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COMPONENT MAINTENANCE MANUAL

AVIATION PRODUCTS

Model FA5000

Rev. 02 Page 35

July 21/17

Description and Operation

23–70

−

Use or disclosure of information on this sheet is subject to

the restrictions on the cover page of this document.

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)

Wire

resistance should not exceed 1 ohm for power leads and should not exceed 5 ohms for sig-

nal leads. All wiring should be MIL–W–22759 or MIL–C–27500.

Only one power source is to be wired per aircraft. If 115 Vac, 400 Hz is supplied, connection

is to be made to pin 2 & 3. If 28 Vdc is supplied, connection is to be made to pins 9. Short-

ing pins 1 & 2 is optional.

Recorder ground connection to be within 1 foot of pin 17, heavy gauge wire. Shields to be

grounded at the recorder using short connections. Pin 17 is used as +28 VDC return. Control

unit may be grounded in the cockpit to a chassis ground.

Jumper in aircraft connector. Without this jumper, the unit will not record or erase previously

recorded information, bulk erase will not activate, and test will indicate NO-GO.

Pin 3 is not a DC return and is not grounded in the recorder. (see Note 3)

Twisted shielded cable. Shields to be grounded at the airframe using short connections. Tie

shields to existing single point GND use for Pin 17. (see Note 3)

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.

BITE status output: Ground = no fault, Open = fault or CVR not installed.

Audio input .05 Vrms

−

3 Vrms maximum. (1Vrms nominal).

10.

Per FAA Action Notice A8300.56 dated Jan. 24, 1990, the wiring to Channels 1 and 3 may be

transposed; that is, Channel 1 will be Pilot and Channel 3 will be Third Crew Member or PA

System.

11.

Test Ind/

−

lines (pins 15 & 16) only p12 Vdc, 1ma output to illuminate the

Control Unit Test Lamp. (This is not sufficient to light an external Annunciator lamp.)

12.

In all CVR configurations provides both 150 (1 sec resolution) and 125 (0.1 min. resolution)

for 429 GMT inputs.

13.

S055 microphone installations required double shielding. For S056 installations, double

shielding is not required for new installations, however, it may be left in place for retrofit in-

stallations.

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

Содержание FA5000

Страница 1: ...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 perso...

Страница 2: ...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 No d...

Страница 3: ...of persons 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 Onl...

Страница 4: ...0 30 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 chec...

Страница 5: ...on Operation Testing Fault Isolation Replaced ULB testing procedure with references to the ULB CMM and I O manuals Automatic Testing Disassembly Added RIPS and equipment storage details Removed the UL...

Страница 6: ...ront Matter Introduction Added updated 90 day ULB details Added new part numbers 5013 5000 30 5013 5001 50 Description Operation Testing Fault Isolation Added updated 90 day ULB details Automatic Test...

Страница 7: ...Comments Initial Release Feb 20 14 Initial Release of CMM Includes all sections in ATA100 format Rev 01 October 6 16 Added updated 90 day ULB details RIPS condi tioning new part numbers added 5013 50...

Страница 8: ...e viii July 21 17 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 onlin...

Страница 9: ...mation on this sheet is subject to the restrictions on the cover page of this document RECORD OF REVISIONS REV NO INSERTION DATE BY REV NO INSERTION DATE BY REV NO INSERTION DATE BY 01 October 6 16 C...

Страница 10: ...70 30 Rev 02 Page x 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 on...

Страница 11: ...r page of this document July 21 17 SERVICE BULLETIN LIST SERVICE BULLETIN DATE EFFECTIVITY DESCRIPTION FA5000 SB004 23 70 40 04 June 16 15 FA5000 Family Cut in of 90 day ULB to newly manufac tured rec...

Страница 12: ...23 70 30 Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document July 21 17 THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is onl...

Страница 13: ...ul 21 17 xx Jul 21 17 xxi Jul 21 17 xxii Jul 21 17 xxiii Jul 21 17 xxiv Jul 21 17 xxv Jul 21 17 xxvi Jul 21 17 xxvii Jul 21 17 xxviii Jul 21 17 xxviii Jul 21 17 xxix Jul 21 17 xxx Jul 21 17 xxxi Jul 2...

Страница 14: ...1 17 54 Jul 21 17 55 Jul 21 17 56 Jul 21 17 57 Jul 21 17 58 Jul 21 17 Testing and Troubleshooting 101 Jul 21 17 102 Jul 21 17 103 Jul 21 17 104 Jul 21 17 105 Jul 21 17 106 Jul 21 17 107 Jul 21 17 108...

Страница 15: ...l 21 17 402 Jul 21 17 403 Jul 21 17 404 Jul 21 17 Check 501 Jul 21 17 502 Jul 21 17 Repair 601 Jul 21 17 602 Jul 21 17 Assembly 701 Jul 21 17 702 Jul 21 17 703 Jul 21 17 704 Jul 21 17 705 Jul 21 17 70...

Страница 16: ...T OF EFFECTIVE PAGES Section Page Date Section Page Date Illustrated Parts List Continued 1005 Jul 21 17 1006 Jul 21 17 1007 Jul 21 17 1008 Jul 21 17 1009 Jul 21 17 1010 Jul 21 17 1011 Jul 21 17 1012...

Страница 17: ...DOCUMENT REQUIREMENTS 3 4 MAINTENANCE PHILOSOPHY 4 5 COMPONENT MAINTENANCE MANUAL CMM DESCRIPTION 4 A FRONT MATTER 4 B DESCRIPTION AND OPERATION 4 C TESTING AND TROUBLESHOOTING 4 D DISASSEMBLY 5 E CLE...

Страница 18: ...e Task 14 E BITE Task 17 F GSE Task 20 G Underwater Locator Beacon ULB 24 H Circuit Boards 25 I Power Control and Monitor Signal Interface Characteristics 25 1 Stop Recording Command 28 2 Control Unit...

Страница 19: ...ent 40 B Software Partitioning 40 C Memory Requirements 40 1 On Board Maintenance System OMS Interface 41 2 Fault Warning System FWS Interface 41 3 Data Link ATC Interface 42 D Push to Test PTT Functi...

Страница 20: ...G SUBJECT DESCRIPTION PAGE 1 GENERAL 101 2 MAINTENANCE PHILOSOPHY 101 A Model FA5000 CVR 101 3 MODEL FA5000 CVR RECORDER IN SERVICE CHECKOUT 102 4 RECORDER INTERFACE UNIT RIU 102 A READ OUT CENTER 7 R...

Страница 21: ...PAGE 11 Crosstalk Data 124 12 FSK Time 125 13 Audio Out Monitor 125 14 Signal To No Signal 125 15 Shutdown 126 16 Capacitor 126 17 Data Link 126 18 OMS 127 19 RIPS 127 20 FRED 127 21 FDR 127 5 READ OU...

Страница 22: ...inal Container 303 B Storage of RIPS Without Original Container 303 4 MODEL FA5000 DISASSEMBLY INSTRUCTIONS 304 A Underwater Locator Beacon Removal See IPL Figure 1 Item 150 304 B Crash Survivable Mem...

Страница 23: ...CTIONS 701 A General Assembly Techniques 702 B Aircraft Interface PWA AI Installation See Figure 701 or IPL Figure 1 Item 105 702 C Rear Cover Installation See 703 or IPL Figure 1 Item 10 703 D Crash...

Страница 24: ...Equipment from Outside the United States Import Compliance 713 9 Payment Information 714 FITS AND CLEARANCES 1 GENERAL 801 2 SYSTEM SPECIFICATIONS 801 3 Physical Characteristics 801 A Electrical Char...

Страница 25: ...NTENTS ILLUSTRATED PARTS LIST SUBJECT DESCRIPTION PAGE 1 GENERAL 1001 2 PURPOSE 1001 3 ABBREVIATIONS 1001 4 EQUIPMENT DESIGNATOR INDEX 1001 5 NUMERICAL INDEX 1001 6 DETAIL PARTS LIST 1002 7 PART NUMBE...

Страница 26: ...Page xxvi Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document July 21 17 THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is on...

Страница 27: ...Figure 12 GSE Task Data Flow Diagram 21 Figure 13 GSE Task Flowchart 22 Figure 14 Model FA5000 CVR P N 500X 500X Functional System Block Diagram 26 Figure 15 Model FA5000 GACVR P N 500X 500X 50 Functi...

Страница 28: ...og Confirmation 117 Figure 119 CATS CVDR Fault History Log 118 Figure 120 CATS Continue Test Confirmation 118 Figure 121 CATS Test Results Screen 119 Figure 301 RIPS Module and FA5000 Connector Covers...

Страница 29: ...er page of this document July 21 17 LIST OF FIGURES Continued 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 1...

Страница 30: ...Page xxx Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document July 21 17 THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is on...

Страница 31: ...46 Table 5 CVR Pins Assigned to RIPS Status Monitoring 47 Table 6 CVR Label 350 Output format 47 Table 7 CVR Fault Reporting Interactions 48 Table 8 CVR Status Word Fault Reporting Criteria 49 Table 1...

Страница 32: ...2 Page xxxii Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document July 21 17 THIS IS INTENTIONALLY LEFT BLANK The document reference is onli...

Страница 33: ...s calibration required F 90 Day Underwater Locator Beacon ULB All installation and testing tasks concerning the ULB are covered in detail in the Underwater Locator Beacon Installation Operation Manual...

Страница 34: ...ilures NVRAM Non Volatile Random Access Memory OMS Onboard Maintenance System PC Personal Computer PI 2 Portable Interface 2 PPI Parallel Peripheral Interface PWA printed wiring assembly PWR power REC...

Страница 35: ...tallation and Operation Manual Cockpit Voice Recorder Model FA5000CVR P N 165E5327 00 F Component Maintenance Manual ED 56A Control Units Preamplifier Micro phone Modules ATA 23 70 05 P N 165E1747 00...

Страница 36: ...T 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 ATA Specification 100 The manual is written...

Страница 37: ...isassembly 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 E CLE...

Страница 38: ...he unit under test conditions as indicated in Table 1 below Table 1 identifies the sections of the CMM that underwent a Shop Verification process and the date of the verification In addition a Compone...

Страница 39: ...by special characters such as the dash character L3AP 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...

Страница 40: ...duction 23 70 30 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...

Страница 41: ...der CVR FA5000CVR P N 5003 5000 00 5003 5000 01 5003 5001 50 5013 5000 30 and 5013 5001 50 Features include F ED 112 compliant F ARINC 757 A characteristics including Greenwich Mean Time GMT interface...

Страница 42: ...of this document 2 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 i...

Страница 43: ...pable of withstanding environmental requirements set forth in ED 112 The unit interfaces to Ground Support Equipment GSE via industry standard network protocols Ethernet Wireless with the GSE operator...

Страница 44: ...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...

Страница 45: ...s used to store fault log information as well as other system related infor mation All tasks will be able to communicate with the BITE task for the purpose of send ing fault information and or system...

Страница 46: ...hannel Audio From CVR and DataLink Task DataLink Interrupt Service Routine Audio Monitor Outputs UTC Discretes DataLink Messages Discretes Datalink Packets Audio Audio Streaming Audio Packets TDM TDM...

Страница 47: ...s task will report a checksum of the loaded code to ensure the integrity of the newly loaded software There will be no user modifiable software and multiple version dissimilar software in the design o...

Страница 48: ...sulting compressed frame of audio data is sent to the proper partition on the CSMU via the Data Storage task Like the CAM data a packet header is sent to the 3 Channel partition for every half sec ond...

Страница 49: ...t to Three Channel Header No Are we in Record Mode Yes No Compress CAM Data and send it to the CAM Partition Get Power Up Count and add it to CAM and the Three Channel Headers Read CAM Data back from...

Страница 50: ...low indicating recorder 2 then the recorder will accept labels 156 227 270 and 276 If the Williamsburg Version 3 protocol is in effect then the CVR Ident signal is not used and all labels 156 157 227...

Страница 51: ...or matted and logged Likewise when an error condition no longer exists a message is sent to the BITE task indicating that a particular error is no longer valid A DataLink fault will be asserted via th...

Страница 52: ...containing 128 128 Kbyte erase blocks per chip 0 1 2 1023 1022 1021 128 Kbyte erase block containing 1024 128 byte pages Block Header Spare Page Header DataLink Messages Each page contains thirty 32...

Страница 53: ...eader Yes No No Yes No Record Mode Data in FIFO Send Data Read FIFO Beginning of Page Send Data Do DataLink Heartbeat Processing Figure 7 DataLink Task Flowchart C OMS Task The OMS task receives statu...

Страница 54: ...it CSMU This task receives audio data from the CVR task and ARINC 429 data from the DataLink task The Data Storage task manages where the data is stored in the CSMU Following the ED 112 specification...

Страница 55: ...h the data originated This is done to implement the read after write BITE functionality of the recorder Each packet of data for the audio and DataLink partitions will be written in one 128 Kbyte block...

Страница 56: ...Progress Yes Erase Request CVR Only Do Bulk Erase Any Writes In Progress Same Partition Read Data Yes Yes No No Yes Check for Erase Aheads In Progress that are done No Any Writes In Progress Done Do...

Страница 57: ...a standard way Each fault will contain a time tag of when the fault took place See Figure 10 BITE Task Data Flow Diagram Get Faults Task Faults Process Faults Fault Log in NVRAM Fault Discrete Output...

Страница 58: ...document 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 rea...

Страница 59: ...t Log Location Create Fault Log Message Queue Received any Faults on Queue Write Fault to Fault Log NVRAM Yes Read Status bits from FPGA No Any New Faults reported from FPGA Generate Fault Does Fault...

Страница 60: ...the CSMU Reading Writing Delet ing interface configuration run On Demand Diagnostics extract Fault logs and get gen eral status of the system See Figure 12 GSE Task Data Flow Diagram Once the task is...

Страница 61: ...n on this sheet is subject to the restrictions on the cover page of this document Command Table Message Queue GSE Task TCP IP Server Command MsgQueue Response MsgQueue Function to be Performed Figure...

Страница 62: ...this document Found Command On Table Wait for Command Message Queue Search for command code on table Command Table Response Message Queue Execute Command Yes Response to Command Create Command and Re...

Страница 63: ...7 pin DPXB style connector The Cockpit Voice Recorder CVR function simultaneously records four separate chan nels of cockpit audio converts the audio to a digital format and stores the data in a mem o...

Страница 64: ...ater 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...

Страница 65: ...to the appropriate status indicators is also integrated into the FA5000 electronics The removable circuit boards include the Aircraft Inter face PWA and Main Processor PWA I Power Control and Monitor...

Страница 66: ...2 2 2 2 2 MAIN PROCESSOR PWA CSMU Crash Survivable Memory Unit ASSEMBLY CRASH PROTECTED SOLID STATE MEMORY TO AIRCRAFT FAULT MONITORING SYSTEM GSE OUTPUT COCKPIT AREA MICROPHONE CAM STOP RECORDING MO...

Страница 67: ...PWA CSMU Crash Survivable Memory Unit ASSEMBLY CRASH PROTECTED SOLID STATE MEMORY TO AIRCRAFT FAULT MONITORING SYSTEM GSE OUTPUT COCKPIT AREA MICROPHONE CAM STOP RECORDING MODEL FA5000 GACVR GACVR FAU...

Страница 68: ...a headset jack for verifying system operation Refer to Component Maintenance Manual ED 56A Control Units Microphones ATA 23 70 05 Part Num ber 165E1747 00 The Model S151 S161 Model S152 S162 and the M...

Страница 69: ...TA 23 70 05 Part Number 165E1747 00 The 18 Vdc is a short circuit protected 30 mA line All control units provide the FA5000 CVR with three control signals Erase A Erase C and Push To Test The Erase A...

Страница 70: ...7 6000 Hz CH 1 HQV 150 3500 Hz CH 2 HQV 150 3500 Hz CH 3 HQV 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...

Страница 71: ...irements of technical standard order TSO C123b TSO 124b TSO 155a EUROCAE ED 56A and EUROCAE ED 112 A Applicable Documents The following documents form a part of or are referenced within this CMM 1 TSO...

Страница 72: ...l Characteristics For specific electrical characteristics refer to Section 800 Fits and Clearances D Environmental Characteristics For specific environmental characteristics refer to Section 800 Fits...

Страница 73: ...y 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...

Страница 74: ...8 9 10 9 9 10 AUDIO OUT LO AUDIO OUT HI RECORD ON B RECORD ON A 28 VDC POWER IN STOP RECORDING PUSH TO TEST TEST INDICATOR TEST INDICATOR CHASSIS GND CVR FAULT GMT IN B ARINC 429 LO GMT IN A ARINC 429...

Страница 75: ...te and test will indicate NO GO 5 Pin 3 is not a DC return and is not grounded in the recorder see Note 3 6 Twisted shielded cable Shields to be grounded at the airframe using short connections Tie sh...

Страница 76: ...B ARINC 429 LO GMT IN A ARINC 429 HI CHANNEL 1 LO CHANNEL 1 HI CHANNEL 2 LO CHANNEL 2 HI CHANNEL 3 LO CHANNEL 3 HI VOICE ERASE A VOICE ERASE C 115 VAC POWER IN HOT 115 VAC POWER IN COLD AUDIO JACK LO...

Страница 77: ...7 see Note 3 7 Using the the Stop Recording function the grounded pin 10 terminates recording within 10 minutes When using the RIPS Active function the CVR has a backup power source or RIPS available...

Страница 78: ...M THEORY OF OPERATION The ARINC 757 A Model FA5000 CVR consists of three subassemblies the Aircraft Interface Printed Wiring Assembly PWA the CPU Main Processor PWA and Crash Survivable Memory Unit CS...

Страница 79: ...d to meet the requirements of RTCA DO 160F Section 22 The ARINC 757 A Aircraft Interface provides input signal conditioning for Audio Channel Inputs Push To Test GMT Voice Erase Data Link Record OMS S...

Страница 80: ...sors DSPs an external program memory for each DSP that contains the executable program code one external NVRAM for non crash critical data storage and a flash memory array located in a Crash Survivabl...

Страница 81: ...NC 429 Low Speed LS input bus for test request by means of CVR input pins 39 40 OMS IN 2 Fault Warning System FWS Interface As per ARINC 757 A the CVR transmits its status at a 1 Hz rate The status is...

Страница 82: ...ush to Test functionality already implemented on existing aircraft and stan dardized in ARINC 757 A specification is used to provide the flight crew with the ability to quickly confirm good serviceabi...

Страница 83: ...by new infor mation F Recorder Synchronization The FA5000CVR equipment is designed to be able to record time code from an AR INC 429 in priority and later FSK source the frequencies used are 3607Hz 3...

Страница 84: ...nments to the rear connector Listed in Table 7 are the difference in the pin as signments of the CVR rear connector for both prior to RIPS and RIPS installation RIPS status will be received and transm...

Страница 85: ...status will be received and transmitted 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...

Страница 86: ...Bit 22 SSCVR Label 351 Bit 20 Not present Open 0 1 Present Ground 1 0 For more information on the RIPS see P N 165E4900 00 Installation and Op eration Instruction Manual for Recorder Independent Powe...

Страница 87: ...n 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 La...

Страница 88: ...T 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 RI...

Страница 89: ...vents 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 Hea...

Страница 90: ...el 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 defi...

Страница 91: ...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 charact...

Страница 92: ...er 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 0...

Страница 93: ...ARINC 429 ARINC 757 A ARINC 758 and ARINC 619 The interface is characterized by the following specifications F Single ARINC 429 High Speed physical layer input interface Pins 33 34 F Williamsburg Ver...

Страница 94: ...by any changes or additions to the ap proved DataLink message set Likewise the CVR DataLink recording function is not affected by the ARINC 619 General Format Identifier GFI coding or by the Extend e...

Страница 95: ...S C Length ASCII Message Area ARINC 623 ATIS Display Server Length 0 2 3 5 1 4 6 Figure 21 Generic DataLink Message Encapsulation Structure As indicated in Section 1 above the FA5000 DataLink CVR also...

Страница 96: ...urg 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 Williamsbur...

Страница 97: ...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 2 can be used...

Страница 98: ...and Operation 23 70 30 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...

Страница 99: ...LSO ENSURE THAT ALL CIRCUIT BOARDS ARE PLACED INTO STATIC SHIELD ING CONDUCTIVE BAGS WHEN HANDLING OR STORING 2 MAINTENANCE PHILOSOPHY A Model FA5000 CVR The EUROCAE ED 112 compliant Model FA5000 CVR...

Страница 100: ...t that is landing gear must be down and brakes locked to allow the CSMU solid state flash memory to be erased To erase the information stored in the flash memory press the ERASE pushbutton for more th...

Страница 101: ...erboard 5 Attach the RIU Sound Card In 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 Ou...

Страница 102: ...uipment Software ROSE 4 7 17TES0058 FA2100 Software Upload Cable Assembly 17TES0076 RUFS Recorder Interface USB Sold Separately 17TES0711 Cable FA5001 Adapter REQUIRED 0249800386 Cable Assembly Ethern...

Страница 103: ...11 AC J7 J6 RIU AUDIO OUTPUT SPKRS J9 RCDR AC PWR TEST DO NOT CONNECT RECORDER INTERFACE UNIT RIU 17TES0710 SND OUT GREEN 17TES0413 J4 J2 J1 L SPKR R SPKR YELLOW AC RED DC AC 1A DC 5A USB BLUE GREEN S...

Страница 104: ...ROC to start the software The applic ation will launch with the Channels control screen displayed as illustrated in Figure 102 Figure 102 CATS Channels Control Screen 2 In the Channels control screen...

Страница 105: ...to the restrictions on the cover page of this document Figure 103 Volume Control 4 Under Applications click Sound Systems then click the Recording tab This will display the Sound control window illus...

Страница 106: ...the cover page of this document 5 Highlight and select Line in 6 Click on Properties 7 Select the Levels tab Figure 105 Line In Properties Line In Level 8 Make sure that the Line In level is set at 10...

Страница 107: ...sclosure of information on this sheet is subject to the restrictions on the cover page of this document Figure 106 Sound Playback Devices 10 Highlight Speakers 11 Click on Properties 12 Select the Lev...

Страница 108: ...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...

Страница 109: ...nformation on this sheet is subject to the restrictions on the cover page of this document Figure 108 Volume Mixer Speaker Levels 17 In the Volume Mixer make sure both sliders are all the way up 18 Cl...

Страница 110: ...CATS Autotest using DC power only follow the procedures below a Ensure that the recorder has no power applied power is removed if not already done Connect a CVR to the RIU using the cable p n 17TES04...

Страница 111: ...necting to the recorder status window appears Observe Figure 109 CATS Connecting Pop Up g On the tool bar select Power ON Figure 110 CATS Power Toggle NOTE When DC power is applied verify the appropr...

Страница 112: ...Start Test Toggle k In the Test Mode and Options dialog box select either Return to Ser vice or Selectable Test Options then click on OK Figure 112 CATS Test Mode and Options Screen NOTE If a full ret...

Страница 113: ...from the CATS Test Mode and Options Screen Figure 113 CATS CVDR Test Confirmation NOTE Follow the instructions displayed in the confirmation window l Read and click on Yes Figure 114 CATS CVDR Warning...

Страница 114: ...Input n 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 116 CATS CVDR...

Страница 115: ...page of this document Figure 117 CATS CVDR Fault History Log p Click on Yes on the dialog box to clear the fault logs Figure 118 CATS CVDR Clear Fault Log Confirmation q Observe the Fault History Log...

Страница 116: ...Confirmation s 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 provide...

Страница 117: ...page of this document Figure 121 CATS Test Results Screen u If the autotest is successful power off the recorder from the CATS menu bar v Turn 28VDC power off and remove the crossover and RIU cables f...

Страница 118: ...enter the DC power consumption in amps or watts Please enter the DC power consumption in amps or watts Please connect the recorder front panel cable and press the OK button Example report message s 0...

Страница 119: ...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 P...

Страница 120: ...QV2 5 4 SQV3 5 4 SQC 56 6 dBV 08 05 40 PASSED Channel Bal 1000 Hz 0 1 ref All within 3 dB except HQC Results HQ1 8 3 HQ2 8 2 HQ3 8 4 HQC 9 4 SQV1 8 0 SQV2 8 1 SQV3 8 1 SQC 293 8 dBV 8 Frequency Respon...

Страница 121: ...1600 2000 2500 and 3500 Hz Frequencies for HQCAM and SQCAM only is 3150 Hz Frequencies for HQCAM only are 4148 and 6000 Hz Example Return to Service report message s 11 24 20 PASSED SN D 150 Hz 1 0 r...

Страница 122: ...2 127 4 HQ3 11 1 HQC 104 4 SQV 11 4 SQC 72 0 dBV 08 42 19 PASSED Crosstalk Audio 1000 Hz 1 0 ref Expected Driven Non Driven 40 dB Results HQ1 304 9 HQ2 304 9 HQ3 111 7 HQC 11 1 SQV 72 4 SQC 11 4 dBV 1...

Страница 123: ...HQ3 Playback Expected 9 patterns Results 9 good patterns 14 50 53 PASSED FSK Time HQ3 GMT Switch Expected 9 patterns Results 9 good patterns 13 Audio Out Monitor Record simulated 1000 Hz data for eac...

Страница 124: ...D Shutdown CVDR Fault Expected CVDR fault to occur Res ult CVDR Fault 08 56 27 PASSED Shutdown Push to Test Expected 1000 Hz frequency Results 999 9 Hz 16 Capacitor Power off recorder and verify recor...

Страница 125: ...ver 9 minutes after power is removed Example report message s 09 00 02 RIPS Initialization Power has been removed Please wait 9 minutes 09 09 15 PASSED RIPS Expected no CVR Fault for over 9 minutes Re...

Страница 126: ...ult 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 the Save button 3 Select either Full Audio Data Download...

Страница 127: ...e of this document 6 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 M...

Страница 128: ...CVDR 05 Audio O P Audio Monitor Output Low The signal path is open No audio voice is present Unable to monitor audio 05 Audio O P Audio Monitor Output Low The signal path is shorted No audio voice is...

Страница 129: ...gnal path is shorted No Effect No Effect 14 Power O P Preamp Power Output Hot The signal path is open The Preamp Power Output Hot Signal fails Unable to hear cockpit audio no audio is recor ded 14 Pow...

Страница 130: ...s 6 dB at tenuation Internal Pre Amp Attenu ator N6DB signal soft ware receives continuous 6 dB attenuation 21 Discrete I P Internal Pre Amp At tenuator N12DB The signal path is open No Effect No Effe...

Страница 131: ...RS422 Dif ferential FDR Data Input B The signal path is shorted Loss of ability to ac quire coherent FDR data Input B FDR records corrupt garbled RS422 data 28 RS422 Dif ferential FDR Data Input A The...

Страница 132: ...Link Input B Unable to store ARINC 429 B Data Link signal data into the CSMU 34 Differential ARINC429 A Data Link Input A The signal path is open Data disrupted cor rupted Loss of abil ity to acquire...

Страница 133: ...disrupted and not recorded No OMS 429 data provided recorded 40 Differential ARINC429 OMS In 429 A The signal path is shorted OMS Input A 429 sig nal data is disrupted and not recorded No OMS 429 dat...

Страница 134: ...he FDR Maintenance signal always indicates no maintenance 46 Discrete FDR Maintenance The signal path is shorted The FDR Mainten ance signal always indicates mainten ance NOTE Depends upon customer wi...

Страница 135: ...a Microphone Loss of audio from Area Microphone 53 Differential Audio Area Mic Input Low The signal path is open Audio from the Area Mic Input Low Signal is disrupted Fails to record no audio is recor...

Страница 136: ...is document Table 103 Aircraft Interface Troubleshooting Chart Continued Pin ID Signal Type Signal Function Failure Mode Local Effect End Effect 57 Differential Analog Voice Erase C Supply The signal...

Страница 137: ...aces fail The MP PWA fails to operate The CVDR fails to operate Watch Dog Timer ARINC 429 RX TX Did crete I Ps and O Ps FDR Data Frequency Counter CSMU Inter face Power Supply Status Single Event Upse...

Страница 138: ...id crete I Ps and O Ps FDR Data Frequency Counter CSMU Inter face Power Supply Status ARINC 717 RS422 Incorrect O P The CSMU In terface fails The DSP and FPGA internal resources re gisters are un able...

Страница 139: ...Memory fails Unable to store data and the SDRAM is un able to copy data The MP PWA fails to operate The CVDR PWA fails to oper ate Non Volatile Memory Electrical In terference Software glitch flips da...

Страница 140: ...tatus of the recorder and man age the Fault Log A008 RTC Timing Loss of Power The Real Time Clock fails Un able to set get the date and time The CVDR has no valid time stamp or date The CVDR has no va...

Страница 141: ...io tone test from the DSP No audio tone test is per formed No Effect Audio I P Audio I P Tone Test 0 is shorted Audio CODEC receives re cords either no audio tone test or a continuous tone test from t...

Страница 142: ...rom the DSP No audio tone test is per formed No Effect Audio I P Audio I P Tone Test 4 is shorted Audio CODEC receives re cords either no audio tone test or a continuous tone test from the DSP No audi...

Страница 143: ...note available to the Cockpit Area Micro phone or the Preamplifier Power Loss of Cockpit Area Micro phone Preamplifier Power Loss of Cockpit Area Micro phone Preamplifier Power Audio I P Power The CAM...

Страница 144: ...itor Output Channel LO G023 UART 1 GSE UART1 TxD The UART1 TxD GSE is open There is no communication between the UART1 and the front panel RJ 45 GSE port The MP PWA has no GSE capability Communication...

Страница 145: ...e to shut down properly The CVDR is unaware something is wrong Power Supply Status The Voltage Regulator Bank is shor ted The Voltage Regulator Bank fails The CVDR shuts down The CVDR shuts down J028...

Страница 146: ...Disrupted FDR Data Output ARINC 717 High echoed back to the AI PWA Disrupted FDR Data Output ARINC 717 High echoed back to the AI PWA K032 FDR Data Out LO Differential ARINC757 Data 0 P LO is open Dis...

Страница 147: ...Event Upset SEU The FPGA initially does not operate It is in an undeter mined condition The MP PWA initially does not operate The CVDR initially does not operate Some data may be corrupt lost and or...

Страница 148: ...Memory Electrical Inter ference Software glitch flips data bits causing data corruption such as lost missing or scrambled data The CSMU does not oper ate properly Some data may be corrupt and may not...

Страница 149: ...THE PRINTED CIRCUIT BOARD USELESS PRIOR TO HANDLING A PRINTED CIRCUIT BOARD ENSURE PROPER PERSONNEL GROUND ING TECHNIQUES ARE USED ALSO ENSURE THAT ALL CIRCUIT BOARDS ARE PLACED INTO STATIC SHIELDING...

Страница 150: ...within this requirement no monitoring is required The RIPS battery is an on demand maintenance item and required maintenance will be indicated over the recorder s ARINC 429 OMS No regular maintenance...

Страница 151: ...o provide a moisture proof package and place in a cool dry location Refer to Section B if the RIPS has been stored for one year or more B Storage of RIPS Without Original Container If the original con...

Страница 152: ...ssis 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 CSM...

Страница 153: ...required proceed with the following procedure CSMU REMOVAL PROCEDURE 1 Remove the two screws 1 115 used to secure the CSMU cable cover plate 1 110 and remove cover plate 2 Remove the two screws 1 130...

Страница 154: ...MU Memory Assembly 1 120 1 130 Qty 2 1 95 REF Figure 302 CSMU Memory Assembly Removal Diagram C Rear Cover Removal See Figure 304 or IPL Figure 1 Item 10 REAR COVER REMOVAL PROCEDURE 1 Loosen the six...

Страница 155: ...Removal Diagram D Aircraft Interface AI PWA Removal See Figure 304 or IPL Figure 1 Item 25 AIRCRAFT INTERFACE PWA REMOVAL PROCEDURE 1 Remove the rear cover as described in Paragraph C Rear Cover Remov...

Страница 156: ...s subject to the restrictions on the cover page of this document July 21 17 1 25 1 30 Qty 6 Qty 4 1 35 Rear Connector J 1 Some parts are removed for clarity purposes NOTE Figure 304 Aircraft Interface...

Страница 157: ...ecification Isopropyl Alcohol P D 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 obta...

Страница 158: ...ng the center contact of the beacon water switch at least once every 24 months more frequently under high humidity conditions Make sure the beacon case and water switch are free of dirt and or grease...

Страница 159: ...document Rev 02 Page 403 Crash Survivable Memory Unit CSMU 1 120 Left Beacon Mount Bracket 1 140 Right Beacon Mount Bracket 1 140 Underwater Acoustic Beacon 1 150 1 4 Hex Screw 1 145 1 4 2 3 Cross Pa...

Страница 160: ...Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document Rev 02 Page 404 THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online...

Страница 161: ...general physical integrity of the recorder i e J2 Ethernet GSE connector Underwater Locator Beacon and J1 rear panel connector pins 2 Check that dust cover is serviceable exhibiting no undue deterior...

Страница 162: ...con 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 Loc...

Страница 163: ...cordance with L3AP Factory test calibration and repair specifications As a result the Model FA5000 s maintenance philosophy is replacement of failed assem blies In the case of the Model FA5000 at this...

Страница 164: ...osure of information on this sheet is subject to the restrictions on the cover page of this document Rev 02 Page 602 July 21 17 THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is online p...

Страница 165: ...ures 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 Item Manufacturing and Specification Us...

Страница 166: ...ure 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 a The Assembl...

Страница 167: ...gure 1 Item 10 REAR COVER INSTALLATION PROCEDURE 1 Align the guide on the AI PWA 1 25 attached to the Rear Cover 1 10 with the receptacle on the MP PWA 1 45 2 Slide rear cover 1 10 straight in the rea...

Страница 168: ...le 1 15 Torque 9 10in lbs Figure 702 Rear Cover Installation Diagram D Crash Survivable Memory Unit CSMU Installation See Figure 703 or IPL Figure 1 Item 185 CSMU INSTALLATION PROCEDURE 1 Carefully gu...

Страница 169: ...of 5 10 in lbs 4 Install CSMU cable cover plate 1 110 and secure with installing two screws 1 115 Tighten screws to a torque value of 5 6 in lbs 1 110 1 95 Some parts are removed for clarity purposes...

Страница 170: ...nce item and is NOT field re pairable Replacement of the module s battery requires replacement of the entire RIPS Module No regular maintenance is required A RIPS Shelf Life The RIPS requires inspecti...

Страница 171: ...livered or installed with the RIPS connected To in stall the RIPS take the following steps as illustrated in Figure 705 1 Ensure that the CVDR is not powered 2 Remove protection cap from the RIPS conn...

Страница 172: ...his CMM NOTE The RIPS Module should provide sufficient holdup time after the first application of power for at least 15 minutes Once charged the battery should remain sufficiently charged for at least...

Страница 173: ...Condition RIPS Module After Expired Shelf Life One Year in Storage The RIPS Module should be conditioned as it reaches one year of storage 1 Install the RIPS Battery Pack in a known good recorder 2 A...

Страница 174: ...ainer to provide a moisture proof package and place in a cool dry location NOTE If the RIPS has been stored for one year refer to Section E B Storage Without Original Container If the original contain...

Страница 175: ...L3T com 7 Place an Order For questions about purchasing equipment F Call 941 371 0811 or F E mail DLAR aviationsales L3T com 1 Create a Purchase Order and include the following information F Purchase...

Страница 176: ...7 5554 F E mail DLAR repairstation L3T com 1 Create a Purchase Order and include the following information F Purchase Order Number F Customer Name F Contact Name and Phone Number F Ship To Address Ins...

Страница 177: ...A shipment package kit P N 147E5161 01 may be ordered from L3 Aviation Products if the original container is not available B Return Equipment from Outside the United States Import Compliance All Inte...

Страница 178: ...Rev 02 Page 714 July 21 17 9 Payment Information For questions contact Lawanna Hall F Call 941 371 0811 Ext 5142 F E mail Lawanna Hall L3T com F Mailing Address P O Box 3041 Sarasota FL 34230 USA NOT...

Страница 179: ...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 Measurement Height...

Страница 180: ...phone 150 6000 Hz bandwidth Audio Input Level 50 mVrms to 3 Vrms Audio Quality Meets ED112 specifications Signal to noise plus distortion ratio SINAD of the signal when reproduced 24 dB 6 distortion f...

Страница 181: ...hour 60 minutes 1100_C and 10 hours 260_C Impact ED 112 3400 g s 6 5 ms half sine shock wave Penetration ED 112 500 lbs 10 feet 1 4 probe D Environmental Characteristics Refer to Table 801 for the Mod...

Страница 182: ...iation 5 A Humidity 6 B Shock 7 B Vibration 8 R Curve E E1 H Curve P Explosion Atmosphere 9 E H Env II Water Proofness 10 Y W Fluid Susceptibility 11 F Sand and Dust 12 D Fungus Resistance 13 F Salt F...

Страница 183: ...bject to the restrictions on the cover page of this document Rev 02 Page 805 July 21 17 2 3 CG B HOLE B HOLE 2 5 CG 4 2 CG 12 6 6 48 Figure 801 Sheet 1 of 2 Outline Dimension Drawing Model FA5000 Cock...

Страница 184: ...this document Rev 02 Page 806 July 21 17 Forward View 4 88 4 12 5 02 2x12 13 4 1 3 22 2x FOR HOLES MARKED B SEE DETAIL A TRAYLESS MOUNTING DIMENSIONS 26 Rear View DETAIL A 20 26 15 Figure 801 Sheet 2...

Страница 185: ...Cable RIU to DC Power In 17TES0413 Cable RIU to Sound Card 2 ea 17TES0415 Cable RIU to USB 17TES0418 Cable RIU to CVDR 17TES0420 CATS Software FA2100 V 2 1 17TES0070 CICC 2 Assembly 17TES0072 Cable A...

Страница 186: ...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 840E54...

Страница 187: ...17TES0415 RIU AC POWER INPUT 17TES0411 AC J7 J6 RIU AUDIO OUTPUT SPKRS J9 RCDR AC PWR TEST RECORDER INTERFACE UNIT RIU 17TES0710 SND OUT GREEN 17TES0413 J4 J2 J1 L SPKR R SPKR YELLOW AC RED DC AC 1A...

Страница 188: ...ersonal computer containing specific required hardware running under the Windows 7t 32 bit or Windows XP SP3t operating software with Microsoft Direct X version 9 0 or higher The minimum recommended h...

Страница 189: ...into a ROC 7 using the Ethernet Cable b Use the Portable Interface 2 PI 2 Unit P N 17TES0062 with Mod Dot 1 This device is used to download the FA5000CVR voice and data link information to a SD CF mem...

Страница 190: ...Use or disclosure of information on this sheet is subject to the restrictions on the cover page of this document Rev 02 Page 906 July 21 17 THIS PAGE IS INTENTIONALLY LEFT BLANK The document referenc...

Страница 191: ...onnel 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 assembl...

Страница 192: ...ustration in which the item is shown and the item number listed on the illustration Figure numbers are shown for the first entry of each figure and at the top of each subsequent column When there is m...

Страница 193: ...s the end of attaching parts The EFFECTIVITY CODE column establishes parts relationship with units or assemblies which are essentially the same but have variations These units or assemblies are the le...

Страница 194: ...tainless and Titanium Crash Survivable Memory Units CSMU for all Models of recorders using the L3AP 90 Day Underwater Locator Beacon PN 266E5542 00 brackets and mounting screws that make up the ULB Co...

Страница 195: ...sted below are the current configurations for the FA5000 Flight Data Recorder FDR Part Number 5000 310X XX is capable of storing 25 hours of flight data 5003 5000 00 ARINC 757 2 HR CVR 1 2 ATR SHORT 2...

Страница 196: ...1 100 2 010E5161 00 1 110 1 016E1589 00 1 140 2 016E5852 00 1 41 1 024E5161 00 1 80 1 042E5161 02 1 95 1 075E5161 02 1 10 1 075E5352 00 1 55 1 1110 4 AL 9 1 65 1 136E5161 02 1 5 1 189E5161 00 1 135 1...

Страница 197: ...DELETED 1 253E5851 00 1 120B 1 253E5851 01 1 120C 1 253E5851 02 1 120D 1 253E5851 03 1 120E 1 266E0305 00 1 150A 1 266E0305 01 1 150B 1 266E0305 02 1 150C 1 266E5422 00 1 150D 1 500 4030 000 2 1A RF 5...

Страница 198: ...ions on the cover page of this document Rev 02 Page 1008 July 21 17 95 45 120 10 125 130 110 115 135 QTY 4 QTY 2 QTY 2 5 80 90 85 50 QTY 2 QTY 2 55 60 65 75 70 QTY 2 A A B B 108 QTY 4 86 Figure 1000 S...

Страница 199: ...ctions on the cover page of this document Rev 02 Page 1009 July 21 17 150 QTY 6 15 140 100 10 QTY 6 20 35 40 145 105 QTY 4 QTY 2 QTY 4 REF QTY 4 25 30 View A QTY 2 QTY 2 View B 41 116 Figure 1000 Shee...

Страница 200: ...COCKPIT VOICE RECORDER FA5000 CVR ARINC 757A 2 HR GA CVR 1 2 ATR SHORT 28 VDC ONLY D RF 1E 5003 5000 01 COCKPIT VOICE RECORDER NAND FA5000 CVR ARINC 757 2 HR CVR 1 2 ATR SHORT 28 VDC ONLY LIGHTWEIGHT...

Страница 201: ...8 PWA AI FA5000 ROHS ARINC F 1 ATTACHING PARTS 30 MS51957 26 SCR PNH 6 32 X1 4 V06141 2290200083 6 35 MS24693 C4 SCR FLH 4 40 X3 8 V06141 2290200356 4 40A 230E5488 00 SEAL ARINC 404 CONNECTOR SUPSD BY...

Страница 202: ...OD 115ID 5 16 V55582 2399800255 1 70 MW0242 006 S SPRING WAVE S S V06141 2429800057 2 75 0639805057 CONN SEAL RJ45 COND VQ3554 0639805057 1 80 024E5162 00 CABLE ASSEMBLY RIPS POWER 1 ATTACHING PARTS 8...

Страница 203: ...200362 4 108 22902002 29 SCR FLH 10 32X1 2 4 110 010E516100 PLATE COVER 1 ATTACHING PARTS 115 MS24693 C3 SCR FLH 4 40 X5 16 V06141 2290200219 2 116 230E5161 01 SEAL MEMORY CONNECTOR 1 120A 253E5162 01...

Страница 204: ...NO NOMENCLATURE 1234567 EFF CODE UNITS PER ASSY 1000 ATTACHING PARTS 125 BB1P14H12 SCR PNH 1 4 20X3 4 SEALING V06141 2299800558 4 130 MS51957 12 SCR PNH 4 40 X3 16 V06141 2290200072 2 135 189E5161 00...

Страница 205: ...47E0305 00 C D E 1 150B 266E0305 01 BEACON ACOUSTIC UNDERWATER SUPSD BY 150D PER SB004 DUKANE V94970 DK 120 FOR BATTERY REPLACEMENT ORDER 30 DAY BATTERY KIT 147E0305 00 C D E 1 150C 266E0305 02 BEACON...

Страница 206: ...of information on this sheet is subject to the restrictions on the cover page of this document Rev 02 Page 1016 July 21 17 1 Figure 1001 Model 500 Recorder Independent Power Supply RIPS The document...

Страница 207: ...or disclosure of information on this sheet is subject to the restrictions on the cover page of this document Rev 02 Page 1017 July 21 17 THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is...

Страница 208: ...to the restrictions on the cover page of this document Rev 02 Page 1018 July 21 17 FIG ITEM PART NUMBER AIRLINE PART NO NOMENCLATURE 1234567 EFF CODE UNITS PER ASSY 1001 1 500 4030 000 RECORDER INDEP...

Страница 209: ...or disclosure of information on this sheet is subject to the restrictions on the cover page of this document Rev 02 Page 1019 July 21 17 THIS PAGE IS INTENTIONALLY LEFT BLANK The document reference is...

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