. Shop Verification Procedure Chapter Date of Verification Testing & Fault Isolation Mar. 25/13 Automatic Testing Mar. 25/13 Disassembly Mar. 18/13 Assembly Mar. 18/13 Note: Contact L-3 Aviation Recorders, to verify this date sensitive information when using this manual to develop other documentation.
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Rotor Speed Encoder (RSE) and Greenwich Mean Time (GMT) inter- face. The FA2100 CVR recorder is designed as a maintenance free recorder. There is no periodic or scheduled maintenance required for this recorder. It is considered an “install and forget it box.”...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR HARDWARE AND SOFTWARE MODIFICATIONS CSMU GSE CONNECTOR (BEHIND DUST COVER) Figure 1. Model FA2100 Cockpit Voice Recorder (FA2100CVR) 2. FA2100 CONFIGURATIONS The current configurations of the FA2100CVR’s are listed in Table 2 below, and with its specific part number in the IPL Section Figure 1, Item 1A through Item 1AB.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Table 2. FA2100 CVR Descriptions Figure Weight! Part Number Description (lbs) Reference 2100-1010-00 ARINC 757, 30 MIN. CVR, 1/2 ATR SHORT * 10.0.5 Figure 1 2100-1010-50 ARINC 757, 30 MIN. GA CVR, 1/2 ATR SHORT, 28 VDC ONLY * 9.5.5...
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Interconnection between the recorder and the control unit is accom- plished using aircraft wiring. The FA2100 CVR is connected to the aircraft wiring via a 57-pin, DPXB-style connector. The Aircraft Interface PWA provides for all input and out- put signals.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Circuit Boards The FA2100CVR electronics contain all the necessary power supplies and circuitry to input, record, monitor and playback data. In addition, circuitry to perform self– test functions and provide signals to the appropriate status indicators is also inte- grated into the FA2100CVR electronics.
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ASSEMBLY RIPS Status Monitoring. 2100-1025-22/-24 (CRASH PROTECTED SOLID STATE MEMORY) & 2100-1026-XX only. Figure 2. Model FA2100 CVR, (2100‐1010‐00, 2100‐1X20‐00/02, 2100‐1X25‐XX, 2100‐1X26‐XX and 2100‐1X27‐XX) Functional System Block Diagram 23–70–04 Use or disclosure of information on this sheet is subject Description and Operation to the restrictions on the cover page of this document.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR ERASE A ERASE C AIRCRAFT WIRING INTERLOCKS PUSH TO TEST (LANDING GEAR MUST BE DOWN AND BRAKE LOCKED TO ALLOW MEMORY TO BE ERASED) GEAR BRAKE COCKPIT AREA MICROPHONE (CAM) RECORD ON CHANNEL 4 FA2100 GACVR AUDIO OUT CHANNEL 3...
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Control Unit Operating Power and Monitor Audio Signals The FA2100 CVR provides the control unit with +18 Vdc operating power, monitor audio to the headset jack, and a TEST indicator signal. Refer to Figure 4, an Audio Output channel for test monitoring provides a combina- tion of four High Quality (for 30-minute recorders) or two Standard Quality (for 120-minute recorders and 2100−1020−XX pre MOD−DOT #7) or four High Quality...
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CH – Channel HQ – High Quality SQ – Standard Quality Figure 4. (Sheet 1 of 2) Model FA2100 CVR, 30‐Minute and 120‐Minute Audio Monitor Schemes 23–70–04 Use or disclosure of information on this sheet is subject Description and Operation to the restrictions on the cover page of this document.
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ATA 23–70–05, Part Number 165E1747-00. The +18 Vdc is a short-circuit protected 30 mA line. All control units provide the FA2100 CVR with three control signals: Erase “A”, Erase “C”, and Push-To-Test. The Erase “A” and Erase “C” signals are used to initiate a bulk erasure of the crash protected solid-state memory.
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Refer to Paragraph 5 for detailed pin-outs of the rear interface connector. In the −02 FSK version of the FA2100 CVR, CH 1 or CH 3 may have an FSK GMT input applied along with the standard audio signal.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Data Recording Storage Refer to Figure 5 for a diagram of the FA2100CVR recording schemes used in the 30-minute and 120-minute recorders and Table 1 for a breakdown of the recording durations for each of the High Quality and Standard Quality combined channels. The audio received from the cockpit area microphone (CAM) is applied to the CAM input channel (CH4).
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CH – Channel HQ – High Quality SQ – Standard Quality Figure 5. (Sheet 1 of 2) Model FA2100 CVR, 30-Minute and 120-Minute Recording Schemes 23–70–04 Use or disclosure of information on this sheet is subject Description and Operation to the restrictions on the cover page of this document.
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OMS − On board Maintenance System* * P/N 2100−1025/1026−XX only Figure 5. (Sheet 2 of 2) Model FA2100 CVR, 30-Minute and 120-Minute Recording Schemes Output Audio Quality The FA2100CVR’s audio quality meets or exceeds the audio quality specified in Chapter 3 of ED–56A and Part I of ED−112. Specifically, the Reference Signal is 1-kHz at 3 Vrms for the voice channels, and 1-kHz at 2 Vrms for the CAM channel.
Audio data. In the case of the 30-minute Model FA2100 CVR, p/n: 2100–1010–( ), 30 minutes of GMT/RSE data is stored. In the case of the 120-minute Model FA2100 CVR, p/n: 2100–1X2X–( ), a full 120 min- utes of GMT/RSE data is stored.
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OMS computer four times per second. When the recorder is in Interactive mode, the OMS computer can request the status of the recorder through a series of menus. The OMS feature can be found on the FA2100 CVR p/n: 2100−1X25/1X26/1X27−( ) only.
Data Link system will continue to send Aloha mes- sages until the recorder’s status changes. The Data Link feature can be found on the FA2100 CVR p/n: 2100−1X25/1X26/1X27−( ) only. For p/n 2100−1X25/1X26/1X27−XX CVRs, the Audio and Data Link Playback (ADPL) soft- ware may be used to download and analyze the audio data.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Data Retrieval Incorporated into the FA2100CVR aircraft installation is a “Record On” jumper. Dur- ing bench test of the FA2100CVR, removal of the jumper disables the record func- tion of the recorder, thereby allowing playback of the recorded data. While in the Playback mode, replaying of recorded data is controlled by the Portable Interface (PI) Unit p/n: 17TES0043 or Portable Interface/2 (PI/2) Unit P/N: 17TES0062.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Data Reproduction A standard cassette, reel-to-reel tape, or digital audio tape recorder can be used to produce a high fidelity copy of the Model FA2100CVR recorded data. To do so, the inputs of the copy recorder are connected to any one of the output RCA phono jacks located on the Portable Interface (PI) Unit’s PI Audio Read-out Cable, p/n 17TES0051.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CVR FAULT LIGHT REAL TIME OPEN = FAULT GND = NO FAULT ANNUNCIATOR PANEL RELAY ENERGIZE = OPEN (NO CVR FAULT) DE-ENGERIZED = GRN (CVR FAULT) Figure 6. GACVR Fault Circuit for Pin 23 Crash Survivable Memory Unit The Crash Survivable Memory Unit (CSMU) is the environmentally hardened memory storage assembly of the Model FA2100.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR The Model S151/S161, Model S152/S162, and the Model S251/S261 Control Units are for use in FA2100CVR System installations that comply with ARINC Characteris- tic 757, TSO−C123a and EUROCAE ED–56A. The Model S151/S161, and Model S251/S261 Control Units house the Microphone Preamplifier PWA, and the TEST and Bulk ERASE switches.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR O. Ground Support Equipment Interface The interface to the Ground Support Equipment (GSE) is via a bi-directional high- speed serial link available at the front-panel GSE connector. A facility for retrieving the stored data from the CSMU to Ground Support Equip- ment, GSE, is provided for high-speed downloading of the voice data.
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,...
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR (12) RTCA DO–160C Environmental Conditions and Test Procedures for Airborne Equipment (13) RTCA DO–178B Software Considerations in Airborne Systems and Equipment Certification to Level D The Model FA2100CVR meets the performance requirements of ED-56A, chapters 2, 3, 4, and 5, ED–55 chapter 7 and ED−112, chapter 2, and Part I, while conforming to the in- put interface required in ARINC 557/757/757A.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR The FA2100CVR is connected to its control unit or preamplifier 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 Unit &...
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ON WHEELS For GACVR versions refer to Figure 9. Wiring for all CVR's except for 2100-1025-XX and 2100-1026-XX, are compliant to ARINC 757-3. Figure 7. Interwiring Diagram, Recorder FA2100 CVR (2100-1010-00, 2100-1X20-00/-02, & 2100-1X25/1X26-XX) 23–70–04 Use or disclosure of information on this sheet is subject Description and Operation to the restrictions on the cover page of this document.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Notes for Figure 7: Recommended minimum wire size is #22: #24 is electrically permissible except for power leads, where #18 wire is desirable on long-runs (pins 2, 3, 9, & 17) Wire resistance should not exceed 1 ohm for power leads and should not exceed 5 ohms for signal leads. All wiring should be MIL–W–22759 or MIL–C–27500.
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VOICE ERASE ”C” MIC LOW (SHEILD)) BRAKE GEAR BULK ERASE INTERLOCK (TYPICAL) Figure 8. ARINC 757A Interwiring Diagram, Recorder FA2100 CVR (2100-1X27-XX) 23–70–04 Use or disclosure of information on this sheet is subject Description and Operation to the restrictions on the cover page of this document.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Notes for Figure 9: Recommended minimum wire size is #22; however, wire size #24 is electrically permiss- ible except for long−run power leads where #18 wire is recommended (pins 3, 9, & 17). Wire resistance should not exceed 1 ohm for DC power leads and should not exceed 5 ohms for other leads.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR STANDARD INTERWIRING FOR GACVR INSTALLATIONS TO DC POWER IN AUDIO OUT LO 28 VDC AUDIO OUT HI AMPS RECORD ON B RECORD ON A CONTROL PANEL* +28 VDC POWER IN AUDIO JACK LO STOP RECORDING AUDIO JACK HI ATTENUATION COMMON PUSH TO TEST...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Notes for Figure 9 Recommended minimum wire size is #22; however, wire size #24 is electrically per- missible except for long-run power leads where #18 wire is recommended (pins 9 & Wire resistance should not exceed 1 ohm for power leads and should not ex- ceed 5 ohms for signal leads.
PWAs. The software level theory describes the modes of operation of the recorder software. MODEL FA2100 CVR SYSTEM THEORY OF OPERATION The ARINC 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 (CSMU).
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Aircraft Interface (AI) PWA The Aircraft Interface (AI) PWA mounts within the rear of the Cockpit Voice Recorder chassis and provides the interface between the aircraft and the Cockpit Voice Re- corder’s Audio Compressor (AC) and Acquisition Processor (AP) functions. The Air- craft Interface PWA also includes the storage power supply and provides RF filtering and lightning protection for all input and output signals that interface with the aircraft.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR * Only for P/N 205E2503−01 and 205E1763−08. The ARINC 557/757 Aircraft Interface provides output signal conditioning for: CVR Fault Audio Out for Monitoring at the Control Unit headset. Data Link and OMS (Only for P/N: 205E2503−01 and 205E1763−08) The Aircraft Interface also includes the storage supply portion of the power supply.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Table 3. (Cont.) ARINC 557/757/757A Aircraft Interface Signals Signal Name Description GMT IN GMT input signal. ARINC 429 format. Low Speed (12.5 kbps). (A, B) (429) The 205E1849−00 and 205E1849−03 Audio Compressor cards provide both 150 (1 sec resolution) and 125 (0.1 min. resolu- tion) for 429 GMT inputs.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Table 4. Aircraft Interface PWA to Audio Compressor PWA Interface Signals Signal Name Description CH 1 IN HI Single ended, Channel 1 audio output to Audio Compressor. Signal level is 2 Vrms $10% with reference signal applied to CVR Channel 1 input.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR ARINC 557/757A Aircraft Interface Signals Table 5 lists the signal interfaces between the FA2100 Aircraft Interface PWA and Acquisition Processor PWA. Table 5. Aircraft Interface PWA to Acquisition Processor PWA Interface Signals Signal Name Description 36.6 $2 volt dc output provides up to 16 watts, maximum, to the 39VDC...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR The Audio Compressor PWA receives conditioned audio, GMT, rotor speed, and discrete command/control data from the AI concurrently. Audio and ARINC 429 in- put data are processed by the AC and formatted into 16–bit wide words for serial Time Division Multiplexed (TDM) Bus transmission to the AP.
The Acquisition Processor PWA actually consists of two separate processors: the Store Manager Processor (SMP) and the Flight Data Processor (FDP). However, in the FA2100 CVR configuration the SMP is the only processor functioning, with the exception of p/n: 205E2502−14 since the Data Link signals utilize the FDP proces- 23–70–04...
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR sor. The Store Manager Processor gathers audio data from the Audio Compressor, packetizes the data, and saves the data into the flash memory contained in the Crash Survivable Memory Unit (CSMU). Table 7. Acquisition Processor (AP) PWA Current Configuration Where Used Acquisition Processor Model Effectivity Notes...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Test mode as well as operating voltages of $5 V are also routed through this interface. Crash Survivable Memory Unit The Crash Survivable Memory Unit (CSMU) Interface consists mainly of the buffered high speed serial bus of the SMP. Command and data messages are transmitted by the Acquisition Processor (AP) to the CSMU.
As defined in RTCA/DO–178B, the Criticality Category of the Model FA2100CVR is classi- fied as Minor. Accordingly, the software in the FA2100 CVR will comply with the Level D requirements of RTCA/DO–178B. Store Manager Processor Software Organization The SMP software is organized as a multi−tasking environment with individual mod-...
FA2100CVR Software Operating States The FA2100 CVR software operates in several states which include initialization, re- cording, power down, data playback, bulk erase, and push to test. Of these states, the CVR operates in the record state for most of its power on time. Each of the states will be discussed in the following sections.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR found, the indices are set to a pre−determined top of memory location. Once the indices are restored, the CVR is ready to transition to the record state. Record State Figure 11 shows the word partition structure for the 2-Hr FA2100CVR, refer to this figure for the following description.
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(1) 36‐Word Special Frame per 4 Superframes * Block headers & Block boundaries Not Shown Figure 11. 2–Hr FA2100 CVR (pre MOD−DOT #7) Word Partition Structure Streams 23–70–04 Use or disclosure of information on this sheet is subject Description and Operation to the restrictions on the cover page of this document.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR The CVR Executive manages the storage of received channel specific au- dio data packets to the CSMU. The CVR Executive examines the packet, determines which memory partition should be addressed, and sends the complete packet to the Flash Manager for storage in the CSMU. The CVR Executive task also manages the erase look−ahead function to insure that there is always a new erased block of flash memory available for impend- ing memory write operations.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR dio Reconstructer task is also shutdown to free resources and CPU band- width. The Audio Channelizer task receives the shutdown message, but contin- ues to process any 8 ms blocks of audio data that may be in its input queue.
Data Structures The primary data structure utilized in the FA2100 CVR is the organization of the crash protected flash memory contained in the CSMU. The partitioning of the...
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2100-1025-( ), which is a SQC = Standard Quality CAM 2-hour HQ only recorder. Figure 12. 2–Hr FA2100 CVR Memory Structure 23–70–04 Use or disclosure of information on this sheet is subject Description and Operation to the restrictions on the cover page of this document.
Kwords long. An erase block is the smallest physical block of a flash memory device that can be erased at one time. The FA2100 CVR software partitions each 32 Mb Erase Block into an eight word header followed by 910 logical packets of 36 words each. These packets are the fundamental units which are built and stored into the CSMU.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Any detected fault condition asserts the fault output from the CVR. Some faults are “latched’ meaning that the fault indication will continue to be asserted (regardless of power cycling) until it is cleared by maintenance action. Other faults may relent, al- lowing normal CVR operation to continue.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 8. SOFTWARE CONSIDERATIONS (P/NS: 2100−1X25/1X26/1X27−( ) and 2100−1X20−( ) MOD−DOT#7) Equipment Environment The hardware environment for the 2100−1X25/1X26/1X27−( ) and 2100−1X20−( ) MOD−DOT #7 Solid State Cockpit Voice Recorder is composed of a pair of TMS320C50 Digital Signal Processors (DSPs), an external program memory for each DSP that contains the executable program code, one external NVRAM for non−crash critical data storage and a flash memory array located in a Crash Surviv-...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Channel Monitor/Test Select Output CVR Fault Output GMT Input Push−To−Test Input Record On Input Rotor Speed Input Stop Record Input Test Good Output The system level interfaces used by all configurations are: Power In Power Return GSE Input GSE Output...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR The fault signal is indicated for any of the following (as per ED112 §2−1.4.2): failure of the audio or digital interface and processing equipment. failure of the recording medium and/or drive mechanism. failure of the recorder to store the information in the storage medium as shown by checks fo the recorded material including, if reasonably practi- cable, correct correspondence with the inputs.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Push−to−Test (PTT) Functionality The Push−to−Test functionality (already implemented on existing aircraft and stan- dardized in ARINC 757A specification) is used to provide the flight crew with the abil- ity to quickly confirm good serviceability of the CVR before flight as required by the applicable regulation.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR G. Recorder Synchronization The FA2100CVR equipment is designed to be able to record time code from an ARINC 429 in priority and later FSK source (the frequencies used are 3607Hz +/− 30Hz and 4193Hz +/− 30Hz), depending on the source used on the aircraft. For Models FA2100CVR, p/n: 2100−1X20−02/2100−1X25−( ), 2100−1X26−( ), and 2100−1X27−( ) the recorder automatically detects which source is received, ac- quires the time data, and stores it into memory.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CVR RIPS status monitoring (P/N: 2100−1X25−22/−24, 2100−1X26−( ), and 2100−1X27−( ) only) The Recorder Independent Power Supply (RIPS) is an ON−CONDITION LRU de- signed to provide 10 minutes CVR backup power as per ARINC Characteristic 777−1.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR RIPS Fault The CVR will use Pin 29 to receive the RIPS Failure Status Discrete output. This discrete input is presently assigned in ARINC 757A as FDR Rate A for combination recorder applications. This discrete input is not presently utilized by the pre RIPS CVR software.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR moved from an aircraft with RIPS and re−installed on an aircraft without RIPS, it is possible that previous flight leg RIPS fault information, stored in the CVR fault log while installed on the aircraft with RIPS, will be displayed. This is not considered a likely event since when a CVR is removed from an aircraft it is re- quired to pass a ”return to service”...
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR As an additional capability, this CVR also monitors the status of an attached Record- er Independent Power Supply, if present, and includes that status with the OMS out- put reporting. The RIPS status is monitored using the CVR input pins listed in Table 1.2: Table 12.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CVR Recording Failure (Record Enable) 0: OK 1 : Failure RIPS Maintenance Status (Battery) (pin 38) 0: No Maint. 1 : Maint. Req. RIPS Active Status (pin 10) 0: Not Active 1 : RIPS Active RIPS Presence Status (Pin 42) 0: Not Pres.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Like any other internal CVR fault, this audio circuit failure will be reported using: the Label 350 output Bit 11, the CVR Fault Status discrete output, and the Push−to−Test results. If an audio input circuit failure occurs after a successful Push−to−Test oper- ation, it will not be detected, or reported, until the next Push−to−Test is initiated.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CVR Record Enable CVR “Record Enable” jumper status (pins 7/8). (Pins 7/8) RIPS Maintenance Status RIPS Maintenance Status as reported on pin 38 input (Battery) (Pin 38) (if present). RIPS Active Status (Pin 10) RIPS Active Status as reported on pin 10 input (if present).
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Not used 2531 Second character of part number Parity d. Part Number (continued) Bit No Function Status 18 Label 354 11101100 915 Third character of part number Not used 1723 Fourth character of part number Not used 2531 Fifth character of part number...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR h. Serial Number (continued) Bit No Function Status 18 Label 354 11101100 915 Second character of serial number Not used 1723 Third character of serial number Not used 2531 Fourth character of serial number Parity Serial Number (continued) Bit No...
12 can be ignored. 10. CVR DATALINK INPUT INTERFACE The FA2100 CVR, part numbers 2100−1X25−02/−22/−24 and 2100−1X26−02, was developed specifically to satisfy recent requirements for Controller Pilot DataLink Communications (CPDLC or “DataLink”) recording in addition to the two hour audio recording capability.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR DataLink Valid Discrete input (Pin 56) DataLink Fault Discrete output (Pin 31) All Label 270, 276, 157, and 156 words input on the CVR DataLink interface will be recorded to crash protected memory regardless of the parity (good or bad). Like- wise, these inputs, if present, will be recorded regardless of the state of the DataLink Valid discrete input (Pin 56).
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Williamsburg V3 protocol payload protocol ARINC 619 Header payload Common Header Header Payload = one of the following styles CPDLC Header Length ASCII or Unaligned PER Message ADS−C Header Length ASCII or Bit Encoded Message AFN, ARINC 623 DC and ARINC 623 OC 2,3,5 Length...
270 heartbeat is detected, and DataLink Valid (Pin 56) is not asserted. Williamsburg Bit−Oriented Protocol Version Support It should be noted that the FA2100 CVR does not currently support Williamsburg Version 1 protocol or a low speed ARINC 429 interface for input of DataLink informa- tion.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR DataLink Memory Capacity The CVR is currently configured with 32 Mbytes of dedicated DataLink recording memory. This provides for a recording duration far in excess of the existing two hour requirement. DataLink Retrieval Recorded DataLink information is retrieved from the CVR in much the same way as audio data.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–04 Use or disclosure of information on this sheet is subject Description and Operation to the restrictions on the cover page of this document. Rev. 15 Page 72 Apr.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR TESTING 1. GENERAL NOTE: The 17TES0400 ROC/6 was manufactured from 2006 to 2011. Support for the PC operating system (Microsoft Windows XP) has been discontinued by Microsoft. L−3AR continues to pro- vide technical support and repair; however operators are en- couraged to upgrade to the current production 17TES0700 ROC/7.
When it has been determined that an as- sembly is faulty, it should be removed from service, properly packaged, and returned to L3 Communications, Aviation Recorders for repair or replacement. No trouble- shooting procedure is provided for any of these assemblies. Attempting field repair on any of these assemblies will void their warranty.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Model S151/S161, S152/S162, and S251/S261 Control Units The Model S151/S161, S152/S162, and S251/S261 Control Units have been de- signed for use with the Model FA2100CVR’s in ED−56A compatible systems and contain a Microphone Preamplifier PWA manufactured with SMT devices. Refer to ED-56A Control Unit and Microphone CMM, p/n: 165E1747-00 for detail Testing Pro- cedures for these units.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR The CVR test indicator wires, pins 15 and 16 (1mA) may be omitted in installations where ARINC 557 compatibility is not needed. CVR FAULT LIGHT REAL TIME OPEN = FAULT GND = NO FAULT ANNUNCIATOR PANEL RELAY...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 4. TEST EQUIPMENT REQUIRED The Model FA2100CVR has been designed as a direct line replaceable unit (LRU) for the existing Cockpit Voice Recorders, Models A100, A100A, A100S and A200S. As such, the Model FA2100CVR is to be tested using the same special test equipment built for the earlier model recorders with the exception of the Model A860 Test Panel which is no longer supported.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 5. READ−OUT CENTER/6 (ROC/6), WINDOWS XP, AUTO−TESTING This section provides instructions for connecting the Recorder Interface Unit to the ROC/6 and FA2100CVR under test. Refer to Figure 201 for the ROC/6 w/CVR Automated Test Station Software (CATS) FA2100CVR test setup diagram.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR NOTE: Note: Make the following audio connections from the RIU to Sound Blaster sound card. Note that the sound card is located in an expan- sion slot not on the motherboard. Attach the RIU Sound Card In (SND IN (J3)) cable to the Sound Card Line−In (or Microphone−In) which is the blue connector.
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INTERFACE COMMUNICATIONS CABLE ASSY. 17TES0072 * Note: Speakers are optional and not incld with ROC/6 FA2100 CVR RECORDER To order speakers from L-3AR use: p/n: 17TES0425 (110V) or 17TES00426 (220V). Figure 102. ROC/6 w/CVR Automated Test Station Software (CATS) FA2100CVR TEST SETUP 23–70–04...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR READ−OUT CENTER/6 (ROC/6) Sound Card Setup Double−click the CATS (CVR Tester) icon on the ROC/6 to start the software then follow this procedure. Click the Speaker button (Volume Control) to display the Playback Control menu.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 104. Line In Input Level 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 and Line−In. All other boxes should not be checked.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR (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, Volume Levels (14) Close the Play Control menu by clicking on the “X”...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR READ−OUT CENTER/6 (ROC/6) − CATS AUTOTEST CAUTION:Ensure power is removed from the the RIU before proceeding. If the cable, p/n: 17TES0416 is connected to rear of the unit with the power applied to the RIU, the RIU may be damaged.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Read and click on Yes. Figure 107. CVR Test, Start Toggle (m) Read and click on OK. Figure 108. CVR Test, Warning Message Remove front cable and click on OK. Figure 109. CVR Test, Instruction Message Enter in the current value in amps (typically .17) in window and click on 23–70–04 Use or disclosure of information on this sheet is subject...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 110. CVR Test, Power Consumption Entry Verify that the DC LED on the front of the RIU is on. Enter the current value in amps (typically .52) in window and click on OK. Figure 111.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 113. CVR Test, Proceed Message 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 in the Information section of the test.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR From the pull down menu , click on Test=> Test Mode=> Return−to−Ser- vice Test. Ensure that the Return−to−Service is checked. From the pull down menu, click on Test=>Start Test. Follow the instructions below as it appears presented by the software. (m) Read and click on Yes.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 117. CVR Test, Power Consumption Entry Verify that the AC LED on the front of the RIU is on. Enter the current value in amps (typically .21) in window and click on OK. Figure 118.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 120. CVR Test, Proceed Message (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 in the Information section of the test.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Fault Log Displays the current recorder fault log for user review and prompts the user: Continue CVR Tests? Example report message(s): 08:02:32 PASSED Fault History Bulk Erase Part 1 – record audio out and verify 400 Hz bulk erase tone. Part 2 –...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 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 2% of sent frequency.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR (13) Signal To No Signal Record simulated 1000 Hz data for each channel 1,2,3 and 4 and store results then record no data for channels 1,2,3 and 4 and compare differences between signal data results and no signal data results. Verify difference is less than −48 dB. Example report message(s): 08:47:12 PASSED Sig To No Sig 0 Hz 1.0 ref (Expected HQ <...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR (16) FSK Time (V1.1 BETA) Cycle power to recorder to reset for FSK input then record simulated 16000 sps FSK data and then simulated GMT 429 data (label 150) first with channel 1 output and again with channel 3 output.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR ROC/6 − Audio Setup Procedure NOTE: L−3AR recommends that an Audio Setup check be performed every two years, or if the Sound Blaster Audio card is replaced on the ROC/6−CATS RIU System. The Sound Blaster Audio Card in the ROC/6 must be set up to ensure that the prop- er reference voltage levels of the audio test signals are sent to the RIU for testing the FA2100CVR.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Ensure that the RIU Sound Card Out (SND OUT (J5)) cable is connected to the Sound Card Line−Out (green connector). Apply DC or AC power to the RIU. If the CATS test page is not shown, Click the L−3 CVR Test Icon on the Window desktop.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 123. Audio Reference Level Utility, Menu Load 1000Hz full amplitude .wav file by selecting File => Open File on the Audio Reference Utility. Select Setup_1000Hz.wav. and click on Open. Figure 124. Audio Reference Level Utility, File Open Menu Ensure the MultiMeter is connected to the Audio Setup Loop−back cable.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 125. Audio Reference Level Utility, Play Sound Adjust the Audio Reference Level menu volume slider so that the meter reads 3 Volts RMS or as close as possible to this voltage (without going over 3 Volts RMS).
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Select Store Result =>Output Results. A pop−up window will appear dis- playing the current REFERENCE, and the new VOICE VOLUME and CAM VOLUME values. Figure 127. Audio Reference Level Utility, Confirmation (m) Select Yes to update the Setup reference level file with the values dis- played, or select No to cancel the update of the Setup reference level file.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 129. Audio Reference Level Utility, Menu Load 1000Hz full amplitude .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 From the menu bar under Utilities, select Audio Reference Utility.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 131. Audio Reference Level Utility, Play Sound Adjust the Audio Reference Level volume slider so that the meter reads 2.45 Volts RMS or as close as possible to this voltage. From the Audio Reference Level menu select Sound => Record Sound to record the input sound.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 133. CVR Tester, Update Reference Level Select Yes to update the audio setup reference level file with the values displayed, or select No to cancel the update of the audio setup reference level file. (m) Close the Audio Reference Level menu by selecting the Close button.
AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR ROC/6 − AUDIO DOWNLOAD & PLAYBACK NOTE: ROSE 4.0 or higher on a ROC or RAU is recommended to download directly from a CVR and convert audio into a .WAV for playback. Re- fer to the Read-Out Support Equipment / Recorder Interface Software version 4.0 or Higher Operator’s Manual, p/n 165E1696-03, to Re- trieve Flight Data and / or Audio Data from a Recorder.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR READOUT CENTER/6 (ROC/6) − Parts List Table 101. 17TES0400 Part Number Description Mfg. Read-Out Center/6 − Full CVR/FDR Configuration 17TES0400 L-3 Com (The following items are included with the ROC/6). Recorder Interface Unit (RIU) L-3 Com 17TES0410 Cable, RIU to AC Power In...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR READ−OUT CENTER/7 (ROC/7), WINDOWS 7, AUTO−TESTING This section provides instructions for connecting the Recorder Interface Unit to the ROC and FA2100 under test. Refer to Figure 134 for the ROC/7 w/CVR Automated Test Sta- tion Software (CATS) FA2100CVR test setup diagram.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Connect the DIN CABLE from the speakers to the middle Speaker Out (SPKRS OUT (J6)) connector on the front panel of the RIU. After all connections are made to the RIU, apply power to the RIU. This can be either 28 Vdc or 115 Vac, 400 Hz.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CVR AUTOMATED TEST J4 USB 4‐PIN SOFTWARE (CATS 2.0) RIU UNIVERSAL SERIAL 17TES0420 BUS INTERFACE 17TES0415 POWER INPUT RIU DC POWER INPUT SELECT 17TES0412 (DC)- J8 RIU AC POWER INPUT 17TES0411 (AC)- J7 RECORDER INTERFACE UNIT (RIU) 17TES0710 R-SPKR *...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CVR AUTOMATED TEST J4 USB 4‐PIN SOFTWARE (CATS 2.0) RIU UNIVERSAL SERIAL 17TES0420 BUS INTERFACE 17TES0415 POWER INPUT RIU DC POWER INPUT SELECT 17TES0412 (DC)- J8 RIU AC POWER INPUT 17TES0411 (AC)- J7 GREEN RECORDER INTERFACE UNIT (RIU) 17TES0710...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR READ−OUT CENTER/7 (ROC/7) − Sound Card Setup Double−click the CVDR Test icon on the ROC to start the software. The applic- ation will launch with the Channels control screen displayed, as illustrated in Figure 136. Figure 136.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 137. Volume Control Under Applications, click Sound Systems, then click the Recording tab. This will display the Sound control window illustrated on the following page. Figure 138. Sound Control, Recording Select the Recording tab. 23–70–04 Use or disclosure of information on this sheet is subject Testing &...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Highlight and select Line−in. Click on Properties. Figure 139. Line−In Properties, Line−In Level Select the Levels tab. Make sure that the Line−In level is set at 100 (move the Line−In slider to maximum.) Click on OK. 23–70–04 Use or disclosure of information on this sheet is subject Testing &...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 140. Sound, Playback Devices (10) Click on the Playback tab. (11) Highlight Speakers. (12) Click on Properties. 23–70–04 Use or disclosure of information on this sheet is subject Testing & Fault Isolation to the restrictions on the cover page of this document. Rev.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 141. Speaker Properties, 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, Auxiliary, and S/PDIF−In are all muted.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 142. Volume Mixer, Speaker Levels (17) In the Volume Mixer, make sure both sliders are all the way up. (18) Close the Volume Mixer. 23–70–04 Use or disclosure of information on this sheet is subject Testing &...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR READ−OUT CENTER/7 (ROC/7) − CATS Autotest CAUTION:Ensure power is removed from the the RIU before proceeding. If the cable, p/n: 17TES0418 is connected to rear of the unit with the power applied to the RIU, the RIU may be damaged.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Observe Figure 143. CATS, Connecting Pop-Up 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. Click on the Information tab in the Test section of the menu. Enter appropriate information into Department, Part Number, and Serial Number fields.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 145. CATS, Start Test Toggle 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 is not desired then select the “Se- lectable Test Options”...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR NOTE: 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 confirmation window. Read and click on Yes.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 149. CATS, CVDR Instruction Window 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 150.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 152. CATS, CVDR Instruction Window Observe the Fault History Log window appears. Select Print if you want to save the fault history or Close to continue. Figure 153. CATS, CVDR Fault History Log Click on Yes on the dialog box to clear the fault logs.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 154. CATS, CVDR Clear Fault Log Confirmation 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 Click on Ok.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 157. CATS, CVDR Fault History Log Click on Yes. The autotest will now proceed in completing the autotest which will take approximately 30 minutes or less. Figure 158. CATS, Continue Test Confirmation (w) At the end of the test, save the report by selecting File => Test Report => Save Report.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 159. CATS, Test Results Screen CAUTION:Ensure power is removed from the the RIU before proceeding. If the cable, p/n: 17TES0418 is connected to rear of the unit with the power applied to the RIU, the RIU may be damaged.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Observe Figure 160. CATS, Connecting Pop-Up From the 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. On the tool bar, select Power.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Enter appropriate information into Department, Part Number and Serial Number fields. On the tool bar, select Start Test. Figure 162. CATS, Start Test Toggle In the “Test Mode and Options” dialog box, select either Re- turn-to-Service or Selectable Test Options, and then click on OK.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR NOTE: If a full return to service test is not desired then select the “Se- lectable Test Options” radio button and choose the test options desired. NOTE: Figure 164 is only displayed if you select “Selectable Test Op- tion”...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 166. CATS, CVDR Instruction Window Read the current AC 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 167.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 169. CATS, CVDR Instruction Window Observe the Fault History Log window appears. Select Print if you want to save the fault history or Close to continue. Figure 170. CATS, CVDR Fault History Log Click on Yes on the dialog box to clear the fault logs.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 171. CATS, CVDR Clear Fault Log Confirmation Click on Yes on the dialog box to clear the latched faults and fault history log. Figure 172. CATS, CVDR Clear Fault Log Confirmation Click on Ok. Figure 173.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 174. CATS, CVDR Fault History Log (w) Click on Yes. The autotest will now proceed in completing the autotest which will take approximately 30 minutes or less. Figure 175. CATS, Continue Test Confirmation At the end of the test, save the report by selecting File =>...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 176. CATS, Test Results Screen 23–70–04 Use or disclosure of information on this sheet is subject Testing & Fault Isolation to the restrictions on the cover page of this document. Rev. 15 Page 161 Apr.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR READ OUT CENTER/7 (ROC/7) − Autotest Descriptions The following provides detailed descriptions of the test performed during the autotest function. Power Test Test Prompts the user for AC/DC power usage as in the following AC example: Please remove the front panel cable from the recorder now and click ”OK”.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 08:02:58 PASSED Bulk Erase #3 with No Recording (Expected <> 400 Hz) Results = 3334.6 Hz 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 = Push−To−Test indicator set GMT 429 Record simulated GMT−429 data (label 125 first and label 150 second) and verify 10...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 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 ref (Expected HQ > 24.0 dB SQ > 20.0 dB) Results = HQ1 34.6 /HQ2 34.4 /HQ3 34.8 /HQC 36.4 /SQV1 30.9 /SQV2 31.0 /SQV3 30.6 /SQC 31.4 dB 11:26:44 PASSED SN+D 1000 Hz 1.0 ref (Expected HQ >...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 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 (11) Crosstalk Data This is a test for CVDR recorders where both flight data and voice data are being recorded.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR (13) Audio Out Monitor Record simulated 1000 Hz data for each channel 1,2,3 and 4 and verify amplitudes by part number: Example report message(s): 08:26:43 PASSED Audio Out Monitor 1000 Hz (Expected 2.45 +/−20 percent VRMS) Results = HQ1 2.319 /HQ2 2.338 /HQ3 2.317 /HQC 2.355 VRMS (14) Signal To No Signal Record simulated 1000 Hz data for each channel 1,2,3 and 4 and store results;...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR (16) Capacitor Power off recorder and verify recorder is still powered after 200 milliseconds but not powered after 2 seconds. Example report message(s): 08:56:32 PASSED Capacitor − GSE powered after 200 milliseconds but not after 2 seconds (17) Data Link Record simulated data link messages and verify 10 good data link messages.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR (21) FDR Clear 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 Results = 1 minute(s) of good data NOTE: The Data Link test, OMS test and FDR tests requires a CATS V2 RIU and rear panel cable.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR READ−OUT CENTER/7 (ROC/7) − AUDIO DOWNLOAD & PLAYBACK NOTE: ROSE 4.0 or higher on a ROC or RAU is recommended to download directly from a CVR and convert audio into a .WAV for playback. Re- fer to the Read-Out Support Equipment / Recorder Interface Software version 4.0 or Higher Operator’s Manual, p/n 165E1696-03, to Re- trieve Flight Data and / or Audio Data from a Recorder.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR READOUT CENTER/7 (ROC/7) − Parts List Table 102. 17TES0700 Part Number Description Mfg. Read-Out Center/7 − Full CVDR/FDR Configuration 17TES0700 L-3 Com (The following items are included with the ROC/7). 17TES0710 Recorder Interface Unit (RIU) L-3 Com 17TES0411 Cable, RIU to AC Power In...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Table 103. Underwater Locator Beacon Test Using L−3AR Test Set P/N: 17TES0015 PROCEDURE This test should be performed after the 90−Day Beacon is installed. It verifies the proper operation of the Beacon after mounting on the CSMU. 1) Turn the test set ON using the small slide switch located on the left side of the housing.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Table 104. Underwater Locator Beacon Test Using Test Set P/N: 42A12( ) and 10 Mohm High Impedance Voltmeter PROCEDURE This test should be performed after the 90−Day Beacon is installed. It verifies the proper operation of the Underwater Locator Beacon after mounting on the CSMU.
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PRIOR TO HANDLING A PRINTED WIRING BOARD, ENSURE PROPER PERSONNEL GROUNDING TECHNIQUES ARE USED. ALSO, ENSURE THAT ALL PRINTED WIRING ASSEMBLIES BOARDS ARE PLACED INTO STATIC SHIELDING CONDUCTIVE BAGS WHEN HANDLING OR STORING. Table 105. FA2100 CVR Fault Code Corrective Actions Failure Mode Corrective Action Fault Code 1) Remove Memory.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Table 105. FA2100 CVR Fault Code Corrective Actions (Continued) Fault Code Failure Mode Corrective Action see previous page 6902 Negative 5 volt power supply failure. 6903 12 volt (VPP) power supply failure 1) Remove and replace Acquisition Processor PWA,...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Table 105. FA2100 CVR Fault Code Corrective Actions (Continued) Fault Code Failure Mode Corrective Action 1) Run Memory test. 885e The total number of CVR errors exceeded the 2) If fault codes persist, then remove and replace allowable threshold.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Table 105. FA2100 CVR Fault Code Corrective Actions (Continued) Fault Code Failure Mode Corrective Action 1) Remove and replace Acquisition Processor PWA, 89d7 The SMP timed out p/n: 205E3977‐XX. waiting for audio channelizer to shutdown.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 10. FA2100CVR SOFTWARE UPLOAD PROCEDURE Computer Interface Communications Cable/2 (CICC/2) is shown in Figure 177. In the event that the original Acquisition Processor (AP) PWA, p/n: 205E1591−00 or 205E1931−00, is required to be replaced in the FA2100CVR, it will be replaced with the Acquisition Processor PWA, p/n 205E2502−11, or −14 in the case of the 2100−1025−( ), and the software that is required to be loaded onto this PWA.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Turn ON the power to the PC. Insert the FA2100 Utility Bundle CD 883E1894−01 into the PC. When ask to select, Click on the “Open folder to view files using Windows Explorer” . To install the Upload utility from the CD, click open the CICCLdr folder and then click on the “Setup”...
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Note: The ROC rear connections shown in this diagram are for general reference and may not reflect the exact connector location or configuration your ROC system computer. FA2100 CVR RECORDER Note: The 17TES0058 cable assembly should only be attached during upload process. Not used when downloading data or getting recorder status.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR To upload the FA2100 Software perform the following steps: If using the CICC/2 Cable refer to Figure 177 and perform the following steps: Connect the FA2100 Software Upload Cable Assembly (p/n: 17TES0058) to the FA2100 Recorder front panel GSE connector and the opposite end to the FA2100 to Computer Interface Communications Cable/2 (CICC/2), (p/n: 17TES0072).
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Insert the FA2100 CD into the PC, RAU, or ROC/5−ROC/6−ROC−7 Ground Station system CD. From the Windows 98 or XP desktop, activate the (put in new PC & SW) CICC Loader utility program by double−clicking on the CICCLdr Icon. (10) When the CICC Loader window appears select the Browse button at the Load Directory and set the source to “D:\.”...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Match the listed Software Part Number and SMP Checksum with the one listed on the recorder software distribution CD. If the software distribution CD is un- available, refer to Table 106 for a list of checksums. Left click the OK button and left click the X button in the upper right corner of the CICC Loader Menu to exit the utility and return to the Windows 98 or XP desktop.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–04 Use or disclosure of information on this sheet is subject Testing & Fault Isolation to the restrictions on the cover page of this document. Rev. 15 Page 186 Apr.
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COMPONENT MAINTENANCE MANUAL FA2100CVR AUTOMATIC TESTING 1. GENERAL There are no Automatic Test Procedures for the FA2100 CVR. 23–70–04 Use or disclosure of information on this sheet is subject Automatic Testing to the restrictions on the cover page of this document.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–04 Use or disclosure of information on this sheet is subject Automatic Testing to the restrictions on the cover page of this document. Rev. 15 Page 202 Apr. 14/16 The document reference is online, please check the correspondence between the online documentation and the printed version.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR DISASSEMBLY 1. GENERAL This section contains the information required to disassemble the Model FA2100 Cockpit Voice Recorder (FA2100CVR). Access to the major assemblies within the Model FA2100CVR is described such that there is minimal disturbance to other assemblies. Ex- treme care should be exercised when removing these assemblies.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR NOTE: All attaching parts such as cable assemblies, stand−offs, screws, washers, etc. that are not damaged, should be retained with the chassis for reinstallation with the repaired LRUs. The FA2100CVR replaceable PWAs or modules consist of the Acoustic Beacon, Air- craft Interface PWA, Audio Compressor PWA, Acquisition Processor PWA, and the Crash Survivable Memory Unit (CSMU).
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR BEACON REMOVAL PROCEDURE To remove the Underwater Acoustic Beacon (1-80) from the Beacon Mount Bracket (1-70), use a 3/16” Allen hex-wrench, remove the two left 1/4–20, hex- cap screws (1-75) that secures the left Beacon Mount Bracket to the CSMU. 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.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Crash Survivable Memory Unit (CSMU) Removal (See Figure 305 or IPL Figure 1, Item 185) The Model FA2100CVRs CSMU is mounted to the top of the recorder chassis by (4) pan-head sealing screws (MOD−DOT 4). It interfaces to the Acquisition Processor PWA through the Memory Interface Cable assembly attached to the Acquisition Processor PWA’s J1 connector.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Lift and disconnect the CSMU memory assembly as per the appropriate instruc- tions below. For Pre-MOD DOT 6 units only, carefully tilt the CSMU memory assembly to the left side (same side as cable) to gain access to the J1 connector located on the Acquisition Processor PWA (1-175).
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Memory Interface Cable Assembly CSMU Memory Assembly (1‐185) Acquisition Processor PWA (AP) (1‐175) Recorder Chassis (1‐5) Figure 304. CSMU Memory Assembly Removal Diagram (POST-MOD DOT 6 & PRE-MOD DOT 13) For Post-MOD DOT 13 units only, carefully lift the CSMU memory assem- bly directly up without pulling the memory interface cable to gain access to the J5 connector located on the Acquisition Processor PWA (1-175).
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Memory Interface Cable Assembly CSMU Memory Assembly (1‐185) Acquisition Processor PWA (AP) (1‐175) Recorder Chassis (1‐5) Figure 305. CSMU Memory Assembly Removal Diagram (POST-MOD DOT 13) For GACVR’s, p/ns: 2100−1010−5X and 2100−1020−5X, remove RTV from the bottom of the CSMU and the Chassis at the seating surface for the CSMU memory assembly.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Remove the CSMU memory assembly (1-185) as described in paragraph B. above. To gain full access to the Acquisition Processor PWA (1−175) remove the 10 pan- head sealing screws (1-25) and lift chassis cover (1-20) from the recorder chassis. NOTE: Pan-head sealing screws (1-25) are one time use items that should be discarded when removed and replaced with new...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR tor; and to the Aircraft Interface PWA via cable assembly W002 through the J1 con- nector. Remove the CSMU memory assembly (1-185) as described in paragraph B. above. Remove the 10 pan-head screws (1-25) which secure the chassis cover (1-20) to the recorder chassis (1−5).
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR (12) Remove the Assembly Support Tool fixture, Table 701: item 5 from under the Air- craft Interface PWA. (13) Carefully lift the Audio Compressor PWA from the rear panel assembly observing proper ESD handling precautions. (14) If the Audio Compressor PWA is the faulty component, then package it in an static- resistant container for shipment to the factory for repair.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR (10) Carefully lift the Aircraft Interface PWA from the rear panel assembly observing proper ESD handling precautions. (11) Remove 2 pan-head screws (1-125) which mount the two lower standoffs (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.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–04 Disassembly Use or disclosure of information on this sheet is subject Rev. 15 Page 314 to the restrictions on the cover page of this document. Apr. 14/16 The document reference is online, please check the correspondence between the online documentation and the printed version.
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This section contains a list of all required cleaning materials, general cleaning proce- dures, applicable cautions and warnings related to the use of any cleaning material, and instructions for cleaning the Model FA2100 CVR major assemblies. 2. MATERIALS REQUIRED Refer to Table Table 401 for a listing of required cleaning materials: Table 401.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CAUTION: DO NOT IMMERSE ANY PRINTED WIRING ASSEMBLY MOUNTED ELECTRONIC PARTS IN THE CLEANING SOLVENT; OTHERWISE, CIRCUIT BOARD AND/OR COMPONENT DAMAGE MAY RESULT. Printed Wiring Assembly Cleaning Remove dust, dirt, and foreign matter from all surfaces, using soft-bristle brush. Wipe finished surfaces and contacts, using a cloth moistened in solvent.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CHECK 1. GENERAL This section contains the various checks that should be performed on the Model FA2100 Cockpit Voice Recorder during shop maintenance. Check procedures, when required, are written in step-by-step procedures wherever practicable, and include specific meth- ods, techniques, and equipment required.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Check the circuit boards for broken parts and bad solder joints. Check for burnt parts. Check the circuit boards for cracks and abrasions. Inspect the nameplate for legibility. Reassemble recorder in accordance with the steps of procedure outlined in Section 700: Assembly.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR REPAIR 1. GENERAL This section is intended to contain information required to restore a worn or damaged part to a serviceable condition. However, the Fairchild Model FA2100 Cockpit Voice Recorder is a completely solid-state device that does not contain any electro-mechanical moving parts.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–04 Repair Use or disclosure of information on this sheet is subject Rev. 15 Page 602 to the restrictions on the cover page of this document. Apr. 14/16 The document reference is online, please check the correspondence between the online documentation and the printed version.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR ASSEMBLY 1. GENERAL This section contains procedures describing the assembly of the Model FA2100 Cockpit Voice Recorder as well as storage instructions after assembly. There is no special testing necessary during assembly. However, once assembly is completed, the operational test procedure provided in the Testing and Troubleshooting Section 100 should be performed to verify proper operation of the Recorder.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 3. ASSEMBLY INSTRUCTIONS CAUTION: THE FA2100 CIRCUIT BOARDS ARE SUSCEPTIBLE TO ELECTRO– STATIC DESTRUCTION (ESD). PRIOR TO HANDLING PWAs, ENSURE PROPER PERSONNEL GROUNDING TECHNIQUES ARE USED. ENSURE THAT CARDS ARE PLACED INTO STATIC SHIELDING CONDUCTIVE BAGS WHEN HANDLING OR STORING.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Processor PWA also provides an interface between the FA2100CVR and Ground Support Equipment, GSE, directly through front panel GSE connector J3. Remove the Acquisition Processor PWA (1-175) from its static-resistant container ensuring that none of the connector contacts are touched and general ESD han- dling precautions are observed.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR For GACVRs, p/n: 2100−1010−51 and 2100−1020−51, verify that the three un- used holes on the rear of the chassis (1−5) are filled with RTV. If the unused holes are not filled with RTV, place polymide tape (Table 701: Item 4) over the holes on the inside of the chassis (1−5).
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR capacitor (1−130) to the top of the rear panel assembly using the support ca- pacitor bracket (1−141). (14) Connect the red blade connector (39 Vdc Hot) to the top, J4, connector on the front side of the Aircraft Interface PWA. (15) Connect the black blade connector (39 Vdc Return) to the lower, J5, connector on the front side of the Aircraft Interface PWA.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 703. Aircraft Interface & Audio Compressor PWA Installation Diagram (POST MOD DOT 6) Insert the rear panel assembly with attached Aircraft Interface PWA and Audio Compressor PWA into the recorder chassis (1-5). (10) To secure the rear panel assembly, insert six flat-head screws (1-95) coated with adhesive, Table 701: item 1, three to each side of the rear panel assembly, but do not fully tighten down.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Position the chassis cover seal (1-28) into place on the Seal Alignment Tool, Table 701: item 6, (see Figure 704, frame 1). Carefully peel the paper backing from the chassis cover seal (1-28) to end of the alignment tool ensuring that you do not stretch the seal.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR (13) Secure the CSMU (1-185) to the recorder as described in Paragraph F. (14) For GACVR p/ns: 2100−1010−5X and 2100−1020−5X, apply RTV (Table 701: Item 3) to the entire seam where the chassis cover (1−20B) meets the chassis (1−5), as indicated in Note 2, Figure 705.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR ALIGN CHASSIS COVER OVER ALIGN SEAL OVER SEAL & PRESS IN FIXTURE HOLES PLACE REMOVE SEAL BACKING AND SMOOTH OUT PUSH TOOL FIRMLY TO AFFIX SEAL TO HOLES IN SEAL SIDE SHOULD LINE UP WITH HOLES IN CHASSIS COVER ASSEMBLY DO NOT STRETCH...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Note 1: Apply RTV to Note 2: Two Front Screw Heads and the front seam where Apply RTV to entire seam, the Chassis Cover meets where Chassis Cover meets the Chassis. the Chassis, after the CSMU is installed and tight- ened.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Torque Sequence (9−10 in./lbs.) Chassis Cover Seal-Screws (Qty 10) Note 1: Apply RTV to Note 2: two front bend relieves in Apply RTV to Chassis Cover Two Front Screw Heads Figure 706. FA2100CVR Chassis Cover Installation Crash Survivable Memory Unit (CSMU) Installation (See Figure 710 or IPL Figure 1, Item 185) The Model FA2100’s Crash Survivable Memory Unit, CSMU, is a sealed unit and...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Remove the damaged seal, if necessary, by peeling the seal up from the edge. Ensure that the flat underside surface of the CSMU is clean. CSMU Cover Seal Apply RTV to seal Memory Cable Slit Figure 707.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Location of memory cable clasp Figure 708. Crash Survivable Memory Unit (CSMU) Seal Application (Post-MOD DOT 13) Secure the loose cable to the side, ensuring that it is away from the bot- tom of the CSMU. This will keep the cable out of access while applying the new CSMU seal.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR the cable assembly slit in the seal around the memory interface cable as- sembly. Apply RTV, DOW Corning, 3145 Adhesive silicone sealant between the slit in the CSMU cover seal where memory interface cable assembly passes through the seal as shown in Figure 709.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CSMU Mounting Torque Sequence Seal-Screws 75 in/lb (1−190B) (Qty 4) Note: After attached, apply RTV to seal Memory Cable Slot Crash Survivable Memory Unit (CSMU) (1‐185) Memory Interface Cable Assembly Recorder Chassis Assembly Acquisition (1-5) Processor PWA (AP)
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CSMU Mounting Torque Sequence Seal-Screws 75 in/lb (1−190B) (Qty 4) Note: Crash Survivable After attached, apply RTV Memory Unit to seal Memory Cable Slot (CSMU) (1‐185) Memory Interface Cable Assembly Recorder Chassis Assembly Acquisition (1-5) Processor PWA (AP)
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CSMU Mounting Torque Sequence Seal-Screws 75 in/lb (1−190B) (Qty 4) Note: Crash Survivable After attached, apply RTV to seal Memory Cable Slot Memory Unit (CSMU) (1‐185) Memory Interface Cable Assembly Recorder Chassis Assembly Acquisition (1-5) Processor PWA (AP)
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Underwater Acoustic Beacon Assembly & Installation (See Figure 713 and IPL Figure 1, Item 80) The Underwater Acoustic Beacon is mounted on the Model FA2100’s CSMU front bracket with the beacon’s water switch facing to the left (refer to Figure 713, 1–80). NOTE: When replacing the 30−day ULB it is recommended that new mounting hex screws (MS 16995-54) are used to en-...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Note: - Must use the L-3AR Conversion Kit, PN 068E5542-00 when converting from a 30-Day ULB to a 90-Day ULB. Mark Name Plate Hardware MOD-DOT #15 Underwater Right Beacon Acoustic Beacon Mount Bracket (1-80) (1-70) Crash Survivable Memory Unit...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 4. STORAGE INSTRUCTIONS NOTE: A Return-To-Service bench test is recommended after storage of more than one year. Refer to Automatic Test Section 200 for specific test and check-out procedures. Storage in Original Containers When possible, the FA2100 Cockpit Voice Recorder should be stored in its original container(s).
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR NOTES: CONTAINER TO MEET ATA SPEC 300 CATEGORY II. MATERIAL: OUTER SHELL FIBER BOARD TO BE TYPE 1, CLASS 2, PER PPP−8−836 BOUBLE WALL 275 LBS CONSTRUCTION REF: CONTINOUS STITCHING MATERIAL PACKING FOAM (1.50 IN. THICK) 1.8 LBS/ STAPLE APPROX 1.0 CUBIC FOOT WITH A COMPRESSION SET OF 95%.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR FITS AND CLEARANCES 1. GENERAL This section provides the FA2100CVR recorder’s specifications and outline and dimen- sions. Since the recorder uses solid−state memory recording technology, there are no in- ternal fits and clearances or tension values normally associated with older technology electromechanical tape recorder units.
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Audio Output: 2.55 Vrms into 600−ohms Environmental Characteristics Refer to Table 801 for the FA2100 CVR environmental characteristics. 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 6.5 msec.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Table 801. FA2100 CVR Environmental Characteristics Conditions RTCA/ Description DO–160C Section Temperature & Altitude Categories A2 & F2 Ground Survival: Low Temperature 4.5.1 (–55_C) High Temperature 4.5.2 (+85_C) Low Temperature Operating 4.5.1 (–55_C) High Temperature Short–time 4.5.2...
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REAR PANEL CONTAINS HOLES TO MATE WITH GUIDE PINS IN ARINC 404 MOUNTING TRAYS. Figure 801. (Sheet 1 of 2) Outline & Dimension Drawing Model FA2100 CVR Recorder P/N: 2100-1010-( ) & 2100-102X-( ) 23–70–04 Use or disclosure of information on this sheet is subject Fits and Clearances to the restrictions on the cover page of this document.
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4.98 View Figure 801. (Sheet 2 of 2) Outline & Dimension Drawing Model FA2100 CVR Recorder P/N: 2100-1010-( ) & 2100-102X-( ) 23–70–04 Use or disclosure of information on this sheet is subject Fits and Clearances to the restrictions on the cover page of this document.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–04 Use or disclosure of information on this sheet is subject Fits and Clearances to the restrictions on the cover page of this document. Rev. 15 Page 806 Apr.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR SPECIAL TOOLS, FIXTURES 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 FA2100CVR special test equipment.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 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-3 Com. 17TES0070 CICC/2 Assembly Dwg. L-3 Com. 17TES0071 Cable Assembly, F1000−CICC/2 L-3 Com.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 17TES0057 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) Optional Note: The FA2100 Software Program P/N, listed below for the specific recorder, is needed to perform the upload function.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR FA2100 CVR Software Disk Part Number Description Mfg. 840E1658-07 FA2100CVR p/n: 2100-1010-00, 30-Min. L-3 Com. Program Software 840E1657-07 FA2100CVR, p/n: 2100-1020-00 120-Min. L-3 Com. Program Software 840E1663-07 FA2100 GACVR p/n: 2100-1010-50/51, L-3 Com. 30-Min. Program Software...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 2. GROUND SUPPORT EQUIPMENT (GSE) DESCRIPTIONS Portable Interface Unit, p/n: 17TES0043 Refer to Figure 901 and Figure 902. The Portable Interface (PI) Unit, Part Number 17TES0043, can be used to check the recorder status and download FA2100CVR audio data from the recorder to the PI Memory Module, Part Number 17TES0053, while installed in the aircraft.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CVR: MONITOR PLAYBACK TO RECORDER GSE CONNECTOR STATUS / CONTROL SPECIAL FUNCTIONS GMT/ROTOR AUDIO SELECT DELETE MENU Sarasota, Florida PI AUX READOUT CABLE 17TES0052 PI AUDIO READOUT CABLE 17TES0051 CH 1 COMB Figure 901. Portable Interface Unit, p/n: 17TES0043 23–70–04 Special Tools and Test Equipment...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR MAIN MENU CVR: MONITOR MONITOR MENU PLAYBACK PLAYBACK MENU HQ VOICE CH 1 OFF/ON CVR PLAYBACK CH 2 OFF/ON MODE: STOP CH 3 OFF/ON POSITION: HRS : MIN : SEC ROTOR: __HZ HQ CAM CH 4 OFF/ON GMT:...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Figure 902. Sheet 1 of 2 Portable Interface (PI) Unit, CVR Menu Structures. DISPLAY GMT/ROTOR FILE DELETION MENU FILE DELETION DELETE THIS FILE: (FILE NAME): XXXX.CVR ROTOR: XXXX HZ (FILE ID): XXXX XXXX.CVR DATE: 0I−JAN−1999 GMT:: X:XX::XX TIME RECORDED: HRS : MIN : SEC...
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ROC system computer. Note: The 17TES0058 cable assembly should only be attached FA2100 CVR during upload process. Not used when downloading data RECORDER or getting recorder status.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 28VDC 115VAC 36.0 115VAC HOT 115VAC COLD 28VDC FDR DATA OUT LO * FDR DATA OUT HI * MONITOR WIRE A MONITOR WIRE B * FDR DATA IN LO * FDR DATA IN HI * ACID 6 * ACID 7 * * These signal lines are not used with the FA2100CVR,...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CICC/2 PNR 17−TES0070 3.3 + .2 SER XXXXXXXXX MFR 06141 DMF MMYYYY 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.
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INTERFACE COMMUNICATIONS CABLE ASSY. 17TES0072 * Note: Speakers are optional and not incld with ROC/6 FA2100 CVR RECORDER To order speakers from L-3AR use: p/n: 17TES0425 (110V) or 17TES00426 (220V). Figure 907. ROC/6 w/CVR Automated Test Station Software (CATS) FA2100CVR TEST SETUP 23–70–04...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 6.0 IN Signal Name From Signal Name From CHANNEL 1 AUDIO IN LO P1−30 P2−30 PWR IN 115 VAC (HOT) P1−2 P3−1 DATA LINK FAULT P1−31 P2−5 PWR IN 115 VAC (COLD) P1−3 P3−2 CHANNEL 1 AUDIO IN HI P1−32...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR CABLE, PWR, AC LABEL, “115V/400Hz” LABEL, “17−TES0411” Figure 909. AC 115 VAC/400Hz Power Input Cable Assembly P/N: 17TES0411 Strip and Tin 1.0 IN 144.0 .13 IN 2X 2.00 2X 1.00 .13 I 5 (See Note) * WIRE CHART Note: TRIM SHIELD EVEN WITH OUTER JACKET.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR LOOP BACK CONNECTOR Figure 911. Audio Setup Cable Assembly, 17TES0417 MICROPHONE SWITCH INPUT GAIN TUNNING BAT. TEST AUDIO OUTPUT ULTRASONIC TEST SET UNDERWATER MODEL 42A12( ) LOCATOR 42A12( ) DEVICE ULTRASONIC TEST SET Figure 912. ULD Test Set-Up Audio Data Link Player Software The FA2100CVR Audio &...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR All other Model FA2100CVR part numbers can use this utility software to playback the CVR audio data but will not be able to analyze any data link messages since these other CVR part number recorders do not support the recording of data link messages.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR Hardware Requirements for Downloading CVR Data The FA2100CVR must be removed from the aircraft prior to downloading voice data. Data Link messages, however, can be downloaded while the recorder is on the aircraft as this data is accessed in a similar manner to standard flight data.
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AC COMMON COLD +27.5 VDC INPUT +27.5 VDC INPUT CHASSIS GND CHASSIS GND CONNECTS TO CONNECTS TO FA2100 CVR CVR TRAY Figure 913. FA2100CVR Download Cable, p/n 17TES0078, Wiring Diagram 23–70–04 Special Tools and Test Equipment Use or disclosure of information on this sheet is subject Rev.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR ILLUSTRATED PARTS LIST 1. GENERAL This section contains the following sections: introduction, equipment designator list, nu- merical index, and detailed parts list. The introduction of this section describes usage of the IPB, a listing of abbreviations, and a list of vendor names, addresses, and codes per the current issue of “Federal Supply Code for Manufacturers”, catalog handbook H4–1.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 5. NUMERICAL INDEX The Numerical Index is a complete listing of parts included in the Detail Parts List, cross– referenced to the applicable figure and item number, L-3’s part numbers, the manufactur- er’s part numbers and total quantity required. Part numbers are arranged in a alphanumerical sequence beginning at the extreme left–...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR ber is also shown enclosed in parentheses in the NOMENCLATURE column. When stan- dard parts (such as MS, AN, RC, CP, etc.) are used, vendor codes are not assigned to these parts. However, for non–standard parts the vendor code is assigned in the NO- MENCLATURE column and is preceded by the letter “V.”...
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Form 8130’s, and certification documents with the format: 266−E0305−00. 8. MANUFACTURER’S CODE Due to the Level−2 maintenance philosophy used with the FA2100 CVR, all spare parts will be ordered through L−3 Communications. L3AR Vendor Code, manufacturer name and address, as listed in the “Federal Supply Codes for Manufacturers” Cataloging Hand- book H4/H8, Commercial and Government Entity (CAGE) codes, (formerly FSCM), and/or the NATO Code as applicable (Ref.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR To ensure integrity of the locating device function 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 used when converting from a 30−Day ULB to a 90−Day ULB.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR 10. CONFIGURATION MATRIX Listed below are the current configurations for the FA2100 Cockpit Voice Recorder (CVR). Part Number 2100-1010-( ) is capable of storing 30 minutes of voice data while p/n: 2100-1020-( ) is capable of storing 2 hours of voice data, p/n: 2100−1020−02 has FSK capability, p/n: 2100−1025/1026/1027−( ) has OMS capability.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR (W2) (W3) (W1) (farside) Figure 1. (Sheet 1 of 2) Model FA2100 Cockpit Voice Recorder PN: 2100-1010-( ) & 2100-1X2X-( ) 23–70–04 Illustrated Parts List Use or disclosure of information on this sheet is subject Rev.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR View 80A/B/C REFERENCE ONLY REPLACEMENT DATE View View Figure 1. (Sheet 2 of 2) Model FA2100 Cockpit Voice Recorder PN: 2100-1010-( ) & 2100-1X2X-( ) 23–70–04 Illustrated Parts List Use or disclosure of information on this sheet is subject Rev.
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ITEM NUMBER PART NO. CODE ASSY 1234567 2100−1010−00 COCKPIT VOICE RECORDER FA2100 CVR, ARINC 757, 30 MIN. CVR, 1/2 ATR SHORT (OBSOLETE) 2100−1020−00 COCKPIT VOICE RECORDER FA2100 CVR, ARINC 757, 2−HR. CVR, 1/2 ATR SHORT 2100−1020−02 COCKPIT VOICE RECORDER FA2100 CVR, ARINC 757, 2−HR. CVR W/ FSK, 1/2 ATR SHORT 2100−1020−91...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR UNITS FIG. PART AIRLINE NOMENCLATURE ITEM NUMBER PART NO. CODE ASSY 1234567 042E1597−00 .CHASSIS, SHORT 1/2 ATR ARINC A, B, C, E, F, G, H, L, M, N, P, R, U, V, W, Y, AA, AC 042E1597−01 .CHASSIS, SHORT 1/2 ATR ARINC, AP...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR UNITS FIG. PART AIRLINE NOMENCLATURE ITEM NUMBER PART NO. CODE ASSY 1234567 192E1599−00 .FRONT PANEL ASSEMBLY 027E1590−00 .CAP,PROTECTIVE METAL ATTACHING PARTS 229E0574−00 .SCREW, JACK, KNURLED − 1256 .DELETED − 166E1647−00 .LABEL, IDENT, COCKPIT VOICE RECORDER 111−98−00097 .FASTENER, HOOK, NAS622 (V94867) (MFG.
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR UNITS FIG. PART AIRLINE NOMENCLATURE ITEM NUMBER PART NO. CODE ASSY 1234567 266E0305-01 .BEACON, ACOUSTIC, UNDERWATER A, B, C, (SUPSD BY 80D PER SB022) E, F, G, DUKANE (V94970) (DK-120) H, L, M, N, P, R, FOR BATTERY REPLACEMENT ORDER 30−DAY BATTERY KIT (147E0305−00) 266E0305-02...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR UNITS FIG. PART AIRLINE NOMENCLATURE ITEM NUMBER PART NO. CODE ASSY 1234567 105A 205E1593-00 .PWA, AIRCRAFT INTERFACE, ARINC 757 A, B, C (SUPSD BY 105E, PER SB015) 105B 205E1763-00 .PWA, AIRCRAFT INTERFACE, GA, E, F, G, ARINC 757 (OBS, SUPSD BY 105C, PER ECO 9432) 105C...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR UNITS FIG. PART AIRLINE NOMENCLATURE ITEM NUMBER PART NO. CODE ASSY 1234567 125A MS51957-14 .SCREW, PAN HEAD, 4-40 X 5/16 A, B, C, (V06141) (2290200074) E, F, G, H, L, M, N, P, R, U, V, W, Y, AA, AC...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR UNITS FIG. PART AIRLINE NOMENCLATURE ITEM NUMBER PART NO. CODE ASSY 1234567 MS15795-803 .WASHER, #4, FLAT, STAINLESS STEEL (V06141) (2730200004) (SUPSD BY 146, PER SB016) 146A 016E4797−00 .BRACKET, CAPACITOR A, B, C, (SUPSDS ITEM 145, PER SB016) E, F, G, H, L, M, N, P, R,...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR UNITS FIG. PART AIRLINE NOMENCLATURE ITEM NUMBER PART NO. CODE ASSY 1234567 155D 205E1849-02 .PWA, AUDIO COMPRESSOR, w/ AGC E, F (SUPSDS 155A, SN377 PER ECO 8893) G, H (SUPSD BY 155L, PER SB009) 155E 205E1849-04 .Deleted...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR UNITS FIG. PART AIRLINE NOMENCLATURE ITEM NUMBER PART NO. CODE ASSY 1234567 155S 205E3977−22 .PWA, AUDIO COMPRESSOR, w/ AGC E, F (SUPSDS 155L, PER SB015) G, H 155T 205E3977−23 .PWA, AUDIO COMPRESSOR (SUPSDS C, V ITEM 155M, PER SB015) 155U 205E3977−24...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR UNITS FIG. PART AIRLINE NOMENCLATURE ITEM NUMBER PART NO. CODE ASSY 1234567 175A 205E1591-00 .PWA, ACQUISITION PROCESSOR (SUPSD BY 175B, PER SB002) 175B 205E1931-00 .PWA, ACQUISITION PROCESSOR A, B, C, (SUPSDS 175A, PER SB002) E, F, G, (SUPSD BY 175D, PER SB006) 175C...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR UNITS FIG. PART AIRLINE NOMENCLATURE ITEM NUMBER PART NO. CODE ASSY 1234567 ATTACHING PARTS MS51957-14 .SCREW, PAN HEAD, 4–40 X 5/16 (V06141) (2290200074) 185A 253E1568-01 .MEMORY (CSMU) ASSEMBLY, 7X32 MEG A, E (SUPSD BY 185G PER SB008) 185B 253E1568-00 .MEMORY(CSMU) ASSEMBLY, 15X32 MEG...
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR UNITS FIG. PART AIRLINE NOMENCLATURE ITEM NUMBER PART NO. CODE ASSY 1234567 185J 253E1568-41 .MEMORY (CSMU) ASSEMBLY, 7X128 MEG 3V STRATA FLASH, TITANIUM (SUPSDS 185D, PER SB008) (SUPSD BY 185M PER SB019) 185K 253E4427-33 .MEMORY (CSMU) ASSEMBLY, 9X128 MEG 3V STRATA FLASH MEG, CYRILLIC (RUSSIAN TEXT)
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AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL FA2100CVR UNITS FIG. PART AIRLINE NOMENCLATURE ITEM NUMBER PART NO. CODE ASSY 1234567 200B 230E5675−00 .SEAL, CSMU COVER, SHORT-BOX (SUPSDS 200A, PER SB019) 9030100047 .LABEL, ESD − 147E1679-00 SHIPPING PACKAGE KIT − 197E1746-00 .CONTAINER, SHIPPING, SHORT −...
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