L3 Aviation Products FA2100 CVR Installation/Operation Instruction Manual Download

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Model FA2100 CVR

Instruction Manual

Installation & Operation

Rev. 07
Jan. 01/03

165E1846–00

Page A–43

ÉÉÉÉ

ÉÉÉ

1.625

ÉÉÉ

ÅÅ

2.02

1.625

93–CVR117B

2.02

6–32

TAPPED

HOLE

4 PLACES

2.00

DIA.

2.56

0.25

1.20

MAX.

2.87

CANNON TM–RB1–M–0
TWINAX RECEPTACLE

CONFIGURATION/

NAMEPLATE

NOTES:

MATING PLUGS FOR SPECIFIED RECEPTACLE ARE

CANNON TM–PL–F–39 OR TM–PL2–F–39.

COMPANY LOGO

DIMENSIONS ARE IN INCHES.

Part Number

Panel Color

Microphone Type

Weight

(

0.1 lbs.)

93A055–10

Black

Condenser

0.5 lbs.

93A055–30

Brown, Boeing

Condenser

0.5 lbs.

93A055–50

Black

Non-Magnetic

0.5 lbs

Figure A–31.

Outline and Dimensions, Model A55B Panel-Mount Microphone Module, Rear Connector

Does Not Comply with ED–56A

Summary of Contents for FA2100 CVR

Page 1: ...orida 34230 CAGE Code 06141 RECORDER PART NUMBERS 2100 1010 00 2100 1020 00 2100 1020 02 2100 1020 90 2100 1020 91 2100 1020 93 CONTROL UNIT MODEL NUMBERS S151 S161 S152 S162 S251 S261 A151B A152B MICROPHONE PREAMPLIFIER S150 S160 MODULE MODEL NUMBERS A150 REMOTE MICROPHONE S055 S056 MODEL NUMBERS A55B Manufactured in Accordance with FAA TSO C123a EUROCAE ED 56A ARINC 757 P N 165E1846 00 ...

Page 2: ...orida 34230 941 371 0811 FAX 941 377 5591 CAGE Code 06141 This manual contains date sensitive information necessary to install recorders in aircraft Contact L 3 Communications Aviation Recorders to verify this date sensitive information prior to using this manual to develop other documentation The recorder products software are being exported from the United States in accordance with the Export Ad...

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

Page 4: ...Model FA2100 CVR Instruction Manual Installation Operation Page iv Jan 01 03 165E1846 00 Rev 07 THIS PAGE IS INTENTIONALLY LEFT BLANK ...

Page 5: ...solidated the Appendixes 02 May 01 00 Added 2100 1020 93 configuration and S160 S161 and S161 Control Units 03 Oct 01 00 Added 2100 1020 90 and S056 Microphone 04 Mar 01 01 Clarified when the Audio System Check is reĆ quired 05 Aug 15 01 Fixed Control Unit drawings to seperate the S151 drawing from the S161 drawing and the S152 drawing from the S162 drawing in AppenĆ dix A Clarified GMT FSK operat...

Page 6: ...Model FA2100 CVR Instruction Manual Installation Operation Page vi Rev 07 Jan 01 03 165E1846 00 THIS PAGE IS INTENTIONALLY LEFT BLANK ...

Page 7: ...onyms 7 2 0 EQUIPMENT LIMITATIONS SPECIFICATIONS 7 2 1 Applicable Documents 7 2 2 Physical Characteristics 8 2 3 Electrical Characteristics 8 2 4 Environmental Characteristics 13 2 5 Crash and Fire Survival Characteristics 13 3 0 INSTALLATION PROCEDURES AND LIMITATIONS 13 3 1 Installation Precautions 13 3 2 General Information 13 3 3 Installation Acceptance by Field Approval Method 14 3 4 Recorder...

Page 8: ...TING INSTRUCTIONS 21 8 0 FLIGHT CHECKOUT PROCEDURE 21 8 1 Operational Notes 21 8 2 Flight Checkout 21 9 0 MAINTENANCE AND CALIBRATION 23 9 1 Recorder 23 9 2 Underwater Locator Device 23 9 3 Product Support 23 9 4 Authorized Repair Facilities 23 9 5 Loaner Rental Program 23 Appendixes Appendix Page A OUTLINE DIMENSIONS MICROPHONES CONTROL UNITS EXTERNAL PREAMPLIFIERS A 1 B ENVIRONMENTAL QUALIFICATI...

Page 9: ...ions Model S161 Control Unit A 7 A 5 Interwiring Diagram FA2100 Recorder S161 Control Unit S056 Remote Microphone A 8 A 6 Outline and Dimensions Model S251 Control Unit A 10 A 7 Interwiring Diagram FA2100 Recorder S251 Control Unit S055 Remote Microphone A 11 A 8 Outline and Dimensions Model S261 Control Unit A 13 A 9 Interwiring Diagram FA2100 Recorder S261 Control Unit S056 Remote Microphone A 1...

Page 10: ...52B Control Unit with Internal Microphone Such Installations Do Not Comply with ED 56A A 36 A 27 Outline and Dimensions Model A150 External Preamplifier Module Does Not Comply with ED 56A A 38 A 28 Interwiring Diagram FA2100 Recorder A150 External Preamplifier A55B Remote Microphone Such Installations Do Not Comply with ED 56A A 39 A 29 Outline and Dimensions Model A55B Surface Mount Directional M...

Page 11: ...mendations about the installation operation and check out of the FA2100 CVR should be sent to L 3 Communications Aviation Recorders Product Support Department at the address shown in section 9 3 1 2 Equipment and Document Requirements The following equipment and documents are or may be required for on aircraft installation and check out of these FA2100 CVRs F This Installation Operation Instructio...

Page 12: ...lbs 2100 1020 90 ARINC 404A 1 2 ATR Short Case ARINC 757 120 Minutes Military 10 0 lbs 2100 1020 91 ARINC 404A 1 2 ATR Short Case ARINC 757 120 Minutes w INSITU Playback 10 0 lbs 2100 1020 93 ARINC 404A 1 2 ATR Short Case ARINC 757 120 Minutes w 8 ohm output and no Bulk Erase when used with 93A152 16 Control Unit 10 0 lbs 1 Weight is with Underwater Locator Device installed 1 4 1 Recorder Unit The...

Page 13: ...t Area Microphone CAM Input Part Number 2100 1020 records a fifth internal audio stream for a minimum of 120 minutes This fifth internal audio stream is a standard quality recording of the combination of the Pilot Co Pilot and Public Address or Third Crew Member audio inputs Part Number 2100 1020 also records a sixth audio stream a standard quality recording of the Cockpit Area Microphone CAM audi...

Page 14: ...OL UNIT CHANNEL 1 CHANNEL 4 CHANNEL 2 CHANNEL 3 AIRCRAFT INTERFACE PWA 18 VDC OPERATING POWER MONITOR AUDIO TO HEADSET JACK AREA MICROPHONE 2 2 2 2 2 2 ACQUISITION PROCESSOR PWA CSMU Crash Survival Memory Unit ASSEMBLY CRASH PROTECTED SOLID STATE MEMORY TO AIRCRAFT FAULT MONITORING SYSTEM GSE OUTPUT COCKPIT AREA MICROPHONE CAM 4 STOP RECORDING AUDIO COMPRESSOR PWA FA2100 CVR CVR FAULT TO GROUND ST...

Page 15: ...ction via a green push button and an indicator Bulk Erasure of the FA2100 CVR storage media is also accomplished by pressing the Control Unit s red Bulk ERASE push button All Control Units contain a headset jack for verifying system operation The Model S151 S161 Model S152 S162 and the Model S251 S261 Control Units are for use in FA2100 CVR ARINC 757 ED 56A System installations The Model S151 and ...

Page 16: ...older Part Number MS3111F 8 3P For Model S160 and A150 External Preamplifier 19 Pin Solder Part Number 063 98 01897 3 Pin Solder Part Number 063 98 01898 1 4 3 Remote Microphone Module The Model S055 and Model S056 Remote Microphone Modules are available to complete an ED 56A compatible installation The Model S055 Microphone is required with the S151 and S251 Control Units and with the S150 Preamp...

Page 17: ...ic 404A Aeronautical Radio Inc Air Transport Equipment Cases and Racking ARINC Characteristic 757 Aeronautical Radio Inc Cockpit Voice Recorder ARINC Report 604 1 Aeronautical Radio Inc Design Guidance for Design and Use of Built In Test Equipment ARINC Report 624 1 Aeronautical Radio Inc Design Guidance for Onboard Mainte nance System EUROCAE MOPS ED 55 European Organization for Civil Aviation Eq...

Page 18: ...r Compatible with ARINC 757 Part Number 063E1072 00 Cannon Part Number DPXB 36571 59 Main Rear Mating Connectors Crimp Part Number 063 98 01474 Cannon Part Num ber DPXBMA 57 33S 0001 Solder Part Number 9300 435 Cannon Part Number DPXB 57 33S 0001 Ground Support Equipment Connector Part Number 063 98 01962 AMP Part Number 748481 6 1 Weight is with Underwater Locator Device installed 2 3 Electrical ...

Page 19: ...hen repro duced 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 Rotor Speed Input Signal 2 Vrms to 122 Vrms from 7 to 6000 Hz per ARINC 757 Discrete Inputs Bulk Erase 2 discrete inputs Erase A Erase C Push to Test 1 discrete Record On 2 discrete inputs Stop Recording 1 discrete Digital Outputs CVR Fault 1 ...

Page 20: ...WEIGHT POWERS ARE MAXIMUMS AND WEIGHTS ARE NOMINAL WITH 1 RECORDER COLOR IS INTERNATIONAL ORANGE NO 12197 PER FED STD 595 FRONT AND SIDE LABELS ARE REFLECTIVE WHITE BACKGROUND WITH BLACK LETTERING NAMEPLATE IN VIEW A A HAS LIGHT GRAY BACKGROUND WITH BLACK MARKING 5 LBS TOLERANCE 4 OVERALL EQUIPMENT SIZE AND MOUNTING SCHEME COMPLY WITH ARINC 404 AND 404A REAR PANEL CONTAINS HOLES TO MATE WITH GUIDE...

Page 21: ... NUMBERS PN 063 E1072 00 CANNON DPBX 36571 59 MATING CONNECTORS CRIMP PN 063 98 01474 CANNON DPXBMA 57 33S 0001 SOLDER PN 9300 435 CANNON DPXB 57 33S 0001 4 88 04 5 5 2 4 12 4 98 04 CRASH SURVIVABLE MEMORY UNIT UNDERWATER LOCATING DEVICE GROUND SUPPORT EQUIPMENT CONNECTOR AMP 748481 6 4 063 98 01962 2100 1010 00 H 2100 1020 00 G 01 REPLACEMENT DATE Figure 3 Sheet 2 of 2 Outline Dimensions FA2100 C...

Page 22: ...E RAILS TABS FLANGES AND WEIGHT REDUCING HOLES MAY VARY PICTORIALLY FROM THIS DRAWING 2 WEIGHT 1 3 LBS MAX 3 CONNECTOR MOUNTING HOLE IS DESIGNED FOR CRIMP PN 063 98 01474 CANNON DPXBMA 57 33S 0001 SOLDER PN 9300 435 CANNON DPXB 57 33S 0001 4 SUGGESTED MOUNTING HARDWARE TO ATTACH CONNECTOR TO MOUNT 8 EACH 4 40 X 7 16 PAN HEAD SCREWS PN 229 02 00076 MS51957 16 OR EQUIV AND 4 40 SELF LOCKING NUTS PN ...

Page 23: ...isdiction of the FAA or other certifying authority before beginning recorder installation Refer to the following statement which was extracted from FAA TSO C123a The conditions and tests required for TSO approval of this article are minimum perfor mance standards It is the responsibility of those desiring to install this article either on or within a specific type or class of aircraft to determine...

Page 24: ...the recommended locations identified in FAA Advisory Circular 25 1457 1A and in accordance with the instructions contained in this Installation Manual The applicant should submit all appropriate data and drawings to the inspector before the installation of the Cockpit Voice Recorder Any deviations to the installation instructions contained in this Installation Manual must be brought to the inspect...

Page 25: ...nterface The FA2100 CVR is used in an ARINC 757 configuration with interface to the aircraft provided through a 57 pin DPXB rear panel connector The range of acceptable audio input levels for the Model FA2100 CVR is from 50 mVrms to 3 Vrms Nominal audio level input is 1 Vrms The Model FA2100 CVR provides for four audio inputs which are connected as follows Channel 1 Cockpit Spare Audio Input 3rd C...

Page 26: ...n illustration of the preferred placement for the Cockpit Area Microphone Ensure that the microphone is mounted such that the exposed portion of the microphone element is unobstructed 3 3 1 2 2 RECOMMENDED MICROPHONE LOCATIONS ARE NUMBERED IN ORDER OF PREFERENCE Figure 5 Recommended Cockpit Area Microphone Mounting Location 3 10 Cessation of Recording Federal Air Regulations 23 1457 d 2 25 1457 d ...

Page 27: ...onsideration 1 Before applying power to the FA2100 CVR System and associated components verify that all connections are secure and that a continuity or other interconnect assurance test has been con ducted 2 Apply power to the system and activate the FA2100 CVR s self test To activate self test press and hold the green TEST button for a minimum of five seconds 3 For installations containing a Mode...

Page 28: ... as FSK audio mixed with channel 1 or 3 with the 2100 1020 02 recorder NOTE The PI does not display ARINC 429 GMT or rotor speed in the Monitor Mode This can only be done with the PI in the Playback Mode 6 The Bulk Erase function can occur only when the aircraft is resting on its landing gear After pressing and holding the Control Unit s bulk ERASE push button for a minimum of 2 se conds release i...

Page 29: ... of recorder used the FA2100CVR s recorded data can be copied one channel at a time or all of the individual channels can be copied simultaneously 2 FSK output for recorded GMT and or Rotor Speed audio signal 3 Analog outputs for recorded voice data PI AUX READOUT CABLE 17TES00521 2 TO RECORDER GSE CONNECTOR PI AUDIO READOUT CABLE 17TES0051 1 3 DATA FROM RECORDER ROTOR GMT PORTABLE INTERFACE PI 17...

Page 30: ... Audio Boom Mask and Hand Held Microphone Input Channel 3 Pilot s Audio Boom Mask and Hand Held Microphone Input Channel 4 Cockpit Area Microphone CAM Input 1 Connect the PI to the FA2100 CVR s GSE connector as shown in Figure 6 2 Using the PI s SELECT button activate the Monitor Menu and turn HQ VOICE CH 1 ON While someone is speaking into the Channel 1 source verify that the audio is clear and d...

Page 31: ... mind that to obtain a satisfactory recording on the area microphone channel clear enunciation in a natural voice is essential 8 1 Operational Notes Depending on its part number the FA2100 CVR will preserve 30 or 120 minutes of recorded information A test program not exceeding 30 or 120 minutes of recording time depending on recorder version should be planned prior to the test flight The FA2100 CV...

Page 32: ...hone and the hand held microphone d Open FA2100 CVR circuit breaker 4 Descent Touchdown and Rollout a Close FA2100 CVR circuit breaker b At an appropriate altitude accelerate until Mmo or Vmo clacker sounds and identify reduce speed approximately 5 knots so that clacker stops Hold this speed and have crew member identify flight status via the area microphone to acquire a reasonable amount of recor...

Page 33: ... Sarasota Florida 34230 3041 Attention Product Support Mail Stop 20 Telephone 941 371 0811 Telefax 941 377 5591 SITA SRQLFCR Web Site www L 3ar com 9 4 Authorized Repair Facilities Aviation Recorders performs repair and readout services for the Model FA2100 CVR System Items needing repair should be shipped to the following address L 3 Communications Aviation Recorders 6000 East Fruitville Road Sar...

Page 34: ...Model FA2100 CVR Instruction Manual Installation Operation 165E1846 00 Jan 01 03 Rev 07 Page 24 THIS PAGE IS INTENTIONALLY LEFT BLANK ...

Page 35: ...Model FA2100 CVR Instruction Manual Installation Operation Rev 07 Jan 01 03 165E1846 00 Page A 1 APPENDIX A OUTLINE DIMENSIONS MICROPHONES CONTROL UNITS EXTERNAL PREAMPLIFIERS ...

Page 36: ...Model FA2100 CVR Instruction Manual Installation Operation Jan 01 03 Rev 07 Page A 2 165E1846 00 THIS PAGE IS INTENTIONALLY LEFT BLANK ...

Page 37: ...0030 00 S162 0040 00 S251 1120 00 S251 1130 00 S251 1170 00 S261 1120 00 S261 1130 00 Panel Thickness 25 Illuminated Non Illuminated Gray Black Brown Boeing Brown ATR Blue DO328 Gray BD100 Reqs S055 Microphone COLOR Note 01 version is used with 8ĆOhm 0 21 inch Headphone Jack J2 Reqs S056 Microphone D type Connector Circular Connector Filtered Connector Non Filtered Connector Attenuated Output Pane...

Page 38: ... SWITCH GREEN LAMP RECORDER COCKPIT VOICE AND MODIFICATIONS 1 125 002 000 030 5 375 015 FILTERED RECEPTACLE MS3112E20 41P 41ĆPIN CIRCULAR 2 11 07 3 00 2 50 1 05 KEYWAY 000 020 905 E1019 18K 12 communications Sarasota Florida PNR S151 XXXX XX SER XXXXXXXXX MFR 06141 TSO C123a ED 56A MODIFICATIONS 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 DATE MMYYYY CONTROL UNIT MODEL S151 2D BAR CODE Figure A 2 Outline ...

Page 39: ...52 53 54 55 56 57 5 AMPS TO DC POWER IN 28 VDC BRAKE GEAR BULK ERASE INTERLOCK TYPICAL INPUT CHANNEL 3 INPUT CHANNEL 2 INPUT CHANNEL 1 INPUT CHANNEL 4 COCKPIT AREA MICROPHONE VOICE RECORDER UNIT STANDARD INTERWIRING PER ARINC SPEC 757 MODEL S151 CONTROL UNIT TO AC COLD TO 115 VAC 400 HZ 1 AMP 2 8 3 4 3 3 7 8 6 9 10 10 11 10 11 OR 115 VAC POWER IN HOT 115 VAC POWER IN COLD PREAMP PWR OUT GND PREAMP...

Page 40: ...s 7 Twisted shielded cable Shields to be grounded at the recorder using short connections 8 If the power source has battery back up a means for terminating recording after a crash should be included in the aircraft wiring Grounding pin 10 terminates recording within 10 minutes 9 BITE status output ground no fault open fault or CVR not installed 10 Audio input 05 Vrms 3 Vrms maximum 1Vrms nominal 1...

Page 41: ...CORDER AND MODIFICATIONS 1 125 005 000 030 5 365 005 FILTERED RECEPTACLE MS3112E20 41P 41ĆPIN CIRCULAR 2 10 MAX 3 00 2 50 1 04 000 020 905 E2367 18A 12 STATIC ALERT LABEL FARSIDE SWITCH SWITCH GREEN LAMP communications Sarasota Florida PNR S161 XXXX XX SER XXXXXXXXX MFR 06141 TSO C123a ED 56A MODIFICATIONS 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 DATE MMYYYY CONTROL UNIT MODEL S161 2D BAR CODE Figure A...

Page 42: ...9 50 51 52 53 54 55 56 57 5 AMPS TO DC POWER IN 28 VDC BRAKE GEAR BULK ERASE INTERLOCK TYPICAL INPUT CHANNEL 3 INPUT CHANNEL 2 INPUT CHANNEL 1 INPUT CHANNEL 4 COCKPIT AREA MICROPHONE VOICE RECORDER UNIT STANDARD INTERWIRING PER ARINC SPEC 757 MODEL S161 CONTROL UNIT TO AC COLD TO 115 VAC 400 HZ 1 AMP 2 8 3 4 3 3 7 8 6 9 10 10 11 10 11 OR 115 VAC POWER IN HOT 115 VAC POWER IN COLD PREAMP PWR OUT GN...

Page 43: ...pins 7 Twisted shielded cable Shields to be grounded at the recorder using short connections 8 If the power source has battery back up a means for terminating recording after a crash should be included in the aircraft wiring Grounding pin 10 terminates recording within 10 minutes 9 BITE status output ground no fault open fault or CVR not installed 10 Audio input 05 Vrms 3 Vrms maximum 1Vrms nomina...

Page 44: ...8 2 50 47 28 905 E1120 18L COCKPIT VOICE RECORDER TEST HOLD 5 SEC HEADSET 1 125 562 5 375 5 75 188 GREEN LAMP SWITCH SWITCH ERASE NAME PLATE AND MODIFICATIONS STATIC ALERT LABEL FARSIDE communications Sarasota Florida PNR S251 XXXX XX SER XXXXXXXXX MFR 06141 TSO C123a ED 56A MODIFICATIONS 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 DATE MMYYYY CONTROL UNIT MODEL S251 2D BAR CODE Figure A 6 Outline and Dim...

Page 45: ...TO TEST TEST INDICATOR TEST INDICATOR CHASSIS GND CVR FAULT GMT IN 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 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 PUSH TO TEST PREAMP PWR GND PREAMP P...

Page 46: ...corder using short connections 7 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 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 Notice A8300 56 dated Jan 24 1990 the wirin...

Page 47: ... HEADSET 1 13 5 75 GREEN LAMP SWITCH SWITCH ERASE OR communications Sarasota Florida PNR S261 1130 00 SER XXXXXXXXX MFR 06141 TSO C123a ED 56A MODIFICATIONS 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 DATE MMYYYY CONTROL UNIT MODEL S261 2D BAR CODE STATIC ALERT LABEL FARSIDE communications Sarasota Florida PNR S261 1120 00 SER XXXXXXXXX MFR 06141 TSO C123a ED 56A MODIFICATIONS 1 2 3 4 5 6 7 8 9 10 11 12 1...

Page 48: ...DING PUSH TO TEST TEST INDICATOR TEST INDICATOR CHASSIS GND CVR FAULT GMT IN 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 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 PUSH TO TEST PREAMP PWR GN...

Page 49: ...recorder using short connections 7 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 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 Notice A8300 56 dated Jan 24 1990 the wir...

Page 50: ...ODIFICATIONS 1 125 005 000 030 5 365 005 FILTERED RECEPTACLE MS3112E20 41P 41ĆPIN CIRCULAR 2 10 MAX 3 00 2 50 1 04 000 020 905 E1926 18B 12 SWITCH SWITCH GREEN LAMP ÍÍÍ ÍÍÍ ÍÍÍ MICROPHONE communications Sarasota Florida PNR S152 00X0 X0 SER XXXXXXXXX MFR 06141 TSO C123a ED 56A MODIFICATIONS 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 DATE MMYYYY CONTROL UNIT MODEL S152 2D BAR CODE STATIC ALERT LABEL FARSI...

Page 51: ...ODIFICATIONS 1 125 005 000 030 5 365 005 FILTERED RECEPTACLE MS3112E20 41P 41ĆPIN CIRCULAR 2 10 MAX 3 00 2 50 1 04 000 020 905 E2387 18A 12 SWITCH SWITCH GREEN LAMP ÍÍÍ ÍÍÍ ÍÍÍ MICROPHONE communications Sarasota Florida PNR S162 00XX 00 SER XXXXXXXXX MFR 06141 TSO C123a ED 56A MODIFICATIONS 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 DATE MMYYYY CONTROL UNIT MODEL S162 2D BAR CODE STATIC ALERT LABEL FARSI...

Page 52: ...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 1 LO CHANNEL 1 HI CHANNEL 2 LO CHANNEL 2 HI CHANNEL 3 LO CHANNEL 3 HI 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 PUSH TO TEST PREAMP P...

Page 53: ... not grounded in the recorder 6 Pins p q and r may be jumpered The control unit does not use these pins 7 Twisted shielded cable Shields to be grounded at the recorder using short connections 8 If the power source has battery back up a means for terminating recording after a crash should be included in the aircraft wiring Grounding pin 10 terminates recording within 10 minutes 9 BITE status output...

Page 54: ... 528 020 236 020 236 020 5 000 030 1 968 020 2 746 030 389 020 3 937 030 531 020 1 727 030 860 020 1 778 020 3 378 020 2X 125 020 905 E0986 18D Part Number Housing Color Weight 0 1 lbs S150 0020 00 Black 0 7 lbs communications Sarasota Florida PNR S150 0020 00 SER XXXXXXXXX MFR 06141 TSO C123a ED 56A MODIFICATIONS 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 DATE MMYYYY PREAMPLIFIER MODEL S150 2D BAR CODE ...

Page 55: ...EAMPLIFIER 4 3 3 6 COCKPIT AREA MICROPHONE PREAMP PWR 18 VDC REGULATED 7 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...

Page 56: ...tery 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 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 Notice A8300 56 dated Jan 24 1990 the wiring to Channels 1 and 3 may be transposed that is Channel 1 wi...

Page 57: ...23 4 99 1 97 2 74 39 3 92 54 020 1 75 2X 1 00 1 78 05 3 38 05 06 S160 0020 00A Part Number Housing Color Weight 0 1 lbs S160 0020 00 Black 0 65 lbs SOURIAU SOURIAU communications Sarasota Florida PNR S160 0020 00 SER XXXXXXXXX MFR 06141 TSO C123a ED 56A MODIFICATIONS 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 DATE MMYYYY PREAMPLIFIER MODEL S160 2D BAR CODE Figure A 15 Outline and Dimensions Model S160 Ex...

Page 58: ...KPIT AREA MICROPHONE PREAMP PWR 18 VDC REGULATED 7 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...

Page 59: ...attery 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 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 Notice A8300 56 dated Jan 24 1990 the wiring to Channels 1 and 3 may be transposed that is Channel 1 ...

Page 60: ...OTES 1 MIC SHIELD OUTER SHIELD PIGTAIL YELLOW PIGTAIL GREEN LENGTH MINIUM 2 DIMENSIONS ARE IN INCHES SEE CHART FOR MICROPHONE MODEL S055 PNR S055 00XX 00 SER XXXXXXXXXX MFR 06141 DMF MMYYYY TSO C123a ED 56A 2D BAR CODE communications Sarasota Florida USA NAMPLATE INFORMATION Part Number Housing Color Weight 0 1 lbs Minimum Cable Lenght S055 0064 00 Gray BD 100 0 2 lbs 17 S055 0065 00 Gray No 36116...

Page 61: ...TING PLUGS FOR SPECIFIED RECEPTACLE ARE CANNON TM PL F 39 OR TM PL2 F 39 COMPANY LOGO INDICATED PORTION OF MICROPHONE MUST BE UNOBSTRUCTED FOR PROPER OPERATION DIMENSIONS ARE IN INCHES 2 3 MICROPHONE MODEL S055 PNR S055 0030 00 SER XXXXXXXXXX MFR 06141 DMF MMYYYY TSO C123a ED 56A 2D BAR CODE communications Sarasota Florida USA NAMPLATE INFORMATION Part Number Panel Color Weight 0 1 lbs S055 0030 0...

Page 62: ...ndicated portion of microphone must be unobstucted for proper operation 1 2 Dimensions are in inches 905 E1771 18G MICROPHONE MODEL S056 PNR S056 00XX 00 SER XXXXXXXXXX MFR 06141 DMF MMYYYY TSO C123a ED 56A 2D BAR CODE communications Sarasota Florida USA NAMPLATE INFORMATION Part Number Housing Color Weight 0 1 lbs S056 0047 00 Gray No 36118 0 2 lbs S056 0048 00 Black No 37038 0 2 lbs S056 0049 00...

Page 63: ...per operation 1 2 Dimensions are in inches 905 E1838 18D MICROPHONE MODEL S056 PNR S056 1048 00 SER XXXXXXXXXX MFR 06141 DMF MMYYYY TSO C123a ED 56A 2D BAR CODE communications Sarasota Florida USA NAMPLATE INFORMATION Part Number Panel Color Weight 0 1 lbs S056 1048 00 Black 0 2 lbs Figure A 20 Outline and Dimensions Model S056 Panel Mount Microphone Module ...

Page 64: ... RESP REFER TO CHART ELEMENT CAPACITANCE 17pF 1 kHz CAPACITANCE PIćFILTER 4000pF 20 100 WVDC WORKING VOLTAGE 10 VDC MAX OUTPUT LEVEL 1 kHz SENSITIVITY 7 TO 17 5 mV 11 mV NOM 100dB SPL WITH A 16 9 kOHM LOAD RESISTOR 1 kHz 5 FEET DIMENSIONS SEE DRAWING SPECIAL FEATURE CARDIOID POLAR RESPONSE SHELL BRASS COLOR BLACK COLOR 27038 PER FEDĆSTDĆ595 Used On Remote Mic Part Numbers S055 0065 00 S055 0066 00...

Page 65: ...O CHART OUTPUT LEVEL 155mV NOMINAL 4dB AT 1KHz 94dB SPL AT 1 METER DIMENSIONS SEE DRAWING ABOVE SPECIAL FEATURE CARDIOID POLAR RESPONSE CABLE TEFLON INSULATED SHIELDED 2 COND 22 GAGE STRANDED ONE WHITE ONE BLACK WITH A WHITE OUTER JACKET MICROPHONE COLOR BLACK Used On Remote Mic Part Numbers S056 0047 00 S056 0048 00 S056 0049 00 S056 0050 00 S056 1048 00 0 180 270 90 30 60 120 210 240 300 330 1 8...

Page 66: ... 12 PART PANEL METER NUMBER COLOR ILLUMINATION 93A151 20 Gray None 93A151 30 Black None 93A151 40 Brown Boeing None 93A151 50 Brown ATR 42 None 93A151 60 DO328 BLUE 28V 93A151 70 DO328 BLUE None 1 125 002 5 37 NOTES 1 WEIGHT 0 9 LBS 0 1 lbs 2 DIMENSIONS ARE IN INCHES METER PLUG BUTTON RECEPTACLE 93 CVR120C NAMEPLATE AND MODIFICATIONS KEYWAY WITH CONFIG AS REQ D Figure A 23 Outline and Dimensions M...

Page 67: ... ERASE SWITCH A ERASE SWITCH C OUTPUT LOW OUTPUT HIGH MIKE CABLE SHIELD MIKE INPUT HI MIKE INPUT LO FILTER COMMON FILTER 1 000 HZ AUDIO JACK LO AUDIO JACK HI 6 DB ATTENUATION ATTENUATOR_ COMMON 12 DB ATTENUATION 24 DB ATTENUATION MIC OUTPUT HI AUDIO MIC OUTPUT LO DC IN MIC SHIELD CONNECTOR SHELL 1 AMP TO 115 VAC HOT 400HZ TO AC COLD 5 AMPS 3 A B C D E F G H J K L M N P R S T U V W X Y Z a b c d e ...

Page 68: ...ble Shields to be grounded at the recorder using short connections 8 If the power source has battery back up a means for terminating recording after a crash should be included in the aircraft wiring Grounding pin 10 terminates recording within 10 minutes 9 BITE status output ground no fault open fault or CVR not installed 10 Audio input 05 Vrms 3 Vrms maximum 1Vrms nominal 11 Per FAA Action Notice...

Page 69: ...NEL METER NUMBER COLOR ILLUMINATION 93A152 20 Gray None 93A152 25 Gray None 93A152 30 Black 28V 93A152 35 Gray 28V 93A152 40 Gray 5V 93A152 50 Brown ATR 42 None 93A152 60 Brown ATR 42 5V 93A152 70 Black None 1 125 002 5 37 NOTES 1 WEIGHT 1 2 LBS 0 15 LBS 2 DIMENSIONS ARE IN INCHES MS3112Ć20Ć41P RECEPTACLE KEYWAY METER 93 CVR119B NAMEPLATE AND MODIFICATIONS WITH CONFIG AS REQ D Figure A 25 Outline ...

Page 70: ... INDICATOR 16 INDICATOR 17 CHASSIS GROUND 18 19 20 21 22 23 CVR FAULT 24 25 GMT IN B ARINC 429 LO 26 GMT IN A ARINC 429 HI 27 28 29 30 LO 31 CHANNEL 1 32 HI 33 34 35 LO 36 CHANNEL 2 37 HI 38 DATA RATE B 39 40 41 LO 42 CHANNEL 3 43 HI 44 45 LO 46 CHANNEL 4 47 HI 48 ROTOR SPEED IN LO 49 ROTOR SPEED IN HI 50 51 52 53 54 55 ERASE A 56 57 ERASE C BRAKE GEAR 5 AMPS 3 A B C D E F G H J K L M N P R S T U ...

Page 71: ...d shielded cable Shields to be grounded at the recorder using short connections 8 If the power source has battery back up a means for terminating recording after a crash should be included in the aircraft wiring Grounding pin 10 terminates recording within 10 minutes 9 BITE status output ground no fault open fault or CVR not installed 10 Audio input 05 Vrms 3 Vrms maximum 1Vrms nominal 11 Per FAA ...

Page 72: ...SOURIAU 8525 10R 8B 3ASN SOURIAU 8525 10R 14B 19SN 3 947 MAX 1 05 1 75 2X 0 12 0 24 NOTES 1 DIMENSIONS ARE IN INCHES AND MODIFICATIONS 93 CVR104D 0 54 04 1 78 05 3 38 05 Part Number Housing Color Weight 0 1 lbs 93A150 20 Black 0 65 lbs Figure A 27 Outline and Dimensions Model A150 External Preamplifier Module Does Not Comply with ED 56A ...

Page 73: ...1 52 53 54 55 ERASE A 56 57 ERASE C PRE AMP POWER 18 VDC PRE AMP POWER GND PRE AMP OUT HI PRE AMP OUT LO ATTENUATION MASTER CHASSIS GROUND 24 DB ATTENUATION 12 DB ATTENUATION 6 DB ATTENUATION 1 AMP TO 115 VAC HOT 400HZ TO AC COLD 5 AMPS 3 A B C D E F G H J K L M A B C 1 2 3 3 7 TO 27 5VDC MODEL A150 EXTERNAL PREAMPLIFIER MODEL A55B MICROPHONE COCKPIT AREA MICROPHONE 2 8 OR VOICE RECORDER UNIT FROM...

Page 74: ...7 Twisted shielded cable Shields to be grounded at the recorder using short connections 8 If the power source has battery back up a means for terminating recording after a crash should be included in the aircraft wiring Grounding pin 10 terminates recording within 10 minutes 9 BITE status output Ground no fault Open fault or CVR not installed 10 Audio input 05 Vrms 3 Vrms maximum 1Vrms nominal 11 ...

Page 75: ...ÉÉÉÉ ÉÉÉÉ ÉÉÉÉ ÉÉÉÉ 1 09 ÉÉÉ ÉÉÉ ÉÉÉ ÉÉÉ ÅÅÅ ÅÅÅ ÅÅÅ 1 19 64 FOAM DAMPER 84 DIA c L 1 NOTES 2 DIMENSIONS ARE IN INCHES 2 25 CONFIG P N 1 12 LEVEL 30 1 0 50 FOR PART NOS 93A055 60 93A055 65 93A055 67 0 89 FOR PART NO 93A055 66 Part Number Housing Color Microphone Type Weight 93A055 60 Gray Directional 0 2 lbs 93A055 65 Brown ATR 42 Directional 0 2 lbs 93A055 66 Gray Directional 0 2 lbs 93A055 67 Bl...

Page 76: ...DAMPER 84 DIA c L 2 25 CONFIG P N 1 12 LEVEL 38 DC SUPPLY 6V SIGNAL OUTPUT SIGNAL GND NAMEPLATE 92 700 WHITE BLACK SHIELD 15 c L 6ć32 THD X 22 DEEP 2 PLACES SHIELDED WIRE 22 AWG TWISTED PAIR LENGTH 17 INCHES 30 Part Number Housing Color Microphone Type Weight 93A055 40 Gray MiniĆCondenser 0 2 lbs 93A055 45 Brown ATR 42 MiniĆCondenser 0 2 lbs Figure A 30 Outline and Dimensions Model A55B SurfaceĆMo...

Page 77: ...M RB1 M 0 TWINAX RECEPTACLE CONFIGURATION NAMEPLATE NOTES 1 MATING PLUGS FOR SPECIFIED RECEPTACLE ARE CANNON TM PL F 39 OR TM PL2 F 39 COMPANY LOGO 2 DIMENSIONS ARE IN INCHES Part Number Panel Color Microphone Type Weight 0 1 lbs 93A055 10 Black Condenser 0 5 lbs 93A055 30 Brown Boeing Condenser 0 5 lbs 93A055 50 Black Non Magnetic 0 5 lbs Figure A 31 Outline and Dimensions Model A55B Panel Mount ...

Page 78: ...AX CANNON TM RB1 M 0 TWINAX RECEPTACLE CONFIGURATION NAMEPLATE NOTES 1 MATING PLUGS FOR SPECIFIED RECEPTACLE ARE CANNON TM PL F 39 OR TM PL2 F 39 COMPANY LOGO 2 DIMENSIONS ARE IN INCHES 0 47 0 25 Part Number Housing Color Mic Element Type Weight 0 1 lbs 93A055 20 Black Condenser 0 55 lbs 93A055 55 Black Non Magnetic 0 55 lbs Figure A 32 Outline and Dimensions Model A55B Panel Mount Microphone Modu...

Page 79: ...Instruction Manual Installation Operation Model FA2100 CVR Jan 01 03 Rev 07 Page B 1 165E1846 00 APPENDIX B ENVIRONMENTAL QUALIFICATION FORMS EQFs ED 56A AND RTCA DO 160C ...

Page 80: ...Model FA2100 CVR Instruction Manual Installation Operation Jan 01 03 Rev 07 Page B 2 165E1846 00 THIS PAGE IS INTENTIONALLY LEFT BLANK ...

Page 81: ...ed Tests Temperature and Altitude 1 Low Temperature Ground Survival Operating 4 0 4 5 1 4 5 1 Equipment tested to Categories A2 F2 2 55 C 55 C High Temperature Ground Survival Operating 4 5 2 4 5 3 85 C 70 C Altitude 4 6 1 55 000 feet Decompression 4 6 2 55 000 feet Overpressure 4 6 3 15 000 feet Temperature Variation 1 5 0 Equipment tested to Category B Humidity 1 6 0 Equipment tested to Category...

Page 82: ...AC and DC source power Tested to Normal and Emergency Conditions Tested to Normal and Emergency Conditions Voltage Spike 1 17 0 Equipment tested to Category A Tested with AC and DC source power Audio Frequency Susceptibility 1 18 0 Equipment tested to Category Z Tested with AC and DC source power Induced Signal Susceptibility 1 Magnetic Fields Magnetic Fields Electric Fields Spikes 19 0 19 3 1 19 ...

Page 83: ...rmed at the Category A2 specified pressure 3 For helicopter installations and other severe environments vibration mount Part Number 9300 343 or equivalent or heavy duty vibration mount Part Number 93 955 or equivalent are recommended Remarks All tests except Crash Safety Sustained RTCA DO 160C paragraph 7 3 2 2 Explosion Proofness RTCA DO 160C paragraph 9 0 and Impact Shock EUROCAE ED 56A paragrap...

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Page 85: ...e and Altitude Low Temperature Ground Survival Operating 4 0 4 5 1 4 5 1 Equipment tested to Categories A2 F2 1 55 C 55 C High Temperature Ground Survival Operating 4 5 2 4 5 3 85 C 70 C Altitude 4 6 1 55 000 feet Decompression 4 6 2 55 000 feet Overpressure 4 6 3 15 000 feet Temperature Variation 5 0 Equipment tested to Category B Humidity 6 0 Equipment tested to Category A Standard Operational S...

Page 86: ... 18 0 Equipment tested to Category Z Tested with AC and DC source power Induced Signal Susceptibility Magnetic Fields Magnetic Fields Electric Fields Spikes 19 0 19 3 1 19 3 2 19 3 3 19 3 4 Equipment tested to Category Z Equipment Cables Cables Cables Radio Frequency Susceptibility Conducted and Radiated 20 0 Equipment tested to Category U Emission of Radio Frequency Energy Conducted Radiated 21 0...

Page 87: ...perature Ground Survival Operating 4 0 4 5 1 4 5 1 Equipment tested to Category A2 Altitude Decompression tested to Category D2 55 C 15 C High Temperature Ground Survival Operating 4 5 2 4 5 3 85 C 70 C Altitude 4 6 1 50 000 feet Decompression 4 6 2 50 000 feet Overpressure 4 6 3 15 000 feet Temperature Variation 5 0 Equipment tested to Category C Humidity 6 0 Equipment tested to Category A Standa...

Page 88: ...Spike 17 0 Equipment identified as Category X no test required Audio Frequency Susceptibility 18 0 Equipment identified as Category X no test required Induced Signal Susceptibility Magnetic Fields Magnetic Fields Electric Fields Spikes 19 0 19 3 1 19 3 2 19 3 3 19 3 4 Equipment tested to Category Z Equipment Cables Cables Cables Radio Frequency Susceptibility Conducted and Radiated 20 0 Equipment ...

Page 89: ...ound Survival Operating 4 0 4 5 1 4 5 1 Equipment tested to Category A2 Decompression tested to 55 000 feet 55 C 15 C High Temperature Ground Survival Short Time Operating 4 5 2 4 5 2 4 5 3 85 C 70 C 70 C Altitude 4 6 1 15 000 feet Decompression 4 6 2 55 000 feet Overpressure 4 6 3 15 000 feet Temperature Variation 5 0 Equipment tested to Category C Humidity 6 0 Equipment tested to Category A Stan...

Page 90: ...Spikes 19 0 19 3 1 19 3 2 19 3 3 19 3 4 Equipment tested to Category Z Equipment Cables Cables Cables Radio Frequency Susceptibility Conducted and Radiated 20 0 Category X Equipment tested to 3ma 2V m and 2V m per ED 56A paragraph 420 Exception 2 Emission of Radio Frequency Energy Conducted Radiated 21 0 21 3b 21 4 Equipment tested to Category Z Current probe method Lightning Induced Transient Sus...

Page 91: ...Ground Survival Operating 4 0 4 5 1 4 5 1 Equipment tested to Categories A2 F2 1 55 C 55 C High Temperature Ground Survival Operating 4 5 2 4 5 3 85 C 70 C Altitude 4 6 1 55 000 feet Decompression 4 6 2 55 000 feet Overpressure 4 6 3 15 000 feet Temperature Variation 5 0 Equipment tested to Category B Humidity 6 0 Equipment tested to Category A Standard Operational Shocks Crash Safety Operational ...

Page 92: ...o Frequency Susceptibility Conducted and Radiated 20 0 Equipment tested to Category T 2 Emission of Radio Frequency Energy Conducted Radiated 21 0 21 3b 21 4 Equipment tested to Category Z Current probe method Lightning Induced Transient Susceptibility 22 0 Equipment tested to Category XXZ2 Lightning Direct Effects 23 0 Equipment identified as Category X no test required Icing 24 0 Equipment ident...

Page 93: ...Temperature Ground Survival Operating 4 0 4 5 1 4 5 1 Equipment tested to Category F2 55 C 55 C High Temperature Ground Survival Operating 4 5 2 4 5 3 85 C 70 C Altitude 4 6 1 55 000 feet Decompression 4 6 2 55 000 feet Overpressure 4 6 3 15 000 feet Temperature Variation 5 0 Equipment tested to Category B Humidity 6 0 Equipment tested to Category A Standard Operational Shocks Crash Safety Operati...

Page 94: ... Voltage Spike 17 0 Equipment identified as Category X no test required Audio Frequency Susceptibility 18 0 Equipment identified as Category X no test required Induced Signal Susceptibility Magnetic Fields Magnetic Fields Electric Fields Spikes 19 0 19 3 1 19 3 2 19 3 3 19 3 4 Equipment tested to Category Z Equipment Cables Cables Cables Radio Frequency Susceptibility Conducted and Radiated 20 0 E...

Page 95: ...ature Ground Survival Operating 4 0 4 5 1 4 5 1 Equipment tested to Categories A2 F2 1 Temperature Tests combined with Tempera ture Vibration Test Section 5 0 55 C 55 C High Temperature Ground Survival Operating 4 5 2 4 5 3 85 C 70 C Altitude 4 6 1 55 000 feet Decompression 4 6 2 55 000 feet Overpressure 4 6 3 15 000 feet Temperature Variation 5 0 Equipment tested to Category B This test combined ...

Page 96: ...t tested to Category Z Power Input 16 0 Equipment identified as Category X no test required Voltage Spike 17 0 Equipment tested to Category A Tested with DC and AC source power Audio Frequency Susceptibility 18 0 Equipment tested to Category Z Tested with DC and AC source power Induced Signal Susceptibility Magnetic Fields Magnetic Fields Electric Fields Spikes 19 0 19 3 1 19 3 2 19 3 3 19 3 4 Equ...

Page 97: ...on from Category A2 is performed at the F2 altitude Overpressure is performed at the Category A2 specified pressure 2 A double shielded microphone cable is required to achieve this category Remarks All tests except Crash Safety Sustained RTCA DO 160C paragraph 7 3 2 2 and Explosion Proofness RTCA DO 160C paragraph 9 0 were conducted at L 3 Communications Aviation Recorders Sarasota Florida Crash S...

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Page 99: ...uipment tested to Categories A2 Altitude and Decompression tested to Category D2 Temperature Tests combined with Temperature Vari ation Test Section 5 0 55 C 15 C High Temperature Ground Survival Operating 4 5 2 4 5 3 85 C 70 C Altitude 4 6 1 15 000 feet Decompression 4 6 2 55 000 feet Overpressure 4 6 3 15 000 feet Temperature Variation 5 0 Equipment tested to Category C This test com bined with ...

Page 100: ...19 0 19 3 1 19 3 2 19 3 3 19 3 4 Equipment tested to Category Z Equipment Cables Cables Cables Radio Frequency Susceptibility Conducted and Radiated 20 0 Equipment tested to 2 V m Emission of Radio Frequency Energy Conducted Radiated 21 0 21 3b 21 4 Equipment tested to Category Z Current probe method Lightning Induced Transient Susceptibility 22 0 Equipment tested to Category XXZ2 Lightning Direct...

Page 101: ... of Conducted Tests Temperature and Altitude Low Temperature Ground Survival Operating 4 0 4 5 1 4 5 1 Equipment tested to Categories A2 F2 1 55 C 55 C High Temperature Ground Survival Operating 4 5 2 4 5 3 85 C 70 C Altitude 4 6 1 55 000 feet Decompression 4 6 2 55 000 feet Overpressure 4 6 3 15 000 feet Temperature Variation 5 0 Equipment tested to Category B Humidity 6 0 Equipment tested to Cat...

Page 102: ...udio Frequency Susceptibility 18 0 Equipment identified as Category X no test required Induced Signal Susceptibility Magnetic Fields Magnetic Fields Electric Fields Spikes 19 0 19 3 1 19 3 2 19 3 3 19 3 4 Equipment tested to Category Z Equipment Cables Cables Cables Radio Frequency Susceptibility Conducted and Radiated 20 0 Equipment tested to Category T Emission of Radio Frequency Energy Conducte...

Page 103: ...Survival Operating 4 0 4 5 1 4 5 1 Equipment tested to Categories A2 except decom pression 55 000 feet 55 C 15 C High Temperature Ground Survival Operating 4 5 2 4 5 3 85 C 70 C Altitude 4 6 1 15 000 feet Decompression 4 6 2 55 000 feet Overpressure 4 6 3 15 000 feet Temperature Variation 5 0 Equipment tested to Category C Humidity 6 0 Equipment tested to Category A Standard Operational Shocks Cra...

Page 104: ...ed Voltage Spike 17 0 Equipment identified as Category X no test requi red Audio Frequency Susceptibility 18 0 Equipment identified as Category X no test requi red Induced Signal Susceptibility Magnetic Fields Magnetic Fields Electric Fields Spikes 19 0 19 3 1 19 3 2 19 3 3 19 3 4 Equipment tested to Category Z Equipment Cables Cables Cables Radio Frequency Susceptibility Conducted and Radiated 20...

Page 105: ...tude Low Temperature Ground Survival Operating 4 0 4 5 1 4 5 1 Equipment tested to Categories A2 F2 1 55 C 55 C High Temperature Ground Survival Operating 4 5 2 4 5 3 85 C 70 C Altitude 4 6 1 55 000 feet Decompression 4 6 2 55 000 feet Overpressure 4 6 3 15 000 feet Temperature Variation 5 0 Equipment tested to Category B Humidity 6 0 Equipment tested to Category A Standard Operational Shocks Cras...

Page 106: ...t tested to Category Z Tested with DC and AC power Induced Signal Susceptibility Magnetic Fields Magnetic Fields Electric Fields Spikes 19 0 19 3 1 19 3 2 19 3 3 19 3 4 Equipment tested to Category Z 2 Equipment Cables Cables Cables Radio Frequency Susceptibility Conducted and Radiated 20 0 Equipment tested to Category T 2 Radio Frequency Emissions Conducted Radiated 21 0 21 3b 21 4 Equipment test...

Page 107: ...ound Survival Operating 4 0 4 5 1 4 5 1 Equipment tested to Categories F2 55 C 55 C High Temperature Ground Survival Operating 4 5 2 4 5 3 85 C 70 C Altitude 4 6 1 55 000 feet Decompression 4 6 2 55 000 feet Overpressure 4 6 3 15 000 feet Temperature Variation 5 0 Equipment tested to Category A Humidity 6 0 Equipment tested to Category A Standard Operational Shocks Crash Safety Operational Shock C...

Page 108: ... required Voltage Spike 17 0 Equipment identified as Category X no test required Audio Frequency Susceptibility 18 0 Equipment identified as Category X no test required Induced Signal Susceptibility Magnetic Fields Magnetic Fields Electric Fields Spikes 19 0 19 3 1 19 3 2 19 3 3 19 3 4 Equipment tested to Category Z Equipment Cables Cables Cables Radio Frequency Susceptibility Conducted and Radiat...

Page 109: ...Instruction Manual Installation Operation Model FA2100 CVR Jan 20 02 Rev 07 Page C 1 165E1846 00 APPENDIX C ACCESSORY EQUIPMENT ...

Page 110: ...Model FA2100 CVR Instruction Manual Installation Operation Page C 2 Jan 01 03 Rev 07 165E1846 00 THIS PAGE IS INTENTIONALLY LEFT BLANK ...

Page 111: ... 453 3 Inertia Switch is a highly reliable latching inertia impact switch used in various military and commercial aviation applications These units are factory preset at certain g levels When predetermined g levels are exceeded by the aircraft certain systems such as voice data recording emergency lighting and fire control can be automatically turned on and off ...

Page 112: ...50 1 750 38 TERMINALS 2 625 3 00 1 37 19 RESET BUTTON 187 DIA ACCELERATION 1 187 125 INERTIA SWITCH INC 260 NORTH ROUTE 303 WEST NYACK NEW YORK 10994 PHONE 914 358Ć9070 FAX 914 358Ć1014 SPECIFICATIONS RANGE 1 to 10 g s CURRENT 5 Amps 28 V dc 5 Amps 125 V ac SHOCK 100 g s 11ms WEIGHT 9 oz C G Figure C 1 Inertia Impact Switch Model 3LO 453 3 ...

Page 113: ...Instruction Manual Installation Operation Model FA2100 CVR Jan 20 02 Rev 07 Page C 5 165E1846 00 Figure C 2 Sheet 1 of 2 Aerodyne Controls Corp Environmentally Sealed Impact Switch Assembly ...

Page 114: ...Model FA2100 CVR Instruction Manual Installation Operation Page C 6 Jan 01 03 Rev 07 165E1846 00 Figure C 2 Sheet 2 of 2 Aerodyne Controls Corp Environmentally Sealed Impact Switch Assembly ...

Page 115: ...lace of internal loudspeaker impedance 10 ohms nominal Beacon Operational Tests D Set TUNING control between 35 and 40 kHz Turn GAIN control clockwise and check for operation by jingling keys or coins near microphone D Short water switch on Beacon Tune Test Set for best audible signal D Beacon operation will be indicated by a pulsing audible tone D Determine pulse repetition rate by counting pulse...

Page 116: ...Model FA2100 CVR Instruction Manual Installation Operation Page C 8 Jan 01 03 Rev 07 165E1846 00 THIS PAGE IS INTENTIONALLY LEFT BLANK ...

Page 117: ...Instruction Manual Installation Operation Model FA2100 CVR Jan 01 03 Rev 07 Page D 1 165E1846 00 APPENDIX D ABBREVIATIONS AND ACRONYMS ...

Page 118: ...Model FA2100 CVR Instruction Manual Installation Operation Jan 01 03 Rev 07 Page D 2 165E1846 00 THIS PAGE IS INTENTIONALLY LEFT BLANK ...

Page 119: ...ation Equipment FAA Federal Aviation Administration FAR Federal Aviation Regulation FED STD Federal Standard FSK frequency shift keyed frequency shift keying GMT Greenwich Mean Time GND ground GSE Ground Support Equipment HQ high quality Hz Hertz cycles per second lbs pounds LRU Line Replaceable Unit mA milliamperes Mic microphone ms milliseconds mVrms millivolts route mean squared MOPS Minimum Op...

Page 120: ...Model FA2100 CVR Instruction Manual Installation Operation Jan 01 03 Rev 07 Page D 4 165E1846 00 THIS PAGE IS INTENTIONALLY LEFT BLANK ...

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