L3 2100-1010-00 Component Maintenance Manual With Illustrated Parts List Download Page 317

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COMPONENT MAINTENANCE MANUAL

AVIATION RECORDERS

FA2100CVR

Rev. 15 Page 1010

Apr. 14/16

Illustrated Parts List

23–70–04

Use or disclosure of information on this sheet is subject

to the restrictions on the cover page of this document.

PART NUMBER

TTL

REQ

ITEM

FIG.

AIRLINE

PART NO.

230E2521

230E5675

200B

253E1568

−

185B

253E1568

−

185A

253E1568

−

185C

253E1568

−

185D

253E1568

−

185E

253E1568

−

185F

253E1568

−

185G

253E1568

−

185H

253E1568

−

185J

253E4427-33

185K

253E5675-00

185L

253E5675-11

185M

253E5675-20

185N

266E0305

−

80A

266E0305

−

80B

266E0305

−

02 (DEL.)

80C

266E5542

−

80D

297

−

00087

120A

297

−

00257

115

297

−

00283

110

297

−

00319

120B

3M#7201 (DEL.)

100

742E1619

−

135A

742E1619

−

135B

9300

−

388

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

Summary of Contents for 2100-1010-00

Page 1: ...0 91 93 Contact L 3AR Product Support WARNING THIS TECHNICAL DATA IS CONTROLLED UNDER THE EXPORT ADMINISTRATION REGULATIONS EAR ECCN 7E994 AND MAY NOT BE EXPORTED TO A FOREIGN PERSON EITHER IN THE U S OR ABROAD WITHOUT A LICENSE OR EXCEPTION FROM THE U S DEPARTMENT OF COMMERCE DISTRIBUTION STATEMENT THIS DOCUMENT CONTAINS L 3 AVIATION RECORDERS PRIVILEGED INFORMATION AND MUST NOT WITHOUT THE PRIOR...

Page 2: ...art of this manual may be repro duced or utilized in any form or by any means electronic or mechanical including photocopying recording or by in formation storage and retrieval system without permission in writing Inquiries should be addressed to L 3 Communications Aviation Recorders Publications Vendor Code 06141 P O Box 3041 Sarasota Florida 34230 Phone 941 371 0811 FAX 941 377 5591 The document...

Page 3: ...rsons working with static sensitive devices When handling or servicing equipment containing static sensitive devices adequate precautions must be taken to prevent device damage or destruction Only those who are thoroughly familiar with industry accepted techniques for handling static sensitive devices should attempt to service circuitry with these devices In all instances measures must be taken to...

Page 4: ...itle 23 70 04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 5: ...P version numbers updated Software checksums updated Model configuration tables added for clarity Au tomatic Test Section revised Revision 12 Jul 03 13 Corrected page number errors and updated the LOEP and Table of Contents Revision 11 May 21 13 Added automatic testing section Added p n 2100 1027 02 Revised IPL Revision 10 Jun 15 12 Added configuration Updated Numerical Parts Index to reflect chan...

Page 6: ...ervice bulletins Updated the IPL to reflect p n 21001026 02 Revision 06 May 01 07 Added new Section 200 Automatic Testing for operational testing of CVR to include the ROC6 w CATS software Revised Disassembly As sembly sections to include p n s 2100 1025 12 22 Audio Compressor and Crash Survivable Memory Unit Revised Description Section for new p n 2100 1025 12 22 Audio Compres sor and Crash Survi...

Page 7: ...r Underwater Locator Device Added new CVR label and change of location Added 2100 1020 90 version Revision 04 Jan 01 03 Revised Disassembly Assembly sections to in clude the moisture resistant seals introduced in SB004 Identified an approved ATA300 shipping container in the Assembly section Added the CICC 2 upgraded cable assembly to the Test Troubleshooting sections Updated the IPL to re flect th...

Page 8: ...closure of information on this sheet is subject to the restrictions on the cover page of this document Rev 15 Page viii Apr 14 16 THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 9: ...ated unit weights Added obsolete notes Removed A860 Testing Fault Isolation All Page headers updated Removed A860 Updated Software tables Automatic Testing All Page headers updated Removed section Disassembly All Page headers updated ULB information updated Cleaning All Page headers updated Check All Page headers updated Repair All Page headers updated Assembly All Page headers updated ULB informa...

Page 10: ... footer Added 2100 1220 00 2100 1220 02 2100 1225 22 2100 1226 02 2100 1225 24 2100 1227 02 and 2100 1925 22 Added 90 Day ULB Description Operation All Updated to include legal reference in footer Added 2100 1220 00 2100 1220 02 2100 1225 22 2100 1226 02 2100 1225 24 2100 1227 02 and 2100 1925 22 Added 90 Day ULB Testing Fault Isolation All Updated to include legal reference in footer Added 2100 1...

Page 11: ...ip ment All Updated to include legal reference in footer Illustrated Parts List and Schem atic Diagrams All Updated to include legal reference in footer Removed 2100 1020 91 2100 1020 93 and 2100 1020 90 Added 2100 1220 00 2100 1220 02 2100 1225 22 2100 1226 02 2100 1225 24 2100 1227 02 and 2100 1925 22 Added 90 Day ULB The document reference is online please check the correspondence between the o...

Page 12: ...ated ROSE version updat ed Model configuration tables added Testing Fault Isolation 105 142 145 147 150 ROSE version updated ADLP added Software and directory labels updated Updated setup diagram Software checksums updated Automatic Testing 201 209 211 212 220 255 264 269 271 278 Reformatted section updated figure labels removed redundant steps corrected test sequences and streamlined procedure Di...

Page 13: ...or revised are outlined below together with the highlights of Revision 12 dated July 3 2013 Section Page Description Front Matter LOEP TOC Changed the List of Effective Pages to reflect Revision 12 changes Changed the Table of Contents to reflect the Revision 12 changes Automatic Test 201 290 Reformatted section to include figure labels and removed redundant steps The document reference is online ...

Page 14: ... 30 34 35 36 43 48 56 64 67 Added part number 2100 1027 02 ARINC 757A compliant Added NAND memory to part number matrix Adds description of PI 2 Added description of acquisition processor 205E2502 34 Removed descrip tion of FA2100 CVR p n S2100 1020 91 Testing Fault Isolation Section 101 102 140 145 148 149 151 152 Added notes about ROC 6 ROC 6 and ROC 7 concerning compatibil ity with CATS 2 0 Add...

Page 15: ...e highlights of Revision 10 dated Jun 15 2012 Section Page Description List of FSB s n a Front Matter xix xxxiv Changed the List of Effective Pages to reflect the Revision 10 changes Changed the Table of Contents to reflect the Revision 10 changes Testing 118 120 Updated procedure to accommodate PI MOD DOT 8 Illustrated Parts List and Schem atic Diagrams n a Added 2100 1025 24 configuration Added ...

Page 16: ...reflect the Revision 09 changes Introduction 2 5 6 Added Rose 4 0 Updated L 3 Address Updated shop verication dates Description Operation 9 19 21 45 54 66 Added note on test tones for P N 2100 1025 6 02 Added BIT and Fault Detection paragraph Added TSO C123b Testing Fault Isolation 105 150 Revised P N for the Variac Added Table 107 Software FDP check sum Added Section 9 Onboard Maintenance System ...

Page 17: ...up with support equipment Updated Table 106 with new software P N s for the CVR P N 2100 1025 22 and 2100 1026 02 Added note for the CICC 3 Automatic Testing 201 203 207 212 213 216 218 219 221 Added Caution on power input select switch Revised Figure 201 showing the back of the ROC 6 Updated and added to Section 3 the CATS auto test procedures Disassembly Assembly Fit and Clear ances Special Tool...

Page 18: ...3 Testing Fault Isolation 105 107 114 126 131 137 148 150 Added Beacon Test note added Acquisition Processor configuration added reference to ROC 6 Updated Software Checksums Added p n 2100 1026 02 Removed p n 2100 1020 91 93 Automatic Testing 201 203 205 216 Updated part numbers corrected test setup diagram added RIU power cautions verified ROC 6 part list Revised the Auto testing pro cedure to s...

Page 19: ...ompressor and Crash Survivable Memory Unit CSMU p ns Changed 2100 1025 02 to 2100 1025 or XX Added EURO CAE ED 112 Revised text for Per and Post MOD DOT 7 configu rations of P N 2100 1020 XX Revised beacon battery replacement date Testing Fault Isolation 101 103 105 107 110 112 115 120 123 125 132 139 146 148 150 Changed 2100 1025 02 to 2100 1025 or XX Updated Test Procedures and Checksum Informat...

Page 20: ...Updated Table 1 FA2100 Recording Specifications to include the 2100 1025 02 Added OMS and Data link information Added Control Unit information on the S161 1390 00 Updated Figure 8 Interwiring Diagram to include OMS and Data LInk pins Testing Fault Isolation 101 105 112 114 118 122 124 127 141 142 Updated test section procedure to include p n 2100 1025 02 2 hour HQ only recorder Updated FA2100 CVR ...

Page 21: ...rary Disk information Modified Figure 910 CVR Menu Structures to include p n 2100 1025 02 Added Audio Data Link Player Software information Illustrated Parts List Schematic Diagrams 1004 1015 Updated the Configuration Matrix Numerical Index Figure 1 and the IPL to include p n 2100 1025 02 and associated parts Added new Acquistion Processor board for the FA2100 CVR The document reference is online ...

Page 22: ... informa tion for Uploading Software changes for 2100 1010 and added 2100 1020 90 along with new checksums in Table 105 for SW Rev 02 Per SB005 Disassembly 302 309 Corrected nomenclature inconsistancies with IPL Changed removal procedure for Acquisition Processor PWA Cleaning 402 403 Changed beacon manufacturer information Check 501 502 Changed beacon manufacturer information Assembly 701 716 Modi...

Page 23: ...corporated new label and updated label position Incorporated all GACVR s are DC only Incorporated Software changes for 2100 1010 and added 2100 1020 90 along with new checksums in Table 105 Disassembly Section 302 Corrected ULD cleaning requirements Cleaning Section 402 Corrected ULD cleaning requirements Assembly Section 709 710 Added steps and figure to include the assembly of the 99 version cus...

Page 24: ...and manufacturer information Disassembly Section 302 303 306 307 Updated information for ULDs Updated the beacon removal proce dure Added IPL Tag for 205E1849 04 Audio Compressor PWA Cleaning Section 402 403 Updated cleaning and manufacturer information for ULD Check Section 502 Updated manufacturer information for ULDs Assembly Section 705 707 708 Added IPL Tag for Audio Compressor PWA Updated as...

Page 25: ... Testing Fault Isolation Section 101 140 Added the GACVR Fault Circuitry for Pin 23 Modified testing proce dure for GACVRs p ns 2100 1010 51 and 2100 1020 51 Updated the Acquisition Processor test point locations Added new CVR soft ware upload procedure along with Rose utility software upload proce dure Added Table 105 CVR Software Checksums Disassembly Section 303 309 Added steps necessary to dis...

Page 26: ...closure of information on this sheet is subject to the restrictions on the cover page of this document Rev 15 Page xxvi Apr 14 16 THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 27: ...ISIONS REV NO INSERTION DATE BY REV NO INSERTION DATE BY REV NO INSERTION DATE BY 15 Apr 14 16 JG 14 Jul 13 15 JG 13 Dec 09 13 JG 12 Jul 03 13 JG 11 May 21 13 DN 10 Jun 15 12 JM 09 Apr 30 10 GM 08 Jul 30 09 GM 07 Dec 01 08 GM 06 May 01 07 GM 05 Oct 01 04 GW 04 Jan 01 03 JG 03 Mar 01 01 GW 02 Jun 01 00 JG 01 Feb 01 00 GW The document reference is online please check the correspondence between the o...

Page 28: ... 04 Rev 15 Page xxviii Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 29: ...1010 P N 2100 1020 Introduce Moisture Resistant Seals self sealing Chassis Cover CSMU screws to pro tect against excessive moisture intrusion MOD DOT 4 FA2100 CVR FSB005 23 70 04 05 Apr 16 02 P N 2100 1010 00 2100 1010 50 51 Corrects Software Download problem with 30 min recorders Software Revision 02 FA2100 CVR FSB006 23 70 04 06 Sep 22 04 P N 2100 1020 P N 2100 1020 This modification includes re...

Page 30: ...00 1025 Factory modification to track internal produc tion processes for new recorders MOD DOT 8 FA2100 CVR FSB013 23 70 04 13 Dec 14 07 P N 2100 1010 5 P N 2100 1020 5 Introducing a replacement Acquisition Pro cessor PWA p n 205E2502 52 with a coating that protects conductive surfaces from con densation MOD DOT 9 FA2100 CVR FSB014 23 70 04 14 Nov 26 07 P N 2100 1025 02 This modification upgrades ...

Page 31: ... CVR FSB019 23 70 04 19 Feb 13 13 NAND Memory change NAND Memory change Introduction of New Crash Survivable Memory Unit CSMU MOD DOT 14 FA2100 CVR FSB020 23 70 04 020 Jan 10 13 Released Intro of SW Rev 06 Introduction Software Revision 06 FA2100 CVR FSB021 23 70 04 021 Jan 22 14 All P Ns Introduction Software Revision Various FA2100 CVR FSB022 23 70 04 022 Jul 01 15 All P Ns Introduction of the n...

Page 32: ...ce Bulletin 23 70 04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 33: ...partment of Commerce HTSUS Sch B 4901 10 0040 4901 10 0000 LIMITED RIGHTS LEGEND Notice to persons receiving this document and or data This document and or data con tains information in which L 3 Communications Corporation Aviation Recorders Division has a protectable interest and is subject to change without notice The use duplication and or disclosure by persons receiving this document and or da...

Page 34: ... Serial Number Effectivity Part Number Beginning Serial Number New Software Version Audio Compressor PWA P N 2100 3083 00 000840345 and greater 840E2261 07 205E3977 19 2100 3083 10 000849079 and greater 840E3565 08 205E3977 19 2100 3083 50 000846290 and greater 840E3555 07 205E3977 25 B Concurrent Requirements None C Reason A product improvement has been made to the CVDR which enhances the softwar...

Page 35: ...val Operators are not required to apply for modifica tion approval for this change as it does not affect the form fit or function of the top level LRU nor the FA2100CVDR TSO G Manpower 3 0 hours with testing H Weight and Balance Not affected I Electrical Load Data Not changed J Software Accomplishment Summary Model FA2100CVR Document No 818 E1436 20 Revision K K Reference L 3AR Notifications of Ch...

Page 36: ...into the CVDR Customers must specify their request for the new part number on the Repair Exchange order For the 2100 3083 50 the current 205E3997 22 Audio Compression Circuit Board must be sent to the Factory Repair Station for exchange Customers will be sent P N 205E3997 25 ready for installation into the CVDR Custom ers must specify their request for the new part number on the Repair Ex change o...

Page 37: ... Exchange 30 Days For 2100 3083 50 Audio Compres sion Circuit Board 1 ea 205E3977 25 1 746 New 90 Days For 2100 3083 50 Audio Compres sion Circuit Board 1 ea 205E3977 25 1 222 Exchange 30 Days B Tooling For those ROC 6 and ROC 7 test stations operating Microsoft XP and with the in ternal 17TES0046 RECORDER INTERFACE ADAPTER circuit board L 3AR re commends an update to the Recorder Interface ROC 6 ...

Page 38: ...and Availability Keyword Quantity Part Number Price U S D Delivery Read Out Center 7 ROC 7 1 ea 17TES0700 48 000 90 Days Read Out Center 6 ROC 6 1 ea 17TES0400 N A 90 Days CVDR Recorder Interface RI Cable Assembly 1 ea 17TES0057 2 243 90 Days USB Recorder Interface 1 ea 17TES0076 2 060 90 Days The document reference is online please check the correspondence between the online documentation and the...

Page 39: ... RI ADAPTER 17TES0076 FA2100 COMPUTER INTERFACE COMMUNICATIONS CABLE CICC 2 17TES0070 and 17TES0072 READ OUT CENTER 6 or 7 17TES0400 or 17TES0700 Power Input Select RECORDER SOFTWARE CDROM The 17TES0058 cable assembly must only be attached during an upload process and not used when downloading data or getting recorder status CICC LOADER SOFTWARE CDROM CICC INTERFACE SOFTWARE CDROM Typical Bench Se...

Page 40: ...the ROC 3 At the Windows desktop shut down the Recorder Interface RI by right clicking on the RI Icon in the Windows System Tray at the bottom right of the screen Select shutdown 4 To install the CICC Loader from the Windows Start Menu use the Browse button to locate the setup exe file on the CDROM and click the OK button 5 Follow the instructions on the Install Wizard and accept all defaults The ...

Page 41: ...able 2 CICC 2 Interface Cable P N 17TES0072 5 Apply power to the FA2100CVDR Recorder under test 6 Turn ON the power to the ROC 7 Shut down the Recorder Interface RI by right clicking on the RI Icon in the Windows System Tray at the bottom right of the screen Select shut down NOTE You can not use RI and CICC Loader at the same time 8 Note the FDP SMP version and checksum values listed on the label ...

Page 42: ... Loader Window 15 Remove power from the recorder and Exit the CICC Loader utility pro gram 16 Disconnect the Software Upload Cable 17TES0058 from the FA2100 front panel GSE connector and CICC Cable Assembly C To Verify the Software Upload Once the FA2100 software has been loaded it needs to be verified using the CICC Interface utility program on the ROC 6 or ROC 7 Ground Station 1 Connect Computer...

Page 43: ...t the Version Command from the list and left click the Send Command button Observe that a pop up window appears showing the recorder software Part Number and SMP FDP Checksums 7 Match the listed SW Part Number and SMP FDP Checksums with the ones listed on the recorder software CD 8 Left click the OK button and left click the Exit button on the CICC Loader Menu to exit the utility and return to the...

Page 44: ...3555 07 250 30 Days CICC Loader Utility Software Ver 3 0 1 ea 883E1893 12 No Charge 30 Days CICC Interface Utility Software Ver 3 7 1 ea 883E1827 18 No Charge 30 Days For 2100 3083 00 10 Audio Com pression Circuit Board 1 ea 205E3977 19 1 746 New 90 Days For 2100 3083 00 10 Audio Com pression Circuit Board 1 ea 205E3977 19 1 222 Exchange 30 Days For 2100 3083 50 Audio Compres sion Circuit Board 1 ...

Page 45: ...partment of Commerce HTSUS Sch B 4901 10 0040 4901 10 0000 LIMITED RIGHTS LEGEND Notice to persons receiving this document and or data This document and or data con tains information in which L 3 Communications Corporation Aviation Recorders Division has a protectable interest and is subject to change without notice The use duplication and or disclosure by persons receiving this document and or da...

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

Page 47: ...partment of Commerce HTSUS Sch B 4901 10 0040 4901 10 0000 LIMITED RIGHTS LEGEND Notice to persons receiving this document and or data This document and or data con tains information in which L 3 Communications Corporation Aviation Recorders Division has a protectable interest and is subject to change without notice The use duplication and or disclosure by persons receiving this document and or da...

Page 48: ...ith recorders model number FA2100 FA2200 and FA2300 assembled with the NAND memory C Description L 3 Aviation Recorders is now manufacturing model FA2100 FA2200 and FA2300 products with NAND memory devices in the Crash Survivable Memory Unit CSMU Recorders equipped with NAND memory can be identified by their Mod Dot status as shown in Table 1 Additionally NAND recorders will feature the L 3 logo o...

Page 49: ...e PI Unit will be crr The file extension for non modified CVRs older units with NOR memory remains as cvr for all audio downloads Downloaded files with the crr extension may be converted into wav files in the same manner as the cvr files The following are three L 3 AR software products that include the file conversion utilities 1 ROSE Read Out Support Equipment software p n 17TES0321 Version 4 7 a...

Page 50: ...Product Support Engineers or at the factory repair station The cost for the update is 435 00 USD G Tooling Not applicable H Weight and Balance Not affected I Reference Portable Interface PI Unit Operator s Manual part number 165E1630 00 and ECN 015750 II MODIFICATION INFORMATION Incorporation of this Service Bulletin shall be identified by marking Modification 9 on the Portable Interface name labe...

Page 51: ... Interface Mod Dot 9 for 435 The Portable Interface PI Unit must be returned to the Aviation Recorder factory Repair Station for modification Shipping Address L 3 Communications Aviation Recorders 100 Cattlemen Road Sarasota FL 34232 USA Attn Aviation Recorders Repair Department Tel 941 377 5558 L 3 Communications Aviation Recorders Dave Dowding Product Support Manager SB Issue Date Sep 04 2013 Re...

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

Page 53: ...ev 15 xxviii Apr 14 16 Service Bulletin List Rev 15 xxix Apr 14 16 Rev 15 xxx Apr 14 16 Rev 15 xxxi Apr 14 16 Rev 15 xxxii Apr 14 16 List of Effective Pages Rev 15 xxxiii Apr 14 16 Rev 15 xxxiv Apr 14 16 Rev 15 xxxv Apr 14 16 Rev 15 xxxvi Apr 14 16 Rev 15 xxxvii Apr 14 16 Rev 15 xxxviii Apr 14 16 Table of Contents Rev 15 xxxix Apr 14 16 Rev 15 xl Apr 14 16 Rev 15 xli Apr 14 16 Rev 15 xlii Apr 14 1...

Page 54: ...Rev 15 42 Apr 14 16 Rev 15 43 Apr 14 16 Rev 15 44 Apr 14 16 Rev 15 45 Apr 14 16 Rev 15 46 Apr 14 16 Rev 15 47 Apr 14 16 Rev 15 48 Apr 14 16 Rev 15 49 Apr 14 16 Rev 15 50 Apr 14 16 Rev 15 51 Apr 14 16 Rev 15 52 Apr 14 16 Rev 15 53 Apr 14 16 Rev 15 54 Apr 14 16 Rev 15 55 Apr 14 16 Rev 11 56 Apr 14 16 Rev 15 57 Apr 14 16 Rev 15 58 Apr 14 16 Rev 15 59 Apr 14 16 Rev 15 60 Apr 14 16 Rev 15 61 Apr 14 16 ...

Page 55: ...16 Rev 15 144 Apr 14 16 Rev 15 145 Apr 14 16 Rev 15 146 Apr 14 16 Rev 15 147 Apr 14 16 Rev 15 148 Apr 14 16 Rev 15 149 Apr 14 16 Rev 15 150 Apr 14 16 Rev 15 151 Apr 14 16 Rev 15 152 Apr 14 16 Rev 15 153 Apr 14 16 Rev 15 154 Apr 14 16 Rev 15 155 Apr 14 16 Rev 15 156 Apr 14 16 Rev 15 157 Apr 14 16 Rev 15 158 Apr 14 16 Rev 15 159 Apr 14 16 Rev 15 160 Apr 14 16 Rev 15 161 Apr 14 16 Rev 15 162 Apr 14 1...

Page 56: ...5 706 Apr 14 16 Rev 15 707 Apr 14 16 Rev 15 708 Apr 14 16 Rev 15 709 Apr 14 16 Rev 15 710 Apr 14 16 Rev 15 711 Apr 14 16 Rev 15 712 Apr 14 16 Rev 15 713 Apr 14 16 Rev 15 714 Apr 14 16 Rev 15 715 Apr 14 16 Rev 15 716 Apr 14 16 Rev 15 717 Apr 14 16 Rev 15 718 Apr 14 16 Rev 15 719 Apr 14 16 Rev 15 720 Apr 14 16 Rev 15 721 Apr 14 16 Rev 15 722 Apr 14 16 Rev 15 723 Apr 14 16 Rev 15 724 Apr 14 16 Fits a...

Page 57: ... 16 Rev 15 1004 Apr 14 16 Rev 15 1005 Apr 14 16 Rev 15 1006 Apr 14 16 Rev 15 1007 Apr 14 16 Rev 15 1008 Apr 14 16 Rev 15 1009 Apr 14 16 Rev 15 1010 Apr 14 16 Rev 15 1011 Apr 14 16 Rev 15 1012 Apr 14 16 Rev 15 1013 Apr 14 16 Rev 15 1014 Apr 14 16 Rev 15 1015 Apr 14 16 Rev 15 1016 Apr 14 16 Rev 15 1017 Apr 14 16 Rev 15 1018 Apr 14 16 Rev 15 1019 Apr 14 16 Rev 15 1020 Apr 14 16 Rev 15 1021 Apr 14 16 ...

Page 58: ... MATTER 3 B DESCRIPTION AND OPERATION 3 C TESTING AND TROUBLESHOOTING 4 D DISASSEMBLY 4 E CLEANING 4 F CHECK 4 G REPAIR 4 H ASSEMBLY 4 I SPECIAL TOOLS AND TEST FIXTURES 5 J ILLUSTRATED PARTS LIST 5 7 DOCUMENT VERIFICATION 5 8 COMPONENT MAINTENANCE MANUAL CMM EFFECTIVITY 6 9 PART NUMBER FORMATTING 6 DESCRIPTION AND OPERATION 1 GENERAL 1 2 FA2100 CONFIGURATIONS 2 3 SYSTEM DESCRIPTION 4 A Underwater ...

Page 59: ...ce 22 P BIT and Fault Detection 22 4 FA2100 CVR SPECIFICATIONS 23 A Applicable Documents 23 B Physical Characteristics 24 C Electrical Characteristics 24 D Environmental Characteristics 24 E Crash and Fire Protection 24 F CSMU Torque Requirement 24 5 INSTALLATION 24 6 THEORY OF OPERATION 32 A MODEL FA2100 CVR SYSTEM THEORY OF OPERATION 32 B Aircraft Interface AI PWA 33 C Audio Compressor AC PWA 37...

Page 60: ...ard Maintenance System Interface 60 A Label 350 Status Word Output 61 B Label 354 LRU Identification Output 64 C Label 377 ARINC 429 Equipment Identification Word Output 67 D OMS Input 67 10 CVR DATALINK INPUT INTERFACE 67 A Data Link Input and Encapsulation 68 B DataLink Heartbeat 70 C Williamsburg Bit Oriented Protocol Version Support 70 D DataLink Memory Capacity 71 E DataLink Retrieval 71 TEST...

Page 61: ... OUT CENTER 7 ROC 7 CATS Autotest 145 D READ OUT CENTER 7 ROC 7 Autotest Descriptions 162 7 READ OUT CENTER 7 ROC 7 AUDIO DOWNLOAD PLAYBACK 170 8 Underwater Locator Beacon Testing 171 9 MODEL FA2100CVR TROUBLESHOOTING 174 10 FA2100CVR SOFTWARE UPLOAD PROCEDURE 178 A Installing Software Upload Utility and CICC Interface Programs 178 B To upload the FA2100 Software perform the following steps 181 C ...

Page 62: ...nted Wiring Assembly Cleaning 402 B Connector Cleaning 402 C Underwater Locator Device Beacon Cleaning 402 CHECK 1 GENERAL 501 2 CHECKS 501 A Main Recorder Assembly 501 B Mechanical Inspection 501 C Electrical Inspection 502 D Underwater Locator Device ULD 502 REPAIR 1 GENERAL 601 ASSEMBLY 1 GENERAL 701 2 REQUIRED MATERIALS 701 3 ASSEMBLY INSTRUCTIONS 702 A General Assembly Techniques 702 B Acquis...

Page 63: ...3 and IPL Figure 1 Item 80 721 4 STORAGE INSTRUCTIONS 723 A Storage in Original Containers 723 B Storage Without Original Containers 723 C Shipment Container Kit 723 FITS AND CLEARANCES 1 GENERAL 801 2 SYSTEM SPECIFICATIONS 801 A Physical Characteristics 801 B Electrical Characteristics 802 C Environmental Characteristics 802 D Crash and Fire Protection 802 E Torque Requirements 802 SPECIAL TOOLS ...

Page 64: ...BLE OF CONTENTS Cont ILLUSTRATED PARTS LIST 1 GENERAL 1001 2 PURPOSE 1001 3 ABBREVIATIONS 1001 4 EQUIPMENT DESIGNATOR INDEX 1001 5 NUMERICAL INDEX 1002 6 DETAIL PARTS LIST 1002 7 PART NUMBERING 1004 8 MANUFACTURER S CODE 1004 9 L 3 AVIATION RECORDERS L 3AR AUTHORIZED PARTS 1004 10 CONFIGURATION MATRIX 1006 The document reference is online please check the correspondence between the online document...

Page 65: ...Diagram Recorder FA2100 CVR 2100 1X27 XX 28 9 Interwiring Diagram Recorder FA2100 GACVR 2100 10X0 50 51 with Customer Furnished Control Panel 30 10 FA2100 CVR Overall Function Block Diagram 32 11 2 Hr FA2100 CVR pre MOD DOT 7 Word Partition Structure Streams 46 12 2 Hr FA2100 CVR Memory Structure 50 13 Generic DataLink Message Encapsulation Structure 69 101 CVR Fault Circuit for Pin 23 104 102 ROC...

Page 66: ...8 127 Audio Reference Level Utility Confirmation 129 128 Audio Reference Level Utility Warning Message 129 129 Audio Reference Level Utility Menu 130 130 Audio Reference Level Utility File Open Menu 130 131 Audio Reference Level Utility Play Sound 131 132 Sound Card Input Results 131 133 CVR Tester Update Reference Level 132 134 ROC 7 with CVR Automated Test Station Software CATS 2 0 FA2100CVR TES...

Page 67: ...ed Faults and Log Successful 151 157 CATS CVDR Fault History Log 152 158 CATS Continue Test Confirmation 152 159 CATS Test Results Screen 153 160 CATS Connecting Pop Up 154 161 CATS Power Toggle 154 162 CATS Start Test Toggle 155 163 CATS Test Mode and Options Screen 155 164 CATS CVDR Test Confirmation 156 165 CATS CVDR Warning Message 156 166 CATS CVDR Instruction Window 157 167 CATS Power Test I...

Page 68: ...05 FA2100 GACVR Chassis RTV Installation 713 706 FA2100CVR Chassis Cover Installation 714 707 Crash Survivable Memory Unit CSMU Seal Application Pre MOD DOT 13 715 708 Crash Survivable Memory Unit CSMU Seal Application Post MOD DOT 13 716 709 Crash Survivable Memory Unit CSMU Seal Application Post MOD DOT 13 716 710 Crash Survivable Memory Unit CSMU Assembly PRE MOD DOT 6 718 711 Crash Survivable ...

Page 69: ...tion Software CATS FA2100CVR TEST SETUP 914 908 Recorder Interface Cable Assembly 17TES0416 915 909 AC 115 VAC 400Hz Power Input Cable Assembly P N 17TES0411 916 910 DC 28VDC Power Input Cable Assembly P N 17TES0412 916 911 Audio Setup Cable Assembly 17TES0417 917 912 ULD Test Set Up 917 913 FA2100CVR Download Cable p n 17TES0078 Wiring Diagram 920 1 Model FA2100 Cockpit Voice Recorder PN 2100 101...

Page 70: ...ault Warning Failures 55 10 CVR RIPS Pin Assignment for P N 2100 1X25 22 24 2100 1X26 1X27 58 11 CVR OMS Output Words 60 12 CVR Pins Assigned to RIPS Status Monitoring 61 13 CVR Label 350 Output Format 61 14 CVR Fault Reporting Interactions 62 15 CVR Status Word Fault Reporting Criteria 63 101 17TES0400 READOUT CENTER 6 ROC 6 Parts List 134 102 17TES0700 READOUT CENTER 7 ROC 7 Parts List 171 103 U...

Page 71: ...0 04 Rev 15 Page li Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 72: ...0 minute and 2 hour memory storage versions of the FA2100CVR The FA2100CVR is designed as maintenance free recorder No periodic adjustments calibration or maintenance is required to maintain this unit The Model FA2100CVR is considered an ON CONDITION LRU 2 ACRONYMS AND ABBREVIATIONS The following list defines the acronyms and abbreviations used throughout this CMM AC Alternating Current ADLP Audio...

Page 73: ...nent Maintenance Manual F Portable Interface Operator s Manual Part Number 165E1630 00 F Portable Interface 2 Operator s Manual Part Number 165E1630 01 F Installation and Operation Manual Cockpit Voice Recorder Model FA2100CVR Part Number 165E1846 00 F Component Maintenance Manual ED 56A Control Units Preamplifier Micro phone Modules ATA 23 70 05 Part Number 165E1747 00 F FA2100CVR Audio Data Link...

Page 74: ...that one or more of these assemblies is faulty the assem bly ies should be removed and returned to L 3 Aviation Recorders for repair or replacement Attempts to repair any discrete components of these assemblies will void the warranty 6 COMPONENT MAINTENANCE MANUAL CMM DESCRIPTION This CMM consists of a single volume The manual conforms to the intent and form of Air Transport Association of America...

Page 75: ...cuit board assemblies The steps of each procedure are coordi nated with the TESTING AND TROUBLESHOOTING Section Access to subassem blies within the FA2100CVR is described such that there is minimal disturbance to other subassemblies Each major disassembly task is accompanied with a line art exploded view of the subassembly area which is cross referenced to the applicable Illustrated Parts List IPL...

Page 76: ... p n 2100 1010 30 minute and p n 2100 102X 2 hour currently produced 7 DOCUMENT VERIFICATION All CMM drawings illustrations wiring diagrams and block diagrams were validated against existing engineering source material All Testing Fault Isolation Disassembly and Assembly procedures have been verified against the actual performance of the unit under test conditions as indicated in Table 1 below Tab...

Page 77: ...s and product serial number Effectivity of the manual is identified by a list of effective pages in the front of the manual 9 PART NUMBER FORMATTING L 3AR does not delineate its part numbers by special characters such as the dash character L 3AR considers its part numbers with or without the use of special characters to be the same for example there is no difference between part number 266 E0305 0...

Page 78: ...that is used to date time stamp the downloaded voice or flight data files This is not a function of the readout time displayed for voice or data The GMT inputs are the true time of the recording Data can also be displayed during readout as relative time based on file size If the file date time stamp is not displaying the proper time of the download this is not a fault condition that will im pede t...

Page 79: ...U ULD GSE CONNECTOR BEHIND DUST COVER HARDWARE AND SOFTWARE MODIFICATIONS Figure 1 Model FA2100 Cockpit Voice Recorder FA2100CVR 2 FA2100 CONFIGURATIONS The current configurations of the FA2100CVR s are listed in Table 2 below and with its specific part number in the IPL Section Figure 1 Item 1A through Item 1AB The document reference is online please check the correspondence between the online do...

Page 80: ...0 1025 22 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY W RIPS 10 6 max Figure 1 2100 1025 24 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY W RIPS S W 10 6 max Figure 1 2100 1026 02 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY W RIPS 10 6 max Figure 1 2100 1027 02 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY W RIPS 10 6 max Figure 1 2100 1220 00 ARINC 757 2 HR CVR 1 2 ATR SHORT 90 DAY BE...

Page 81: ...cquisition Processor PWA and the Crash Survivable Memory Unit CSMU which contains the solid state flash memory used as the recording medium A Underwater Acoustic Beacon The Model FA2100 FDR has an underwater acoustic beacon mount located on its front panel which also acts as the recorders carrying handle The ULB mount will accept ei ther a 30 day or a 90 day underwater locator beacon The ULB meets...

Page 82: ...te grated into the FA2100CVR electronics The removable circuit boards include the Aircraft Interface PWA Audio Compressor PWA and Acquisition Processor PWA C Power Control and Monitor Signal Interface Characteristics Input power may be 115 Vac 400 Hz or 28 Vdc PN 2100 10X0 5X units are 28 Vdc only At normal power level an interruption equal to or less than 200 millisec onds will not affect the Mod...

Page 83: ...MORY TO AIRCRAFT FAULT MONITORING SYSTEM GSE OUTPUT COCKPIT AREA MICROPHONE CAM STOP RECORDING AUDIO COMPRESSOR PWA FA2100 CVR CVR FAULT TO GROUND STATION TEST EQUIPMENT GMT_IN_B 429 GMT_IN_A 429 ROTOR_SPEED_IN_LO ROTOR_SPEED_IN_HI GEAR BRAKE AUDIO OUT 18 VDC For GA versions refer to Figure 4 28 VDC OR 115 VAC 400 Hz S055 Mics have 4 Lines to the C U S056 MICS have 3 Lines to the C U OMS OUTPUT A ...

Page 84: ...TED SOLID STATE MEMORY TO AIRCRAFT FAULT MONITORING SYSTEM GSE OUTPUT COCKPIT AREA MICROPHONE CAM 3 STOP RECORDING AUDIO COMPRESSOR PWA FA2100 GACVR CVR FAULT TO GROUND STATION TEST EQUIPMENT GMT_IN_B 429 GMT_IN_A 429 ROTOR_SPEED_IN_LO Input Z 100 Kohms ROTOR_SPEED_IN_HI GEAR BRAKE AUDIO OUT ATTENUATION 4 1 Used for GA versions only The GA versions do not use a control unit however the other input...

Page 85: ...t panel of the control unit via a 600 ohm headset The monitor audio signal has a reference input level of 2 55 Vrms into 600 ohms applied to one input channel In the 2100 1010 30 minute recorders the monitored Audio Output signal to the control unit is developed by summing together the High Quality Voice for Channels 1 2 3 and the Cockpit Area Microphone CAM Channel 4 In the 2100 1020 pre MOD DOT ...

Page 86: ... 400 Hz ERASE A C 3rd Crew Member Spare Audio Cockpit Area Mic CAM Audio CH 4 CH 2 HQ 150 3500 Hz CH 3 HQ 150 3500 Hz CH 4 HQ 150 6000 Hz ERASE TO CONTROL UNIT HEADSET JACK AUDIO OUT CH 2 CH 1 CH 3 CH 1 HQ 150 3500 Hz FA2100 CVR PUSH TO TEST 620 Hz 660 Hz HQ CH1 HQ CH2 HQ CH3 HQ CAM BULK ERASE 400 Hz ERASE A C CH 2 HQ 150 3500 Hz CH 3 HQ 150 3500 Hz CH 4 HQ 150 6000 Hz ERASE TO CONTROL UNIT HEADSE...

Page 87: ...61 Control Units Refer to the Component Maintenance Manual ED 56A Control Units Preamplifier Microphone Modules ATA 23 70 05 Part Number 165E1747 00 The 18 Vdc is a short circuit protected 30 mA line 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 st...

Page 88: ...is used in an ARINC 557 757A configuration with interface to the air craft provided through a 57 pin DPXB rear panel connector The Reference Signal as required by ED 56A ED 112 is defined as an input signal with a frequency of 1 kHz at an input level of 3 Vrms for Channels 1 2 and 3 and 2 Vrms for Channel 4 The Audio input sensitivity level is 05 Vrms 3 Vrms for Channels 1 2 and 3 and 02 2 Vrms fo...

Page 89: ...tial pulse code modulation ADPCM processor These four streams are recorded as high quality HQ audio for a 30 minute dura tion In the case of P N 2100 1X25 1X26 1X27 XX and 2100 1X20 XX MOD DOT 7 these HQ Channels are recorded for 120 minutes The rate of the data stream recorded varies with the type of audio as follows F 24 kbps for CH 1 2 and 3 HQV F 48 kbps for CH 4 HQC In the 120 minute FA2100CV...

Page 90: ...ed 30 minutes GMT 2 Wds per 1 Sec 120 minutes RSE 2 Wds per 1 2 Sec 120 minutes 429 GMT Time Code Rotor Speed CSMU FLASH MEMORY CH 1 HQV 150 3500 Hz CH 2 HQV 150 3500 Hz CH 3 HQV 150 3500 Hz CH 4 HQC 150 6000 Hz Pilot Audio CH3 3rd Crew Member Spare Audio CH1 Cockpit Area Mic CAM Audio CH 4 Co Pilot Audio CH2 Low Speed ARINC 429 GMT 12 5 kbps RSE 7 6000 Hz Pilot Audio CH3 3rd Crew Member Spare Aud...

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

Page 92: ...20 minutes 120 minutes 120 minutes 120 minutes Not available Not available NOTE All of the times indicated in the above chart are minimum recording times 2 GMT FSK Output Signals In addition to the voice channel inputs in the 2100 1010 and 2100 1X2X configurations GMT is applied as low speed 12 5 kbps ARINC 429 to pins 25 and 26 with the exception of 2100 1X20 02 configurations FSK option In the 2...

Page 93: ...ed to the rear connector pins 39 and 40 as a low speed ARINC 429 signal The OMS output signal is sent out on pins 50 and 51 as a high speed ARINC 429 signal along with the Data Link output signal The Recorder records the FA2100 CVR OMS status word only but is also used to send status messages to the aircraft s OMS computer Basically there are two modes for sending messages to the OMS computer Norm...

Page 94: ... a security feature implemented to protect the rights of pilots and other flight crew members The Cockpit Area Microphone CAM pilot co pilot and spare audio can be moni tored during recording using a headset plugged into the 1 4 inch 600 ohm phone jack mounted on the front panel of the associated control unit G Storage Capacity The Model FA2100CVR storage media is designated as the Crash Survivabl...

Page 95: ...1X27 model any one of the high quality audio channels or the cockpit area microphone channel The PI or PI 2 Unit also has the capability to search through the stored data using the fast forward and fast reverse command keys The fidelity of the FA2100CVR audio data output at the PI or PI 2 Unit is such that its internal speaker allows quality analysis of the recorded data The PI or PI 2 Unit also s...

Page 96: ...form a continuous test of all bits within the solid state memory located in the Crash Survivable Memory Unit CSMU An additional built in test is initiated by pressing a green TEST pushbutton located on the front panel of the control unit Models S151 S161 S152 S162 or S251 S261 A green TEST indicator is located on the front panel of the Model S151 S161 S152 S162 and S251 S261 Control Units to indic...

Page 97: ...rotection requirements of EUROCAE ED 56A ED 112 and TSO 123a M Control Unit Microphone Preamplifier Equipment Refer to Aviation Recorders ED 56A Compliant Control Unit Preamplifier and Micro phone CMM ATA No 23 70 05 Part Number 165E1747 00 for more detailed infor mation of these ancillary recorder components A Control Unit or Preamplifier is a required component of a CVR installation and function...

Page 98: ...ply with TSO C123a and EUROCAE ED 56A However because ARINC Characteristic 757 does not address microphone preamplifiers the Model S150 S160 Preamplifiers are not considered ARINC 557 757 compliant The S150 S160 provides the same preampli fier circuit for the cockpit area microphone as the Model S151 S161 Model S152 S162 and Model S251 S261 Control Units The FA2100CVR is compatible with installati...

Page 99: ...vely cleared by a properly operating Store Manager Processor SMP as the recorder powers up Next a watchdog circuit monitors the operation of the SMP and associated circuitry This assures that a fault is asserted in the event of a processor failure including par tial failures such as arithmetic errors inordinate increments and logic errors The watchdog circuit will also be activated in the event of...

Page 100: ...ecorder Systems 1 TSO C123b Federal Aviation Agency Technical Standard Order TSO C123b Techni cal Standard Order for Cockpit Voice Recorder Equipment 2 EUROCAE MOPS ED 55 European Organization for Civil Aviation Electronics Minimum Operational Performance Specification for Flight Data Recorder Systems 3 EUROCAE MOPS ED 56A European Organization for Civil Aviation Electronics Minimum Operational Pe...

Page 101: ...ental characteristics refer to Section 800 Fits and Clearances E Crash and Fire Protection For specific crash and fire protection specifications refer to Section 800 Fits and Clearances F CSMU Torque Requirement For specific CSMU torque requirements refer to Section 800 Fits and Clearances 5 INSTALLATION The information provided in this section is for general knowledge use only For authorized deta...

Page 102: ...ier 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 Microphone information can be found in CMM ATA No 23 70 05 p n 165E1747 00 for ED 56A installations or the FA2100CVR Installation Operation manual p n 165E1846 00 The document reference is onli...

Page 103: ...28 Vdc 1 2 7 FROM CAPTAIN S CLOCK AREA MICROPHONE FROM ROTOR SPEED SENSOR TO PILOT MICROPHONE SPARE MICROPHONE TO 3RD CREW MEMBER OR PA SYSTEM TO CO PILOT MICROPHONE 4 7 3 9 11 9 11 8 STANDARD INTERWIRING PER ARINC SPEC 757 Refer to Notes for Figure 7 BRAKE GEAR BRAKE 3 3 6 10 1A 5A OR TO C U GND 28 Vdc POWER IN STOP RECORDING RIPS ACTIVE INPUT 12 8 For GACVR versions refer to Figure 9 13 ERASE C ...

Page 104: ...IPS Active function the CVR has a backup power source or RIPS available pins 10 29 38 and 42 will be used for the RIPS Status Monitoring 8 BITE status output ground no fault open fault or CVR not installed 9 Audio input 3 Vrms maximum 10 In 2100 1010 and 2100 1X20 configurations GMT is inputted as low speed 12 5 kbps ARINC 429 to pins 25 and 26 with the exception of 2100 1X20 02 configurations FSK...

Page 105: ...ONTROL UNIT TO AC COLD TO 115 VAC 400 HZ 1 AMP 2 8 3 4 3 3 7 8 6 9 10 10 11 10 11 OR 115 VAC POWER IN HOT 115 VAC POWER IN COLD PREAMP PWR OUT GND PREAMP PWR OUT HOT 18 VDC REG PUSH TO TEST PREAMP PWR GND PREAMP PWR HOT 18 VDC REG CHASSIS GND VOICE ERASE A VOICE ERASE C OUTPUT LO OUTPUT HI MIC INPUT LO MIC INPUT HI MIC BIAS AUDIO MONITOR LO AUDIO MONITOR HI MIC BIAS WHITE MIC HIGH BLACK MIC LOW SH...

Page 106: ...ields to be grounded at the airframe using short connections Tie shields to existing single point GND used for Pin 17 see Note 3 8 If the power source has battery back up a means for terminating recording after a crash should be included in the aircraft wiring Grounding pin 10 terminates recording within 10 minutes 9 BITE status output ground no fault open fault or CVR not installed 10 Audio input...

Page 107: ...OCK TYPICAL AUDIO JACK LO AUDIO JACK HI ATTENUATION COMMON 6dB ATTENUATION 12dB ATTENUATION 24dB ATTENUATION 6 STOP RECORDING CVR FAULT 8 MICROPHONE CONTROL PANEL OPEN IN FLIGHT CLOSED WEIGHT ON WHEELS TO ANNUNCIATOR PANEL ERASE C NC NO PUSH TO TEST MOMENTARY PUSH BUTTON GMT IN B 429 LO GMT IN A 429 HI FROM CAPTAIN S CLOCK FROM ROTOR SPEED SENSOR ROTOR SPEED IN LO ROTOR SPEED IN HI TEST INDICATOR ...

Page 108: ...rt connec tions Tie shields to existing single point GND use for Pin 17 see Note 4 6 If the power source has battery back up a means for terminating recording after a crash should be included in the aircraft wiring Grounding pin 10 terminates record ing within 10 minutes 7 Audio input 3V rms maximum 8 Wiring shown for fixed attenuation of 18 dB 9 Per FAA Action Notice A8300 56 dated Jan 24 1990 th...

Page 109: ...NC 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 The re corder interfaces with the aircraft s cockpit recorder control unit and microphone through the rear panel connector J1 and with the Ground Station Equipment through the front panel GSE c...

Page 110: ...ere Used Aircraft Interface PWA P N Model Effectivity Notes 205E250305 2100 1010 00 2100 1020 00 2100 1020 02 2100 1220 00 2100 1220 02 205E250301 2100 1025 02 2100 1025 12 2100 1025 22 2100 1025 24 2100 1026 02 2100 1225 22 2100 1225 24 2100 1226 02 205E250308 2100 1027 02 2100 1227 02 Data Link On board Maintenance System OMS 205E176311 2100 1010 50 2100 1010 51 2100 1020 50 2100 1020 51 Specifi...

Page 111: ...put power as defined in RTCA DO 160C Section 16 AUDIO OUT HI LO Combined high quality voice and CAM channels to provide au dio monitor output With the reference signal applied to one channel the output level is 2 45 Vrms 30 into a 600 ohm load 350 400 mVrms into an 8 ohm load for the 93 configura tion RECORD ON A B CVR is in Record Mode when A and B are jumpered A is grounded internally 28 VDC POW...

Page 112: ...ce is greater than 10 kohms CHANNEL 4 AUDIO IN HI LO CAM audio input Reference signal is 1 kHz at 2 Vrms Input impedance is greater than 10 kohms ROTOR SPEED IN HI LO Rotor speed input data as defined in ARINC 557 757 7 6000 Hz Analog Frequency Input VOICE ERASE A C No Bulk Erase if A is grounded or connected to C for less than 0 5 seconds Bulk Erase occurs if A is connected to C for 2 or more sec...

Page 113: ...output 5 V through 15 kohms when not asserted Ground through 10 kohms when asserted TEST L Conditioned PUSH TO TEST signal output 5 V through 10 kohms for not asserted Less than 0 4 V sinking 3 5 ma when asserted AUDIO OUT Audio monitor data input from Audio Compressor Signal level is 2 55 Vrms 30 into 622 ohms when Reference Signal is applied to one CVR audio input AUDIO OUT RTN Return signal for...

Page 114: ...e is 2 volts Current requirement is less than 25 ma 15VDC 15 volt output made from Storage Supply input voltage Tracks the unregulated input below about 15 volts and then regulates at that lev el 18VDC of the main supply is diode coupled to this signal and provides the power after the main supply is running Maximum cur rent required by Aircraft Interface is 20 ma The Aircraft Interface can supply ...

Page 115: ...dio Compressor are output to the Aircraft Interface for audio moni toring Power ground and a master reset for the Audio Compressor are derived from the Acquisition Processor PWA The Audio Compressor PWA interfaces with the Aircraft Interface and the Acquisition Processor The AC AI interface comprises four audio input channels an audio monitoring output channel a serial ARINC 429 GMT data input cha...

Page 116: ... inputs The ED 56A and ED 112 reference voltage input to the AC for Channels 1 3 is 2 0 Vrms into a 10 kohm load and a specified bandwidth of 150 3500 Hz Input Channel 4 cor responds to the Cockpit Area Microphone CAM audio input This channel has an ED 56A and ED 112 reference voltage input of 1 33 Vrms input into a 10 kohm load with a specified bandwidth of 150 6000 Hz An audio channel return gro...

Page 117: ...or Interface The AC AP Interface includes the following signals a Serial TDM Bus signals TCLK TFRM TADD and TDAT b Master Clock Input F8 192 MHz c Master Reset AC RESET L d BIT Control Input TEST MODE L e Power Ground Signals V5N V5P and GND The TCLK and TFRM signals are generated by the Acquisition Processor and provide bit and TDM frame synchronization respectively TADD and TDAT are bidirectiona...

Page 118: ...02 205E250238 2100 1010 50 2100 1010 51 2100 1020 50 2100 1020 51 Compatible with 3V Intel Memory The Acquisition Processor interfaces with three internal functional modules Aircraft Interface Audio Compressor and CSMU Additionally is an external interface to the Ground Support Equipment GSE 1 Aircraft Interface The Aircraft Interface AI Interface involves the following external power inputs and o...

Page 119: ... data messages to the AP only in response to commands issued by the AP Additionally 5 V and 12 V power for the CSMU and CSMU reset are routed through this interface 4 Ground Support Equipment Interface The Ground Support Equipment GSE Interface consists of the buffered TDM bus the multiplexed buffered high speed serial buses multiplexer control in put test mode control input program flash power co...

Page 120: ... audio data This software is self contained and runs separately from the system software As defined in RTCA DO 178B the Criticality Category of the Model FA2100CVR is classi fied as Minor Accordingly the software in the FA2100 CVR will comply with the Level D requirements of RTCA DO 178B A Store Manager Processor Software Organization The SMP software is organized as a multi tasking environment wi...

Page 121: ...state for recovery of recorded audio The CVR Executive processes the input digital audio channel data and man ages the actual record or playback operations The Flash Manager acts as a server task supporting all accesses to the crash protected flash memory devices Likewise the NVRAM Manager task provides a similar interface function to the non volatile RAM used for memory index and configuration in...

Page 122: ...reams into a form ready for storage into the CSMU The complete sequential process is described in the steps be low a The TDM interrupt handler receives the audio data stream from the Audio Compressor hardware and buffers it into 8 ms blocks of data Each of these blocks contains four 2 ms frames of interleaved digital samples of the HQV HQC SQV and SQC audio channels Each 2 ms frame also contains s...

Page 123: ...C SF SF SQV 2 36 Word Frames per 72 ms Superframe 1 36 Word Special Frame per 4 Superframes SQV SF SPCL X SF SF SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SQC SF SQC SQC 2 36 Word Frames per 72 ms Superframe Special Frame Rotor Speed GMT Discretes FDR Sync Mark Block headers Block boundaries Not Shown SPCL X 36 Wd 36 Wd 36 Wd 36 Wd SF SQV SQV SF SQV SQV SF SQV SQV SF SQV SQV SF SQ...

Page 124: ...has been completely processed through the CSMU While in the record state the Mode Executive monitors the delayed shutdown input to the CVR If asserted and held this will cause the Mode Executive to start a shutdown timer If the timeout occurs within 10 minutes Mode Execu tive will set a shutdown flag which is polled by the CVR Executive This results in a shutdown of record operation until the dela...

Page 125: ...ta before the power fail re set occurs e After the NVRAM values have been updated the CVR executive enters an idle loop waiting for power to drop If the power fail indicator relents the CVR executive will perform a re initialization and re enter the record state 4 Data Playback State Data Playback state is enabled when the SMP Mode Executive task detects a playback request command from the GSE via...

Page 126: ... push to test state which is initiated and controlled by the push to test discrete input to the CVR Assertion of the push to test input usually by depressing a push button on the control unit in the cockpit is detected by the Mode Executive task Once this input is detected the Mode Executive will start the test sequence which takes about two seconds to complete A 640 Hz analog tone of about 200 ms...

Page 127: ...s many memory devices for 30 minutes of high quality recording as it does for 120 minutes of standard quality recording For 30 minute recorders the total amount of physical memory capacity is 24 megabytes For 120 minute recorders the memory capacity is 60 megabytes 2M Words HQV 4 Chips 30 Min HQC 3 Chips 30 Min SQV 4 Chips 120 Min SQC 4 Chips 120 Min HQV High Quality Voice HQC High Quality CAM SQV...

Page 128: ...omalies This includes all messaging between tasks SMP to CSMU and SMP to GSE The digitized audio data input stream from the Audio Compressor board is also monitored for integrity The software also monitors itself for illegal or unexpected operations Fault informa tion is stored in the NVRAM fault history log The log can contain about 275 entries Of these the first 255 entries are considered as pri...

Page 129: ...on The type of event field categorizes the general nature of the fault conditions Reported categories include Table 8 Fault Processing Event Types and Descriptions Type of Event Description Internal Faults illegal or unexpected software errors CSMU flash memory errors flash memory write or erase errors BITE errors detected power supply faults Communications errors illegal or unexpected GSE message...

Page 130: ...e of two DSPs One DSP called the Flight Data Processor FDP is responsible for the collection processing and forwarding of Data Link messages The other processor called the Storage Management Proc essor SMP is responsible for the collection of audio data the management of the CSMU and other ancillary functions Communication between the two processors will be over the device specific TDM time divisi...

Page 131: ...X26 1X27 only The CVR is identified as a BITE Standard A equipment so as to be portable to other AIRBUS programs The CVR interfaces with the OMS through a system BITE such that the CVR will pass fault information to the OMS via SCI and receive test request based on two ARINC 429 buses as per a BITE Type 1 principle F Use of one ARINC 429 High Speed HS output bus for continuous fault reporting by m...

Page 132: ...audio circuit Control Unit loads Its pow er supply below 15 5 Volts Failure of the recording medium Failure of the recording medium Failure of the recorder to store Information In the storage medium Failure of the recorder to store Information In the storage medium Insufficient audio or UTC time record duration Insufficient datalink record duration CVR Inhibited pin 10 acti vated CVR Inhibited pin...

Page 133: ... that the crew can re initiate the test after a fault is detected in the hope of recovering the re corder test is specified to act as a reset of the recorder F Bulk Erase As per ARINC 757A the CVR provides a Bulk erase function In order to ensure reli able operation the function is inhibited to prevent inadvertent or untimely erasure while the aircraft is capable of moving under its own power In a...

Page 134: ... event FSK or ARINC 429 time reference is not available Label 350 Bit 17 indicates the status of the clock as the following 0 ok and 1 fail ure H Data downloading P N 2100 1X25 1X26 1X27 only It is possible to download the Data Link message data from the crash protected me dium while the recorder is installed on the aircraft as per ED112 Part IV IV 2 2 3 The L 3AR Portable Interface 17TES0043 PI 1...

Page 135: ... the data will be able to be retrieved using the existing support equipment for analysis Table 10 CVR RIPS Pin Assignment for P N 2100 1X25 22 24 2100 1X26 1X27 Pin Number Pre RIPS Pin Assignment RIPS Pin Assignment 10 CVR Stop Recording RIPS Active Input 29 FDR Rate A RIPS Fault Input 38 FDR Rate B RIPS Maintenance Input 42 CVR Ident Pin Program RIPS Present Pin Program 1 RIPS Active The CVR will...

Page 136: ...itted in the Label 350 Label 351 and new Label 352 outputs as follows RIPS Mainten ance Status CVR Discrete in put Pin 38 SSCVR Label 350 and 352 Bit 20 SSCVR Label 351 Bit 19 No Mainten ance required Open 0 1 Maintenance required Ground 1 0 4 RIPS Present Use of CVR Pin 42 CVR Ident is being used for the RIPS Present Pin Pro gram Since we do not anticipate more than one CVR installed on any curre...

Page 137: ...information on the RIPS see P N 165E4900 00 Installation and Operation Instruction Manual for Recorder Independent Power Supply RIPS 9 On board Maintenance System Interface The 2100 1025 22 24 CVR includes an ARINC 429 high speed On board Main tenance System OMS output interface Pins 50 51 and an ARINC 429 low speed OMS input interface Pins 39 40 The OMS input interface is only used for OMS heartb...

Page 138: ...Required 42 RIPS Present Pin Program Open No RIPS Installed Ground RIPS Present If the RIPS is not present then the CVR will not monitor the RIPS status inputs and they will not be reported default to 0 in Label 350 output A Label 350 Status Word Output The CVR will report status using Label 350 on the OMS ARINC 429 output word as shown in Table 1 3 below Table 13 CVR Label 350 Output Format BIT N...

Page 139: ...able 14 CVR Fault Reporting Interactions L350 BIT N FUNCTION REPORTED WITH L350 BIT 11 REPORTED WITH PUSH TO TEST REPORTED WITH CVR FAULT DIS CRETE 11 CVR Status Audio Recording Failure YES YES YES 12 CMC Bus Status OMS Input NO NO NO 13 CVR Control Unit Failure YES YES YES 14 FDR Status not used NO NO NO 15 RIPS Fault Status Pin 29 NO NO NO 16 CVR DataLink Recording Failure NO NO NO 17 Clock Stat...

Page 140: ...ng Criteria L350 BIT N FUNCTION FAILURE CRITERIA 11 CVR Status Audio Record ing Failure Any internal CVR failure that prevents correct record ing of the audio inputs including CU failure and Push to Test audio input circuit failure May relent depending on fault severity 12 CMC Bus Status OMS In put Loss of OMS input Heartbeat valid Label 227 input for more than 3 seconds Relents if OMS Heartbeat i...

Page 141: ...appropriate ground support equipment for review and analysis B Label 354 LRU Identification Output The CVR LRU IDENTIFICATION consists of multiple ARINC 429 words for the trans mission of the CVR part number and serial number The group of eleven ARINC 429 words defined below is transmitted twice per second a Start of Transmission Word Bit No Function Status 1 8 Label 354 11101100 9 16 Number of wo...

Page 142: ...atus 1 8 Label 354 11101100 9 15 Sixth character of part number 16 Not used 0 17 23 Seventh character of part number 24 Not used 0 25 31 Eighth character of part number 32 Parity f Part Number continued Bit No Function Status 1 8 Label 354 11101100 9 15 Ninth character of part number 16 Not used 0 17 23 Tenth character of part number 24 Not used 0 25 31 Eleventh character of part number 32 Parity ...

Page 143: ...rial Number continued Bit No Function Status 1 8 Label 354 11101100 9 15 Fifth character of serial number 16 Not used 0 17 23 Sixth character of serial number 24 Not used 0 25 31 Seventh character of serial number j Serial Number continued Bit No Function Status 1 8 Label 354 11101100 9 15 Eighth character of serial number 16 Not used 0 17 23 Ninth character of serial number 24 31 Not used 0000000...

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

Page 145: ...e ARINC 619 formatting which provides the Network layer interface However the FA2100CVR records data at the link layer in terface level and is unaffected by any link layer or above data content This means that the CVR will record all 32 bits of each and every SAL 157 or 156 word received on the DataLink input As a result the CVR will not be impacted by any changes or additions to the ap proved Dat...

Page 146: ...S C Length ASCII Message Area ARINC 623 ATIS Display Server Length 0 2 3 5 1 4 6 Figure 13 Generic DataLink Message Encapsulation Structure As indicated in Section 1 above the FA2100 DataLink CVR also includes an ARINC 429 OMS output interface Pins 50 51 that provides a Label 350 CVR status word output once per second This word in its entirety along with any DataLink Label 270 or 276 input status ...

Page 147: ...ently support Williamsburg Version 1 protocol or a low speed ARINC 429 interface for input of DataLink informa tion However the CVR does support the Williamsburg ALOHA exchange even though it is not required for Williamsburg Version 3 DataLink input In the event that the CVR receives a valid ALO input on the SAL Label 157 or 156 it will respond with a valid Label 304 ALR output indicating support ...

Page 148: ...e same way as audio data All or a portion of the DataLink recording can be downloaded from the CVR using Ground Support Equipment supplied by L 3 Aviation Recorders The Portable Interface can be used to download the DataLink recording to a PCMCIA memory card The DataLink recording can also be downloaded using the CICC 2 or CICC 3 interface cable connected to a PC The downloaded DataLink file can t...

Page 149: ... and Operation 23 70 04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 150: ...00 1X27 XX require the ROC 7 and CATS 2 0 This section provides operational level testing procedures for the Model FA2100 Cockpit Voice Recorder when using the CVR Automated Test Station CATS software p n 17TES0420 The CATS software v1 0 or 1 1 is contained on the L 3AR Read Out Center 6 ROC 6 p n 17TES0400 and is used in conjunction with the L 3AR Recorder Interface Unit RIU p n 17TES0410 The CAT...

Page 151: ... surface mount technology SMT The repair of a PWA containing SMT de vices requires specialized training and factory equipment along with special trouble shooting and soldering techniques therefore L 3 Communications Aviation Record ers has deemed that PWAs containing SMT devices are not to be repaired in the field As a result the Model FA2100CVR s maintenance philosophy is to level 2 board replace...

Page 152: ...built in test feature has been designed to perform a continuous test of all bits within the solid state memory located in the Crash Survivable Memory Unit CSMU Any faults with the unit are stored in non volatile RAM as a fault history log to aid in troubleshooting An additional built in test is initiated by pressing a green TEST pushbutton located on the front panel of the control units Model S151...

Page 153: ... into the microphone at a normal voice level You should be able to hear your words without any significant distortion Bulk erasure of the Model FA2100CVR storage medium is accomplished using the associated control unit red ERASE pushbutton switch Aircraft wiring interlocks must be set that is landing gear must be down and brakes locked to allow the CSMU solid state flash memory to be erased To era...

Page 154: ...ead Out Center 6 ROC 6 P N17TES0400 L 3AR Read Out Center 7 ROC 7 P N17TES0700 CVR Automated Test Station Software CATS P N 17TES0420 L 3AR Beacon Test Set P N 17TES0015 Dukane Beacon Test Set Dukane 42A12 10 Mohm High Impedance Voltmeter Commercially Available Audio Data Link Player ADLP Software P N 17TES0423 ADLP Software is only required for FA2100CVR P N 2100 1X25 1X26 1X27 for playback only ...

Page 155: ... ROC 6 Interconnects CAUTION Make certain that all power is turned off before attaching cables Failure to turn off power before attaching cables will result in immediate and serious damage to the unit CAUTION Only connect DC OR AC input voltage Do not connect both input voltages at the same time 1 Connect input power as detailed below depending on the type of input power used a For DC power connec...

Page 156: ...SND IN J3 cable to the Sound Card Line In or Microphone In which is the blue connector 6 Attach the RIU Sound Card Out SND OUT J5 cable to the Sound Card Line Out which is the green connector 7 Connect the DIN CABLE from the speakers to the middle Speaker Out SPKRS OUT J6 connector on the front panel of the RIU 8 After all connections are made to the RIU apply power to the RIU This can be either 2...

Page 157: ...PUT SPKRS J9 RCDR AC PWR TEST RECORDER INTERFACE UNIT RIU 17TES0410 SND IN BLUE 17TES0413 SND OUT GREEN 17TES0413 J4 J2 J1 L SPKR R SPKR YELLOW AC RED DC AC 1A DC 5A USB Note Speakers are optional and not incld with ROC 6 To order speakers from L 3AR use p n 17TES0425 110V or 17TES00426 220V FA2100 SOFTWARE UPLOAD CABLE ASSEMBLY 17TES0058 use for software uploading only BLUE GREEN SND IN SND OUT S...

Page 158: ...en follow this procedure 2 Click the Speaker button Volume Control to display the Playback Control menu 3 Click on the Options pull down and then click on Properties 4 Click the Recording radio button 5 Select the Line In check box all other boxes should not be checked 6 Click Ok Figure 103 Volume Control Properties 7 At the Record Control menu under Line In check the Select box 8 Move the Line In...

Page 159: ...f this document Figure 104 Line In Input Level 9 Click on the Options pull down and then click on Properties 10 Select the Playback radio button 11 Select the following check boxes Play Control Wave and Line In All other boxes should not be checked 12 Click Ok Figure 105 Sound Card Properties The document reference is online please check the correspondence between the online documentation and the ...

Page 160: ... page of this document 13 Move the Playback and the Wave Volume Controls to full volume and check the Mute box on the Line in Mute should not be checked for all others Figure 106 Playback Control Volume Levels 14 Close the Play Control menu by clicking on the X in the upper right corner The document reference is online please check the correspondence between the online documentation and the printe...

Page 161: ...IU us ing the cable p n 17TES0416 for the recorder rear connector and cable p n 17TES0072 for the recorder front connector b Setup an in line RMS multimeter Set to DC amps c Apply power to the RIU using 28 Vdc d If the CATS test page is not shown Click the L 3 CVR Test Icon on the Window desktop Click the Ok button on the Monitor Audio Channel Pop up menu e From the pull down menu click on Power a...

Page 162: ...age of this document l Read and click on Yes Figure 107 CVR Test Start Toggle m Read and click on OK Figure 108 CVR Test Warning Message n Remove front cable and click on OK Figure 109 CVR Test Instruction Message o Enter in the current value in amps typically 17 in window and click on OK The document reference is online please check the correspondence between the online documentation and the prin...

Page 163: ...in window and click on OK Figure 111 CVR Test Power Consumption Entry r Connect the recorder front cable and click on OK Figure 112 CVR Test Instruction Message s Verify that the DC LED on the front of the RIU is on t Observe the Fault History Log window appears Select Print if you want to save the fault history or Close to continue u Click on Yes The autotest will now proceed in completing the au...

Page 164: ...a Ensure that the RIU has no power applied Power is removed Connect a CVR to the RIU using the 17TES0416 for the recorder rear connector and 17TES0072 for the recorder front connector b Setup an in line RMS multimeter Set to AC amps c Apply power to the RIU using 115Vac d If the CATS test page is not shown Click the L 3 CVR Test Icon on the Window desktop Click the OK button on the Monitor Audio C...

Page 165: ...ice is checked k From the pull down menu click on Test Start Test l Follow the instructions below as it appears presented by the software m Read and click on Yes Figure 114 CVR Test Instruction Message n Read and click on OK Figure 115 CVR Test Warning Message o Remove front cable and click on OK Figure 116 CVR Test Instruction Message p Enter in the current value in amps typically 085 in window a...

Page 166: ...in window and click on OK Figure 118 CVR Test Power Consumption Entry s Connect the recorder front cable and click on OK Figure 119 CVR Test Instruction Message t Verify that the AC LED on the front of the RIU is on u Observe the Fault History Log window appears Select Print if you want to save the fault history or Close to continue v Click on Yes The autotest will now proceed in completing the au...

Page 167: ... the fault history log by the pull down menu click on Test Clear Fault History D READ OUT CENTER 6 ROC 6 Autotest Descriptions The following provides detailed descriptions of the test performed during the autotest function 1 Power 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 the OK but ton Please ente...

Page 168: ...08 02 42 PASSED Bulk Erase 1 Expected 400 Hz Results 400 0 Hz 08 02 50 PASSED Bulk Erase 2 with active Rotor Speed Expected 400 Hz Results 123 0 Hz 08 02 58 PASSED Bulk Erase 3 with No Recording Expected 400 Hz Results 3334 6 Hz 4 Test Tone Enable push to test and verify push to test indicator is set Example report message s 08 03 06 PASSED Test Tone Expected Push To Test indicator Results Push To...

Page 169: ...00 Hz 1 10 reference level data for each channel 1 2 3 and 4 and verify amplitude all within 3 dB Example report message s 08 04 52 PASSED Channel Bal 1000 Hz 0 5 ref All within 3 dB Results HQ1 5 2 HQ2 5 3 HQ3 5 1 HQC 5 1 SQV1 5 0 SQV2 5 4 SQV3 5 4 SQC 5 5 dBV 08 05 40 PASSED Channel Bal 1000 Hz 0 1 ref All within 3 dB Results HQ1 8 3 HQ2 8 2 HQ3 8 4 HQC 9 4 SQV1 8 0 SQV2 8 1 SQV3 8 1 SQC 9 1 dBV...

Page 170: ... and 3500 Hz Frequencies for HQCAM and SQCAM are 217 314 454 656 949 1372 1984 and 2869 Hz Frequencies for HQCAM only are 4148 and 6000 Hz Verify HQ 24 0 dB and SQ 20 0 dB Example report message s 08 09 38 PASSED SN D 150 Hz 1 0 ref Expected HQ 24 0 dB SQ 20 0 dB Results HQ1 35 0 HQ2 34 6 HQ3 35 3 HQC 36 9 SQV1 32 1 SQV2 31 6 SQV3 32 0 SQC 31 6 dB 08 35 07 PASSED SN D 150 Hz 1 0 ref Expected HQC 2...

Page 171: ...d simulated GMT 429 and calculate channel results minus channel balance results Verify difference is less than 34 dB Example report message s 08 43 07 PASSED Channel Bal 1000 Hz 1 0 ref All within 3 dB Results HQ1 11 2 HQ2 11 2 HQ3 11 0 HQC 11 1 SQV1 11 0 SQV2 11 3 SQV3 11 4 SQC 11 5 dBV 08 43 23 PASSED Crosstalk Data 6000 Hz 1 0 ref Expected Crosstalk Channel Bal 34 dB Results HQ1 304 9 HQ2 125 7...

Page 172: ...2 2 SQV3 80 7 SQC 85 0 dB 14 Shutdown Part 1 enable delayed shutdown Part 2 verify shutdown is detected CVR fault set after 9 and 10 minutes Part 3 verify shutdown is terminated following a push to test and recording is re sumed Example report message s 08 47 13 PASSED Shutdown Initialization Shutdown issued Please wait 9 10 minutes 08 56 14 PASSED Shutdown CVR Fault Expected CVR fault to occur Re...

Page 173: ...again with channel 3 output Verify 9 good FSK data patterns and a switch to 9 good GMT 429 data patterns for each channel 1 and channel 3 Example report message s 14 50 07 PASSED FSK Time HQ1 Playback Expected 9 patterns Results 9 good patterns 14 50 07 PASSED FSK Time HQ1 GMT Switch Expected 9 patterns Results 9 good patterns 14 50 53 PASSED FSK Time HQ3 Playback Expected 9 patterns Results 9 goo...

Page 174: ... Setup Cable Assembly p n 17TES0417 refer to Figure 121 LOOP BACK CONNECTOR Figure 121 Audio Setup Cable Assembly 17TES0417 NOTE Selections on the toggle switches of the Audio Setup Cable Assembly pn 17TES0417 override channel selections made in the CATS software For example if the user selects channels 1 2 3 4 in the Audio Reference Setup Utility but selects CH1 on the cable toggle switches the A...

Page 175: ...Observe the con necting to recorder status window appears g From the pull down menu click on Power DC Power On or AC Power On NOTE Observe the connecting to recorder status window appears h Verify that the DC LED or AC LED on the front of the RIU is on i Click the Speaker button Volume Control to display the Playback Control menu j Please refer to and perform steps 2 through 14 of Section 5 B Read...

Page 176: ...ference Utility Select Setup_1000Hz wav and click on Open Figure 124 Audio Reference Level Utility File Open Menu d Ensure the MultiMeter is connected to the Audio Setup Loop back cable Set the toggle switches to the following settings Switch Settings Chan nel 1 and No Audio Out e At the Audio Reference Level menu ensure that the Channel 1 check box is selected Select Sound Play Sound to output th...

Page 177: ... h Set the toggle switches on the loop back connector to the following set tings Switch Settings Channel 4 and No Audio Out i At the Audio Reference Level menu ensure that the Channel 4 check box is selected and Channel 1 is deselected Select Sound Play Sound to output the 1000 Hz wave file to the sound card Figure 126 Audio Reference Level Utility Play Sound j Adjust the Audio Reference Level men...

Page 178: ...udio Reference Level menu by selecting the Close button NOTE The Audio Reference Utility volume value is used to define the VOICE VOLUME for channels 1 2 3 and the CAM VOLUME for channel 4 for output to the recorder during CVR tests 3 Part 2 Sound Card Input Adjustment a Set the toggle switches on the Loop Back Connector to the following set tings Switch Settings Channel 1 and Audio Out b Select U...

Page 179: ...de wav file by selecting File Open File on the Audio Reference Utility Select Setup_1000Hz wav and click on Open Figure 130 Audio Reference Level Utility File Open Menu e From the menu bar under Utilities select Audio Reference Utility Select the check box next to Channel 1 and deselect Channel 4 check box Se lect Sound Play Sound to output the 1000 Hz wave file to the sound card The document refe...

Page 180: ...input sound h From the Audio Reference Level menu select Sound Stop Record to stop recording i From the Audio Reference Level menu select Sound Stop Play to stop audio output from the sound card j From the Audio Reference Level menu select Store Results Input Results to calculate and display the REFERENCE value or Correction Factor CF Figure 132 Sound Card Input Results k Click OK to continue with...

Page 181: ...to adjust the audio voltages read from the audio output of a 600 ohm recorder during CVR tests For example if 1 952 Volts RMS is read from the sound card then Correction Factor 2 45 VRMS 1 952 VRMS If the Volts RMS value read is less than 1 Volt RMS then and error message will be displayed In this case verify that all of the cables are working and are installed correctly NOTE The setup reference l...

Page 182: ...sing the CATS soft ware The FA2100CVRs that have Hardware MOD DOT 7 installed have full two hour High Quality for all four audio channels as does all 30 Minute FA2100CVRs 1 Click on the Copy button Set the File Name to Filename cvr the system will use a default file name with the part number of the recorder and serial number that was entered in the information fields of the test section 2 Click on...

Page 183: ...L 3 Com 17TES0413 Cable RIU to Sound Card 2ea L 3 Com 17TES0415 Cable RIU to USB L 3 Com 17TES0416 Cable RIU to CVR L 3 Com 17TES0417 Cable Assembly Audio Setup L 3 Com 17TES0420 CATS Software FA2100 L 3 Com 17TES0070 CICC 2 Assembly L 3 Com 17TES0072 Cable Assembly FA2100 CICC 2 L 3 Com 17TES0321 Read Out System Equipment Software ROSE 4 X L 3 Com 17TES0058 FA2100 Software Upload Cable Assembly L...

Page 184: ...wer connector J8 on the rear of the RIU to a DC power supply that can generate 28 Volts 1 Amp b For AC power connect the AC power cable 17TES0411 from the AC Power connector J7 into a watt meter that handles 115Vac 400 Hz Plug the watt meter into a 115 Vac 400Hz AC power supply 2 Plug the cable 17TES0418 for ROC 7 into the rear of the recorder to be tested Plug the SCSI connector into Rear Connect...

Page 185: ...nnect the DIN CABLE from the speakers to the middle Speaker Out SPKRS OUT J6 connector on the front panel of the RIU 8 After all connections are made to the RIU apply power to the RIU This can be either 28 Vdc or 115 Vac 400 Hz 9 Apply power to the PC the ROC and observe that the PC boots to the Win dows desktop The document reference is online please check the correspondence between the online do...

Page 186: ...RCDR AC PWR TEST RECORDER INTERFACE UNIT RIU 17TES0710 SND IN BLUE 17TES0413 SND OUT GREEN 17TES0413 J4 J2 J1 L SPKR R SPKR YELLOW AC RED DC AC 1A DC 5A USB Note Speakers are optional for ROC 7 To order speakers from L 3AR use p n 17TES0425 110V or 17TES0426 220V FA2100 SOFTWARE UPLOAD CABLE ASSEMBLY 17TES0058 use for software uploading only BLUE GREEN SND IN SND OUT SPKRS OUT GSE INTFC REAR CONNE...

Page 187: ...S J9 RCDR AC PWR TEST RECORDER INTERFACE UNIT RIU 17TES0710 SND IN BLUE 17TES0413 SND OUT GREEN 17TES0413 J4 J2 J1 L SPKR R SPKR YELLOW AC RED DC AC 1A DC 5A USB Note Speakers are optional for ROC 7 To order speakers from L 3AR use p n 17TES0425 110V or 17TES0426 220V FA2100 SOFTWARE UPLOAD CABLE ASSEMBLY 17TES0058 use for software uploading only BLUE GREEN SND IN SND OUT SPKRS OUT GSE INTFC REAR ...

Page 188: ...ROC to start the software The applic ation will launch with the Channels control screen displayed as illustrated in Figure 136 Figure 136 CATS Channels Control Screen 2 In the Channels control screen click OK The Channels control screen will dis appear 3 Click the Volume control icon it is the icon that looks like a speaker The Volume Mixer Speakers SB Audigy control displays see Figure 137 The do...

Page 189: ...ns on the cover page of this document Figure 137 Volume Control 4 Under Applications click Sound Systems then click the Recording tab This will display the Sound control window illustrated on the following page Figure 138 Sound Control Recording 5 Select the Recording tab The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 190: ...strictions on the cover page of this document 6 Highlight and select Line in 7 Click on Properties Figure 139 Line In Properties Line In Level 8 Select the Levels tab 9 Make sure that the Line In level is set at 100 move the Line In slider to maximum c Click on OK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 191: ...osure of information on this sheet is subject to the restrictions on the cover page of this document Figure 140 Sound Playback Devices 10 Click on the Playback tab 11 Highlight Speakers 12 Click on Properties The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 192: ...es 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 Volume slider levels do not need modification since these input volumes have been muted 16 Click OK The document reference is online please check the corresponden...

Page 193: ...formation on this sheet is subject to the restrictions on the cover page of this document Figure 142 Volume Mixer Speaker Levels 17 In the Volume Mixer make sure both sliders are all the way up 18 Close the Volume Mixer The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 194: ... C 2 When autotesting using both DC and AC power to CATS Autotest using AC and DC power paragraph C 2 1 ROC 7 CATS Autotest using DC power To perform the CATS Autotest using DC power only follow the procedures below a Ensure that the RIU has no power applied power is removed if not al ready done Connect a CVR to the RIU using the cable p n 17TES0418 ROC 7 for the recorder rear connector and cable ...

Page 195: ...necting Pop Up g On the tool bar select Power Figure 144 CATS Power Toggle NOTE When DC power is applied verify the appropriate LED is lit up on the RIU h Click on the Information tab in the Test section of the menu i Enter appropriate information into Department Part Number and Serial Number fields j On the tool bar select Start Test The document reference is online please check the correspondenc...

Page 196: ... In the Test Mode and Options dialog box select either Return to Ser vice or Selectable Test Options then click on OK Figure 146 CATS Test Mode and Options Screen NOTE If a full return to service test is not desired then select the Se lectable Test Options radio button and choose the test options desired Figure 147 will appear as confirmation The document reference is online please check the corre...

Page 197: ...E 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 l Read and click on Yes Figure 148 CATS CVDR Warning Message m Remove front cable and click on OK The document reference is online please check the correspondence between the online do...

Page 198: ...meter on the power supply or from the inline RMS multimeter And enter in the value in amps in window and click on OK Figure 150 CATS Power Test Input o Read the current DC amps value from the built in 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 151 CATS Power Test Input p Connect the recorder front cable and click...

Page 199: ...cover page of this document Figure 152 CATS CVDR Instruction Window q Observe the Fault History Log window appears Select Print if you want to save the fault history or Close to continue Figure 153 CATS CVDR Fault History Log r Click on Yes on the dialog box to clear the fault logs The document reference is online please check the correspondence between the online documentation and the printed ver...

Page 200: ...firmation s Click on Yes on the dialog box to clear the latched faults and fault history log Figure 155 CATS CVDR Clear Latched Faults and Log Confirmation t Click on Ok Figure 156 CATS CVDR Clear Latched Faults and Log Successful u Observe the Fault History Log window appears Select Print if you want to save the fault history or Close to continue The document reference is online please check the ...

Page 201: ...Confirmation 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 The test report is located in the following default location C Program Files L 3Com CVRTester Reports This file is in an ASCII text file format x If the autotes...

Page 202: ...totest using AC power To perform the CATS Autotest using AC power only follow the procedures below a Ensure that the RIU has no power applied power is removed If not al ready done Connect a CVR to the RIU using the cable p n 17TES0418 ROC 7 for the recorder rear connector and cable p n 17TES0072 for the recorder front connector b If the power supply does not include a built in multimeter set up an...

Page 203: ... menu bar select Power Recorder Interface Reset NOTE This will load the Altera chip in the RIU unit Observe the con necting to the recorder status window appears h On the tool bar select Power Figure 161 CATS Power Toggle NOTE When AC power is applied verify the appropriate LED is lit up on the RIU i Click on the Information tab in the test section of the menu The document reference is online plea...

Page 204: ...r appropriate information into Department Part Number and Serial Number fields k On the tool bar select Start Test Figure 162 CATS Start Test Toggle l In the Test Mode and Options dialog box select either Re turn to Service or Selectable Test Options and then click on OK Figure 163 CATS Test Mode and Options Screen The document reference is online please check the correspondence between the online...

Page 205: ...le Test Options radio button and choose the test options desired NOTE Figure 164 is only displayed if you select Selectable Test Op tion from the CATS Test Mode and Options Screen Figure 164 CATS CVDR Test Confirmation NOTE Follow the instructions in Figure 165 as displayed by the software m Read and click on Yes Figure 165 CATS CVDR Warning Message n Remove front cable and click on OK The documen...

Page 206: ...meter on the power supply or from the inline RMS multimeter And enter in the value in amps in window and click on OK Figure 167 CATS Power Test Input p Read the current AC amps value from the built in 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 168 CATS Power Test Input q Connect the recorder front cable and click...

Page 207: ...cover page of this document Figure 169 CATS CVDR Instruction Window r Observe the Fault History Log window appears Select Print if you want to save the fault history or Close to continue Figure 170 CATS CVDR Fault History Log s Click on Yes on the dialog box to clear the fault logs The document reference is online please check the correspondence between the online documentation and the printed ver...

Page 208: ...Log Confirmation t Click on Yes on the dialog box to clear the latched faults and fault history log Figure 172 CATS CVDR Clear Fault Log Confirmation u Click on Ok Figure 173 CATS CVDR Clear Latched Faults and Log Successful v Observe the Fault History Log window appears Select Print if you want to save the fault history or Close to continue The document reference is online please check the corres...

Page 209: ...Confirmation x At the end of the test save the report by selecting File Test Report Save Report NOTE The test report is named with the part number of the Unit Under Test and the serial number provided in the Information section of the test The test report is located in the following default location C Program Files L 3Com CVRTester Reports This file is in an ASCII text file format y If the autotes...

Page 210: ...ault Isolation 23 70 04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document Figure 176 CATS Test Results Screen The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 211: ...esults 12 watts 4 watts 8 watts 08 02 23 PASSED Power DC Expected 11 watts Results 12 375 watts 2 2 watts 10 175 watts 2 Fault Log Displays the current recorder fault log for user review and prompts the user Clear fault log Select yes when testing the FA2100 recorder and the full fault log is NOT to be written to the test report Continue CVDR Tests Select yes to continue or no to stop testing Exam...

Page 212: ...lts 10 good patterns 6 Rotor Speed Part 1 Record simulated 6000 Hz rotor speed data and verify data is within 2 of sent frequency Part 2 Record simulated 7 Hz rotor speed data and verify data is within 2 of sent frequency Example report message s 08 03 52 PASSED Rotor Speed 6000 Hz Expected 4 patterns 5880 0 Hz 6120 0 Hz Results 5998 0 Hz 6026 4 Hz 6026 4 Hz 6026 4 Hz 08 04 03 PASSED Rotor Speed 7...

Page 213: ...C 1 4 SQV1 3 9 SQV2 3 9 SQV3 3 9 SQC 3 9 dBV 08 07 15 Frequency Resp 1000 Hz 0 5 ref Results HQ1 5 2 HQ2 5 3 HQ3 5 1 HQC 5 1 SQV1 5 4 SQV2 5 4 SQV3 5 4 SQC 5 4 dBV 08 08 02 Frequency Resp 3500 Hz 0 5 ref Results HQ1 3 3 HQ2 2 9 HQ3 2 5 HQC 5 1 SQV1 3 7 SQV2 3 7 SQV3 3 8 SQC 3 5 dBV 08 08 12 Frequency Resp 5000 Hz 0 5 ref Results HQC 4 9 dBV 08 08 23 Frequency Resp 6000 Hz 0 5 ref Results HQC 4 9 d...

Page 214: ...1 0 ref Expected HQC 24 0 dB Results HQC 30 6 dB 11 31 07 PASSED SN D 6000 Hz 1 0 ref Expected HQC 24 0 dB Results HQC 27 7 dB NOTE Running the Signal to Noise and Distortion test in the Selectable Test mode will perform additional tests at 200 250 315 400 500 630 800 1250 1600 2000 3150 and 4000 Hz 10 Crosstalk Audio Record simulated 1000 Hz data for each channel 1 2 3 4 and calculate difference ...

Page 215: ...3 dB Results HQ1 11 2 HQ2 11 2 HQ3 11 0 HQC 11 1 SQV1 11 0 SQV2 11 3 SQV3 11 4 SQC 11 5 dBV 08 43 23 PASSED Crosstalk Data 6000 Hz 1 0 ref Expected Crosstalk Channel Bal 34 dB Results HQ1 304 9 HQ2 125 7 HQ3 304 8 HQC 49 8 SQV 83 4 SQC 82 8 dB 12 FSK Time This test cycles power to recorder to reset for FSK input then records simulated 16000 sps FSK data and then simulated GMT 429 data label 150 fi...

Page 216: ...han 48 dB Example report message s 08 47 12 PASSED Sig To No Sig 0 Hz 1 0 ref Expected HQ 48 dB SQ 40 dB Results HQ1 304 9 HQ2 122 6 HQ3 108 4 HQC 115 4 SQV1 82 7 SQV2 82 2 SQV3 80 7 SQC 85 0 dB 15 Shutdown Remove recorder power and verify recorder continues to operate for 9 and 10 minutes after power is removed and shutdown is terminated following a push to test Part 1 enable delayed shutdown Par...

Page 217: ...imulated data link messages 18 OMS Read the OMS status words and verify CVR fault status and CVR part number and serial number Example report message s 08 59 00 PASSED OMS Part 1 Expected OMS Status to match 08 59 10 PASSED OMS Part 2 Expected OMS Part and Serial Numbers to match Results pn2100 1025 22 sn000000000 19 RIPS Clear the FA2100 fault log and existing faults that might prevent RIPS test ...

Page 218: ...r 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 The document reference is online please check the correspondence between the o...

Page 219: ...verted using the CATS soft ware The FA2100CVRs that have Hardware MOD DOT 7 installed have full two hour High Quality for all four audio channels as does all 30 Minute FA2100CVRs 1 Click on the Copy button Set the File Name to Filename cvdr the system will use a default file name with the part number of the recorder and serial number that was entered in the information fields of the test section 2...

Page 220: ...057 Cable Assembly CVDR Interface L 3 Com 17TES0071 Cable Assembly F1000 CICC 2 L 3 Com 17TES0321 Read Out System Equipment Software ROSE 4 5 L 3 Com 17TES0058 FA2100 Software Upload Cable Assembly L 3 Com 883E4557 00 CD Soundblaster Audigy L 3 Com 17TES0076 RUFS Recorder Interface USB L 3 Com 17TES0425 Speakers 2 110 Vac U S Standard Optional 17TES0426 Speakers 2 220 Vac Non U S Standard Optional...

Page 221: ...tact with the metal pad at the center of the water switch 4 Read the battery voltage from the test set display If the battery voltage is at or above 2 97 volts the battery is operable If the battery voltage is below 2 97 volts remove the Beacon from service 5 To perform an operational test of the Beacon place the probes on the Beacon as described above and press the red button on the test set the ...

Page 222: ...eacon turn on the test set by rotating the front panel GAIN control clockwise until it clicks 4 On the front panel of the test set set the INT EXT switch to INT 5 Rotate TUNING control to a setting between 35 and 40 kHz 6 Use a metal braid or other flexible metal conductor to temporarily short the metal pad at the center of the water switch to the Beacon case and activate the unit 7 Make sure that...

Page 223: ...orrective Actions Fault Code Failure Mode Corrective Action cde0 An invalid partition map was found 1 Remove Memory 09d7 The SMP Check timed out waiting for audio channelizer to shutdown 1 ck cables 2 If fault codes persist then remove and replace Audio Compressor PWA p ns 205E3977 3 Run autotest recheck recorder status 4 Remove and replace Acquisition Processor PWA PN 205E2502 89d2 Next power up ...

Page 224: ...If fault codes still present in status report then return the recorder to factory for repair 59db System Error CVR test failed Test tone failed 1 Remove and replace Audio Compressor PWA PN 205E3977 2 Run autotest recheck recorder status 3 If fault codes still present in status report then return the recorder to factory for repair 85da 51d9 0855 6900 85da An overflow occurred in the audio channeliz...

Page 225: ...or PWA p n 205E2502 XX 2 Run autotest recheck recorder status 3 If fault codes still present in status report then return the recorder to factory for repair 89d1 The non volatile memory on the CVR has a bad CRC This problem is usually related to a bad chip on the Acquisition Processor 89d2 The non volatile memory contains bad indices 89d2 09d4 89d2 System Error The non volatile memory on the CVR c...

Page 226: ...977 XX 2 Run autotest recheck recorder status 3 If fault codes still present in status report then return the recorder to factory for repair 8453 Read After Write Errors Too Long Erase Event and Error 1 Remove and replace CSMU p n 253E1568 2 Run autotest recheck recorder status 3 If fault codes still present remove and replace Acquisition Processor PWA p n 205E2502 4 Run autotest recheck recorder ...

Page 227: ...cludes the Computer Interface Communications Cable 2 p n 17TES0070 and the FA2100 to CICC 2 cable p n 17TES0072 The software upload procedure is also necessary when replacing a faulty Turbo Acquisi tion Processor PWA p n 205E2502 10 11 with a known good AP board from the facto ry since the factory spare PWA s are shipped without the recorder firmware preloaded The specific recorder software for ei...

Page 228: ...stributed with ROSE 3 1 or lower will not work with the updated CICC 2 Interface Newer versions of the software are back ward compatible and will work with the original CICC Inter face 5 To load the Interface program and to verify the upload process perform the following Open up the the FA2100 Utility Bundle CD To install the Interface utility click open the CICCIfc folder and then click on the Se...

Page 229: ... Note Firmware Distribution Diskette P N will match the FA2100 Software Part Number located on the recorder s Name Plate Label TO ENHANCED PARALLEL PORT EPP FA2100 SOFTWARE UPLOAD BOOTLOAD CABLE ASSEMBLY 17TES0058 use for software uploading only Note RI Recorder Interface ROSE Read Out Support Equipment ROC Read Out Center ROC 5 6 or 7 Note The ROC rear connections shown in this diagram are for ge...

Page 230: ... using the CICC 2 2 At the FA2100 J1A connector use the Recorder Interface RI Cable Assy P N 17TES0057 to connect either 115 Vac 400 Hz or 28 Vdc to the pig tail con nectors Alternatively 28Vdc power may be directly applied to J1A 9 and Ground to J1A 17 or connect 115Vac 400Hz to J1A pins 2 3 3 Apply power to the FA2100CVR Recorder 4 Note the SMP version and checksum value listed on the label of t...

Page 231: ...pecified in the CICCLDR ini file matches the ad dress of the parallel port connected to the CICC 14 Turn off power from the recorder and Exit the CICC Loader utility program 15 Disconnect the 17TES0058 Upload Cable from the FA2100CVR Front Panel ATE connector and the 17TES0072 CICC 2 Cable Assembly 16 Reconnect the 17TES0072 CICC 2 Cable Assembly to the ATE connector 17 Proceed to paragraph C to v...

Page 232: ...as listed in Section 100 of this manual Table 106 FA2100CVR Software SMP Checksums Software P N Recorder P N SMP Checksum SMP Ver 840 E1657 01 2100 1020 00 2100 1020 02 0X5609 6 1 840 E1657 03 2100 1020 00 2100 1020 02 0X67EE 7 4 840 E1657 04 2100 1020 00 2100 1020 02 0X313B 7 5 840 E1657 05 2100 1020 00 2100 1020 02 0XAD9F 7 9 840 E1657 06 2100 1020 00 2100 1020 02 0XA84B 8 7 840 E1657 07 2100 10...

Page 233: ...20 51 0X3152 7 5 840 E1664 05 2100 1020 50 2100 1020 51 0XADB6 7 9 840 E1664 06 2100 1020 50 2100 1020 51 0X8A62 8 7 840 E1664 09 2100 1020 50 2100 1020 51 840 E3408 04 2100 1025 12 0XD857 8 1 840 E3408 05 2100 1025 02 0X046A 8 1 840 E4568 06 2100 1025 22 0XD8A2 8 5 840 E4568 09 2100 1025 22 2100 1125 02 0XF168 8 8 840 E4568 10 2100 1025 22 0X8D8E 8 9 840 E4568 11 2100 1025 22 2100 1225 22 0X6118 ...

Page 234: ...2100 1025 02 2100 1025 12 0X44A9 1 8 840 E3408 05 2100 1025 02 2100 1025 12 0X44A9 1 8 840 E4568 06 2100 1025 22 2100 1125 02 0X486D 2 1 840 E4568 09 2100 1025 22 2100 1125 02 0X5E5E 2 3 840 E4568 11 2100 1025 22 2100 1125 02 2100 1225 22 0X5E5E 2 3 840 E4568 12 2100 1025 22 2100 1225 22 2100 1925 22 0XF9F1 2 5 840 E5022 02 2100 1026 02 0X9834 2 1 840 E5022 03 2100 1026 02 0X8190 2 1 840 E5022 04 ...

Page 235: ...ult Isolation 23 70 04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 236: ...or disclosure of information on this sheet is subject to the restrictions on the cover page of this document AUTOMATIC TESTING 1 GENERAL There are no Automatic Test Procedures for the FA2100 CVR The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 237: ...ic Testing 23 70 04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 238: ...NSURE PROPER PERSONNEL GROUND ING TECHNIQUES ARE USED ALSO ENSURE THAT ALL CIRCUIT BOARDS ARE PLACED INTO STATIC SHIELDING CONDUCTIVE BAGS WHEN HANDLING OR STORING SYMBOL FOR ESD GROUND CONNECTING O ESD WARNING SYMBOL 2 MODEL FA2100CVR DISASSEMBLY INSTRUCTIONS Special tools fixtures and equipment that are needed to disassemble and repair the Model FA2100CVR are listed in Figure 901 NOTE Numbers sh...

Page 239: ...rtification 30 Day ULB s already in service may still be used and a ULB Battery Kit p n 147E0305 00 is available for battery replacement The 30 Day ULB p n 266E0305 00 is no longer manufactured due to the cancel lation of TSO 121 and TSO 121a as of Dec 1 2015 A 90 Day ULB Conversion Kit pn 068E5542 00 is available for retrofit of a 30 Day ULB to 90 Day beacon to an existing recorder When convertin...

Page 240: ...he CSMU 2 Loosen the lower right hex cap screw 1 75 which secures the right Beacon Mount Bracket to the CSMU and holds the beacon in the bracket 3 The beacon can now be removed from the Beacon Mount Bracket 4 If the CSMU requires removal then remove the right beacon bracket mount from the CSMU assembly Left Beacon Mount Bracket 1 70 Right Beacon Mount Bracket 1 70 Underwater Acoustic Beacon 1 80 1...

Page 241: ...ry for repair If replacement of the CSMU is required proceed with the fol lowing procedure CSMU REMOVAL PROCEDURE 1 Remove the Underwater Acoustic Beacon 1 80 as described in paragraph A above 2 Remove the four 1 4 20 1 pan head sealing screws 190 that secure the CSMU memory assembly 1 185 to the recorder chassis 1 5 a For Pre MOD DOT 13 units only carefully remove the RTV from around the memory i...

Page 242: ...e Acquisition Processor PWA Note the pins of J1 can be easily dam aged if handled incorrectly Memory Interface Cable Assembly P1 J1 Acquisition Processor PWA AP CSMU Memory Assembly 1 185 1 175 Recorder Chassis 1 5 Figure 303 CSMU Memory Assembly Removal Diagram PRE MOD DOT 6 b For Post MOD DOT 6 Pre MODT DOT 13 units only carefully tilt the CSMU memory assembly to the left side same side as cable...

Page 243: ...Memory Assembly Removal Diagram POST MOD DOT 6 PRE MOD DOT 13 c For Post MOD DOT 13 units only carefully lift the CSMU memory assem bly directly up without pulling the memory interface cable to gain access to the J5 connector located on the Acquisition Processor PWA 1 175 Carefully unplug P1 of the Memory Interface Cable Assembly from J5 on the Acquisition Processor PWA Note the pins of J5 can be ...

Page 244: ...down ori ented so that this circuitry is not underneath the CSMU Failure to do this will result in damage to the CSMU Memory Assembly 6 Package CSMU memory assembly and return to L 3 Aviation Recorders for repair C Acquisition Processor AP PWA Removal See Figure 306 or IPL Figure 1 Item 175 The Model FA2100 s Acquisition Processor PWA 1 175 is mounted in the bottom of the recorder chassis just bel...

Page 245: ...ct the Audio Compressor PWA interconnection cable assembly W003 1 165 from J4 on the Acquisition Processor PWA 5 Remove 8 flat head screws 1 95 that secure the rear panel assembly 1 90 with attached Aircraft Interface PWA and Audio Compressor PWA into the recorder Chassis 1 5 NOTE Flat head screws 1 95 are one time use items that should be discarded when removed and replaced with new screws 6 Lift...

Page 246: ...01 1 170 Rear Panel Assy 1 90 J5 Figure 306 Acquisition Processor PWA Removal Diagram D Audio Compressor PWA AC Removal See Figure 307 or IPL Figure 1 Item 155 The Model FA2100 s Audio Compressor PWA is mounted to the Aircraft Interface PWA located in the rear panel assembly of the recorder chassis It provides digital conversion and compression of the input audio stream It interfaces to the Acquis...

Page 247: ...ove 8 flat head screws 1 95 that secure the rear panel assembly 1 90 with attached Aircraft Interface PWA and Audio Compressor PWA into the recorder Chassis 1 5 NOTE Flat head screws 1 95 are one time use items that should be discarded when removed and replaced with new screws 7 Lift the rear panel assembly away from the chassis 8 Disconnect the interconnection cable assembly W002 1 170 from J1 on...

Page 248: ...cessor PWA AP 1 175 1 95 Qty 8 1 90 1 20 1 25 Qty 10 1 110 Qty 2 1 115 1 125 Qty 3 A 1 125 Aircraft Interface PWA AI 1 105 Audio Compressor PWA AC 1 155 1 120 Qty 4 W001 1 170 W002 1 165 J3 1 135 W003 1 165 J1 J3 1 130 Qty 4 1 160 Qty 4 J1 J2 1 105 1 155 1 125 Qty 2 Post MOD DOT 11 1 141 1 135 REF 1 146 1 151 J5 Figure 307 Aircraft Interface Audio Compressor PWA Removal Diagram The document refere...

Page 249: ...WA 1 155 from the rear panel assembly as de tailed in Para D above 2 Disconnect the interconnection cable assembly W001 1 165 from J2 and W002 1 170 from J3 on the Aircraft Interface PWA Keep these cables for later use 3 Remove 4 flat head screws 1 130 that attach the J1A Main connector on the Air craft Interface PWA to rear panel assembly 1 90 4 Disconnect the storage capacitor red blade connecto...

Page 250: ...tandoffs 1 120 on the Aircraft Interface PWA 12 Remove the remaining single pan head screw 1 125 which attaches the center standoff 1 115 to the Aircraft Interface PWA 13 Using a 3 16 hex wrench unscrew the four top standoff s 1 110 1 120 on the Aircraft Interface PWA 14 Save all Aircraft Interface PWA attaching parts for use with replacement Aircraft In terface PWA 15 Package Aircraft Interface P...

Page 251: ...ssembly 23 70 04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 252: ...ent MIL PRF 680 Soft Bristle Brush Cotton Swabs Lint Free Cotton Cloth NOTE Equivalent substitutes may be used for all cleaning materials All ma terials and chemicals may be obtained from any commercial source 3 CLEANING PROCEDURES WARNINGS 1 OBSERVE ALL FIRE PRECAUTIONS WHEN USING FLAMMABLE MATERIALS FOR CLEANING PURPOSES 2 PERFORM OPERATIONS INVOLVING CLEANING SOLVENT IN A WELL VENTILATED AREA A...

Page 253: ...Wiring Assembly Cleaning 1 Remove dust dirt and foreign matter from all surfaces using soft bristle brush 2 Wipe finished surfaces and contacts using a cloth moistened in solvent B Connector Cleaning 1 Wipe dust and dirt from connectors using a lint free cloth moistened with sol vent C Underwater Locator Device Beacon Cleaning All information for the ULB including the testing and cleaning is conta...

Page 254: ...ECKS A Main Recorder Assembly 1 Check the general physical integrity of the recorder i e front panel ATE connector pins Underwater Locator Device acoustic beacon and J1A rear panel connector pins 2 Check that dust cover is serviceable exhibiting no undue deterioration and is properly painted B Mechanical Inspection 1 Remove the unit dust cover refer to Section 300 Disassembly Section 2 Inspect all...

Page 255: ...ate for legibility 9 Reassemble recorder in accordance with the steps of procedure outlined in Section 700 Assembly C Electrical Inspection Perform all test set up and testing per instructions given in the Testing and Trouble shooting Section 100 of this Component Maintenance Manual D Underwater Locator Device ULD All information for the ULB including the testing and cleaning is contained in the L...

Page 256: ...e FA2100CVR to component level in accordance with L 3AR Factory test calibration and repair speci fications As a result the Model FA2100CVR s maintenance philosophy is replacement of failed as semblies In the case of the Model FA2100CVR the replaceable assemblies are the Air craft Interface PWA the Audio Compressor PWA the Acquisition Processor PWA and the Crash Survivable Memory Unit CSMU When it...

Page 257: ...epair 23 70 04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 258: ...he common assembly materials used with the FA2100 Cock pit Voice Recorder Table 701 Required Assembly Materials Item Manufacturing and Specification Use 1 Adhesive Loctite Grade E Purple No 222 Lock sealant manufactured by Loctite Corp 705 N Mountain Rd Newington CT 06111 V05972 Retain screw 2 Torque Wrench Local tool supplier Range 5 6 in lbs End Range 75 in lbs CSMU Beacon Brack et mounting scre...

Page 259: ...for the FA2100 CVR a known defective circuit board assembly shall be returned to the factory for repair or replacement NOTE Numbers shown in parentheses in the following text are the Illustrated Parts List IPL figure number followed by the IPL item number for a particular part e g 1 115 for IPL Figure 1 Item 115 For items listed in the parts list but not illustrated the item number is preceded by ...

Page 260: ...65 W001 1 170 Rear Panel Assy 1 90 J5 Figure 701 Acquisition Processor AP Installation Diagram The Acquisition Processor PWA provides an interface between the Aircraft Interface PWA through W001 Cable Assembly connected at J2 and the Audio Compressor PWA through W003 Cable Assembly connected at J4 The Acquisition Processor PWA connects to the CSMU via the Memory Interface Cable assembly connected ...

Page 261: ...on Processor requires specifically configured software to oper ate refer to the Test and Troubleshooting Section 100 for detailed procedures on loading the recorder software through the front panel GSE connector C Aircraft Interface PWA AI Installation See Figure 703 or IPL Figure 1 Item 105 The Model FA2100 s Aircraft Interface PWA is mounted in the rear panel assembly of the recorder chassis It ...

Page 262: ... of 5 6 in lbs 6 Position the Aircraft Interface PWA into the rear panel assembly such that the J1A mounting holes and upper standoffs are aligned properly 7 While holding the J1 connector flush with the bottom of the connector opening of the rear panel assembly insert 4 flat head screws 1 130 and tighten down in a cross pattern to ensure a proper alignment of the J1 main connector as sembly with ...

Page 263: ...Ensure that the Aircraft Interface PWA 1 105 is installed into rear panel assembly 1 90 as described in paragraph C above 2 Lay the rear panel assembly on its back with the Aircraft Interface PWA facing up 3 Place the Assembly Support Tool fixture Table 701 item 5 between the Aircraft Interface PWA 1 105 and the rear panel assembly 1 90 Position the fixture such that the inner part of the U shape ...

Page 264: ... 20 1 25 Qty 10 1 110 Qty 2 1 115 1 125 Qty 3 A 1 125 Aircraft Interface PWA AI 1 105 Audio Compressor PWA AC 1 155 1 120 Qty 4 W001 1 170 W002 1 165 W003 1 165 J1 J3 1 130 Qty 4 1 160 Qty 4 1 125 Qty 2 3 1 2 4 Torque Sequence 5 6 in lbs 1 2 3 Torque Sequence 9 10 in lb Each Side 2 3 1 3 1 2 4 Torque Sequence 5 6 in lbs 1 165 W003 Post MOD DOT 11 1 146 1 146 1 135 REF 1 141 Qty 2 Figure 702 Aircra...

Page 265: ... 8 1 90 1 20 1 25 Qty 10 1 110 Qty 2 1 115 1 125 Qty 3 A 1 125 Aircraft Interface PWA AI 1 105 Audio Compressor PWA AC 1 155 1 120 Qty 4 W001 1 170 W002 1 165 J3 1 135 W003 1 165 J1 J3 1 130 Qty 4 1 160 Qty 4 J1 J2 1 105 1 155 1 125 Qty 2 Post MOD DOT 11 1 141 1 135 REF 1 146 1 151 J5 3 1 2 4 Torque Sequence 5 6 in lbs 3 1 2 4 Torque Sequence 5 6 in lbs 1 2 3 Torque Sequence 9 10 in lb Each Side 2...

Page 266: ...hown in Figure 703 13 Turn the chassis over to the opposite side and tighten the remaining three screws to 9 10 in lbs in the same pattern as shown in Figure 703 14 Connect the Aircraft Interface PWA W001 Cable Assembly 1 165 to J2 on the Ac quisition Processor PWA 1 175 15 Connect the W003 Cable Assembly 1 165 between J2 on the Audio Compressor PWA and J4 on the Acquisition Processor PWA 16 Check...

Page 267: ... the seal screw holes line up with the chassis cover screw holes 9 Replace the chassis cover 1 20 by inserting the front end of the cover into the alignment grove and inserting ten attaching pan head sealing screws 1 25 coated with adhesive Table 701 item 1 NOTE Pan head sealing screws 1 25 are one time use items and should be replaced during re assembly These screws should not be retained after d...

Page 268: ... 1 20B meets the chassis 1 5 as indicated in Note 2 Figure 705 15 For GACVR p ns 2100 1010 5X and 2100 1020 5X apply RTV Table 701 Item 3 around the connector including the three keying holes and the seam on the back of the CVR as indicated in Note 3 Figure 705 16 For GACVR p ns 2100 1010 5X and 2100 1020 5X if the three unused holes on the backside of the chassis 1 5 are not filled with RTV apply...

Page 269: ... CHASSIS COVER OVER SEAL PRESS IN PLACE ALIGN SEAL OVER FIXTURE HOLES REMOVE SEAL BACKING AND SMOOTH OUT 1 2 PUSH TOOL FIRMLY TO AFFIX SEAL TO SIDE 3 4 DO NOT STRETCH SEAL MATERIAL HOLES IN SEAL SHOULD LINE UP WITH HOLES IN CHASSIS COVER ASSEMBLY Figure 704 FA2100CVR Chassis Cover Seal Installation The document reference is online please check the correspondence between the online documentation an...

Page 270: ... 4 Apply RTV to entire seam where Chassis Cover meets the Chassis after the CSMU is installed and tight ened Note 2 Apply RTV to Two Front Screw Heads and the front seam where the Chassis Cover meets the Chassis Note 1 Apply RTV to seam on the back of the CVR and around the connector and the 3 keying holes Note 3 Figure 705 FA2100 GACVR Chassis RTV Installation The document reference is online ple...

Page 271: ...185 The Model FA2100 s Crash Survivable Memory Unit CSMU is a sealed unit and must not be opened in the field CSMU is mounted to the top of the recorder chas sis by 4 pan head srews The CSMU interfaces to the Acquisition Processor Board connector J1 through the Memory Interface Cable assembly 1 For GACVR p ns 2100 1010 5X and 2100 1020 5X apply RTV Table 701 Item 3 to the CSMU seating surface on t...

Page 272: ...e on the CSMU memory assembly 1 185 with the sticky side against the CSMU cover See Figure 707 d Smooth the seal down onto the CSMU memory assembly such that the application is toward the memory interface cable assembly Carefully work the cable assembly slit in the seal around the memory interface cable as sembly e Apply RTV DOW Corning 3145 Adhesive silicone sealant between the slit in the CSMU c...

Page 273: ...y affixed to the bottom of the CSMU d Ensure that the flat underside surface of the CSMU is clean CSMU Cover Seal Apply RTV to seal Memory Cable Slit Figure 709 Crash Survivable Memory Unit CSMU Seal Application Post MOD DOT 13 e Carefully peel the paper backing from the CSMU Cover Seal 1 200 and position seal into place on the CSMU memory assembly 1 185 Place the cut out in the seal around the CS...

Page 274: ...hould be con nected to J5 on the Acquisition Processor PWA 4 Apply Locktite 222 to the four pan head sealing screws 1 190 and insert them into the CSMU cover 1 185 NOTE Pan head sealing screws 1 190 are one time use items and should be replaced during re assembly These screws should not be retained after dis assembly 5 While pushing back on the front of the CSMU partially tighten the rear two pan ...

Page 275: ... Assembly P1 J1 Acquisition Processor PWA AP Crash Survivable Memory Unit CSMU 1 185 1 175 Recorder Chassis Assembly 1 5 CSMU Mounting Seal Screws 1 190B Qty 4 Torque Sequence 75 in lb 1 2 3 4 After attached apply RTV to seal Memory Cable Slot Note Figure 710 Crash Survivable Memory Unit CSMU Assembly PRE MOD DOT 6 The document reference is online please check the correspondence between the online...

Page 276: ... P1 J1 Acquisition Processor PWA AP Crash Survivable Memory Unit CSMU 1 185 1 175 Recorder Chassis Assembly 1 5 CSMU Mounting Seal Screws 1 190B Qty 4 Torque Sequence 75 in lb 1 2 3 4 After attached apply RTV to seal Memory Cable Slot Note J5 Figure 711 Crash Survivable Memory Unit CSMU Assembly POST MOD DOT 6 PRE MOD DOT 13 The document reference is online please check the correspondence between ...

Page 277: ...ssembly P1 J1 Acquisition Processor PWA AP Crash Survivable Memory Unit CSMU 1 185 1 175 Recorder Chassis Assembly 1 5 CSMU Mounting Seal Screws 1 190B Qty 4 Torque Sequence 75 in lb 1 2 3 4 After attached apply RTV to seal Memory Cable Slot Note J5 Figure 712 Crash Survivable Memory Unit CSMU Assembly POST MOD DOT 13 The document reference is online please check the correspondence between the onl...

Page 278: ...or more details NOTE Once a unit has been changed to a 90 Day ULB it can not revert to a 30 Day ULB due to the Hardware MOD DOT marking NOTE Refer to the IPL effectivity column as some specific FA2100CVR Part Numbers that only are allowed only 90 Day ULBs to be installed NOTE For complete testing of the ULB and battery replacement procedures refer to the 90 Day Underwater Locator Bea con CMM L 3 p...

Page 279: ...ket 1 70 Underwater Acoustic Beacon 1 80 1 4 Hex Screw 1 75 Crash Survivable Memory Unit CSMU 1 185 Water Switch 1 4 2 3 Cross Pattern Torquing Sequence 75 in lbs Note Must use the L 3AR Conversion Kit PN 068E5542 00 when converting from a 30 Day ULB to a 90 Day ULB Mark Name Plate Hardware MOD DOT 15 Figure 713 Underwater Locator Beacon Assembly The document reference is online please check the c...

Page 280: ...tainer s are not available perform the following procedures to wrap the FA2100CVR system equipment for storage 1 Wrap the recorder unit in plain wrapping paper or newspaper of sufficient thick ness to thoroughly cover all sharp corners and protrusions 2 Enclose the unit in a polyethylene bag 3 mils thick min seal the bag 3 Place the recorder unit in a suitably sized heavy construction cardboard bo...

Page 281: ...RESSION SET OF 95 MATERIAL PACKING FOAM 2 00 IN THICK 1 2 LBS CUBIC FOOT WITH A COMPRESSION SET OF 40 FOAM TO BE BONDED TO CARDBOARD FLUTED SINGLE WALL 200 LBS CONSTRUCTION FOAM BONDED TO INSIDE FLAPS OF CONTAINER FOAM NOT TO EXTEND BEYOND THE CUT EDGE OF THE FLAP REF CONTINOUS STITCHING STAPLE APPROX 1 0 INCH SPACING DOUBLE STAPLE EACH END 25 IN SPACING 8 9 17 1 8 9 8 9 8 9 SHIPPING CONTAINER Sho...

Page 282: ...d 5 and 7 ED 112 chapter 2 and Part I while conforming to the input interface required in ARINC 557 757 When the software detects a fault an CVR FAULT will be as serted immediately with no artificial delay A Physical Characteristics 1 Size Refer to Figure 801 for the FA2100CVR Outline Dimension Drawing Height 5 5 inches Width 4 98 inches Depth 12 6 inches behind front panel 2 Weight 10 0 5 pounds ...

Page 283: ... D Crash and Fire Protection The Crash Survivable Memory Unit CSMU is designed to fully meet the 5 000 pounds crush test requirement of TSO 123a and provides impact protection for up to 3400 g s for 6 5 msec The inner steel casing assembly protects the memory ele ments from deep sea pressures to 20 000 ft The FA2100 s crash protected CVR memory survives ED 56A 5 3 2 d and ED 112 2 4 2 4 High Tempe...

Page 284: ...igh Temperature Short time Operating High Temperature Altitude Decompression Overpressure 4 0 4 5 1 4 5 2 4 5 1 4 5 2 4 5 3 4 6 1 4 6 2 4 6 3 Categories A2 F2 55_C 85_C 55_C 70_C 70_C 55 000 ft 55 000 ft 15 000 ft Temperature Variation 5 0 Category B Humidity 6 0 Category A Standard Shock Operational Shock Crash Safety Impulse Crash Safety Sustained 7 0 7 2 2 7 3 1 1 7 3 2 6 G 11 MS 15 G 11 MS 12 ...

Page 285: ... ARE NOMINAL WITH 5 LBS TOLERANCE 4 OVERALL EQUIPMENT SIZE AND MOUNTING SCHEME COMPLY WITH ARINC 404 AND 404A REAR PANEL CONTAINS HOLES TO MATE WITH GUIDE PINS IN ARINC 404 MOUNTING TRAYS 5 A A 1 RECORDER COLOR IS INTERNATIONAL ORANGE NO 12197 PER FED STD 595 FRONT AND SIDE LABELS ARE REFLECTIVE WHITE BACKGROUND WITH BLACK LETTERING NAMEPLATE IN VIEW A A HAS LIGHT GRAY BACKGROUND WITH BLACK MARKIN...

Page 286: ...NNECTOR PART NUMBERS PN 063 E1072 00 CANNON DPBX 36571 59 MATING CONNECTORS CRIMP PN 063 98 01474 CANNON DPXBMA 57 33S 0001 SOLDER PN 9300 435 CANNON DPXB 57 33S 0001 4 88 04 5 5 2 4 12 4 98 04 CRASH SURVIVABLE MEMORY UNIT UNDERWATER LOCATING DEVICE GROUND SUPPORT EQUIPMENT CONNECTOR AMP 748481 6 4 063 98 01962 Figure 801 Sheet 2 of 2 Outline Dimension Drawing Model FA2100 CVR Recorder P N 2100 10...

Page 287: ... Clearances 23 70 04 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 288: ...dule Obsolete L 3 Com 17TES0054 PI Memory Card Module L 3 Com 17TES0051 PI Audio Readout Cable L 3 Com 17TES0052 PI Aux Readout Cable L 3 Com Portable Interface 2 PI 2 Part Number Description Mfg 17TES0062 Portable Interface PI 2 L 3 Com 024E5002 00 USB 2 0 Cable L 3 Com 147E4785 00 USB Adapter L 3 Com 253E5106 00 USB Key L 3 Com 024E5000 00 FA2XXX FDR Interface Cable L 3 Com FA2100 Software Uploa...

Page 289: ...undblaster Audigy L 3 Com 17TES0425 Speakers 110V Optional 17TES0426 Speakers 220V Optional FA2100 Software Upload Test Equipment Cable Assemblies Software ROC 7 Part Number Description Mfg 17TES0700 Read Out Center 7 Full CVR FDR Configura tion The following items are included with the ROC 7 L 3 Com 17TES0710 Recorder Interface Unit RIU L 3 Com 17TES0411 Cable RIU to AC Power In L 3 Com 17TES0412...

Page 290: ...57 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 The document reference is online please check the correspondence between ...

Page 291: ...nk L 3 Com 840E3408 04 FA2100CVR p n 2100 1025 12 CVR 120 Min Data Link Cyrillic Russian Text L 3 Com 840E4568 09 FA2100CVR p n 2100 1025 22 CVR 120 Min OMS Data Link L 3 Com 804E4568 06 FA2100CVR p n 2100 1025 24 CVR 120 Min OMS Data Link Bombardier Global L 3 Com TBD FA2100CVR p n 2100 1026 02 CVR 120 Min OMS Data Link Airbus L 3 Com TBD FA2100CVR p n 2100 1027 02 CVR 120 Min OMS Data Link Airbu...

Page 292: ... Assembly Distribution Diskettes In the event that the Acquisition Processor PWA p n 205E1591 00 p n 205E1931 00 or p n 205E2502 10 11 requires replacement the FA2100CVR pro gram software must be loaded into the new board using the FA2100 Software Upload cable assembly p n 17TES0058 the FA2100 Software Utility Bundle Pro gram p n 883E1894 01 which contains the CICCLDR and CICCIFC executable files ...

Page 293: ...page of this document CVR MONITOR PLAYBACK STATUS CONTROL SPECIAL FUNCTIONS SELECT DELETE MENU AUDIO GMT ROTOR FSK PI AUX READOUT CABLE 17TES0052 TO RECORDER GSE CONNECTOR PI AUDIO READOUT CABLE 17TES0051 HQ SQ COMB CAM CH 1 2 3 4 Sarasota Florida Figure 901 Portable Interface Unit p n 17TES0043 The document reference is online please check the correspondence between the online documentation and t...

Page 294: ...MENU CLEAR LATCHED FAULT CLEAR FAULT LOG RELEASE FAULT GSE ON FAULT GSE OFF FAULT GSE CVR CVR CVR PLAYBACK CONTROL MENU HQ VOICE CH 1 OFF ON CH 2 OFF ON CH 3 OFF ON HQ CAM CH 4 OFF ON SQ VOICE CH 1 3 OFF ON SQ CAM CH 4 OFF ON UP VOLUME DOWN FILE BACK CVR FILE CONTROL MENU FILE NAME XXXX CVR FILE ID XXXX DATE RECORD MADE FILE SIZE XXXXX Kbytes TIME RECORD MADE RECORD DURATION BACK 03 APR 1999 11 30...

Page 295: ...XX XX PLAY STOP FFWD RWD END BEGIN XXXX XXXX CVR F PLAY CTRL MENU KEYPAD DUMPING FAULT LOG TO XXXX FLT This halts recording DUMPING TRACE LOG TO Note Data enclosed in parentheses does not appear on the PI menus and is provided in these figures for clarification XXXX TRC Press MENU to end FILE ID 11 CHAR LIMIT _ A B C D E F G H I J K L M N O P Q R S T U V W X Y Z _ 0 1 2 3 4 5 6 7 8 9 CLEAR START R...

Page 296: ... DISTRIBUTION DISK 840 EXXX XX Note Firmware Distribution Diskette P N will match the FA2100 Software Part Number located on the recorder s Name Plate Label TO ENHANCED PARALLEL PORT LPT 1 EPP FA2100 SOFTWARE UPLOAD BOOTLOAD CABLE ASSEMBLY 17TES0058 use for software uploading only Note RI Recorder Interface ROSE Read Out Support Equipment ROC Read Out Center ROC 5 6 or 7 Note The ROC rear connecti...

Page 297: ... 23 P1 115VAC HOT 115VAC COLD 28VDC FDR DATA IN LO 22 19 12 13 14 15 2 1 16 17 P2 GND FDR DATA OUT HI FDR DATA OUT LO ACID 7 ACID 6 MONITOR WIRE A MONITOR WIRE B P2 28VDC 115VAC P1A FDR DATA IN HI 24 These signal lines are not used with the FA2100CVR they are used with the Combi Recorder CVDR Figure 904 Recorder Interface Cable Assembly P N 17TES0057 The document reference is online please check t...

Page 298: ...ictions on the cover page of this document PNR 17 TES0070 SER XXXXXXXXX CICC 2 DMF MMYYYY MFR 06141 3 3 2 4 4 2 3 fT 2 IN 1 4 2 NOTE MUST BE USED WITH VER ROSE 3 2 RI 2 0 OR HIGHER SOFTWARE Figure 905 Sheet 1 of 2 Computer Interface Communications Cable 2 CICC 2 P N 17TES0070 The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 299: ... 46 4 15 16 19 20 9 10 3 13 14 21 47 48 49 SER_B0_RX_HI SER_B0_RX_LO SER_A0_I0_HI SER_A0_I0_LO SER_B1_RX_HI SER_B1_RX_LO SER_C1_I0_HI SER_C1_I0_LO SER_B0_TX_HI SER_B0_TX_LO SER_B1_TX_HI SER_B1_TX_LO SER_D0_TX_HI 26 PIN FA2100 P1 DB CONN 1 2 3 4 5 6 7 8 11 10 19 12 13 14 15 16 17 9 18 20 21 22 23 24 25 26 GND TDM_CLK_LO TDM_FRM_HI TDM_FRM_LO TDM_ADD_HI TDM_ADD_LO GND SER_FS_AP_HI SER_FS_AP_LO PRGM_...

Page 300: ...M_HI TDM_FRM_LO TDM_ADD_HI TDM_ADD_LO GND SER_FS_AP_HI SER_FS_AP_LO PRGM_VPP_SW PRGM_REC_L SER_CLK_HI SER_CLK_LO SER_DAT_AP_HI SER_DAT_AP_LO TDM_DAT_HI TDM_DAT_LO SER_DAT_PI_HI SER_DAT_PI_LO SEL_SMP FDP SER_FS_PI_HI SER_FS_PI_LO TEST_MODE_L GSE_PORT_EN 1 2 3 4 5 6 7 8 16 10 15 19 11 24 12 13 14 9 18 17 20 21 22 23 25 26 1 2 3 4 5 6 7 8 16 10 15 19 11 24 12 13 14 9 18 17 20 21 22 23 25 26 P1 P2 Fig...

Page 301: ...O OUTPUT SPKRS J9 RCDR AC PWR TEST RECORDER INTERFACE UNIT RIU 17TES0410 SND IN BLUE 17TES0413 SND OUT GREEN 17TES0413 J4 J2 J1 L SPKR R SPKR YELLOW AC RED DC AC 1A DC 5A USB Note Speakers are optional and not incld with ROC 6 To order speakers from L 3AR use p n 17TES0425 110V or 17TES00426 220V FA2100 SOFTWARE UPLOAD CABLE ASSEMBLY 17TES0058 use for software uploading only BLUE GREEN SND IN SND ...

Page 302: ...ONLY P1 40 P2 34 PREAMP PWR OUT GND P1 13 P2 13 CHANNEL 3 AUDIO IN LO P1 41 P2 41 PREAMP PWR OUT HOT P1 14 P2 14 CVR IDENT PIN P1 43 P2 4 RESERVERED TEST IND P1 15 P2 15 CHANNEL 3 AUDIO IN HI P1 43 P2 43 RESERVERED TEST IND P1 16 P2 16 CHANNEL 4 AUDIO IN LO P1 45 P2 45 CHASSIS GND DC RET P1 17 P2 17 FDR MAINTENANCE P1 46 P2 21 FDR DATA OUT B LO P1 18 P2 18 CHANNEL 4 AUDIO IN HI P1 47 P2 47 FDR DAT...

Page 303: ...ower Input Cable Assembly P N 17TES0411 144 0 1 0 IN 2X 1 00 13 I Strip and Tin 2X 2 00 13 IN 1 2 3 4 WIRE CHART BLACK OUTER WHITE INNER 5 See Note Note TRIM SHIELD EVEN WITH OUTER JACKET APPLY SLEEVING ITEM 5 OVER OUTER JACKET TRANSITION 1 WIRE 22 STRD 2 COND SHLD 2 CONN DC PWR PLUG 3 LABEL DC POWER 4 LABEL 17 TES0412 5 TBG 3 16 THERMO FIT BLK Figure 910 DC 28VDC Power Input Cable Assembly P N 17...

Page 304: ...E SWITCH 42A12 ULTRASONIC TEST SET UNDERWATER LOCATOR DEVICE MODEL 42A12 Figure 912 ULD Test Set Up C Audio Data Link Player Software The FA2100CVR Audio Data Link Player ADLP software provides a user friendly interface for initiating audio and data link message retrieval and playback functions for the Model FA2100CVR part number 2100 1025 It also provides the capa bility to decompress the data in...

Page 305: ...table Dual core CPU 2 5 GHz or greater Motherboard with EPP support compatible with PCMCIA reader below Four USB 2 0 connections 4 GB or greater memory 17 SVGA Color LCD Monitor and Graphics Adapter Must support 1024x768 and 1280 x 1024 Samsung SyncMaster 710n is an example of a compliant monitor 300 GB Hard Drive 7200 RPM or better 8x4x32X or better CD RW DVD RW 104 Keyboard Windows 7 Professiona...

Page 306: ...CIfc utility software in conjunction with the CICC 2 Interface Cable assembly p n 17TES0070 17TES0072 b Using the Portable Interface PI Unit p n 17TES0043 with Mod Dot 6 This device is used to download the FA2100CVR voice and data link infor mation to a PCMCIA memory card which then can be transferred into ei ther a ROC or RAU that has the ADLP software installed for playback For detailed operatio...

Page 307: ...t P1 FA2100 CVR J1 CVR TRAY 115 VAC HOT AC COMMON COLD 27 5 VDC INPUT CHASSIS GND 115 VAC HOT AC COMMON COLD 27 5 VDC INPUT CHASSIS GND 2 3 5 6 7 8 9 12 13 14 15 16 17 2 3 5 6 7 8 9 10 12 13 14 15 16 17 CONNECTS TO CONNECTS TO P1 J1 57 57 10 60in 6 in Figure 913 FA2100CVR Download Cable p n 17TES0078 Wiring Diagram The document reference is online please check the correspondence between the online...

Page 308: ...nufacturing part numbers 2 PURPOSE The purpose of this Illustrated Parts List is to assist maintenance and supply personnel in requisitioning storing issuing and identifying parts to maintain the FA2100 Cockpit Voice Recorder This Illustrated Parts List is not to be taken as the authority for the procedure of assembly or disassembly Overhaul or repair should be done by authorized personnel only 3 ...

Page 309: ...embled or replaced Items that are riveted welded or spun over are not listed Parts made of bulk stock such as wire tape or bonding braid are also not listed Illustra tions are each assigned a figure number commencing with Figure 1 and progressing in sequence The FIGURE AND INDEX NUMBER column reflects the assigned figure number of the il lustration in which the item is shown and the item number li...

Page 310: ...FIG FOR NHA If the vendor is not L 3 Aviation Recorders the manufacturer s vendor code may be in cluded in parentheses in this column The indenture system provided by the numbers 1 through 6 in the heading shows the relationship of one part to another for example a part listed under indenture 3 is a com ponent of the assembly listed under indenture 2 immediately above it Items used to at tach part...

Page 311: ...ok H4 H8 Commercial and Government Entity CAGE codes formerly FSCM and or the NATO Code as applicable Ref ATA Spec 200 is listed below The CAGE code is the vendor V code listed in parentheses in the NOMENCLATUE column of the Detailed Parts List Code Manufacturer V06141 L 3 Aviation Recorders 100 Cattlemen Road Sarasota FL 34232 9 L 3 AVIATION RECORDERS L 3AR AUTHORIZED PARTS L 3AR has performed ad...

Page 312: ...ion 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 Also the four attaching ULB hex screws 1 75 must be replaced when the 90 Day ULB is removed or replaced The document reference is online please ch...

Page 313: ...7 2 HR GA CVR 1 2 ATR SHORT TITANIUM CSMU W RTV 28 VDC ONLY 2100 1025 02 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY 2100 1025 12 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY CYRILLIC 2100 1025 22 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY W RIPS 2100 1025 24 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY W RIPS S W 2100 1026 02 ARINC 757 2 HR CVR W OMS 4 CHANNEL HIGH QUALITY W RIPS 2...

Page 314: ...693 C6 1 141A 2 MS24693 C7 1 141B 2 MS51957 14 1 160 4 MS51957 14 1 180 10 MS51957 14 1 125A 6 MS51957 14 1 125B 7 MS51957 28 1 25A 10 MS51957 45 1 60 4 279800024 1 225 1 2290200365 1 127 1 2529800107 1 235 1 2739800201 1 152 1 9030100047 1 205 1 9030100047 1 245 1 9030100049 1 240A 1 9030100075 1 240B 1 016E1589 00 1 70 2 016E4797 00 1 146A 1 016E5352 00 1 146B 1 024E1620 00 1 165A 2 024E1620 01 ...

Page 315: ...1 191E1603 01 1 90B 1 192E1599 00 1 30 1 197E1746 00 1 220 1 205E1591 00 1 175A 1 205E1593 00 1 105A 1 205E1596 00 1 155A 1 205E1763 00 1 105B 1 205E1763 01 1 105C 1 205E1763 11 1 105F 1 205E1849 00 1 155B 1 205E1849 02 1 155D 1 205E1849 03 1 155C 1 205E1849 04 DEL 1 155E 205E1849 10 1 155F 1 205E1849 13 1 155G 1 205E1849 14 DEL 1 155H 205E1849 17 1 155J 1 205E1931 00 1 175B 1 205E2502 10 1 175C 1...

Page 316: ...3977 24 DEL 1 155U 1 205E3977 29 1 155V 1 205E3977 37 1 155W 1 2100 1010 00 1 1A 1 2100 1010 50 1 1E 1 2100 1010 51 1 1F 1 2100 1020 00 1 1B 1 2100 1020 02 1 1C 1 2100 1020 50 1 1G 1 2100 1020 51 1 1H 1 2100 1020 90 DEL 1 1K 2100 1020 91 DEL 1 1D 2100 1020 93 DEL 1 1J 2100 1025 02 1 1L 1 2100 1025 12 1 1M 1 2100 1025 22 1 1N 1 2100 1025 24 1 1R 1 2100 1026 02 1 1P 1 2100 1027 02 1 1T 1 2100 1220 0...

Page 317: ... 253E1568 07 1 185D 1 253E1568 33 1 185E 1 253E1568 38 1 185F 1 253E1568 39 1 185G 1 253E1568 40 1 185H 1 253E1568 41 1 185J 1 253E4427 33 1 185K 1 253E5675 00 1 185L 1 253E5675 11 1 185M 1 253E5675 20 1 185N 1 266E0305 00 1 80A 1 266E0305 01 1 80B 1 266E0305 02 DEL 1 80C 1 266E5542 00 1 80D 1 297 98 00087 1 120A 4 297 98 00257 1 115 1 297 98 00283 1 110 2 297 98 00319 1 120B 4 3M 7201 DEL 1 100 7...

Page 318: ...on the cover page of this document B B 20 A A B B C C 190 80A 25 80B 5 10 105 110 125 155 135 141 146 175 165 15 farside 160 120 170 180 115 165 160 120 W2 W1 W3 151 A A 205 200 185 185 80C 80D Figure 1 Sheet 1 of 2 Model FA2100 Cockpit Voice Recorder PN 2100 1010 2100 1X2X The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 319: ...he restrictions on the cover page of this document A A 50 40 45 55 60 30 70 80A B C 75 85 90 95 130 B B View View REPLACEMENT DATE 125 C C View REFERENCE ONLY 141 151 141 141 146 Figure 1 Sheet 2 of 2 Model FA2100 Cockpit Voice Recorder PN 2100 1010 2100 1X2X The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 320: ...KPIT VOICE RECORDER FA2100 CVR ARINC 757 30 MIN GA CVR 1 2 ATR SHORT 28 VDC ONLY OBSOLETE E RF 1F 2100 1010 51 COCKPIT VOICE RECORDER FA2100 CVR ARINC 757 30 MIN GA CVR 1 2 ATR SHORT 28 VDC ONLY TITANIUM CSMU W RTV F RF 1G 2100 1020 50 COCKPIT VOICE RECORDER FA2100 CVR ARINC 757 2 HR GA CVR 1 2 ATR SHORT 28 VDC ONLY OBSOLETE G RF 1H 2100 1020 51 COCKPIT VOICE RECORDER FA2100 CVR ARINC 757 2 HR GA ...

Page 321: ...MS T RF 1U 2100 1220 00 COCKPIT VOICE RECORDER FA2100 CVR ARINC 757 2 HR CVR 1 2 ATR SHORT 90 DAY BEACON U RF 1V 2100 1220 02 COCKPIT VOICE RECORDER FA2100 CVR ARINC 757 2 HR CVR W FSK 1 2 ATR SHORT 90 DAY BEACON V RF 1W 2100 1225 22 COCKPIT VOICE RECORDER FA2100 CVR ARINC 757 2 HR CVR 1 2 ATR SHORT OMS 90 DAY BEACON W RF 1Y 2100 1226 02 COCKPIT VOICE RECORDER FA2100 CVR ARINC 757 2 HR CVR 1 2 ATR...

Page 322: ...94 00 TAPE REFLECTIVE ENGLISH FLIGHT RECORDER DO NOT OPEN 1 15 166E1595 00 TAPE REFLECTIVE FRENCH ENREGISTREUR DE VOL NE PAS OUVRIR 1 20A 075E1598 00 COVER CHASSIS SHORT A B C L M N P R T U V W Y AA AB AC 1 20B 075E1806 00 COVER CHASSIS SHORT LIGHTWEIGHT E F G H 1 ATTACHING PARTS 25A MS51957 28 SCREW PAN HEAD 6 32 x 3 8 V06141 2290200085 SUPSD BY 25B PER SB004 10 25B BB1P061H05 SCREW PAN HEAD SEAL...

Page 323: ...LETED 1 50 166E1647 00 LABEL IDENT COCKPIT VOICE RECORDER 55 111 98 00097 FASTENER HOOK NAS622 V94867 MFG NO HDH 4 2 ATTACHING PARTS 60 MS51957 45 SCREW PAN HEAD 8 32 X 1 2 V06141 2290200102 4 65 166 98 00359 DELETED 66 166 98 00361 DELETED 70 016E1589 00 BRACKET BEACON MOUNT 2 ATTACHING PARTS 75 MS16995 54 SCREW SCHCAP 1 4 20 X 1 1 2 V06141 2290200424 4 80A 266E0305 00 BEACON ACOUSTIC UNDERWATER ...

Page 324: ...EACON ACOUSTIC UNDERWATER SUPSD BY 80D PER SB022 DUKANE V94970 ELP 362D FOR BATTERY REPLACEMENT ORDER 30 DAY BATTERY KIT 147E0305 00 A B C E F G H L M N P R T 1 80D 266E5542 00 BEACON LOCATOR UNDERWATER 90 DAY SUPSDS ITEM 80A 80B 80C PER SB022 CODE F HAZMAT CLS9 FOR BATTERY REPLACEMENT ORDER 90 DAY ULB BATTERY KIT 147E5542 00 1 85 9300 388 PLUG 1 90A 191E1603 00 REAR PANEL ASSEMBLY ARINC 757 A B C...

Page 325: ...105B PER ECO 9432 SUPSD BY 105F PER SB015 E F G H 1 105D 205E2503 01 PWA AIRCRAFT INTERFACE ARINC 757 4 L M N P R W Y AA AC 1 105E 205E2503 05 PWA AIRCRAFT INTERFACE ARINC 757 4 SUPSDS ITEM 105A PER SB015 A B C U V 1 105F 205E1763 11 PWA AIRCRAFT INTERFACE GA DC ARINC 757 SUPSDS ITEM 105C PER SB015 E F G H 1 105G 205E2503 08 PWA AIRCRAFT INTERFACE T AB 1 ATTACHING PARTS 4 110 297 98 00283 STANDOFF...

Page 326: ... 2290200365 SCR FLH 8 32 X1 4 T AB 1 130 MS24693 C4 SCREW FLAT HEAD 4 40 X 3 8 V06141 2290200356 4 135A 742E1619 00 CAPACITOR ASSEMBLY STORAGE SUPSD BY 135B PER SB017 1 135B 742E1619 03 CAPACITOR ASSEMBLY STORAGE SUPSDS ITEM 135A PER SB 017 1 ATTACHING PARTS 140 MS24693 C4 SCREW FLAT HEAD 4 40 X 3 8 V06141 2290200356 SUPSD BY 141A PER SB016 2 141A MS24693 C6 SCREW FLAT HEAD 4 40 X 1 2 V06141 22902...

Page 327: ...V W Y AA AC 1 146B 016E5352 00 BRACKET PLASTIC CAPACITOR T AB 1 150 MS21044C04 NUT HEX SELF LOCKING 4 40 V06141 2870200019 SUPSD BY 151 PER SB016 2 151 140E4207 00 INSULATOR LATCH FC SUPSDS ITEM 150 PER SB016 A B C E F G H L M N P R U V W Y AA AC 1 152 2739800201 WASHER SHOULDER 115ID T AB 1 155A 205E1596 00 PWA AUDIO COMPRESSOR SUPSD BY 155B PER ECO 8824 1 155B 205E1849 00 PWA AUDIO COMPRESSOR SU...

Page 328: ... FSK SUPSDS 155C SN377 PER ECO 10365 SUPSD BY 155M PER SB009 C 1 155H 205E1849 14 Deleted 155J 205E1849 17 PWA AUDIO COMPRESSOR HIGH QUALITY ONLY SUPSD BY 155P PER SB009 L 1 155K 205E3977 10 PWA AUDIO COMPRESSOR SUPSDS 155F PER SB009 SUPSD BY ITEM 155R PER SB015 A B 1 155L 205E3977 12 PWA AUDIO COMPRESSOR w AGC SUPSDS 155D PER SB009 SUPSD BY ITEM 155S PER SB015 E F G H 1 155M 205E3977 13 PWA AUDIO...

Page 329: ...W 205E3977 37 PWA AUDIO COMPRESSOR HIGH QUALITY ONLY T AB 1 160 MS51957 14 SCREW PAN HEAD 4 40 X 5 16 V06141 2290200074 4 165A 024E1620 00 CABLE ASSEMBLY FA2100 W001 W003 SUPSD BY ITEM 165B for W001 and 170B for W003 PER SB015 2 165B 024E2659 01 CABLE ASSEMBLY FA2100 W001 SUPSDS ITEM 165A W001 only EFF A B C L M N PER SB015 A B C L M N P R T U V W Y AA AB AC 1 165C 024E3424 03 CABLE ASSEMBLY FA210...

Page 330: ... PER SB006 A B C E F G H 1 175D 205E2502 11 PWA ACQUISITION PROCESSOR SUPSDS 175B 175C PER SB006 CONFIGS E F G H SUPSD BY ITEM 175F PER SB013 CONFIGS A B C SUPSD BY ITEM 175G PER SB015 A B C E F G H 1 175E 205E2502 14 PWA ADV ACQUISITION PROCESSOR W OMS L M N R W AA AC 1 175F 205E2502 52 PWA ACQUISITION PROCESSOR SUPSDS 175D PER SB013 SUPSD BY ITEM 175H PER SB015 E F G H 1 175G 205E2502 21 PWA ACQ...

Page 331: ...1 185C 253E1568 06 MEMORY CSMU ASSEMBLY 7X32 MEG TITANIUM SUPSD BY 185H PER SB008 F 1 185D 253E1568 07 MEMORY CSMU ASSEMBLY 15X32 MEG TITANIUM SUPSD BY 185J PER SB008 H 1 185E 253E1568 33 MEMORY CSMU ASSEMBLY 9X128 MEG 3V STRATA FLASH SUPSD BY 185L PER SB019 L N P R T 1 185F 253E1568 38 MEMORY CSMU ASSEMBLY 7X128 MEG 3V STRATA FLASH SUPSDS 185B PER SB008 SUPSD BY 185L PER SB019 B C G 1 185G 253E15...

Page 332: ...PER SB019 SUPSD BY 185P FOR B C N U V W AA AC PER SB023 A B C E G L N P R T U V W Y AA AB AC 1 185M 253E5675 11 MEMORY CSMU ASSEMBLY 2 GB NAND MEMORY MODULE TITANIUM SUPSDS 185H 185J PER SB019 SUPSD BY 185R FOR H PER SB023 F H 1 185N 253E5675 20 MEMORY CSMU 2GB NAND CYRILLIC NON EMI SUPSDS 185K PER SB019 M 1 185P 253E5675 02 MEMORY CSMU 2GB NAND SUPSDS 185L PER SB023 B C N U V W AA AC 1 185R 253E5...

Page 333: ...SMU COVER SHORT BOX SUPSDS 200A PER SB019 1 205 9030100047 LABEL ESD 1 210 147E1679 00 SHIPPING PACKAGE KIT 1 220 197E1746 00 CONTAINER SHIPPING SHORT 1 225 0279800024 CAP DUST DPX SERIES CONN 1 1 235 2529800107 TAPE WATERPROOF WOVEN BACKED 1 240A 9030100049 BAG PINK ZIPLOCK 9 X 12 SUPSD BY 240B 1 240B 9030100075 BAG 14X24 TRANSPARENT PINK SUPSDS 240A 1 245 9030100047 STATIC AWARENESS LABEL 1 ITEM...

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

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