L3 FA5000 Maintenance Manual
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L3 FA5000 Maintenance Manual

Cockpit voice recorder
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DISTRIBUTION STATEMENT:
information and must not, without prior written consent of L3 Aviation Products, be used or reproduced in
whole or in part, or communicated to any person except as authorized by L3 Aviation Products.
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.
The document reference is online, please check the correspondence between the online documentation and the printed version.
COMPONENT MAINTENANCE MANUAL
Model FA5000
MODEL FA5000
COCKPIT VOICE RECORDER
RECORDER PART NUMBERS:
5003−5000−00
5003−5000−01
5003−5001−50
500−4030−000 RIPS
COMPONENT MAINTENANCE MANUAL WITH
ILLUSTRATED PARTS LIST
P/N: 165E1689−02
IN ACCORDANCE WITH
FAA TSO−C123b
EUROCAE ED−112
ARINC CHARACTERISTIC NO. 757/757A
VENDOR CODE: 06141
This document contains L3 Aviation Products privileged
5013−5000−30
5013−5001−50
23−70−30
Rev. 02
July 21/17

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  • Page 1 This document contains L3 Aviation Products privileged information and must not, without prior written consent of L3 Aviation Products, be used or reproduced in whole or in part, or communicated to any person except as authorized by L3 Aviation Products.
  • Page 2 This manual contains date sensitive information. To verify the latest revision level of this manual, visit our document download site at http://www.L−3ar.net. ECopyright 2017 by L3 Technologies, Aviation Products End User Statement. This manual is intended for aircraft owners and their designated agents for installation of this product.
  • Page 3 COMPONENT MAINTENANCE MANUAL Model FA5000 GENERAL This product and related documentation must be reviewed for familiarization with safety markings and instructions before operation. This instrument was constructed in an ESD (electro–static discharge) protected environ- ment. This is because most of the semiconductor devices used in this instrument are susceptible to damage by static discharge.
  • Page 4 COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70−30 Title Rev. 02 Page iv Use or disclosure of information on this sheet is subject to July 21/17 The document reference is online, please check the correspondence between the online documentation and the printed version.
  • Page 5 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 HIGHLIGHTS Pages which have been added or revised are outlined below, together with the highlights of Revision 02. Section Page Description Title List of FSB’s Front Matter Revised pages to Rev. 02 Introduction Added references to the ULB CMM and I/O manuals.
  • Page 6 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 HIGHLIGHTS Pages which have been added or revised are outlined below, together with the highlights of Revision 01. Section Page Description Title List of FSB’s Front Matter Introduction Added updated 90−day ULB details. Added new part numbers: 5013-5000-30, 5013-5001−50.
  • Page 7 Added updated 90−day ULB details. RIPS condi- Rev. 01 October 6/16 tioning, new part numbers added: 5013-5000-30, 5013-5001−50 Updated L3 company name, added ULB refer- Rev. 02 July 21/17 ence to CMM/I/O, added RIPS conditioning steps, and shipping information. 23–70–30 Highlights Rev.
  • Page 8 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–30 Highlights Rev. 02 Page viii Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.
  • Page 9 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 RECORD OF REVISIONS REV. INSERTION REV. INSERTION REV. INSERTION DATE DATE DATE October 6/16 C.P. July 21/17 C.P. 23–70–30 Record of Revisions Rev. 02 Page ix Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document.
  • Page 10 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–30 Record of Revisions Rev. 02 Page x Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document.
  • Page 11 SERVICE BULLETIN LIST SERVICE BULLETIN DATE EFFECTIVITY DESCRIPTION FA5000 SB004 June 16/15 FA5000 Family Cut−in of 90−day ULB to newly manufac- tured recorders or field modification using 23−70−40−04 the 90−day Beacon Conversion Kit. 23–70–30 Service Bulletin Rev. 02 Page xi...
  • Page 12 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–30 Service Bulletin Rev. 02 Page xii Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.
  • Page 13 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 LIST OF EFFECTIVE PAGES Section Page Date Section Page Date Title Page xxxii Jul. 21/17 xxxiii Jul. 21/17 Jul. 21/17 Introduction Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul. 21/17 Highlights Jul. 21/17 Jul.
  • Page 14 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 LIST OF EFFECTIVE PAGES Section Page Date Section Page Date Description and Operation Jul. 21/17 Jul. 21/17 (Continued) Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul.
  • Page 15 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 LIST OF EFFECTIVE PAGES Section Page Date Section Page Date Testing and Troubleshooting Jul. 21/17 Jul. 21/17 (Continued) Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul. 21/17 Jul.
  • Page 16 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 LIST OF EFFECTIVE PAGES Section Page Date Section Page Date Illustrated Parts List (Continued) 1012 Jul. 21/17 1013 Jul. 21/17 1005 Jul. 21/17 1014 Jul. 21/17 1006 Jul. 21/17 1015 Jul. 21/17 1007 Jul.
  • Page 17 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 TABLE OF CONTENTS INTRODUCTION SUBJECT/DESCRIPTION PAGE GENERAL ..............

  • Page 18: Table Of Contents

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 TABLE OF CONTENTS DESCRIPTION AND OPERATION SUBJECT/DESCRIPTION PAGE GENERAL ..............
  • Page 19 ........... MODEL FA5000 CVR SYSTEM THEORY OF OPERATION .
  • Page 20 ..........MODEL FA5000 CVR RECORDER IN-SERVICE CHECKOUT .
  • Page 21 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 TABLE OF CONTENTS TESTING AND TROUBLESHOOTING − Cont SUBJECT/DESCRIPTION PAGE (11) Crosstalk Data ........... .
  • Page 22 ......MODEL FA5000 DISASSEMBLY INSTRUCTIONS ......
  • Page 23 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 TABLE OF CONTENTS CHECK SUBJECT/DESCRIPTION PAGE GENERAL ..............
  • Page 24 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 TABLE OF CONTENTS ASSEMBLY − Cont SUBJECT/DESCRIPTION PAGE STORAGE INSTRUCTIONS ..........
  • Page 25 ..........1004 L3 AVIATION PRODUCTS (L3AP) AUTHORIZED PARTS ..... . .
  • Page 26 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–30 Table of Contents Rev. 02 Page xxvi Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document.
  • Page 27 ........Figure 2. Model FA5000 Cockpit Voice Recorder Part Number Matrix .
  • Page 28 ..... . . Figure 704. FA5000 Connector Cover and RIPS Connector Cap ..... .
  • Page 29 FIGURE TITLE Page Figure 1000. (Sheet 1 of 2) Model FA5000/5003 CVR Recorders ....1008 Figure 1000. (Sheet 2 of 2) Model FA5000/5003 CVR Recorders .
  • Page 30 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–30 Table of Contents Rev. 02 Page xxx Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document.
  • Page 31 ............Table 1 Model FA5000 CVR Audio Recording Specifications .
  • Page 32 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS IS INTENTIONALLY LEFT BLANK 23–70–30 Table of Contents Rev. 02 Page xxxii Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document.

  • Page 33: General

    INTRODUCTION 1. GENERAL This Component Maintenance Manual (CMM) documents the operation of and suggested maintenance for the Model FA5000 Cockpit Voice Recorder/Flight Data Recorder, herein after referred to as the Model FA5000 or FA5000. FA5013 CVR features: ED-112 compliant recording duration of 2−hours minimum Audio and Data Link On−Board Maintenance System (OMS) monitoring...
  • Page 34 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 File Transfer Protocol General Aviation Greenwich Mean Time ground Ground Support Equipment HTTP HyperText Transfer Protocol Internet Protocol Illustrated Parts List Line Replaceable Unit Megahertz MTBF Mean Time Between Failures NVRAM Non-Volatile Random Access Memory...
  • Page 35 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 3. DOCUMENT REQUIREMENTS The following equipment and documents are, or may be, required for on-aircraft installation and check out of the FA5000s: This Component Maintenance Manual. Portable Interface/2 Operator’s Manual, P/N: 165E1630-01 Installation and Operation Manual, Cockpit Voice Recorder, Model FA5000CVR, P/N: 165E5327-00 Component Maintenance Manual, ED−56A Control Units, Preamplifier, &...
  • Page 36 DESCRIPTION AND OPERATION This section contains the description and operation information for the Model FA5000 Cockpit Voice Recorder. Line art is used to illustrate the unit, its intercon- nections and functionality. This section also contains the Model FA5000 Theory of Operation.
  • Page 37 The steps of each procedure are coordinated with the TESTING AND TROUBLESHOOTING Section. Access to subassemblies within the FA5000 is described such that there is minimal disturbance to other sub- assemblies. 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) drawing for ordering replacement parts.

  • Page 38: Table 1. Shop Verification

    It also provides a description of the Read−Out Cen- ter (ROC)/CVDR Automated Test Station (CATS) as used with the Recorder Inter- face Unit (RIU) to test and download from the FA5000. ILLUSTRATED PARTS LIST This section contains parts location diagrams and parts listings for all versions of the Model FA5000CVR listed on the Title Page of this manual.
  • Page 39 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 7. COMPONENT MAINTENANCE MANUAL (CMM) EFFECTIVITY Effectivity of the CMM is based on effectivity dates and product serial number. Effectivity of the manual is identified by a list of effective pages in the front of the manual.
  • Page 40 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23−70–30 Introduction Rev. 02 Page 8 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.
  • Page 41 COMPONENT MAINTENANCE MANUAL Model FA5000 DESCRIPTION AND OPERATION 1. GENERAL This Component Maintenance Manual describes the Model FA5000, Cockpit Voice Re- corder (CVR). FA5000CVR, P/N: 5003-5000−00, 5003-5000-01, 5003-5001-50, 5013-5000-30, and 5013-5001-50. Features include: ED-112 compliant ARINC 757/A characteristics, including Greenwich Mean Time (GMT) interface Maintenance free −...

  • Page 42: Fa5000 Configurations

    The current configurations of the FA5000s are listed with its specific part number in the IPL Section Figure 1. The specific configuration FA5000 part number is constructed as shown below: Figure 2. Model FA5000 Cockpit Voice Recorder Part Number Matrix 23–70−30...

  • Page 43: System Description

    Model FA5000 3. SYSTEM DESCRIPTION FA5000 CVR software processes incoming analog audio data to digital format and pro- vides large capacity digital memory storage. The software provides built-in test functionali- ty that automatically performs checks of the hardware and software to indicate whether the system is operating normally.

  • Page 44: Figure 3. Cvr Block Diagram

    Model FA5000 Figure 3. CVR Block Diagram Figure 4 Recorder Data Flow Diagram shows the data flow diagram for the Model FA5000 CVR. The diagram shows the relationship between the hardware and the software. The FPGA conditions all of the input data and processes it into packets. Digitized audio data enters the FPGA and is transmitted to the processor via the TDM bus.
  • Page 45 All tasks will be able to communicate with the BITE task for the purpose of send- ing fault information and/or system status information. The user can interface to the Model FA5000 CVR in several different ways. All of the in- terfaces use an Ethernet network as the means for transferring data. The most common interface will be to a web server via an HTTP connection.

  • Page 46: Figure 4. Recorder Data Flow Diagram

    Connections Figure 4. Recorder Data Flow Diagram The Model FA5000 CVR contains a CSMU (non-volatile memory) that is used to store au- dio data, flight data, and DataLink messages. Since the memory size is finite, it is possi- ble for the memory to fill up with the information being stored. This situation will be han- dled by the Data Storage task that is responsible for writing the data to the CSMU.

  • Page 47: Software Module Description

    This is used to coordinate which tasks are running at any giv- en time. The Model FA5000 CVR will be able to be loaded via the TCP/IP interface used by the GSE task. This task will report a checksum of the loaded code to ensure the integrity of the newly loaded software.
  • Page 48 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 er is sent to the CAM partition for every half seconds worth of data. The packet header includes a time tag, a milliseconds since the last second time tag, the current power up counter value, and the packet number from last power up.

  • Page 49: Figure 5. Cvr Task Flowchart

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Initialize SPORT for 4 Channel TDM Mode Open 4 UDP sockets for audio streaming. Set Packet Number to 0. Get Power Up Count Receive 20 Msec 4 channel raw audio frame Stream Data to each...

  • Page 50: Datalink Task

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 DataLink Task The DataLink task is used to process ARINC 429 data received from avionics equipment external to the recorder. Normally, the source of data is some type of Air Traffic Service Unit (ATSU). The DataLink task analyzes the data coming in from the ARINC 429 input port and decides which DataLink protocol is currently being used.
  • Page 51 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 and doing it this way is much simpler than storing just the data portion of the message. Also, storing the entire data word may help the GSE reconstruct the message exchange during post-processing.

  • Page 52: Figure 6. Datalink Memory Format

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Flash Memory Flash Memory Flash Memory Chips Blocks Pages 32 bytes Block Header Spare 32 bytes Page Header 8 bytes 1021 DataLink 1022 120 bytes Messages 1023 128 Kbyte erase Each page block containing contains thirty 1024 128−byte...

  • Page 53: Oms Task

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Record Mode? Valid Send Page Data in Beginning Read FIFO Data? Header of Page? FIFO? Send Data Label Send Data 350? DataLink Heartbeat Processing Figure 7. DataLink Task Flowchart OMS Task The OMS task receives status from the other tasks in the system and creates a status word suitable for output onto the ARINC 429 bus via Label 350.

  • Page 54: Data Storage Task

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 One Second Elapsed? Gather Status Information from other Tasks Format Status Send Status to ARINC 429 bus via Label 350 Send Status to DataLink Task Figure 8. OMS Task Flowchart Data Storage Task The Data Storage task is used to manage the storage of all of the input data streams into a Crash Survivable Memory Unit (CSMU).
  • Page 55 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 When the Data Storage task starts, the first thing that it will do is make sure that the CSMU hardware is present and that the memory needed for data storage within each par- tition is contained in the CSMU.

  • Page 56: Figure 9. Data Storage Task Flowchart

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Validate Partitions Get CSMU Type Read Indices Read Input Queue Need Write Erase−Ahead? Request? Any Writes Read In Progress Read Data Request? (Same Partition)? Start Erase−Ahead Erase Request? Any Writes (CVR Only) In Progress?

  • Page 57: Bite Task

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 BITE Task The BITE task is used to monitor the proper operation of the recorder as defined by the EUROCAE MOPS ED-112 document. It is responsible of keeping track of the current sta- tus of the recorder and managing the fault log.
  • Page 58 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 The recorder hardware will be able to generate status information to describe the current functionality of the unit. These will include power status to different peripherals, non-intru- sive real-time status on certain pieces of hardware, and watchdog maintenance. See Fig- ure 11 −...

  • Page 59: Figure 11. Bite Task Flowchart

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Point to current NVRAM Fault Log Location Create Fault Log Message Queue Pet the Watchdog Received any Faults on Queue? Write Fault to Fault Log NVRAM Does Fault requires setting A Fault Light?

  • Page 60: Gse Task

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 GSE Task The GSE task is used to manage communication between the recorder and the service operators who wish to do things like download data, monitor real-time data, monitor recorder performance, and do return-to-service testing.

  • Page 61: Figure 12. Gse Task Data Flow Diagram

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 TCP/IP Server Message Queue Response Command Msg Queue Msg Queue Command Task Table Function to be Performed Figure 12. GSE Task Data Flow Diagram 23–70−30 Description and Operation Rev. 02 Page 21 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.

  • Page 62: Figure 13. Gse Task Flowchart

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Create Command and Response Msg Queues Wait for Command Message Queue Got Command Search for command Command Table code on table Found Process Command On Next Command Table? Execute Command Error Response Response to...

  • Page 63: Table 1 Model Fa5000 Cvr Audio Recording Specifications

    FA5000 . This connector provides the interface from the recorder to GSE Ethernet con- nection for checkout of the recorder, or to transfer data to a readout device. The FA5000 is connected to aircraft wiring via a 57-pin, DPXB-style connector.

  • Page 64: Underwater Locator Beacon (Ulb)

    G. Underwater Locator Beacon (ULB) The Model FA5000 CVR has an underwater locator beacon mount located on its front panel which also acts as the recorder’s carrying handle. The ULB mount will accept ei- ther a 30−day or a 90−day underwater locator beacon. The ULB meets or exceeds the requirements of the Federal Aviation Administration technical standard order TSO- C121 for 30−day beacons, or TSO−C121b for 90−day beacons.

  • Page 65: Circuit Boards

    Model FA5000 Circuit Boards The FA5000 electronics contain all the necessary power supplies and circuitry to in- put, record, monitor and playback data. In addition, circuitry to perform self–test functions and provide signals to the appropriate status indicators is also integrated into the FA5000 electronics.

  • Page 66: Figure 14. Model Fa5000 Cvr, (P/N: 500X-500X-( ))

    CSMU TO CVR Crash Survivable Memory Unit) ASSEMBLY (CRASH PROTECTED SOLID STATE MEMORY) Figure 14. Model FA5000 CVR, (P/N: 500X-500X-( )) Functional System Block Diagram 23–70−30 Description and Operation Rev. 02 Page 26 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.

  • Page 67: Figure 15. Model Fa5000 Gacvr (P/N: 500X-500X-50)

    TO GACVR Crash Survivable Memory Unit) ASSEMBLY (CRASH PROTECTED SOLID STATE MEMORY) Figure 15. Model FA5000 GACVR (P/N: 500X‐500X‐50) Functional System Block Diagram 23–70−30 Description and Operation Rev. 02 Page 27 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.

  • Page 68: Stop Recording Command

    Model FA5000 Stop Recording Command Assertion of the “Stop Recording” command stops the FA5000 CVR recording within ten minutes. Removal of the “Stop Recording” command or “Push-To-Test” resumes the recording. If the recording is resumed due to the “Push-To-Test” function being activated, the recording will again cease within 10 minutes if the “Stop Recording”...

  • Page 69: Control Unit Test And Bulk Erase Signals

    During this time, a 620 Hz to 660 Hz signal is generated within the FA5000 which is used to test the circuitry of all the audio channels. In a successful test, the FA5000 Recorder provides a TEST INDICATOR signal which 23–70−30...

  • Page 70: Output Audio Quality

    CH – Channel HQ – High Quality OMS − Onboard Maintenance System* Figure 17. Model FA5000 CVR 120-Minute Recording Schemes Output Audio Quality The FA5000CVR’s audio quality meets or exceeds the audio quality specified in Part I of ED−112. Specifically, the Reference Signal is 1-kHz at 3 Vrms for the voice channels, and 1-kHz at 2 Vrms for the CAM channel.

  • Page 71: Fa5000 Specifications

    NOTE: All of the times indicated in the above chart are minimum recording times. 5. FA5000 SPECIFICATIONS Specifications for the Model FA5000 CVR have been developed in close coordination with Aerospace Industry regulatory agencies. As such, the FA5000 meets or exceeds the re- quirements of technical standard order TSO–C123b, TSO-124b, TSO-155a, EUROCAE...

  • Page 72: Physical Characteristics

    Model FA5000 CVR Installation and Opera- tion Instruction Manual, P/N: 165E5327-00. The Model FA5000 CVR is an environmentally hardened unit housed in an ARINC 404A 1/2-ATR short box painted international orange. The FA5000 does not require external shock mounting for installation into the aircraft.
  • Page 73 COMPONENT MAINTENANCE MANUAL Model FA5000 The FA5000 is connected to its control unit or preamplifier module by means of the air- craft wiring. Refer to Figure 18 for the Standard ARINC−757 and Figure 19 for the Stan- dard ARINC−757/A Interface Wiring Diagrams used when installing the FA5000CVR into an aircraft.

  • Page 74: Figure 18. Interwiring Diagram, Recorder Fa5000 Cvr

    MIC. BIAS(WHITE) DATALINK VALID MIC HIGH (BLACK) VOICE ERASE ”C” MIC. LOW (GREEN) Figure 18. Interwiring Diagram, Recorder FA5000 CVR 23–70−30 Description and Operation Rev. 02 Page 34 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.
  • Page 75 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Notes for Figure 18: Recommended minimum wire size is #22; however, wire size #24 is electrically permissible except for long-run power leads where #18 wire is recommended (pins 2, 3, 9, & 17)

  • Page 76: Figure 19. Interwiring Diagram, Recorder Fa500X Gacvr

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 STANDARD INTERWIRING PER ARINC SPEC 757A Model 500X−5001−50 VOICE RECORDER UNIT TO AC COLD 115 VAC POWER IN COLD 115 VAC POWER IN HOT TO 115 VAC, 400 HZ + 28 VDC RETURN...
  • Page 77 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Notes for Figure 19: Recommended minimum wire size is #22; however, wire size #24 is electrically permissible except for long-run power leads where #18 wire is recommended (pins 1, 2, 3, 9, & 17) Wire resistance should not exceed 1 ohm for power leads and should not exceed 5 ohms for signal leads.

  • Page 78: Theory Of Operation

    Model FA5000 7. THEORY OF OPERATION The theory of operation provided for the Model FA5000 CVR describes the function of the recorder both at the system level, PWA level and software operational level. System level theory of operation describes the general operation of the system as a whole. Refer to the Model FA5000 CVR System Block Diagram during the following discussion.

  • Page 79: Aircraft Interface (Ai) Pwa

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Aircraft Interface (AI) PWA The Aircraft Interface (AI) PWA mounts within the rear of the Cockpit Voice Recorder chassis and provides the interface between the aircraft and the Cockpit Voice Recorder’s CPU/Main Processor functions. The Aircraft Interface PWA also in- cludes the storage power supply and provides RF filtering and lightning protection for all input and output signals that interface with the aircraft.

  • Page 80: Software Considerations

    Software Partitioning Software for the Model FA5000 CVR Solid State Flight Recorders will be partitioned into two parts. This is to accommodate the use of two DSPs. One DSP, called the Flight Data Processor (FDP), is responsible for the collection, processing, and for- warding of Data Link messages.

  • Page 81: On−Board Maintenance System (Oms) Interface

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 and Flash memory within the CSMU, that is used to store Data Link and audio data. Each DSP has a total of 10k words of built−in RAM. Each DSP has access to 64k of ROM for the executable program image.

  • Page 82: Data Link (Atc) Interface

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Failure of the recorder to Failure of the recorder to store Information In the store Information In the storage medium storage medium Insufficient audio or UTC Insufficient datalink record time record duration duration...

  • Page 83: Recorder Synchronization

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 already provided at A/C level (interlock devices monitored with the aircraft on− ground information and effective park brake locked), the CVR provides a timed inter- lock for erase. The erase starts by connecting CVR pin 55 to pin 57 for a minimum of 2 seconds and then connecting pin 55 to ground (pin17) before erasing the previ- ously recorded data.

  • Page 84: Cvr Rips Status Monitoring

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 The L−3AR Portable Interface/2, provides a means to download the Data Link mes- sage data at the CVR level so that an operator can easily and quickly download pre- viously recorded Data Link information without removing the recorder from its mount- ing.

  • Page 85: Rips Fault

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 RIPS Active CVR Discrete in- SSCVR Label 350 SSCVR Label 351 Status put (Pin 10) and 352(Bit 21) (Bit 12) Not active Open Active Ground RIPS Fault The CVR will use Pin 29 to receive the RIPS Failure Status Discrete output.

  • Page 86: Onboard Maintenance System Interface

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 If the RIPS is not present, then any reference to RIPS in the Interactive OMS output pages will be suppressed. However, in the case where the CVR is re- moved from an aircraft with RIPS and re−installed on an aircraft without RIPS, it is possible that previous flight leg RIPS fault information, stored in the CVR fault log while installed on the aircraft with RIPS, will be displayed.

  • Page 87: Label 350 Status Word Output

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 As an additional capability, this CVR also monitors the status of an attached Recorder Independent Power Supply, if present, and includes that status with the OMS output reporting. The RIPS status is monitored using the CVR input pins listed in Table 1.2:...

  • Page 88: Table 7. Cvr Fault Reporting Interactions

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 RIPS Maintenance Status (Battery) (pin 38) 0: No Maint. 1 : Maint. Req. RIPS Active Status (pin 10) 0: Not Active 1 : RIPS Active RIPS Presence Status (Pin 42) 0: Not Pres. 1 : RIPS Present 23­29 Spare...

  • Page 89: Table 8. Cvr Status Word Fault Reporting Criteria

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 results. If an audio input circuit failure occurs after a successful Push−to−Test oper- ation, it will not be detected, or reported, until the next Push−to−Test is initiated. This audio input circuit failure is the only fault that would not otherwise be detected and reported by the CVR continuous BITE.

  • Page 90: Label 354 Lru Identification Output

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 RIPS Maintenance Status RIPS Maintenance Status as reported on pin 38 input (Battery) (Pin 38) (if present). RIPS Active Status (Pin 10) RIPS Active Status as reported on pin 10 input (if present).
  • Page 91 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 d. Part Number (continued) Bit No Function Status 1­8 Label 354 11101100 9­15 Third character of part number Not used 17­23 Fourth character of part number Not used 25­31 Fifth character of part number Parity e.

  • Page 92: Label 377 Arinc 429 Equipment Identification Word Output

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 9­15 Second character of serial number Not used 17­23 Third character of serial number Not used 25­31 Fourth character of serial number Parity Serial Number (continued) Bit No Function Status 1­8 Label 354 11101100 9­15...

  • Page 93: Oms Input

    12 can be ignored. 10. CVR DATALINK INPUT INTERFACE The FA5000 CVR was developed specifically to satisfy recent requirements for Con- troller Pilot DataLink Communications (CPDLC or “DataLink”) recording in addition to the two hour audio recording capability. The DataLink recording function of the CVR is generally compatible with ARINC 429, ARINC 757/A, ARINC 758, and ARINC 619.
  • Page 94 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 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.

  • Page 95: Figure 21. Generic Datalink Message Encapsulation Structure

    Figure 21. Generic DataLink Message Encapsulation Structure As indicated in Section 1 above, the FA5000 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 words are also recorded as part of the DataLink stream.

  • Page 96: Datalink Heartbeat

    270 heartbeat is detected, and DataLink Valid (Pin 56) is not asserted. Williamsburg Bit−Oriented Protocol Version Support It should be noted that the FA5000 CVR does not currently support Williamsburg Version 1 protocol or a low speed ARINC 429 interface for input of DataLink informa- tion.

  • Page 97: Datalink Memory Capacity

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 DataLink Memory Capacity The CVR is currently configured with 32 Mbytes of dedicated DataLink recording memory. This provides for a recording duration far in excess of the existing two hour requirement. DataLink Retrieval Recorded DataLink information is retrieved from the CVR in much the same way as audio data.
  • Page 98 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70−30 Description and Operation Rev. 02 Page 58 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.

  • Page 99: Testing And Troubleshooting

    (ROC/7), P/N: 17TES0700 and is used in conjunction with the L3AP Recorder Interface Unit (RIU), P/N: 17TES0710. Testing for the Model FA5000 CVR is based upon an auto- mated operational test procedure. The automated test procedure may serve as an ac- ceptance criteria for the unit, as well as provide pointers to probable malfunctioning as- semblies in the event that the unit is not functioning properly.

  • Page 100: Model Fa5000 Cvr Recorder In-Service Checkout

    4. RECORDER INTERFACE UNIT (RIU) This section provides instructions for connecting the Recorder Interface Unit to the ROC/7 and FA5000 CVR under test. Refer to Figure 201 for the ROC Automated Test Station Software (CATS) FA5000 CVR test setup diagram.
  • Page 101 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Plug the cable (17TES0418) into the rear of the recorder to be tested. Plug the SCSI connector into “Rear Connector Intfc” (J1) and plug the blue connector into the blue “AC RCDR Power Test” (J9) connector. Both of these connectors are on the RIU front panel.

  • Page 102: Table 101. 17Tes0700

    Ethernet Cross−over (REQUIRED) 0249800386 Cable Assembly, 17TES0426 Speakers - 2 (OPTIONAL) * Items are included in ROC/7 Kit but not used with Model FA5000 testing. Table 101. 17TES0700 READOUT CENTER/7 (ROC/7) − Parts List 23–70−30 Testing & Fault Isolation Rev. 02 Page 104...

  • Page 103: Figure 101. Roc/7 W/Cvr Automated Test Station Software (Cats) Model Fa5000 Test Setup

    CABLE ASSY. 17TES0418 FA5000 CVR RECORDER * OPTIONAL Figure 101. ROC/7 w/CVR Automated Test Station Software (CATS) Model FA5000 TEST SETUP 23–70−30 Testing & Fault Isolation Rev. 02 Page 105 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.

  • Page 104: Read−Out Center/7 (Roc/7) − Sound Card Setup

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 READ−OUT CENTER/7 (ROC/7) − Sound Card Setup Double−click the CVDR Test icon on the ROC to start the software. The applic- ation will launch with the Channels control screen displayed, as illustrated in Figure 102.

  • Page 105: Figure 103. Volume Control

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Figure 103. Volume Control Under Applications, click Sound Systems, then click the Recording tab. This will display the Sound control window illustrated in Figure 104. Figure 104. Sound Control, Recording 23–70−30 Testing & Fault Isolation Rev.

  • Page 106: Figure 105. Line−In Properties, Line−In Level

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Highlight and select Line−in. Click on Properties. Select the Levels tab. Figure 105. Line−In Properties, Line−In Level Make sure that the Line−In level is set at 100 (move the Line−In slider to maximum.) Click on OK.

  • Page 107: Figure 106. Sound, Playback Devices

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Figure 106. Sound, Playback Devices (10) Highlight Speakers. (11) Click on Properties. (12) Select the Levels tab. 23–70−30 Testing & Fault Isolation Rev. 02 Page 109 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.

  • Page 108: Figure 107. Speaker Properties, Levels

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Figure 107. Speaker Properties, Levels (13) Make sure Playback Control is set at 100. (move the Playback Control slider to its maximum setting) (14) Make sure that the four remainingVolume slider levels do not need modification since these input volumes have been muted.

  • Page 109: Figure 108. Volume Mixer, Speaker Levels

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Figure 108. Volume Mixer, Speaker Levels (17) In the Volume Mixer, make sure both sliders are all the way up. (18) Close the Volume Mixer. 23–70−30 Testing & Fault Isolation Rev. 02 Page 111...

  • Page 110: Read−Out Center/7 (Roc/7) − Cats Autotest

    RMS multimeter. Set to DC amps Apply power to the RIU using 28 Vdc. If the CATS test page is not shown, click the L3 CVDR Test icon on the Windows desktop. Click the Ok button on the Monitor Audio Channel pop-up menu.

  • Page 111: Figure 109. Cats, Connecting Pop-Up

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 NOTE: This will load the Altera chip in the RIU unit. Observe the “con- necting to the recorder” status window appears. Observe Figure 109. CATS, Connecting Pop-Up On the tool bar, select Power ON.

  • Page 112: Figure 111. Cats, Start Test Toggle

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 On the tool bar, select Start Test. Figure 111. CATS, Start Test Toggle In the “Test Mode and Options” dialog box, select either Return−to−Ser- vice or Selectable Test Options, then click on OK.

  • Page 113: Figure 113. Cats, Cvdr Test Confirmation

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 NOTE: Figure 113 is only displayed if “Selectable Test Option” is cho- sen from the CATS, Test Mode and Options Screen. Figure 113. CATS, CVDR Test Confirmation NOTE: Follow the instructions displayed in the confirmation window.

  • Page 114: Figure 115. Cats, Power Test Input

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Figure 115. CATS, Power Test Input 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.

  • Page 115: Figure 117. Cats, Cvdr Fault History Log

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Figure 117. CATS, CVDR Fault History Log Click on Yes on the dialog box to clear the fault logs. Figure 118. CATS, CVDR Clear Fault Log Confirmation Observe the Fault History Log window appears. Select Print if you want to save the fault history or Close to continue.

  • Page 116: Figure 119. Cats, Cvdr Fault History Log

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Figure 119. CATS, CVDR Fault History Log Click on Yes. The autotest will now proceed in completing the autotest which will take approximately 30 minutes or less. Figure 120. CATS, Continue Test Confirmation At the end of the test, save the report by selecting File =>...

  • Page 117: Figure 121. Cats, Test Results Screen

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Figure 121. CATS, Test Results Screen If the autotest is successful, power off the recorder from the CATS menu bar. Turn 28VDC power off and remove the crossover and RIU cables from the recorder.

  • Page 118: Read Out Center/7 (Roc/7) − Autotest Descriptions

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 READ OUT CENTER/7 (ROC/7) − Autotest Descriptions The following provides detailed descriptions of the test performed during the autotest function. Power Test Test Prompts the user for DC power usage as in the following DC example: Please remove the front panel cable from the recorder now and click ”OK”.

  • Page 119: Bulk Erase

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Bulk Erase Part 1 – record audio out and verify 400 Hz bulk erase tone. Part 2 – record audio out and verify absence of bulk erase tone during rotor data output. Part 3 – record audio out and verify absence of bulk erase with recording disabled.

  • Page 120: Channel Balance

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 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 Hz (Expected 4 patterns > 6.9 Hz < 7.1 Hz) Results = 7.0 Hz, 7.0 Hz, 7.0 Hz, 7.0 Hz...

  • Page 121: Signal To Noise And Distortion

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 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 dBV 08:08:23 PASSED Frequency Resp (All within 6 dB) Signal to Noise and Distortion Record simulated data at each of the following frequencies once at 1.0 reference...

  • Page 122: Crosstalk Data

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 (10) Crosstalk Audio Record simulated 1000 Hz data for each channel 1,2,3 & 4 and calculate difference between driven and non−driven channels. Verify difference is less than −40 dB. Example report message(s): 08:41:34 PASSED Crosstalk (Audio) 1000 Hz 1.0 ref (Expected Driven − Non−...

  • Page 123: Fsk Time

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 (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) first with channel 1 output and again with channel 3 output. It verifies 9 good FSK data patterns and a switch to 9 good GMT 429 data patterns for each channel 1 and channel 3.

  • Page 124: Shutdown

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 (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.

  • Page 125: Oms

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 (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...

  • Page 126: Read−Out Center/7 (Roc/7) − Audio Download & Playback

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 READ−OUT CENTER/7 (ROC/7) − AUDIO DOWNLOAD & PLAYBACK NOTE: ROSE 4.0 or higher on a ROC or RAU is recommended to download directly from a CVR and convert audio into a .WAV for playback. Re- fer to the Read-Out Support Equipment / Recorder Interface Software version 4.0 or Higher Operator’s Manual, p/n 165E1696-03, to Re-...

  • Page 127: Test The Underwater Locator Beacon (Ulb)

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 TEST THE UNDERWATER LOCATOR BEACON (ULB) All installation and testing tasks concerning the ULB are covered in detail in the 90−Day Underwater Locator Beacon Installation & Operation Manual, L3AP P/N: 165E5542−10 and the 90−Day Underwater Locator Beacon CMM, L3AP P/N: 165E5542 −00.

  • Page 128: Aircraft Interface

    Signal Type Signal Function Failure Mode Local Effect End Effect Power O/P 115_VAC_Out_Hot The signal path Loss of 115 VAC (No Loss of FA5000 function- (Not Used) (AC_ Re- is open Power) ality turn_In_757A) Power O/P 115_VAC_Out_Hot The signal path...
  • Page 129 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 103 Aircraft Interface Troubleshooting Chart (Continued) Signal Type Signal Function Failure Mode Local Effect End Effect Ground Internal Pre Amp At- The signal path The Internal Pre Amp Degraded functionality tenuator (Common)
  • Page 130 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 103 Aircraft Interface Troubleshooting Chart (Continued) Signal Type Signal Function Failure Mode Local Effect End Effect RS422 Dif- FDR Data Output (A) The signal path Disrupted FDR data Disrupted FDR data ferential...
  • Page 131 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 103 Aircraft Interface Troubleshooting Chart (Continued) Signal Type Signal Function Failure Mode Local Effect End Effect Shunt Dis- FDR Fault The signal path The FDR Fault Out- Pilot(s) mistakenly be- crete is shorted...
  • Page 132 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 103 Aircraft Interface Troubleshooting Chart (Continued) Signal Type Signal Function Failure Mode Local Effect End Effect Shunt Dis- Data Link Fault The signal path Incorrect Fault Status The Data Link Fault sig-...
  • Page 133 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 103 Aircraft Interface Troubleshooting Chart (Continued) Signal Type Signal Function Failure Mode Local Effect End Effect Differential Channel 2 Audio Input The signal path Degraded Audio Fails to record − no audio...
  • Page 134 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 103 Aircraft Interface Troubleshooting Chart (Continued) Signal Type Signal Function Failure Mode Local Effect End Effect Discrete CVR Replay Inhibit The signal path FDR/CVR − Stops FDR/CVR − Stops the FDR Inhibit...
  • Page 135 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 103 Aircraft Interface Troubleshooting Chart (Continued) Signal Type Signal Function Failure Mode Local Effect End Effect Data Link B Data Link V1 OMS 429 The signal path Loss of ability to re- Unable to record ARINC (−)
  • Page 136 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 103 Aircraft Interface Troubleshooting Chart (Continued) Signal Type Signal Function Failure Mode Local Effect End Effect Differential Voice Erase C Supply The signal path Loss of ability to The recorder does not...

  • Page 137: Main Processor

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 MAIN PROCESSOR Table 103. Main Processor Troubleshooting Chart Item Function Type Failure Local Effect Next Effect End Effect Mode A001 − Watch Dog Timer; Over/Under The DSP fails: The MP PWA The CVDR fails to operate ARINC 429 RX/TX;...
  • Page 138 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 104 Main Processor Troubleshooting Chart (Continued) Item Function Type Failure Local Effect Next Effect End Effect Mode Watch Dog Timer; Single Event The FPGA ini- The MP PWA The CVDR initially does not oper- ARINC 429 RX/TX;...
  • Page 139 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 104 Main Processor Troubleshooting Chart (Continued) Item Function Type Failure Local Effect Next Effect End Effect Mode Non−Volatile Memory: Electrical In- Software glitch The MP PWA The CVDR does not operate Configuration and Error...
  • Page 140 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 104 Main Processor Troubleshooting Chart (Continued) Item Function Type Failure Local Effect Next Effect End Effect Mode A007 − BITE Task Loss of The SEEP- Status of the Status of the CVDR is not cur-...
  • Page 141 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 104 Main Processor Troubleshooting Chart (Continued) Item Function Type Failure Local Effect Next Effect End Effect Mode B011 − Audio I/P Audio I/P Ch No Audio to Ch Ch 3 is unable...
  • Page 142 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 104 Main Processor Troubleshooting Chart (Continued) Item Function Type Failure Local Effect Next Effect End Effect Mode B013 − Audio I/P Audio I/P Audio CODEC No audio tone No Effect Analog Tone Test 3...
  • Page 143 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 104 Main Processor Troubleshooting Chart (Continued) Item Function Type Failure Local Effect Next Effect End Effect Mode B019 − Audio I/P LO Analog Area Inputs Channel The system is Loss of Channel 4 Audio Mi-...
  • Page 144 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 104 Main Processor Troubleshooting Chart (Continued) Item Function Type Failure Local Effect Next Effect End Effect Mode F022 − Audio O/P LO The Analog The high out- The Analog Au- Loss of the Analog Audio Mon-...
  • Page 145 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 104 Main Processor Troubleshooting Chart (Continued) Item Function Type Failure Local Effect Next Effect End Effect Mode UART0 TxD The UART0 There is no The MP PWA Communication is disrupted TxD RIPS is...
  • Page 146 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 104 Main Processor Troubleshooting Chart (Continued) Item Function Type Failure Local Effect Next Effect End Effect Mode K030 − Differential ARINC757 Data I/P LO Loss of ability Unable to re- Unable to record good ARINC (−)

  • Page 147: Crash-Survivable Memory Unit (Csmu)

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 CRASH-SURVIVABLE MEMORY UNIT (CSMU) Table 104. CSMU Troubleshooting Chart Item ID Function Type Failure Mode Local Effect Next Effect End Effect 0001A − Watch Dog Timer; Over/Under The FPGA does not The CVDR does...
  • Page 148 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 105. CSMU Troubleshooting Chart Item ID Function Type Failure Mode Local Effect Next Effect End Effect Non−Volatile Over/Under The Flash Memory The CSMU fails The CVDR does not operate Memory Voltage fails: unable to store...

  • Page 149: Disassembly

    1. GENERAL This section contains the information required to disassemble the Model FA5000 Record- ers. Access to the major assemblies within the Model FA5000 is described such that there is minimal disturbance to other assemblies. Extreme care should be exercised when removing these assemblies.

  • Page 150: Condition Rips Module After Expired Shelf Life (One Year In Storage)

    RIPS Connector Cover (Installed) Torque 4.5 − 5.2 in−lbs. Figure 301. RIPS Module and FA5000 Connector Covers NOTE: The RIPS unit should provide sufficient hold up time after the first application of power for at least 15 minutes. Once charged,...

  • Page 151: Storage Instructions

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 If the RIPS will not fully charge, the unit must be replaced. If the RIPS charges completely, proceed to step 4. Remove the power from the recorder. Remove the RIPS from the recorder.

  • Page 152: Model Fa5000 Disassembly Instructions

    All attaching parts such as cable assemblies, stand−offs, screws, washers, etc. that are not damaged, should be retained with the chassis for reinstallation with the repaired LRUs. The FA5000 re- placeable PWAs or modules consist of the Acoustic Beacon, Aircraft Interface PWA, Main Processor PWA, and the Crash Survivable Memory Unit (CSMU).
  • Page 153 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Memory Interface Cable assembly attached to the J−3 connector Main Processor PWA. The CSMU is a sealed unit and must be returned to the factory for repair. If replacement of the CSMU is required, proceed with the following procedure: CSMU REMOVAL PROCEDURE Remove the two screws (1−115) used to secure the CSMU cable cover plate...

  • Page 154: (See Figure 304 Or Ipl Figure 1, Item 10)

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 1/4” Pan−Head Sealing Screws (1−125) (Qty. 4) (1−95) (REF.) (1−45) CSMU Memory Assembly (1-120) (1−95) (1−130) (Qty. 2) NOTE: Memory Interface Some parts are removed Cable Assembly for clarity purposes (1−110) (1−115) (Qty. 2) Figure 302.

  • Page 155: (See Figure 304 Or Ipl Figure 1, Item 25)

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 (1−5) (REF,) (1−10) (1−15) (Qty. 6) Connector (1−45) (1−25) NOTE: Some parts are removed for clarity purposes Figure 303. Rear Cover Removal Diagram Aircraft Interface (AI) PWA Removal (See Figure 304 or IPL Figure 1, Item 25) AIRCRAFT INTERFACE PWA REMOVAL PROCEDURE Remove the rear cover as described in Paragraph C, Rear Cover Removal.

  • Page 156: Figure 304. Aircraft Interface (Ai) Pwa Removal Diagram

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 (1−35) (Qty. 4) J−1 Rear Connector (1−25) NOTE: Some parts are removed for clarity purposes (1−30) (Qty. 6) Figure 304. Aircraft Interface (AI) PWA Removal Diagram 23–70–30 Disassembly Rev. 02 Page 308 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.

  • Page 157: Cleaning

    This section contains a list of all required cleaning materials, general cleaning proce- dures, applicable cautions and warnings related to the use of any cleaning material, and instructions for cleaning the Model FA5000 major assemblies. 2. MATERIALS REQUIRED Refer to Table Table 401 for a listing of required cleaning materials: Table 401.

  • Page 158: Printed Wiring Assembly Cleaning

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 CAUTION: DO NOT IMMERSE ANY PRINTED WIRING ASSEMBLY MOUNTED ELECTRONIC PARTS IN THE CLEANING SOLVENT; OTHERWISE, CIRCUIT BOARD AND/OR COMPONENT DAMAGE MAY RESULT. Printed Wiring Assembly Cleaning Remove dust, dirt, and foreign matter from all surfaces, using soft-bristle brush.

  • Page 159: Figure 401. Underwater Locator Beacon

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Crash Survivable Memory Unit (CSMU) (1-120) Underwater Acoustic Beacon Right Beacon (1-150) Mount Bracket (1-140) Left Beacon Mount Bracket (1-140) Cross-Pattern 1/4” Hex Screw Torquing Sequence (1−145) (75 in./lbs.) Figure 401. Underwater Locator Beacon 23−70–30...
  • Page 160 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23−70–30 Cleaning Rev. 02 Page 404 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document. July 21/17...

  • Page 161: General

    Model FA5000 CHECK 1. GENERAL This section contains the various checks that should be performed on the Model FA5000 during shop maintenance. Check procedures, when required, are written in step-by-step procedures wherever practicable, and include specific methods, techniques, and equip- ment required.

  • Page 162: Electrical Inspection

    Section 100 of this Component Maintenance Manual. Underwater Locator Beacon (ULB) The ULB beacon used in the Model FA5000 is equipped with a battery which sup- plies the power when activated. The beacon is recommended to be tested every 24 months per the 90−Day Underwater Locator Beacon Installation &...

  • Page 163: Repair

    As a result, the Model FA5000’s maintenance philosophy is replacement of failed assem- blies. In the case of the Model FA5000 at this time, the replaceable assemblies are the Aircraft Interface PWA, and the Crash Survivable Memory Unit (CSMU). If the Main Pro- cessor PWA fails, return the FA5000 Recorder to the factory for repair.
  • Page 164 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–30 Repair Rev. 02 Page 602 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.

  • Page 165: Assembly

    Special equipment required for testing and assembly of the recorder can be found in Table 901 of the Special Tools, Fixtures, and Equipment Section 900 of this CMM. Table 701 provides a list of the common assembly materials used with the FA5000. Table 701. Required Assembly Materials...

  • Page 166: General Assembly Techniques

    Conse- quently, in accordance with the accepted Level-2 repair philosophy for the FA5000 CVR, a known defective circuit board assembly shall be returned to the factory for repair or replacement.

  • Page 167: (See 703 Or Ipl Figure 1, Item 10)

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 (1−35) (Qty. 4) Torque (5−6 in/lbs) J−1 Rear Connector (1−25) NOTE: Some parts are removed for clarity purposes Torque (9−10 in/lbs) (1−30) (Qty. 6) Figure 701. Aircraft Interface PWA Installation Diagram Rear Cover Installation...

  • Page 168: (See Figure 703 Or Ipl Figure 1, Item 185)

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 rear cover (1−10) to the rear part of the Shielded Housing (1−5). Tighten screws to a torque value of 9−10 in./lbs. (1−5) (REF,) (1−10) (1−15) (Qty. 6) Torque Connector (9−10in/lbs) Guide Pin Receptacle (1−45)

  • Page 169: Figure 703. Crash Survivable Memory Unit (Csmu) Assembly

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Install CSMU (1−120) cable connector to the MP PWA (1−45) and secure with installing two screws (1−130). Tighten screws to a torque value of 5−10 in./lbs Install CSMU cable cover plate (1-110) and secure with installing two screws (1−115).

  • Page 170: (See Ipl Figure 1, Item 150)

    Section E. Condition RIPS Module After Expired Shelf Life (One Year in Storage) RIPS Module Connector Cover The FA5000 Connector Cover is to be installed on the Connector when the RIPS Module is not installed. After RIPS Module is removed, the FA5000CVDR Connector Cover must be in- stalled.

  • Page 171: Install Rips Module

    RIPS Connector Cap (Installed) Torque 4.5 − 5.2 in−lbs. Figure 704. FA5000 Connector Cover and RIPS Connector Cap Install RIPS Module Recorders are delivered without the RIPS Module installed. To install the RIPS Mod- ule, take the following steps, as described in “Figure 705 Install RIPS Module“.
  • Page 172 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Torque the RIPS Module retaining screw from 22 to 30 in-lbs. Perform a Return to Service Test on the recorder in accordance with Section 100 of this CMM. NOTE: The RIPS Module should provide sufficient holdup time after the first application of power for at least 15 minutes.

  • Page 173: Condition Rips Module After Expired Shelf Life (One Year In Storage)

    Install the RIPS Battery Pack in a known good recorder. Apply power the recorder and monitor the Status Web Page for amount of RIPS charge. Refer to Section 5.2 FA5000 MADRAS Status Page. The RIPS Battery will fully charge within approximately 15 minutes.

  • Page 174: Storage Instructions

    Model FA5000 Leave the RIPS charging on the recorder until the “Int RIPS Battery Charge” displays on the FA5000 CVR Status Web Page reads 100%. If the RIPS will not fully charge, the unit must be replaced. If the RIPS charges completely, proceed to step 4.

  • Page 175: Product Support

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 6. Product Support Product Support Engineers are available to answer questions about L3 Aviation Products’ equipment. Telephone: (941) 371-0811 FAX: (941) 377-5591 SITA: SRQLFCR Web Site: www.L-3AR.com E-mail: DLAR− aviationproducts@L3T.com Technical Publications Web Site: www.L−3AR.net...

  • Page 176: Return Equipment To Authorized Repair Facility

    End User / User Certification Tail Number (if applicable) 8. Return Equipment to Authorized Repair Facility Items in need of repair overhaul are processed at L3 Aviation Products, in Sarasota, Florida. For questions about returning items for repair or overhaul: Call: (941) 377−5517, or (941) 377-5554...

  • Page 177: Shipping Considerations

    No special shipping precautions are neces- sary. A shipment package kit, P/N: 147E5161-01, may be ordered from L3 Aviation Products if the original container is not available. Return Equipment from Outside the United States − Import Compliance All International shipments must be routed through L3 Aviation Products’...

  • Page 178: Payment Information

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 9. Payment Information For questions contact Lawanna Hall: Call: (941) 371−0811 Ext. 5142 E−mail: Lawanna.Hall@L3T.com Mailing Address: P.O. Box 3041 Sarasota, FL 34230 USA NOTE: Credit cards are accepted. Purchases over $1,000 will incur a 2% fee.

  • Page 179: Fits And Clearances

    The Model FA5000 meets the performance requirements of ED−112, chapter 2, and Part I, while conforming to the input interface required in ARINC 757/757A. 3. Physical Characteristics The Model FA5000 fits within the envelope of an ARINC 404A 1/2-ATR short case. (Re- fer to Figure 801) for outline and dimension illustration. Characteristic...

  • Page 180: Electrical Characteristics

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Electrical Characteristics Table 1. Electrical Specifications Characteristic Description Input Power Requirements 28 VDC 6 watts typical @ 28 VDC for CVR only Power Consumption 12 watts typical @ 28 Volts DC with RIPS charging 0.65...

  • Page 181: Crash- And Fire-Survival Characteristics

    ED–112 3400 g’s, 6.5 ms, half-sine shock wave Penetration ED–112 500 lbs./10 feet/1/4” probe Environmental Characteristics Refer to Table 801 for the Model FA5000 environmental characteristics. Torque Requirements Assembly Item Torque Requirement CSMU & Beacon Bracket Mounting Screws 75 in./lbs.

  • Page 182: Table 801. Model Fa5000 Environmental Characteristics

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Table 801. Model FA5000 Environmental Characteristics The Model FA5000 recorders will be tested to DO−160F categories listed below. DO-160F Section DO-160F Section DO-160F Category Compliance (Not Number including RIPS battery) Temperature and Altitude...
  • Page 183 2.5 CG 4.2 CG 12.6 Figure 801. Sheet 1 of 2 Outline & Dimension Drawing Model FA5000 Cockpit Voice Recorder 23–70–30 Fits and Clearances Rev. 02 Page 805 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.
  • Page 184 Forward View DETAIL ”A” Rear View Figure 801. Sheet 2 of 2 Outline & Dimension Drawing Model FA5000 Cockpit Voice Recorder 23–70–30 Fits and Clearances Rev. 02 Page 806 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.

  • Page 185: Special Tools, Fixtures And Equipment

    Cable Assembly, 17TES0426 Speakers - 2 (OPTIONAL) * Items are included in ROC/7 Kit but not used with Model FA5000 testing. Note: The FA5000 Software Library Program, listed below for the specific recorder, is needed to perform the upload function.
  • Page 186 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 FA5000 CVR Software Library Disk Recorder Software Checksum Part Number Part Number 5003−5000−00 840E5446−03 5132 5003−5000−00 840E5446−04 9C84 5003−5000−00 840E5446−06 0C9D 5003−5000−01 840E5440−03 294C 5003−5000−01 840E5440−05 6C92 5003−5000−01 840E5440−06 AB8B 5003−5000−01 840E5440−07 02DF 5003−5001−50...

  • Page 187: Ground Support Equipment (Gse) Descriptions

    P/N:0249800386 POWER RIU AUDIO OUTPUT (SPKRS) RECORDER INTERFACE CABLE ASSY. 17TES0418 FA5000 CVR RECORDER * OPTIONAL Figure 901. ROC/7 w/CVR Automated Test Station Software (CATS) FA5000CVR TEST SETUP 23–70−30 Special Tools and Test Equipment Rev. 02 Page 903 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.

  • Page 188: Audio Data Link Player Software

    AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Audio Data Link Player Software The FA5000CVR 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 FA5000CVR. It also provides the capability to decompress the data into standard waveform audio files (.wav) for playback using conventional audio me-...
  • Page 189 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 There are two methods to download audio and data link information from the Model FA5000CVR memory: Directly download into a ROC/7 using the Ethernet Cable. Use the Portable Interface/2 (PI/2) Unit, P/N: 17TES0062 with Mod−Dot #1.
  • Page 190 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70−30 Special Tools and Test Equipment Rev. 02 Page 906 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.
  • Page 191 The purpose of this Illustrated Parts List is to assist maintenance and supply personnel in requisitioning, storing, issuing and identifying parts to maintain the FA5000 Cockpit Voice Recorder. This Illustrated Parts List is not to be taken as the authority for the procedure of assembly or disassembly.
  • Page 192 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Part numbers are arranged in a alphanumerical sequence beginning at the extreme left– hand position and continue from left to right, one position at a time. The order to prece- dence in beginning the part number arrangement is as follows: A.
  • Page 193 “(SEE FIG. – FOR DETAIL BREAKDOWN).” The listing of the assembly in the breakdown figure will carry the reference “(SEE FIG. – FOR NHA)”. If the vendor is not L3 Aviation Products, the manufacturer’s vendor code may be in- cluded in parentheses in this column.
  • Page 194 Model FA5000 8. MANUFACTURER’S CODE Due to the Level−2 maintenance philosophy used with the FA5000, all spare parts will be ordered through L3 Technologies. L3AP Vendor Code, manufacturer name and address, as listed in the “Federal Supply Codes for Manufacturers” Cataloging Handbook H4/H8, Commercial and Government Entity (CAGE) codes, (formerly FSCM), and/or the NATO Code as applicable (Ref.
  • Page 195 COMPONENT MAINTENANCE MANUAL Model FA5000 10. CONFIGURATION MATRIX Listed below are the current configurations for the FA5000 Cockpit Voice Recorder (CVR). Part Number 5000-500X−XX is capable of storing 2 hours of voice data and has Internal RIPS, OMS and datalink capabilities.
  • Page 196 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 NUMERICAL INDEX ITEM PART NUMBER AIRLINE FIG. PART NO. BB1P041H05 MS16995−54 MS24693−C28 MS24693−C3 MS24693−C4 MS51957−26 MW0242−006−S NAS622C−E2 010E5161−00 016E1589−00 016E5852−00 024E5161−00 042E5161−02 075E5161−02 075E5352−00 1110−4−AL−9 136E5161−02 189E5161−00 205E5044−02 DELETED 205E5044−07 205E5044−30 205E5170−03 DELETED 205E5170−04...
  • Page 197 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 ITEM PART NUMBER AIRLINE FIG. PART NO. 230E5490−00 230E5490−01 253E5162−01 DELETED 253E5851−00 120B 253E5851−01 120C 253E5851−02 120D 253E5851−03 120E 266E0305−00 150A 266E0305−01 150B 266E0305−02 150C 266E5422−00 150D 500−4030−000 5000−5000−00 DELETED 5000−5001−50 DELETED 5003−5000−00 5003−5000−01...
  • Page 198 QTY 2 QTY 2 QTY 4 QTY 2 QTY 2 Figure 1000. (Sheet 1 of 2) Model FA5000/5003 CVR Recorders 23–70–30 Illustrated Parts List Rev. 02 Page 1008 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.
  • Page 199 (REF) QTY 6 QTY 6 QTY 4 View B Figure 1000. (Sheet 2 of 2) Model FA5000/5003 CVR Recorders 23–70–30 Illustrated Parts List Rev. 02 Page 1009 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.
  • Page 200 5000−5000−00 Deleted 5000−5001−50 Deleted 5003−5000−00 COCKPIT VOICE RECORDER, NAND FA5000 CVR, ARINC 757, 2 HR. CVR, 1/2 ATR SHORT, 28 VDC ONLY 5003−5001−50 COCKPIT VOICE RECORDER FA5000 CVR, ARINC 757A, 2 HR. GA CVR, 1/2 ATR SHORT, 28 VDC ONLY 5003−5000−01...
  • Page 201 .Deleted 205E5170-04 .PWA,AI,757A/757-5,FA5000 C,D,E, (SUPSD BY 25C (EFF E) PER ECN 016337) 205E5170-10 .PWA,AI,FA5000 (SUPSDS 25B (EFF E) PER ECN 016337) 205E5170-08 .PWA,AI,FA5000, ROHS ARINC ATTACHING PARTS MS51957-26 .SCR,PNH ,6-32 X1/4 (V06141) (2290200083) MS24693-C4 .SCR,FLH ,4-40 X3/8 (V06141) (2290200356) 230E5488-00 .SEAL, ARINC 404 CONNECTOR...
  • Page 202 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 UNITS FIG. PART AIRLINE NOMENCLATURE ASSY ITEM NUMBER PART NO. CODE 1234567 1000 075E5352-00 .COVER,RJ45 ,EMI 2299800577 .SCREW,#4-40X5/8 TRUSS HD 1110-4-AL-9 .SPACER,3/16OD,.115ID,5/16 (V55582) (2399800255) MW0242-006-S .SPRING,WAVE,S.S. (V06141) (2429800057) 0639805057 .CONN SEAL,RJ45 COND (VQ3554) (0639805057) 024E5162-00 .CABLE ASSEMBLY,RIPS POWER...
  • Page 203 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 UNITS FIG. PART AIRLINE NOMENCLATURE ASSY ITEM NUMBER PART NO. CODE 1234567 1000 ATTACHING PARTS NAS622C-E2 FASTENER,HOOK,NAS622TYPEE . (V94867) (1119800102) MS24693-C28 .SCR,FLH ,6-32 X1/2 (V06141) (2290200362) 22902002‐29 SCR, FLH, 10‐32X1/2 010E516100 .PLATE,COVER ATTACHING PARTS MS24693-C3 .SCR,FLH ,4-40 X5/16...
  • Page 204 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 UNITS FIG. PART AIRLINE NOMENCLATURE ASSY ITEM NUMBER PART NO. CODE 1234567 1000 ATTACHING PARTS BB1P14H12 .SCR,PNH,1/4-20X3/4,SEALING (V06141) (2299800558) MS51957-12 .SCR,PNH ,4-40 X3/16 (V06141) (2290200072) 189E5161-00 .PAD,CSMU CONNECTOR SEAL 016E1589-00 .BRACKET, BEACON, MOUNT ATTACHING PARTS MS16995−54...
  • Page 205 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 UNITS FIG. PART AIRLINE NOMENCLATURE ASSY ITEM NUMBER PART NO. CODE 1234567 1000 150A 266E0305-00 BEACON, ACOUSTIC, UNDERWATER C, D, E (SUPSD BY 150D PER SB004) DUKANE (V94970) (DK-120) FOR BATTERY REPLACEMENT ORDER 30−DAY BATTERY KIT (147E0305−00)
  • Page 206 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 Figure 1001. Model 500 Recorder Independent Power Supply (RIPS) 23–70–30 Illustrated Parts List Rev. 02 Page 1016 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.
  • Page 207 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–30 Illustrated Parts List Rev. 02 Page 1017 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.
  • Page 208 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 UNITS FIG. PART AIRLINE NOMENCLATURE ASSY ITEM NUMBER PART NO. CODE 1234567 1001 500−4030−000 RECORDER INDEPENDENT POWER SUPPLY (RIPS) 23–70–30 Illustrated Parts List Rev. 02 Page 1018 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.
  • Page 209 AVIATION PRODUCTS COMPONENT MAINTENANCE MANUAL Model FA5000 THIS PAGE IS INTENTIONALLY LEFT BLANK 23–70–30 Illustrated Parts List Rev. 02 Page 1019 Use or disclosure of information on this sheet is subject to July 21/17 the restrictions on the cover page of this document.

This manual is also suitable for:

5003-5000-005003-5000-015003-5001-505013-5000-305013-5001-50500-4030-000 rips

Table of Contents