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L3 500-4030-000 RIPS, Maintenance Manual

The L3 500-4030-000 RIPS is a high-quality Component Maintenance Manual With Illustrated Parts List that ensures optimal maintenance of your product. This comprehensive manual provides detailed instructions and diagrams for easy understanding. Download this essential manual for free from manualshive.com, enabling hassle-free maintenance and efficient repairs.

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COMPONENT MAINTENANCE MANUAL

AVIATION PRODUCTS

Model FA5000

Rev. 02 Page 306

Disassembly

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

(1

−

110)

(1

−

95)

Some parts are removed

for clarity purposes

NOTE:

(1

−

115)

(1

−

45)

(Qty. 2)

Memory Interface

Cable Assembly

1/4” Pan

−

Head Sealing

Screws (1

−

125)

(Qty. 4)

CSMU

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 captive screws (1

−

15) used to secure the rear cover (1

−

10) to

the rear part of the Shielded Housing (1

−

5).

(2) Slide rear cover (1

−

10) straight back from recorder until the AI (1

−

25) and MP

(1

−

45) PWAs separate at each other’s connector.

(3) Remove the rear cover (1

−

10).

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

Summary of Contents for 500-4030-000 RIPS

Page 1: ...s 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 WARNING This technical data is controlled under the Export Administration Regulations EAR ECCN 7E994 and may not be exported to a foreign person either ...

Page 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 distribution to 3rd parties or resale of this manual is permitted Inquiries should be addressed to L3 Technologies Aviation Products Technical Publications 100 Cattlemen Road Sarasota Florida 34232 94...

Page 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 Only those who are thoroughly familiar with industry accepted techniques for handling static sensitive devices should attempt to service circuitry with these devices In all instances measures must be ta...

Page 4: ...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 please check the correspondence between the online documentation and the printed version ...

Page 5: ...ion 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 ULB removal procedure and replaced with reference to the ULB CMM and I O manuals Assembly Referenced the ULB CMM and I O manuals Added RIPS condition ing steps Product Support contact info storage and ...

Page 6: ...Front 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 Testing Disassembly Added RIPS and equipment storage details Assembly Added RIPS and equipment storage details Fit and Clear ances Special Tools and Test Equip ment Illustrated Parts List and Schem atic ...

Page 7: ...e 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 5000 30 5013 5001 50 Rev 02 July 21 17 Updated L3 company name added ULB refer ence to CMM I O added RIPS conditioning steps and shipping information The document reference is online please check the c...

Page 8: ...ge 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 online please check the correspondence between the online documentation and the printed version ...

Page 9: ...rmation 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 P 02 July 21 17 C P The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 10: ...3 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 online please check the correspondence between the online documentation and the printed version ...

Page 11: ...er 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 recorders or field modification using the 90 day Beacon Conversion Kit The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 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 online please check the correspondence between the online documentation and the printed version ...

Page 13: ...Jul 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 21 17 xxxii Jul 21 17 xxxiii Jul 21 17 Introduction 1 Jul 21 17 2 Jul 21 17 3 Jul 21 17 4 Jul 21 17 5 Jul 21 17 6 Jul 21 17 7 Jul 21 17 8 Jul 21 17 Description and Operation 1 Jul 21 17 2 Jul 21 17 3 ...

Page 14: ...21 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 Jul 21 17 109 Jul 21 17 110 Jul 21 17 111 Jul 21 17 112 Jul 21 17 113 Jul 21 17 114 Jul 21 17 115 Jul 21 17 116 Jul 21 17 117 Jul 21 17 118 Jul 21 17 119 Jul 21 17 120 Jul 21 17 121 Jul 21 17 122 Jul...

Page 15: ...ul 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 17 706 Jul 21 17 707 Jul 21 17 708 Jul 21 17 709 Jul 21 17 710 Jul 21 17 711 Jul 21 17 712 Jul 21 17 713 Jul 21 17 714 Jul 21 17 Fits and Clearances 801 Jul 21 17 802 Jul 21 17 803 Jul 21 17 804 Jul 21 17...

Page 16: ...ST 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 Jul 21 17 1013 Jul 21 17 1014 Jul 21 17 1015 Jul 21 17 1016 Jul 21 17 1017 Jul 21 17 1018 Jul 21 17 1019 Jul 21 17 The document reference is online please check the correspondence between the online ...

Page 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 CLEANING 5 F CHECK 5 G REPAIR 5 H ASSEMBLY 5 I SPECIAL TOOLS AND TEST FIXTURES 6 J ILLUSTRATED PARTS LIST 6 6 DOCUMENT VERIFICATION 6 7 COMPONENT MAINTENANCE MANUAL CMM EFFECTIVITY 7 8 PART NUMBER FORMA...

Page 18: ...ge 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 Operating Power and Monitor Audio Signals 28 3 Control Unit Test and Bulk Erase Signals 29 4 Output Audio Quality 30 5 FA5000 SPECIFICATIONS 31 A Applicable Documents 31 B Physical Characteristics 3...

Page 19: ...ment 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 Functionality 42 E Bulk Erase 42 F Recorder Synchronization 43 G Data Downloading 43 H CVR RIPS Status Monitoring 44 1 RIPS Active 44 2 RIPS Fault 45 3 RIPS Maintenance 45 4 RIPS Present 45 9 Onboard Maint...

Page 20: ...NG 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 ROC 7 Interconnects 102 B READ OUT CENTER 7 ROC 7 Sound Card Setup 106 C READ OUT CENTER 7 ROC 7 CATS Autotest 112 1 ROC 7 CATS Autotest using DC power 112 D READ OUT CENTER 7 ROC 7 Autotest Descripti...

Page 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 OUT CENTER 7 ROC 7 AUDIO DOWNLOAD PLAYBACK 128 6 TEST THE UNDERWATER LOCATOR BEACON ULB 129 7 AIRCRAFT INTERFACE 130 8 MAIN PROCESSOR 139 9 CRASH SURVIVABLE MEMORY UNIT CSMU 149 The document reference ...

Page 22: ...ginal 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 Memory Unit CSMU Removal See Figure 302 or IPL Figure 1 Item 120 304 C Rear Cover Removal See Figure 304 or IPL Figure 1 Item 10 306 D Aircraft Interface AI PWA Removal See Figure 304 or IPL Figure 1 It...

Page 23: ...UCTIONS 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 Survivable Memory Unit CSMU Installation See Figure 703 or IPL Figure 1 Item 185 704 E Install Underwater Locator Beacon See IPL Figure 1 Item 150 706 4 RECORDER INDEPENDENT POWER SUPPLY RIPS MODULE ...

Page 24: ...n 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 Characteristics 802 B RIPS Power Logic 802 C Crash and Fire Survival Characteristics 803 D Environmental Characteristics 803 E Torque Requirements 803 SPECIAL TOOLS FIXTURES AND EQUIPMENT 1 GENERAL 901 2...

Page 25: ...ONTENTS 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 NUMBERING 1003 8 MANUFACTURER S CODE 1004 9 L3 AVIATION PRODUCTS L3AP AUTHORIZED PARTS 1004 10 CONFIGURATION MATRIX 1005 The document reference is online please check the correspondence between the online...

Page 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 online please check the correspondence between the online documentation and the printed version ...

Page 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 Functional System Block Diagram 27 Figure 16 Model FA5000 CVR 120 Minute Audio Monitor Schemes 29 Figure 17 Model FA5000 CVR 120 Minute Recording Schemes 30 Figure 18 Interwiring Diagram Recorder FA5000 CV...

Page 28: ...Log 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 302 Figure 302 CSMU Memory Assembly Removal Diagram 306 Figure 303 Rear Cover Removal Diagram 307 Figure 304 Aircraft Interface AI PWA Removal Diagram 308 Figure 401 Underwater Locator Beacon 403 Fi...

Page 29: ...ver 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 1009 Figure 1001 Model 500 Recorder Independent Power Supply RIPS 1016 The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 30: ...2 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 online please check the correspondence between the online documentation and the printed version ...

Page 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 101 17TES0700 READOUT CENTER 7 ROC 7 Parts List 104 Table 102 Aircraft Interface Troubleshooting Chart 130 Table 103 Main Processor Troubleshooting Chart 139 Table 104 CSMU Troubleshooting Chart 149 T...

Page 32: ...02 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 online please check the correspondence between the online documentation and the printed version ...

Page 33: ...ts 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 L3 P N 165E5542 10 and the Underwater Locator Beacon CMM L3 P N 165E5542 00 2 ACRONYMS AND ABBREVIATIONS The following list defines the acronyms and abbreviations used throughout this CMM ADLP Audio...

Page 34: ...ailures 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 LVL Record Level RIU Recorder Interface Unit ROC Read Out Center RTCA Radio Technical Commission for Aeronautics RTMS Requirements Traceability Management System SMT Surface Mount Technology TDM Tim...

Page 35: ...stallation 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 F Audio Data Link Player Software Operator s Manual P N 165E3596 02 F CATS RIU 2 0 Operator s Manual P N 165E4127 01 F Ultrasonic Test Set Underwater Locator Beacon ULB Tester P N 17TES0015 if functi...

Page 36: ...NT 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 for an audience of operators and both intermediate and depot Level maintenance technicians Functional electrical and mechanical aspects of the Model FA5000 are documented that is description specifi...

Page 37: ...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 E CLEANING This section contains a listing of all required cleaning materials procedures for cleaning material use and applicable warnings and cautions related to the use of prescribed cleaning solvents F...

Page 38: ...the 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 Component Maintenance Manual Verifica tion Report that identifies the technician who performed the procedure and Engineer Technical Writer who verified the procedure along with a Quality Assurance Engineer ...

Page 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 E0305 00 266E0305 00 or 266E030500 To be in compliance with ARINC Specifications 100 and 200 the part numbers listed in this manual use the following format 266E0305 00 L3AP typically identifies its...

Page 40: ...oduction 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 please check the correspondence between the online documentation and the printed version ...

Page 41: ...rder 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 F Maintenance free no periodic or scheduled maintenance on condition LRU F Solid state flash memory capable of 2 hour recording RIPS CSMU BEACON MOUNTING CHASSIS MAIN RECORDER J2 J1 Figure 1 Model F...

Page 42: ...e 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 is constructed as shown below Figure 2 Model FA5000 Cockpit Voice Recorder Part Number Matrix The document reference is online please check the correspondence between the online documentation and the ...

Page 43: ...apable 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 interface via an ordinary web browser The browser interface also offers monitoring of real time data and other system functions The following is a list of the inputs and outputs for the CVR systems ...

Page 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 to the processor via the TDM bus All other data is processed into fixed size packets and then sent to the processor via register access The processor responds to the new data sent on the TDM or via ...

Page 45: ...is 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 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...

Page 46: ...Channel 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 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 ...

Page 47: ...is 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 of the Model FA5000 CVR The partitioning of the software is based on the functionality of each of the recorder types Each recorder type has its own set of CSCs that are dependent on the processes need...

Page 48: ...esulting 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 onds 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 A tachometer rotor spee...

Page 49: ...it 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 CAM Partition and compare it to the sent data Data Match No Yes Compress Three Channel Data and send it to the Three Channel Partition Read Three Channel Data back from Partition and compare it to th...

Page 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 156 157 227 270 and 276 are accepted Note that messages with Label 156 should not be sent when using the Williamsburg Version 3 protocol however the recorder will record them if they are sent Label 350 is the CV...

Page 51: ...for 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 the BITE task if the DataLink Valid signal is assert ed and the recorder does not receive status via Label 270 for more than 3 seconds Specifically messages with Label 270 should always be received onc...

Page 52: ...s 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 bit DataLink messages 32 bytes 32 bytes 8 bytes 120 bytes 3 124 Flash Memory Chips Flash Memory Blocks Flash Memory Pages Figure 6 DataLink Memory Format The document reference is online please check...

Page 53: ...Header 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 status from the other tasks in the system and creates a status word suitable for output onto the ARINC 429 bus via Label 350 It does this at a rate of once per second The document reference is online plea...

Page 54: ...nit 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 each type of data will be stored in its own partition Different partitions are defined as follows Microphone Partition CAM Partition DataLink Partition The hardware and software will be architected i...

Page 55: ...ch 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 until the end of the block is reached at which time the packet is written to the next block in the next chip This is because according to ED 112 specifications the Audio CAM and Voice and DataLink p...

Page 56: ...n 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 Read After Write Processing Yes No Write Request Read Request Write Block Header Figure 9 Data Storage Task Flowchart When data is about to be written into a new block for the first time the Data Sto...

Page 57: ...n 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 Outputs Real time Health and Status Info to GSE Interface Task Figure 10 BITE Task Data Flow Diagram The BITE task is responsible for processing the Push to Test discrete and the Voice Erase discrete that ...

Page 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 real time status on certain pieces of hardware and watchdog maintenance See Fig ure 11 BITE Task Flowchart The document reference is online please check the correspondence between the online documentati...

Page 59: ...lt 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 requires setting A Fault Light Turn On Specified Fault Light Yes No Yes No Pet the Watchdog Pet the Watchdog Figure 11 BITE Task Flowchart The document reference is online please check the correspond...

Page 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 spawned it creates a message queue that will be used by the communi cations managers to send commands and get responses The GSE task blocks its pro cessing until it receives a message This means that...

Page 61: ...on 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 12 GSE Task Data Flow Diagram The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 62: ...f 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 Response Msg Queues Got Command No Error Response Process Next Command Figure 13 GSE Task Flowchart The document reference is online please check the correspondence between the online documentation and...

Page 63: ...57 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 ory This CVR is available in in voice recording configuration of 120 minute This CVR configuration records a minimum of 120 minutes of high quality audio from the following four cockpit audio inputs C...

Page 64: ...water 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 FAA TSO C121 was revoked as of March 1 2015 The m...

Page 65: ...s 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 Signal Interface Characteristics Input power is 28 Vdc At normal power level an interruption equal to or less than 200 milliseconds will not affect the Model FA5000 CVR s function Upon application o...

Page 66: ...2 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 MODEL FA5000 CVR CVR FAULT TO GROUND STATION TEST EQUIPMENT GMT_IN_B 429 GMT_IN_A 429 ROTOR_SPEED_IN_LO ROTOR_SPEED_IN_HI GEAR BRAKE AUDIO OUT 18 VDC 115 VAC 400 Hz OMS OUTPUT A 429 OMS OUTPUT B 429 DA...

Page 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 FAULT TO GROUND STATION TEST EQUIPMENT GMT_IN_B 429 GMT_IN_A 429 GEAR BRAKE AUDIO OUT 18 VDC 115 VAC 400 Hz OMS OUTPUT A 429 OMS OUTPUT B 429 DATA LINK FAULT DATA LINK OMS GACVR DATA LINK IN B 429 DATAL...

Page 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 Model S251 S261 Control Units are for use in FA5000CVR ARINC 757 or 757A ED 56A System installations The Model S151 and Model S251 Control Units house the Microphone Preamplifier PWA and have front pa...

Page 69: ...ATA 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 and Erase C signals are used to initiate a bulk erasure of the crash protected solid state memory The ERASE pushbutton must be pressed for more than two seconds and then released to initiate the bulk...

Page 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 17 Model FA5000 CVR 120 Minute Recording Schemes 4 Output Audio Quality The FA5000CVR s audio quality meets or exceeds the audio quality specified in Part I of ED 112 Specifically the Reference Sign...

Page 71: ...uirements 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 C123b Federal Aviation Agency Technical Standard Order TSO C123b Techni cal Standard Order for Cockpit Voice Recorder Systems 2 TSO C124b Federal Aviation Agency Technical Standard Order TSO C124b T...

Page 72: ...al Characteristics For specific electrical characteristics refer to Section 800 Fits and Clearances D Environmental Characteristics For specific environmental characteristics refer to Section 800 Fits and Clearances E Crash and Fire Protection For specific crash and fire protection specifications refer to Section 800 Fits and Clearances F CSMU Torque Requirement For specific CSMU torque requiremen...

Page 73: ...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 The Control Unit Microphone information can be found in CMM ATA No 23 70 05 p n 165E1747 00 for ED 56A installations or the FA5000CVR Installation Opera tion manual p n 165E5327 00 The document refer...

Page 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 HI CHANNEL 3 LO CHANNEL 4 LO CHANNEL 4 HI ROTOR SPEED IN LO ROTOR SPEED IN HI VOICE ERASE A VOICE ERASE C 115 VAC POWER IN HOT 115 VAC POWER IN COLD PREAMP PWR OUT GND PREAMP PWR OUT HOT 18 VDC REG ...

Page 75: ...ate 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 shields to existing single point GND use for Pin 17 see Note 3 7 If the power source has battery back up a means for terminating recording after a crash should be included in the aircraft wiring Ground...

Page 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 AUDIO JACK HI MIC BIAS WHITE MIC HIGH BLACK MIC LOW SHIELD OR MODEL S056 MICROPHONE FROM CAPTAIN S CLOCK TO ANNUNCIATOR OR MAINT COMPUTER SPARE MICROPHONE TO 3RD CREW MEMBER OR PA SYSTEM TO COPILOT M...

Page 77: ...17 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 pins 10 29 38 will be used for the RIPS Status Monitoring 8 BITE status output ground no fault open fault or CVR not installed 9 Audio input 05 Vrms 3 Vrms maximum 1Vrms nominal 10 Per FAA Action Not...

Page 78: ...EM 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 CSMU The recorder interfaces with the aircraft s cockpit recorder control unit and microphone through the rear panel connector J1 and with the Ground Station Equipment through the front panel Ethernet ...

Page 79: ...ed 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 Stop Recording The ARINC 757 A Aircraft Interface provides output signal conditioning for CVR Fault Audio Out for Monitoring at the Control Unit headset Data Link and OMS The Aircraft Interface also i...

Page 80: ...ssors 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 Survivable Memory Unit CSMU In addition there are external interfaces at tached to each DSP to allow external communication for testing purposes interfaces to allow the system to gather data for storage and i...

Page 81: ...INC 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 transmitted on Label 350 per ARINC 429 in the format depicted in Attachment 19 of ARINC 757 A CVR STATUS WORD The fault signal is indicated for any of the following as per ED112 2 1 4 2 F failure of...

Page 82: ...Push 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 serviceability of the CVR before flight as required by the applicable regulation Upon test activation the CVR tests the front end audio inputs each of the four au dios inputs channels and initiates Built In Te...

Page 83: ...a 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 30Hz and 4193Hz 30Hz depending on the source used on the aircraft For Models FA5000CVR the recorder automatically detects which source is received acquires the time data and stores it into memory The ...

Page 84: ...gnments 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 transmitted using Fault Warning Label 350 Label 351 and Label 352 as part of the OMS RIPS status will also be stored within the CSMU memory and the data will be able to be retrieved using the existing supp...

Page 85: ...S 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 351 Bit 19 No Mainten ance required Open 0 1 Maintenance required Ground 1 0 4 RIPS Present Use of CVR Pin 42 CVR Ident is being used for the RIPS Present Pin Pro gram Since we do not anticipate more...

Page 86: ...2 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 Power Supply RIPS 9 Onboard Maintenance System Interface The FA5000CVR includes an ARINC 429 high speed Onboard Maintenance Sys tem OMS output interface Pins 50 51 and an ARINC 429 low speed OMS input in...

Page 87: ...in Program Open No RIPS Installed Ground RIPS Present If the RIPS is not present then the CVR will not monitor the RIPS status inputs and they will not be reported default to 0 in Label 350 output A Label 350 Status Word Output The CVR will report status using Label 350 on the OMS ARINC 429 output word as shown in Table 1 3 below Table 6 CVR LABEL 350 OUTPUT FORMAT BIT N FUNCTION STATUS 1 8 Label ...

Page 88: ...ST REPORTED WITH CVR FAULT DIS CRETE 11 CVR Status Audio Recording Failure YES YES YES 12 CMC Bus Status OMS Input NO NO NO 13 CVR Control Unit Failure YES YES YES 14 FDR Status not used NO NO NO 15 RIPS Fault Status Pin 29 NO NO NO 16 CVR DataLink Recording Failure NO NO NO 17 Clock Status NO NO NO 18 Data Link Input Interface NO NO NO 19 CVR Record Enable Pins 7 8 NO YES YES 20 RIPS Maintenance ...

Page 89: ...events correct record ing of the audio inputs including CU failure and Push to Test audio input circuit failure May relent depending on fault severity 12 CMC Bus Status OMS In put Loss of OMS input Heartbeat valid Label 227 input for more than 3 seconds Relents if OMS Heartbeat is restored 13 CVR Control Unit Failure Loss of 18 VDC Control Unit supply voltage Relents if voltage level returns 14 FD...

Page 90: ...bel 354 LRU Identification Output The CVR LRU IDENTIFICATION consists of multiple ARINC 429 words for the trans mission of the CVR part number and serial number The group of eleven ARINC 429 words defined below is transmitted twice per second a Start of Transmission Word Bit No Function Status 1 8 Label 354 11101100 9 16 Number of words in transmission 11 00001011 17 24 Not used 00000000 25 31 STX...

Page 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 character of part number 16 Not used 0 17 23 Tenth character of part number 24 Not used 0 25 31 Eleventh character of part number 32 Parity g End of Part Number Start of Serial Number Bit No Function Status...

Page 92: ...ter 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 00000000 32 Parity k End of Transmission Word Bit No Function Status 1 8 Label 354 11101100 9 24 Not used 0000000000000000 25 31 EOT 0000100 32 Parity C Label 377 ARINC 429 Equipment Identification Wo...

Page 93: ...h 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 Version 3 Bit Oriented Protocol for link layer interface F Includes support for ALOHA exchange but not required F Records all System Address Label SAL 157 and or 156 full word inputs F Recording of all ...

Page 94: ...d 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 ed GFI header encoding currently defined for message encapsulation This tech nique provides the maximum flexibility in DataLink recording without the need for fu ture CVR changes as the approved messa...

Page 95: ...DS 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 includes an ARINC 429 OMS output interface Pins 50 51 that provides a Label 350 CVR status word output once per second This word in its entirety along with any DataLink Label 270 or 276 input status...

Page 96: ...burg Version 1 protocol or a low speed ARINC 429 interface for input of DataLink informa tion However the CVR does support the Williamsburg ALOHA exchange even though it is not required for Williamsburg Version 3 DataLink input In the event that the CVR receives a valid ALO input on the SAL Label 157 or 156 it will respond with a valid Label 304 ALR output indicating support for the Version 3 prot...

Page 97: ...e same way as audio data All or a portion of the DataLink recording can be downloaded from the CVR using Ground Support Equipment supplied by L 3 Aviation Recorders The Portable Interface 2 can be used to download the DataLink recording to a PCMCIA memory card The DataLink recording can also be downloaded using the Ethernet interface cable connected to a PC The downloaded DataLink file can then be...

Page 98: ...n 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 online please check the correspondence between the online documentation and the printed version ...

Page 99: ...ALSO 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 is considered an ON CONDITION LRU meaning that the unit does not require any special periodic maintenance except for the ULB test procedure Each of its printed wiring assemblies PWAs makes extensive ...

Page 100: ...et 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 than 2 seconds and release A 400 Hertz tone should be heard via the headset for less than 10 seconds Should a problem be detected with the Model FA5000 CVR and its associated control unit remove the un...

Page 101: ...herboard 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 Out which is the green connector 7 Connect the DIN CABLE from the speakers to the middle Speaker Out SPKRS OUT J6 connector on the front panel of the RIU 8 After all connections are made to the RIU app...

Page 102: ...quipment 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 Ethernet Cross over REQUIRED 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 The document referenc...

Page 103: ...411 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 SND IN SND OUT SPKRS OUT GSE INTFC REAR CONNECTOR INTFC J3 J6 J5 LIGHT LIGHT RIU DC POWER INPUT 17TES0412 DC J8 SOUND CARD POWER INPUT SELECT POWER LED ETHERNET CROSS OVER CABLE ASSY P N 0249800386 SN...

Page 104: ...e 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 click OK The Channels control screen will dis appear 3 Click the Volume control icon it is the icon that looks like a speaker The Volume Mixer Speakers SB Audigy control displays see Figure 103 The ...

Page 105: ...t 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 illustrated in Figure 104 Figure 104 Sound Control Recording The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 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 100 move the Line In slider to maximum a Click on OK 9 Click on the Playback tab The document reference is online please check the correspondence between the online documentation and the printed versio...

Page 107: ...isclosure 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 Levels tab The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 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 input volumes have been muted controls Microphone Line In Auxiliary and S PDIF In are all muted 15 Click OK 16 Click on the Playback Control The document reference is online please check the corresp...

Page 109: ...information 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 Close the Volume Mixer The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 110: ...e 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 17TES0418 ROC 7 for the recorder rear connector and crossover cable p n 0249800386 for the recorder front connector J 2 b If the power supply does not include a built in multimeter set up an inline RMS mult...

Page 111: ...n 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 appropriate LED is lit up on the RIU h Click on the Information tab in the Test section of the menu i Verify appropriate information into Department Part Number and Serial Number fields The document referen...

Page 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 return to service test is not desired then select the Se lectable Test Options radio button and choose the test options desired Figure 113 will appear as confirmation The document reference is online pl...

Page 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 Message m 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 The document refe...

Page 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 Instruction Window o Observe the Fault History Log window appears Select Print if you want to save the fault history or Close to continue The document reference is online please check the corresponde...

Page 115: ...r 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 window appears Select Print if you want to save the fault history or Close to continue The document reference is online please check the correspondence between the online documentation and the print...

Page 116: ...t 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 provided in the Information section of the test The test report is located in the following default location C Program Files L 3Com CVRTester Reports This file is in an ASCII text file format t If the autot...

Page 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 from the recorder w If testing another recorder refer back to Paragraph C in this section The document reference is online please check the correspondence between the online documentation and the prin...

Page 118: ...e 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 08 02 23 PASSED Power DC Expected 11 watts Results 12 375 watts 2 2 watts 10 175 watts 2 Fault Log Displays the current recorder fault log for user review and prompts the user Clear fault log Select y...

Page 119: ...g Expected 400 Hz Results 3334 6 Hz 4 Test Tone Enable push to test and verify push to test indicator is set Example report message s 08 03 06 PASSED Test Tone Expected Push To Test indicator Results Push To Test indicator set 5 GMT 429 Record simulated GMT 429 data label 125 first and label 150 second and verify 10 good patterns are recorded for each label Example report message s 08 03 22 PASSED...

Page 120: ...SQV2 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 Response Record simulated 150 Hz reference data for each channel 1 2 3 and 4 Record simulated 1000 Hz reference data for each channel 1 2 3 and 4 Record simulated 3500 Hz reference data for each channel 1 ...

Page 121: ...0 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 ref Expected HQ 24 0 dB SQ 20 0 dB Results HQ1 34 6 HQ2 34 4 HQ3 34 8 HQC 36 4 SQV1 30 9 SQV2 31 0 SQV3 30 6 SQC 31 4 dB 11 26 44 PASSED SN D 1000 Hz 1 0 ref Expected HQ 24 0 dB SQ 20 0 dB Results HQ1...

Page 122: ...Q2 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 11 Crosstalk Data This is a test for CVDR recorders where both flight data and voice data are being recorded A Channel Balance is performed prior to the cross talk data test to determine and store res...

Page 123: ...e 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 each channel 1 2 3 and 4 and verify amplitudes by part number Example report message s 08 26 43 PASSED Audio Out Monitor 1000 Hz Expected 2 45 20 percent VRMS Results HQ1 2 319 HQ2 2 338 HQ3 2 317 HQC 2...

Page 124: ...ED 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 recorder is still powered after 200 milliseconds but not powered after 2 seconds Example report message s 08 56 32 PASSED Capacitor GSE powered after 200 milliseconds but not after 2 seconds 17 Data Link ...

Page 125: ...over 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 Results No CVR Fault after power removed for over 9 minutes 20 FRED Verify FA2100 Flight Recorder Electronic Documentation FRED file exists or can be written Example report message s 09 09 30 PASSED FR...

Page 126: ...ault 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 or Copy data from last XX Hrs XX Mins Click OK Copying of the data will start 4 When the Copy Data is Complete box is shown click on Yes On the Decom pression Options menu select HQV1 through HQV3 an...

Page 127: ...ge 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 Manual L3AP P N 165E5542 10 and the 90 Day Underwater Locator Beacon CMM L3AP P N 165E5542 00 The document reference is online please check the correspondence between the online documentation and the ...

Page 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 present Unable to monitor audio 06 Audio O P Audio Monitor Output High The signal path is open No audio voice is present Unable to monitor audio 06 Audio O P Audio Monitor Output High The signal path...

Page 129: ...ignal 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 Power O P Preamp Power Output Hot The signal path is shorted The Preamp Power Output Hot Signal fails Unable to hear cockpit audio no audio is recor ded 15 Differential Analog Test Indicator The signal ...

Page 130: ...us 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 Effect 21 Discrete I P Internal Pre Amp At tenuator N12DB The signal path is shorted Internal Pre Amp At tenuator N12DB signal software re ceives continuous 12 dB attenuation Internal Pre Amp Attenu ator...

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

Page 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 Data Link Input A Unable to store ARINC 429 A Data Link signal data into the CSMU 34 Differential ARINC429 A Data Link Input A The signal path is shorted Data disrupted cor rupted Loss of abil ity to...

Page 133: ...s 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 data provided recorded 41 Differential Audio Channel 3 Audio Input Pilot Low The signal path is open Degraded Audio Channel 3 Low Sig nal Fails to record no audio is recorded 41 Differential Audio Chann...

Page 134: ...The 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 wiring The FDR Maintenance signal always indicates maintenance 47 Differential Audio Channel 4 Audio Input Area Microphone High The signal path is open Degraded Audio Channel 4 High Sig nal Fails to re...

Page 135: ...ea 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 recorded 53 Differential Audio Area Mic Input Low The signal path is shorted Audio from the Area Mic Input Low Signal is degraded due to interference Degraded EMI 54 Differential Audio Area Mic Input High...

Page 136: ...his 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 path is shorted Loss of ability to erase recorded audio The recorder does not erase recorded audio The document reference is online please check the correspondence between the online documentation an...

Page 137: ...faces 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 Upset SEU The DSP ini tially does not operate The MP PWA initially does not operate The CVDR initially does not op erate some data may be cor rupt lost and or may not be re corded stored or copied NOTE A...

Page 138: ...Did 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 to com municate with the CSMU 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 St...

Page 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 data bits causing data corruption such as lost missing or scrambled data The MP PWA does not oper ate properly and may have corrupted data The CVDR does not operate properly and may have corrup ted dat...

Page 140: ...status 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 valid time stamp or date Timing Over Under Voltage 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 valid time stamp or date Timin...

Page 141: ...dio 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 the DSP No audio tone test or a con tinuous tone test is per formed No Effect B014 Analog Audio Tone Test 1 Audio I P Audio I P Tone Test 1 is open Audio CODEC is unable to re ceive record audio tone ...

Page 142: ...from 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 audio tone test or a con tinuous tone test is per formed No Effect B018 Analog Area MIC Audio HI Audio I P HI Analog Area MIC I P HI is open Inputs Channel 4 and the Area Microphone Channel HI both get p...

Page 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 and Pre Amp Power are shorted The output voltage is not disrupted and the system FPGA DAP softeware is not alerted The system softeware is unable to dis rupt this output via control pin from the FPG...

Page 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 is disrupted with the GSE UART1 TxD The UART1 TxD GSE is shorted There is no communication between the UART1 and the front panel RJ 45 GSE port The MP PWA has no GSE capability Communication is disr...

Page 145: ...le 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 Ether net In ter faces Ethernet The Ethernet Interface is open The ethernet MAC port fails to operate in full duplex modes The CVDR is unable to per form normally but still oper ates The CVDR is unab...

Page 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 Disrupted FDR Data Output ARINC 717 Low echoed back to the AI PWA Disrupted FDR Data Output ARINC 717 Low echoed back to the AI PWA Disrupted FDR Data Output ARINC 717 Low echoed back to the AI PWA Diff...

Page 147: ...e 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 may not be recorded stored or copied NOTE The corrup ted FPGA is erased and re placed 0002A SDRAM Non Volatile Memory Loss of Power All memory is lost The SRAM is unable to execute the sys tem s prog...

Page 148: ...e 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 be copied The CVDR initially does not operate Some data may be corrupt lost and or may not be recorded stored or copied NOTE The Flash Memory resets and is able to store data 0004A Connector J001 Co...

Page 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 CONDUCTIVE BAGS WHEN HANDLING OR STORING SYMBOL FOR ESD GROUND CONNECTING O ESD WARNING SYMBOL 2 RECORDER INDEPENDENT POWER SUPPLY RIPS MODULE The RIPS battery is an internal part of the RIPS When in...

Page 150: ...d 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 is required within one year after being recharged B 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 Insta...

Page 151: ...to 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 container is not available perform the following procedures to wrap the RIPS for storage Refer to Section B if the RIPS has been stored for one year or more 1 Wrap the RIPS in plain wrapping paper or ne...

Page 152: ...assis 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 A Underwater Locator Beacon Removal See IPL Figure 1 Item 150 All installation and testing tasks concerning the ULB are covered in detail in the 90 Day Underwater Locator Beacon Installation Operat...

Page 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 used to secure CSMU cable 1 120 connec tor to the MP PWA 1 45 and remove CSMU cable connector 3 Remove the the four screws 1 125 used to secure the CSMU 1 120 to the front chassis 1 95 4 Remove the C...

Page 154: ...SMU 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 captive screws 1 15 used to secure the rear cover 1 10 to the rear part of the Shielded Housing 1 5 2 Slide rear cover 1 10 straight back from recorder until the AI 1 25 and MP 1 45 PWAs separate at ...

Page 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 Removal 2 Remove the four screws 1 35 used to secure the Rear Connector J 1 to the back of the rear cover 1 10 3 Remove the six screws 1 30 used to secure the AI PWA 1 25 to the rear cover 1 10 4 Remove t...

Page 156: ...is 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 AI PWA Removal Diagram The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 157: ...pecification 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 obtained from any commercial source 3 CLEANING PROCEDURES WARNINGS 1 OBSERVE ALL FIRE PRECAUTIONS WHEN USING FLAMMABLE MATERIALS FOR CLEANING PURPOSES 2 PERFORM OPERATIONS INVOLVING CLEANING SOLVENT IN A...

Page 158: ...ing 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 film If necessary take the beacon out of the Beacon Mounting Bracket as shown in Figure 401 and wipe clean with approved cleaning agent and soft lint free cloth The water switch end insulator must be...

Page 159: ...s 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 Pattern Torquing Sequence 75 in lbs Figure 401 Underwater Locator Beacon The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 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 please check the correspondence between the online documentation and the printed version ...

Page 161: ...e 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 deterioration B Mechanical Inspection 3 Inspect all parts for cracks distortion excessive wear and proper finish 4 Inspect all cast parts for cracks especially at bosses flanges and other critical areas 5 In...

Page 162: ...acon 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 Operation Manu al L3AP P N 165E5542 10 and the 90 Day Underwater Locator Beacon CMM L3AP P N 165E5542 00 The beacon should be removed from service on or before the replacemen...

Page 163: ...ccordance 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 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 When it...

Page 164: ...losure 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 please check the correspondence between the online documentation and the printed version ...

Page 165: ...tures 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 Use 1 Adhesive Loctite Grade E Purple No 222 Lock sealant manufactured by Loctite Corp 705 N Mountain Rd Newington CT 06111 V05972 Retain screw 2 Torque Wrench L3 Technologies Aviation Products P N 930...

Page 166: ...gure 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 Assembly procedures begin with the Main Processor PWA installation then con tinue with the Aircraft Interface PWA installation CSMU installation and Underwater Acoustic Beacon installation B Aircraft Interf...

Page 167: ...igure 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 rear part of Shielded Housing 1 5 until the AI PWA 1 25 and MP PWA 1 45 connectors are fully seated NOTE Apply Loctite to all screw installations for the following proced ures 3 Install four captive scr...

Page 168: ...cle 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 guide the CSMU 1 120 cable thru the slot in the front chassis 1 95 NOTE Apply Loctite to all screw installations for the following proced ures 2 Install the four screws 1 125 used to secure the CSMU 1 ...

Page 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 NOTE 1 115 1 45 Qty 2 Memory Interface Cable Assembly 1 4 Pan Head Sealing Screws 1 125 Qty 4 CSMU Memory Assembly 1 120 1 130 Qty 2 1 95 REF Torque Sequence 75 in lb 1 4 2 3 Figure 703 Crash Surviva...

Page 170: ...ance 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 inspection servicing as it reaches one year of storage Refer to Section E Condition RIPS Module After Expired Shelf Life One Year in Storage B RIPS Module Connector Cover The FA5000 Connector Cover is to be ...

Page 171: ...elivered 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 connector 3 Remove protection cover from the CVDR connector Keep both the RIPS Con nector Cap and Connector Cover for future use 4 Line up the RIPS Module in the most rearward position while aligning the...

Page 172: ...this 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 1 year without application of power to the recorder when operated within this requirement no monitoring is required The RIPS battery is an on demand maintenance item and required main tenance will b...

Page 173: ...E 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 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 The...

Page 174: ...tainer 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 container is not available perform the following procedures to wrap the equipment for storage 1 Wrap the equipment in plain wrapping paper or newspaper of sufficient thick ness to thoroughly cover all sharp...

Page 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 Order Number F Customer Name F Contact Name and Phone Number F Ship To Address Instructions F Bill To Address Instructions F Desired Ship Date F Shipment Routing Carrier Account Number F Freight carr...

Page 176: ...77 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 Instructions F Bill To Address Instructions F Reason for Return F Shipment Routing Carrier Account Number F Freight carrier account number and special shipping instructions if necessary F Item Descripti...

Page 177: ...F 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 International shipments must be routed through L3 Aviation Products freight for warder in Orlando Florida Clearly mark paperwork with American Manufactured Goods Returned Email Transtrade notification of...

Page 178: ...t 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 NOTE Credit cards are accepted Purchases over 1 000 will incur a 2 fee The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 179: ...A 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 6 48 inches nominal Width 5 02 inches nominal front panel 12 6 inches nominal behind front panel Depth 13 1 inches nominal including hold down hooks Weight ULB installed 10 4 pounds for models 5003 5...

Page 180: ...ophone 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 for the most recent 30 minutes of recording 20 dB 10 distortion otherwise Greenwich Mean Time Input Data ARINC 429 Format CVR Input Signal Format ARINC 757 or 757A Rotor Speed Input Signal 2 Vrms to 1...

Page 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 Model FA5000 environmental characteristics E Torque Requirements Assembly Item Torque Requirement CSMU Beacon Bracket Mounting Screws 75 in lbs Rear Cover Screws Aircraft Interface PWA 9 10 in lbs J1 Co...

Page 182: ...riation 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 Fog 14 S Magnetic Effect 15 A Power Input 16 DC ZXX Voltage Spike 17 A Conducted Susceptibility 18 DC Z Induced Signal Susceptibility 19 ZC RF Radiated and Conducted Susceptibility 20 RR RF Radiated a...

Page 183: ...ubject 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 Cockpit Voice Recorder The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 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 of 2 Outline Dimension Drawing Model FA5000 Cockpit Voice Recorder The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 185: ...2 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 Assembly FA2100 CICC 2 2 ea 17TES0042 Cable Assembly Recorder Interface 17TES0057 Cable Assembly CVDR Interface 17TES0071 Cable Assembly F1000 CICC 2 17TES0321 Read Out System Equipment Software ROSE ...

Page 186: ...2 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 840E5447 03 4527 5003 5001 50 840E5447 05 FB91 5003 5001 50 840E5447 06 BDE7 5013 5000 30 840E5446 06 0C9D 5013 5001 50 840E5447 06 BDE7 Audio Data Link Player ADLP Software Part Number Description 17TES04...

Page 187: ...E 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 DC 5A USB BLUE GREEN SND IN SND OUT SPKRS OUT GSE INTFC REAR CONNECTOR INTFC J3 J6 J5 LIGHT LIGHT RIU DC POWER INPUT 17TES0412 DC J8 SOUND CARD POWER INPUT SELECT POWER LED ETHERNET CROSS OVER CABLE ...

Page 188: ...personal 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 hardware specifications for a PC running ADLP software are Dual Core Processor 1 56 Hz each 2 GB memory 4 3 GB EIDE Hard Drive Ethernet or Parallel Port EPP 12 or greater LCD Screen CD drive Type 2 PC...

Page 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 memory card or USB Flash Drive which then can be transferred into a ROC 7 that has the ADLP software installed for play back For detailed operational instructions refer to the Audio Data Link Player Sof...

Page 190: ...0 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 reference is online please check the correspondence between the online documentation and the printed version ...

Page 191: ...sonnel 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 Overhaul or repair should be done by authorized personnel only 3 ABBREVIATIONS The following abbreviations are used in this section Abbreviation Meaning AR As Required ASSY Assembly ...

Page 192: ...lustration 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 more than one type of subassembly for the same function addi tional figures are included with the same number but followed by an additional alpha des ignator such as A B etc Each part number listed in...

Page 193: ...es 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 lead times on each figure These units or assemblies are assigned reference letters such as A B C D etc Parts which are not common to all configurations but are associated with one or more of the coded ...

Page 194: ...Stainless 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 Conversion Kit P N 068E5542 00 These tests were conducted to ensure that the transition from the 30 day ULB to 90 Day ULB for CSMUs used on all Models of L3AP Recorders meet the requirements of DO 160G...

Page 195: ...isted 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 28 VDC ONLY NAND 5003 5001 50 ARINC 757A 2 HR GA CVR 1 2 ATR SHORT 28 VDC INTERNAL RIPS NAND 5013 5001 50 ARINC 757A 2 HR GA CVR 1 2 ATR SHORT 28 VDC ONLY 90 DAY ULB 5003 5000 01 ARINC 757 2 HR CVR 1 ...

Page 196: ...2 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 205E5044 02 DELETED 205E5044 07 1 45B 1 205E5044 30 1 45C 1 205E5170 03 DELETED 205E5170 04 1 25B 1 205E5170 08 1 25D 1 205E5170 10 1 25C 1 229E5161 00 1 15 6 2290200229 1 108 4 2290200072 1 130 2 2...

Page 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 5000 5000 00 1 DELETED RF 5000 5001 50 1 DELETED RF 5003 5000 00 1 1C RF 5003 5000 01 1 1E RF 5003 5001 50 1 1D RF 5013 5000 30 1 1F RF 5013 5001 50 1 1G RF 639805057 1 75 1 67666 SS 12A 1 85 2 765980...

Page 198: ...tions 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 Sheet 1 of 2 Model FA5000 5003 CVR Recorders The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 199: ...ictions 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 Sheet 2 of 2 Model FA5000 5003 CVR Recorders The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 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 E RF 1F 5013 5000 30 COCKPIT VOICE RECORDER NAND FA5000 CVR NICKEL PLATED REAR ARINC 757 90 DAY ULB F RF 1G 5013 5001 50 FA5000 CVR ARINC 757A 2 HR GA CVR 1 2 ATR SHORT 28 VDC ONLY 90 DAY ULB G RF 5 ...

Page 201: ...08 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 40B EFF E PER ECN 016337 C D E G 1 40B 230E5488 01 SEAL ARINC 404 CONNECTOR SUPSDS 40A EFF E PER ECN 016337 E F 1 41 016E5852 00 BRACKET EMI E F 1 45A 205E5044 02 Deleted 45B 205E5044 07 PWA MAIN PR...

Page 202: ...6OD 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 85 67666 SS 12A SCREW JACK 4 40X 25 X3 16 V06141 2299800474 2 86 7659800127 COVER DB25 HD44 EMI 1 90A 230E5490 00 GASKET D SUB CONDUCTIVE SUPSD BY 90B EFF E F PER ECN 016337 C D E F G 1 90B 230E5490 0...

Page 203: ...0200362 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 Deleted 120B 253E5851 00 CRASH SURVIVABLE MEMORY 4 GIG SS C D G 1 120C 253E5851 01 CRASH SURVIVABLE MEMORY TITANIUM SUPSD BY 120E PER ECN 016337 E 1 120D 253E5851 02 CRASH SURVIVABLE MEMORY 4 GIG SS...

Page 204: ...T 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 PAD CSMU CONNECTOR SEAL 1 140 016E1589 00 BRACKET BEACON MOUNT 2 ATTACHING PARTS 145 MS16995 54 SCREW SCHCAP 1 4 20 X 1 1 2 V06141 2290200424 4 The document reference is online please check the corr...

Page 205: ...147E0305 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 ACOUSTIC UNDERWATER SUPSD BY 150D PER SB004 DUKANE V94970 ELP 362D FOR BATTERY REPLACEMENT ORDER 30 DAY BATTERY KIT 147E0305 00 C D E 1 150D 266E5542 00 BEACON 90 DAY UNDERWATER LOCATOR BEACON DUKAN...

Page 206: ...e 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 reference is online please check the correspondence between the online documentation and the printed version ...

Page 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 online please check the correspondence between the online documentation and the printed version ...

Page 208: ...t 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 INDEPENDENT POWER SUPPLY RIPS RF The document reference is online please check the correspondence between the online documentation and the printed version ...

Page 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 online please check the correspondence between the online documentation and the printed version ...

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