L3 Communications FA2100CVR Installation/Operation Instruction Manual Download

Page: 11 / 20

Model FA2100CVR

Instruction Manual

Installation & Operation

Page xi

Rev. 16

165E1846-00

List of Illustrations (Continued)

Figure

Page

Figure A-26. Model S055 Microphone Element Specifications and

Response Diagram

A-42

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Figure A-27. Model S056 Microphone Element Specifications and Response Diagram

A-43

. .

Figure A-28. Outline and Dimensions, Model A151B Control Unit

Does Not Comply with ED-56A

A-44

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Figure A-29. Interwiring Diagram, Voice Recorder Unit, A151B Control Unit,

A55B Remote Microphone Does Not Comply with ED-56A

A-45

. . . . . . . . . . . .

Figure A-30. Outline and Dimensions, Model A152B Control Unit

Does Not Comply with ED-56A

A-47

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Figure A-31. Interwiring Diagram, Voice Recorder Unit, A152B Control Unit with Internal

Microphone Does Not Comply with ED-56A

A-48

. . . . . . . . . . . . . . . . . . . . . . . .

Figure A-32. Outline and Dimensions, Model A150 External Preamplifier Module

Does Not Comply with ED-56A

A-50

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Figure A-33. Interwiring Diagram, Voice Recorder Unit, A150 External Preamplifier,

A55B Remote Microphone
Does Not Comply with ED-56A

A-51

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Figure A-34. Outline and Dimensions, Model A55B Surface‐Mount Microphone Module,

Directional Microphone
Does Not Comply with ED-56A

A-53

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Figure A-35. Outline and Dimensions, Model A55B Surface‐Mount Microphone Module,

Mini‐Condenser Microphone
Does Not Comply with ED-56A

A-54

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Figure A-36. Outline and Dimensions, Model A55B Panel‐Mount Microphone Module, Rear

Connector
Does Not Comply with ED-56A

A-55

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Figure A-37.Outline and Dimensions, Model A55B Panel‐Mount Microphone Module, Top

Connector
Does Not Comply with ED-56A

A-56

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Summary of Contents for FA2100CVR

Page 1: ...NUMBERS 2100 1010 00 2100 1020 00 2100 1020 02 2100 1020 90 2100 1025 02 2100 1025 12 2100 1025 22 2100 1025 24 2100 1026 02 2100 1027 02 CONTROL UNIT MODEL NUMBERS S151 S161 S152 S162 S251 S261 A151B A152B MICROPHONE PREAMPLIFIER S150 S160 MODULE MODEL NUMBERS A150 REMOTE MICROPHONE S055 S056 MODEL NUMBERS A55B Manufactured in Accordance with FAA TSO C123a FAA TSO C123b EUROCAE ED 56A EUROCAE ED ...

Page 2: ...30 941 371 0811 FAX 941 377 5591 CAGE Code 06141 EXPORT CONTROL STATEMENT SSCVR TECHNOLOGY DATA This Solid State Fight Data Cockpit Voice Recorder Technical Data is being exported from the United States in accordance with the Export Administration Regulations ECCN 7E994 No License Required NLR Diversion contrary to U S law is prohibited In accordance with U S Law Title 15 CFR Part 746 and Suppleme...

Page 3: ...power is applied on 2100 1027 02 recorder only if the interconnect wiring are not to ARINC 757A requirements This is because of the power pins are different in the ARINC 757A from the ARINC 757 The mating keys on the connector are rotated different Refer to Figure 5 sheet 2 of 2 of this manual as a safe guard to prevent mating a ARINC 757 type recorder Do not remove or rotate the keys ...

Page 4: ... devices When handling or servicing equipment containing static sensitive devices adequate precautions must be taken to prevent device damage or destruction Only personnel 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 prevent static charge build up...

Page 5: ...rom the S162 drawing in Appen dix A Clarified GMT FSK operation for 02 configurations 06 Jan 20 02 Corrected S261 Control Unit Wire Diagram in Appendix A to show 37 pin connector vs 41 pin connector interface Added S056 Mic Spec 07 Jan 01 03 Updated Control Unit information Changed recommended microphone cabling 08 Oct 15 04 Updated S055 connector information Added new Control Units and associated...

Page 6: ...100 Cattleman Road 13 Jul 30 09 Correct pin call out under Notes for number 14 for figure A 5 A 9 A 13 14 Mar 31 10 Added FAA TSO C123b and 2100 1025 22 EQF Added OMS and Datalink data Deleted FAA Action Notice A8300 56 in all figure notes in Appendix A 15 Feb 24 12 New CAUTION for 757A type recorders inter connect wiring Added new part numbers 2100 1025 24 and 2100 1027 02 16 June 13 12 Updated T...

Page 7: ...6 1 Data Link Input and Encapsulation 13 1 6 2 DataLink Heartbeat 14 1 6 3 Williamsburg Bit Oriented Protocol Version Support 15 1 6 4 DataLink Memory Capacity 15 1 6 5 DataLink Retrieval 15 1 6 6 Control Units and External Preamplifier 17 1 6 7 Remote Microphone Module 18 1 6 8 CVR Mounting Racks 19 1 7 Abbreviations and Acronyms 19 2 0 EQUIPMENT LIMITATIONS SPECIFICATIONS 19 2 1 Applicable Docum...

Page 8: ... 6 0 FA2100CVR READOUT 33 7 0 OPERATING INSTRUCTIONS 34 8 0 FLIGHT CHECKOUT PROCEDURE 34 8 1 Operational Notes 34 8 2 Flight Checkout 34 9 0 MAINTENANCE AND CALIBRATION 36 9 1 Recorder 36 9 2 Data Download Using P N 17TES0078 Cable 36 9 3 Underwater Locator Device 38 9 4 Product Support 39 9 5 Authorized Repair Facilities 39 9 6 Loaner Rental Program 39 Appendixes A OUTLINE DIMENSIONS MICROPHONES ...

Page 9: ... FA2100CVRs using a Portable Interface 32 Figure 9 On Aircraft Setup for Data Download FA2100CVRs using a Portable Interface 38 Figure A 1 Part Number Definition Model S151 S161 Model S152 S162 and Model S251 S261 Control Units A 3 Figure A 2 Outline and Dimensions Model S151 Control Unit A 5 Figure A 3 Interwiring Diagram Voice Recorder Unit S151 Control Unit S055 Remote Microphone A 6 Figure A 4...

Page 10: ...erwiring Diagram Cockpit Voice Recorder Unit S161 Control Unit and S056 Microphone For Airbus A350 Aircraft A 28 Figure A 17 Outline and Dimensions Model S150 External Preamplifier Module A 30 Figure A 18 Interwiring Diagram Voice Recorder Unit S150 External Preamplifier S055 Remote Microphone A 31 Figure A 19 Outline and Dimensions Model S160 External Preamplifier Module A 33 Figure A 20 Interwir...

Page 11: ...corder Unit A152B Control Unit with Internal Microphone Does Not Comply with ED 56A A 48 Figure A 32 Outline and Dimensions Model A150 External Preamplifier Module Does Not Comply with ED 56A A 50 Figure A 33 Interwiring Diagram Voice Recorder Unit A150 External Preamplifier A55B Remote Microphone Does Not Comply with ED 56A A 51 Figure A 34 Outline and Dimensions Model A55B Surface Mount Micropho...

Page 12: ... Page Table 1 FA2100CVR Descriptions 2 Table 2 CVR OMS Output Words 5 Table 3 CVR Pins Assigned to RIPS Status Monitoring 6 Table 4 CVR Label 350 Output format 6 Table 5 CVR Fault Reporting Interactions 7 Table 6 CVR Status Word Fault Reporting Criteria 8 Table 7 Model FA2100CVR Recording Specifications 17 ...

Page 13: ...ay be located at www L 3 com or L 3ar net Comments or recommendations about the installation operation and check out of the FA2100CVR should be sent to L 3 Communications Aviation Recorders Product Support Department at the address shown in section 9 4 1 2 Equipment and Document Requirements The following equipment and documents are or may be required for on aircraft installation and check out of ...

Page 14: ... and a Mounting Tray Interconnec tion between the recorder and control unit or external preamplifier is accomplished using aircraft wiring 1 4 System Overview Table 1 contains a summary description of the FA2100CVRs covered in this manual Table 1 FA2100CVR Descriptions Part Number Description Weight 0 5 lbs 2100 1010 00 ARINC 404A 1 2 ATR Short Case ARINC 757 30 Minutes 10 0 lbs 2100 1020 00 ARINC...

Page 15: ...e of more then six years The ULD meets or exceeds the requirements of FAA TSO C121 The Ground Support Equipment GSE connector is located on the front of the FA2100CVR This connector provides the interface from the recorder to GSE for checkout of the recorder or to transfer data to a readout device The FA2100CVR is connected to aircraft wiring via a 57 pin DPXB style connector CSMU ULD GSE CONNECTO...

Page 16: ... 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 429 OMS OUTPUT B 429 DATA LINK FAULT DATA LINK IN A 429 DATA LINK IN B 429 OMS IN A OMS IN B OMS Data Link are applicable to t...

Page 17: ...peration It may be connected to an annunciator or to an aircraft central maintenance computer At start up the FA2100CVR initiates a Built in Test BIT and then continuously monitors itself for fault conditions Previously recorded information cannot be read from the Model FA2100CVR while it is installed in the aircraft Refer to paragraph 6 0 for additional information 1 5 Onboard Maintenance System ...

Page 18: ...T N FUNCTION STATUS 1 8 Label 350 1 2 3 4 5 6 7 8 1 1 1 0 1 0 0 0 9 10 SDI 10 9 0 0 Normal CVR1 0 1 Not used CVR2 1 0 Not used 1 1 Not used 11 CVR Status Audio Recording Failure 0 OK 1 Failure 12 CMC Bus Status OMS Input 0 OK 1 Failure 13 CVR Control Unit Failure 0 OK 1 Failure 14 FDR Status always set to 1 0 OK 1 Failure 15 RIPS Fault Status Pin 29 0 OK 1 RIPS Fault 16 CVR DataLink Recording Fail...

Page 19: ...expected If the RIPS meets this requirement which ensures it is operating in accordance with its intended func tion on the next power up the OMS discrete bits would indicate a no Maintenance and a no Fault condi tion regardless of the information the RIPS provides to the CVR This no Maintenance and no Fault re porting would also occur if the previous recorder power cycle was less than 10 minutes i...

Page 20: ...will not be detected or reported until the next Push to Test is initiated This audio input circuit failure is the only fault that would not otherwise be detected and re ported by the CVR continuous BITE Push to Test results are reported during the test using the CVR Test Indicator output Pins 15 16 which is usually connected to an indicator lamp or meter on the CVR Control Unit In addition CVR fai...

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