Thales Communications EVR750 AIRBORNE VHF DATA RADIO User Manual 333183

THALES Communications AIRBORNE VHF DATA RADIO 333183

CMM

 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A,  EVR750-03-0100A and EVR750-04-0100A   23-12-30 TITLE Page 1/22003/03/01 LISTE DES RENVOIS  ATA 23-12-30   Fabricant  P/N    Date d'édition originale 2003/03/01 Date d'édition   2003/03/01
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A,  EVR750-03-0100A and EVR750-04-0100A   23-12-30 TS Page 1 of 12003/03/01  TRANSMITTAL SHEET   TO: HOLDERS OF COMPONENT MAINTENANCE MANUAL FOR EVR716 AND EVR750 ATA 23-12-30.   FILING INSTRUCTIONS  −  Revision No. P04 of the CMM replaces the revision No. 3. −  Revision No. 3 is deleted.
 COMMUNICATIONS F0057  FIRST ISSUE: JAN 15/98 Ref/Doc: 36708021-AC REVISION No.: 4  23-12-30 TP Page 1/22003/03/01 COMPONENT MAINTENANCE MANUAL (FOR USE WITH SEPARATE ILLUSTRATED PARTS CATALOG)  PRELIMINARY Enhanced VHF Radio VHF Communications Transceiver P/Ns: EVR716-01-0100A EVR716-01-0200A  EVR750-03-0100A   EVR750-04-0100A      EVR750-04-0200A
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES   23-12-30 ROR Page 1/22003/03/01 RECORD OF REVISIONS INSERTED REV. No. ISSUE DATE  DATE BY 1 JAN 15/99    2 MAY 21/99    3 2002/10/15    P04 2003/03/01                                                                                  INSERTED REVISSUEDATE BY        INSERTED REVISSUEDATE BY
 COMPONENT MAINTENANCE MANUAL MMR TLS755 P/N: TLS755-XX-YYZZK  TITRE Page 2/2 25 April 03 Error! Reference source not found.  INSERTED REV. No. ISSUE DATE  DATE BY
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES   23-12-30 RTR Page 1/22003/03/01 RECORD OF TEMPORARY REVISIONS INSERTED REMOVED TEMP. REV. No.  ISSUE DATE  DATE  BY  DATE BY PAGE No. 1  JUN 30/99      2002/10/15 THALES  114, 117, 901 2  MAR 30/01      2002/10/15 THALES  3A, 3B 3  JUN 25/01      2002/10/15 THALES  4, 706
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES   23-12-30 SBL Page 1/32003/03/01 SERVICE BULLETIN LIST SERVICE BULLETIN NUMBER R E V INCLUDED IN REVISION DATE  OF INCORPORATION TITLE 1 EVR716-23-01 2  3  2002/10/15  To increase the internal test filtering during power switching. To improve the general behaviour of the sidetone, for CLIMAX and COSITE configuration. (P/Ns: EVR716-01-0100A/01-0200A). 2 EVR716-23-02 B A S I C 3  2002/10/15  To upgrade the actual Transmitter Board (TX) to industrial level by a re-layout of the printed circuit board. (P/Ns: EVR716-01-0100A/01-0200A). 3 EVR716-23-03 B A S I C 3  2002/10/15  To upgrade the actual Receiver Board (RX) to industrial level by a re-layout of the printed circuit board. (P/Ns: EVR716-01-0100A/01-0200A). 4 EVR716-23-04 B A S I C 3  2002/10/15  To upgrade the actual HIRF Board to industrial level by a re-layout of the printed circuit board. (P/Ns: EVR716-01-0100A/01-0200A). 5 EVR716-23-05 1  3  2002/10/15  To correct some non-working units at 136.025 MHz Frequency due to the disparity of the CR8 zener diode regulating the 17V Power Supply of MA21. (P/Ns: EVR716-01-0100A/01-0200A). 6 EVR716-23-06 B A S I C   Not issued. 7 EVR716-23-07 B A S I C 3  2002/10/15  To provide the 8.33 KHz channelling compatibility between VHF data radio unit and the control panel on BOEING B777. (P/N: EVR716-01-0200A).
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 SBL Page 2/32003/03/01 SERVICE BULLETIN NUMBER R E V INCLUDED IN REVISION DATE  OF INCORPORATION TITLE 8 EVR716-23-08 3  3  2002/10/15  To improve the interference response due to COSITE Transmitter (especially for ACARS transmissions). To enhance the transmitter spectrum at ± 75 kHz detected by the ground stations. To improve the squelch response at the range limit. To change the monitoring of the power interrupt information. To correct the management of a “busy channel” during autotest. To provide data link improvement for received audio time establishment and for SQP. To provide the 8.33 kHz channelling compatibility between VHF data radio unit and control panel on BOEING 777 whatever the unit P/N is. P/Ns: EVR716-01-0100A/01-0200A 9 EVR716-23-09 1  3  2002/10/15  To convert the EVR716 Radio into a EVR750 “A” Radio. Note: This service bulletin is not included in this C.M.M. Refer to SB No. 9 for technical information. This SB is only for EVR716 version: 01-0100A. 10 EVR716-23-10      Not issued. 11 EVR716-23-11 1  3  2002/10/15  To improve the reliability of the EVR716 P/N: EVR716-01-0200A. 1 EVR7-23-01 1  3  2002/10/15  To improve the reliability of the EVR716 P/N: EVR716-01-0100A EVR750 P/N:EVR750-03-0100A 2 EVR7-23-02 1  3  2002/10/15  To adapt the receivers design to all TCXO suppliers.To correct on some units a random 400ms noise in the headset when the PTT is released. To check C180 polarity on the Tx board.Applicable to P/N EVR716-01-0100A and EVR750-03-0100A.
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES   23-12-30 SBL Page 3/32003/03/01 SERVICE BULLETIN NUMBER R E V INCLUDED IN REVISION DATE  OF INCORPORATION TITLE 1 EVR750-23-01 B A S I C 3  2002/10/15  To upgrade the existing transmitter board (TX) by a re-layout of the printed circuit board. P/Ns: EVR750-03-0100A/03-0200A 2 EVR750-23-02 B A S I C 3  2002/10/15  To upgrade the existing receiver board (RX) by a re-layout of the printed circuit board. P/Ns: EVR750-03-0100A/03-0200A 3 EVR750-23-03 B A S I C 3  2002/10/15  To upgrade the existing HIRF board by a re-layout of the printed circuit board. P/Ns: EVR750-03-0100A/03-0200A 4 EVR750-23-04 B A S I C   Not issued.
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES   23-12-30 SILL Page 1/22003/03/01 SERVICE INFORMATION LETTER LIST SERVICE INFORMATION LETTER No. INCLUDED IN REVISION DATE  OF INCORPORATION  TITLE 1  3  2002/10/15  Initial modifications status of power Supply Unit (PSU), Transmitter Unit (TX), Receiver Unit (RX), Data Processing Unit (DPU) and HIRF Unit. Applicable to P/Ns: EVR716-01-0100A and EVR716-01-0200A. 1 EVR750-23-01 3  2002/10/15  Initial modifications status of EVR750 Transceiver. Applicable to P/Ns: EVR750-03-0100A and EVR750-03-0200A. 2 EVR750-23-02 3  2002/10/15  To adapt the receivers design to all TCXO suppliers. To correct on some units a random 400 ms noise in the headset when the PTT is released. To check C180 polarity on the Transmitter Board. P/Ns: EVR716-01-0X00A and  EVR750-03-0X00A.                                                                           SUBJECT   PAGE   DATE   SUBJECT   PAGE   DATE
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 SBL Page 2/32003/03/01   SUBJECT   PAGE   DATE Title Page  1  2003/03/01  2 Blank    Record of  1  2003/03/01 Revisions 2 Blank    Record of  1  2003/03/01 Temporary 2 Blank Revisions      List of  1  2003/03/01 Effective 2 Blank Temporary   Revisions      Service 1 2003/03/01 Bulletin List  2  2003/03/01  3 2003/03/01  4 Blank    Service 1 2003/03/01 Information 2 Blank Letter List        List of   1  2003/03/01 Effective   2  2003/03/01 Pages 3 2003/03/01  4 2003/03/01  5 2003/03/01  6 2003/03/01  7 2003/03/01  8 Blank    Table of   1  2003/03/01 Contents 2 2003/03/01  3 2003/03/01  4 2003/03/01    Introduction 1 2003/03/01  2 2003/03/01  3 2003/03/01  4 2003/03/01   SUBJECT   PAGE   DATE 5 2003/03/01 6 Blank   Description 1 2003/03/01 and 2 2003/03/01 Operation 3 2003/03/01 4 2003/03/01 5 2003/03/01 6 2003/03/01 7 2003/03/01 8 2003/03/01 9 2003/03/01 10 2003/03/01 11 2003/03/01 12 2003/03/01 13 2003/03/01 14 2003/03/01 15 2003/03/01 16 2003/03/01 17 2003/03/01 18 2003/03/01 19 2003/03/01 20 2003/03/01 21 2003/03/01 22 2003/03/01
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES   23-12-30 LOT Page 12003/03/01 TABLE OF CONTENTS SUBJECT PAGE TRANSMITTAL SHEET.................................................................................................................1 RECORD OF REVISIONS ............................................................................................................1 RECORD OF TEMPORARY REVISIONS..................................................................................... 1 SERVICE BULLETIN LIST............................................................................................................1 SERVICE INFORMATION LETTER LIST .....................................................................................1 LIST OF EFFECTIVE PAGES.......................................................................................................1 TABLE OF CONTENTS ................................................................................................................1 INTRODUCTION ...........................................................................................................................1 1. General...............................................................................................................................1 2. Equipment Identification .....................................................................................................2 A.  Generic Part Number....................................................................................................... 2 B.  Front panel labels............................................................................................................2 3. Uncommon Abbreviations/Acronyms..................................................................................2 DESCRIPTION AND OPERATION ...............................................................................................1 1. Description..........................................................................................................................1 A. General............................................................................................................................1 B. Frontispiece.....................................................................................................................3 2.  Function of Equipment........................................................................................................4 A. Characteristics.................................................................................................................5 B. Description.....................................................................................................................10 3. Operation..........................................................................................................................18 A. General..........................................................................................................................18 B.  Wired Chassis Assembly (CHC)....................................................................................23
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES   23-12-30 INTRO - Page 12003/03/01 INTRODUCTION 1. General This Component Maintenance Manual includes maintenance instructions prepared in accordance with Air Transport Association Specification Nr. 100 for the THALES COMMUNICATIONS Enhanced VHF Radio. Parts lists are provided in a separate Illustrated Parts Catalog ATA: 23-12-30 (Ref/Doc: 36708031). In this issue, the CMM provides informations concerning the EVR716/750 versions. This manual provides procedures for shop testing and repair. It presents detailed circuit theory with emphasis on items which will be especially helpful for effective fault isolation. It contains complete performance tests and adjustment procedures. This Component Maintenance Manual provides shop verified procedures that will enable a technician, unfamiliar with the equipment, to restore it to serviceable condition. The procedures are prepared for the technician that performs shop work and not for the aircraft technician. CAUTION:  THE MATERIAL IN THIS MANUAL IS SUBJECT TO CHANGE. BEFORE ATTEMPTING ANY MAINTENANCE OPERATION ON THE EQUIPMENT COVERED IN THIS MANUAL, VERIFY THAT YOU HAVE COMPLETE AND UP-TO-DATE PUBLICATIONS BY REFERRING TO THE APPLICABLE PUBLICATIONS, SERVICE BULLETIN, SERVICE INFORMATION LETTER INDEXES. Refer to the Table of Contents for the page location of applicable sections. A list of uncommon/acronyms abbreviations used in the manual is described in paragraph 2 of the INTRODUCTION section. The manual will be revised as necessary to reflect current information. We welcome your comments concerning this manual. Although effort has been made to keep it free of errors, some may occur. When reporting a specific problem, please describe it briefly and include the manual part number, the paragraph or figure number, and the page number. Send your comments to: THALES AVIONICS  Aérodrome de Villacoublay B.P59 78 141 VELIZY VILLACOUBLAY CEDEX FRANCE
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 22003/03/01 2. Equipment Identification A.  Generic Part Number The part number has the following format (example). EVR716 -01- 0200AFamily designationVersion of the equipment according to installedHardware evolution indexSoftware evolution indexMaintenanceSoftware version B.  Front panel labels Different kinds of labels are stuck on the front panel of the EVR716/750 unit. According of EVR716 or EVR750 unit versions, all labels are not similar. For more information, refer to the Illustrated Parts Catalog, ATA: 23-12-30 (Ref/Doc: 36708031) Figures 1 and 1A for the localization on the front panel of the unit. 3. Uncommon Abbreviations/Acronyms ABBREVIATION/ACRONYM IDENTIFICATION ACARS Aircraft Communications Addressing and Reporting System ADC  Analog to Digital Converter AF Audio Frequency AGC  Automatic Gain Control AIN Analog INput AM Amplitude Modulation AMU  Audio Management Unit ANT ANTenna ARINC  Aeronautical Radio INCorporated ATE  Automatic Test Equipment BCD  Binary Coded Decimal BER  Bit Error Rate BIT Built-In Test BITE  Built-In Test Equipment BNC BiNary Code BNR BiNaRy CCITT  Comité Consultatif International de Télécommunication et Transmission CDU  Control Display Unit
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES   23-12-30 INTRO - Page 32003/03/01 ABBREVIATION/ACRONYM IDENTIFICATION CFDS  Centralized Fault Display System CHC  CHassis Câblé (Wired Chassis) CODEC COder/DECoder CMC  Centralized Maintenance Computer CMU  Communications Management Unit CPT Counter CPTT  Control Push To Talk CRT  Cathode Ray Tube CS Chip Select CSMA  Carrier Sense Multiple Access CW  Carrier Wave or Continuous Wave DAC  Digital to Analog Converter D/A Digital/Analog dBc DeciBel Carrier dBm  DeciBel referred to 1 Milliwatt DC Direct Current DF Design Function DFIU  Discrete Function Interface Unit DFS  Data Frequency System DISP DISPlay DPU  Data Processing Unit DSP  Digital Signal Processor D8PSK  Differential 8 Phases Shift Keying EEPROM Electrically Erasable PROM EPLD  Erasable Programmable Logical Device EPROM  Electrically Programmable ROM ESDS  ElectroStatic Discharge Sensitive EVR  Enhanced VHF Radio EXT EXTernal FET  Field Effect Transistor FIFO  First In, First Out FILT FILTer FM Frequency Modulation FO Oscillator Frequency FT Functional Test FW Failure Warning GND GrouND HF High Frequency HIRF  High Intensity Rejected Frequency ICAO  International Civil Aviation Organisation (cont’d)
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 42003/03/01 ABBREVIATION/ACRONYM IDENTIFICATION IF Intermediate Frequency IRQ Interrupt ReQuest I/O Input/Ouput IT InTerrupt Ko  Kilo Octet (1024 octets) LED  Light Emitting Diode LF Low Frequency LO Local Oscillator LRU  Line Replaceable Unit LSB Less Significant Bit MAN Manual MCU  Module Control Unit MSB  Most Significant Bit MSK  Minimum Shift Keying MU Management Unit NB Narrow Band NC Normally Closed NR NumbeR NU Not Used NVM  Non Volatile Memory OEM  Original Equipment Manufacturer OMS  On-board Maintenance System PCB  Printed Circuit Board PIN  P (dopping) Intrinseque N (dopping) P/N Part Number PPM  Pulse Position Modulation PRG Program PROM Programmable ROM PTT  Push To Talk PWR Power RAM  Random Access Memory RC Resistor Capacitor RCU  Remote Control Unit RD ReaD RDY ReaDY RF Radio Frequency RMT ReMoTe ROM  Read Only Memory RST Reset R/T Receiver/Transmitter (cont’d)
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES   23-12-30 INTRO - Page 5/62003/03/01 ABBREVIATION/ACRONYM IDENTIFICATION Rx Reception SELCAL SELective CALling SDI Source/Destination Identifier SMD  Surface Mounted Device SRU  Shop Replaceable Unit SWR  Standing Wave Ratio TF Technical Function TP Top Part T/R Transmitter/Receiver TRIG TRIGger Tx Transmission VCO  Voltage Control Oscillator VHF  Very High Frequency VMA  Valid Memory Address Vpp Volt Peak-to-Peak Vrms  Volt Root Mean Square Value VSWR  Voltage Standing Wave Ratio WB Wide Band WRN WaRNing µP  Microprocessor
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A and EVR750-03-0100A   23-12-30 Page 12003/03/01 DESCRIPTION AND OPERATION 1. Description A. General This section gives the description of the EVR716/750 Enhanced VHF Radio (VHF communications transceiver). THALES Part-Number  Features EVR716-01-0100A  118 MHz -136.975 MHz frequency range. 25 kHz and 8.33 kHz channel spacing. Compliant with ICAO Annex 10 FM immunity. Conform to DO-178B and DO-160C requirements. Fault memory. ACARS compatible (analogue interface). 200 ms power drop-out transparency. Software data loading via RS232 interface. Airbus ABD0048 or Boeing D243W220 interface maintenance interface selectable by pin programming with Airbus ABD0048 maintenance interface by default. EVR716-01-0200A  118 MHz-136.975 MHz frequency range. 25 kHz and 8.33 kHz channel spacing. Compliant with ICAO Annex 10 FM immunity. Conforms to DO-178B and DO-160C requirements. Fault memory. ACARS compatible (analogue interface). 200 ms power drop-out transparency. Software dataloading via RS232 interface. Airbus ABD0048 or Boeing D243W220 interface maintenance interface selectable by pin programming with Boeing D243W220 maintenance interface by default. (cont’d)  Table 1 - Part Numbers List
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 22003/03/01  THALES Part-Number  Features EVR750-03-0100A  118 MHz-136.975 MHz frequency range. 25 kHz and 8.33 kHz channel spacing. Compliant with ICAO Annex 10 FM immunity. Conforms to DO-178B and DO-160C requirements. Fault memory. Analogue or Digital Interface ACARS compatible (digital interface with ATSU/CMU-mode A-). 200 ms power drop-out transparency. Software dataloading via RS232 interface. Airbus ABD0048 or Boeing D243W201 interface maintenance. Interface selectable by pin programming with Airbus ABD0048 maintenance interface by default. EVR750-04-0100A  118 MHz-136.975 MHz frequency range. 25 kHz and 8.33 kHz channel spacing. Compliant with ICAO Annex 10 FM immunity. Conforms to DO-178B and DO-160D requirements. Fault memory. Analogue or Digital Interface ACARS compatible (digital interface with ATSU/CMU-mode A-). 200 ms power drop-out transparency. Data transmission (31.5kb/sec) with the VDL mode 2 protocol (D8PSK modulation and CSMA access according to ARINC 750 and SARPS VDL2). Interface with ATSU/CMU mode 2. Software dataloading via RS232 interface. Airbus ABD0048 or Boeing D243W201 interface maintenance. Interface selectable by pin programming with Airbus ABD0048 maintenance interface by default. EVR750-04-0200A  118 MHz-136.975 MHz frequency range. 25 kHz and 8.33 kHz channel spacing. Compliant with ICAO Annex 10 FM immunity. Conforms to DO-178B and DO-160D requirements. Fault memory. Analogue or Digital Interface ACARS compatible (digital interface with ATSU/CMU-mode A-). 200 ms power drop-out transparency. Data transmission (31.5kb/sec) with the VDL mode 2 protocol (D8PSK modulation and CSMA access according to ARINC 750 and SARPS VDL2). Interface with ATSU/CMU mode 2. Software dataloading via RS232 interface. Airbus ABD0048 or Boeing D243W201 interface maintenance. Interface selectable by pin programming with Boeing D243W201 maintenance interface by default. Table 1 - Part Numbers List
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A and EVR750-03-0100A   23-12-30 Page 32003/03/01 B. Frontispiece       Figure 1 - EVR716/750 Unit
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 42003/03/01 2.  Function of Equipment The airborne equipment, called EVR (Enhanced VHF Radio), is a VHF communications transceiver operating in the aeronautical band (118 MHz to 137 MHz or 118 MHz to 152 MHz), used by Air Transport Aircraft as a primary equipment for communications with the ground air traffic control infrastructure (in continental areas) or for communications between aircraft (relay, emergency). The basic version of EVR-716 (EVR716-01-xxxxx) and EVR750 (EVR750-03-xxxxx and EVR750-04-xxxxx) operates in the 118 MHz-137 MHz aeronautical band and a specific version for frequency band extension up to 152 MHz is also available (EVR716-02-xxxxx). Aboard the aircraft, the EVR716/750 transceiver can operate with the following equipment: −  a Frequency Selection System which can be an RCU (Radio Control Unit or control unit) or an RMP (Radio Management Panel) to agree with the aircraft configuration, −  an ACARS MU (Management Unit, ARINC 724) or a CMU (Communications Management Unit, ARINC 758), −  an Audio Management Unit (AMU), −  a maintenance computer: OMS (ARINC 624) or CFDS (ARINC 604), −  a SELCAL decoder system, −  a ATSU/CMU mode 2, −  a VHF antenna. The EVR716 transceiver operates according the following modes of operation: −  Mode 0A: transmits/receives voice signals in one-way mode with 25 kHz channels spacing, Amplitude Modulation and Double Side Bands, −  Mode 0B: transmits/receives voice signals in one-way mode with the channels 8.33 kHz channels spacing, Amplitude Modulation and Double Side Bands, −  Mode 1A: transmits/receives data signals in one-way mode with AM-MSK modulation, MSK modulation being performed externally in the (C) MU (standard ACARS mode). The signal rate is 2.4 kb/sec. with the 25 kHz apart channels spacing. The EVR750 transceiver operates according to the same modes as EVR716 (0A/0B/1A) and in addition according to the following mode: −  Mode 1C: transmits/receives data signals in one-way mode with AM-MSK modulation, MSK modulation being performed internally. The signal rate is 2.4 kb/sec. with the 25 kHz apart channels spacing. −  Mode 2: transmits/receives data signals in one-way mode with D8PSK modulation. The signal rate is 31.5 kb/sec with the 25 kHz apart channel spacing.
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A and EVR750-03-0100A   23-12-30 Page 52003/03/01 A. Characteristics (1) Electrical characteristics CHARACTERISTICS SPECIFICATIONS GENERAL  Operational modes  Voice/25 kHz (0A) Voice/8.33 kHz (0B) Data AM/MSK (1A) (with external modem) Data AM/MSK (1C) (with internal modem) Data D8PSK (2) Power requirements  28 VDC/180 W Mode 2 :28VDC/210W Form factor  3 MCU, ARINC Specification 600 i.e.  200x94x387.5 (mm) Weight  4450 g ± 50 g Operating Temperature Storage Temperature -25 °C to +70 °C (+13°F to +158°F) -55 °C to +85 °C (-67°F to +185°F) Over pressure decompression  In accordance with DO-160C, section 4.6, category A2 and D1 (Cf: SSS and DDP) (DO-160D for EVR750-04-xxxxx) Vibrations  In accordance with DO-160C, section 8, category B (DO-160D for EVR750-04-0x00A) Electromagnetic compatibility  In accordance with DO-160C, section 15, 16, 17, 18, 19, 20, 21 and 22. (DO-160D for EVR750-04-xxxxx) Frequency control  Serial digital in accordance with ARINC 429 Frequency range  117.975 MHz to 137.000 MHz Channel spacing  25 kHz and 8.33 kHz Frequency stability  < ± 5 ppm Duty cycle  Continuous transmission (with ARINC 600 cooling system). Duty cycle of 20% (1mn/4mn) with natural convection Channel Switching  Less than 60 ms Transmit to receive switching time Less than 50 ms in mode 0A, 0B, 1A, 1C Less than 1.5 ms in mode 2 Receive to transmit switching time Less than 50 ms in mode 0A, 0B, 1A, 1C Less than 1.5 ms in mode 2 (cont’d)
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 62003/03/01  CHARACTERISTICS SPECIFICATIONS RECEIVER  ED-23B/DO-186A  Class C and E  ED-92 Class F Sensitivity (modes 0A & 0B)  For a wanted signal of -106 dBm, modulated 1kHz/30%, (S+N)/N* is greater than 6 dB (nominal). (*): CCITT weighted Sensitivity (mode 2)  Better than –98dBm to get a BER (non corrected) better than 1.10-3 Selectivity (mode 0A)  > ± 9 kHz at 6 dB bandwidth < ± 17 kHz at 60 dB bandwidth < ± 25 kHz at 70 dB bandwidth Selectivity (mode 0B)  > ± 2.78 kHz at 6 dB bandwidth < ± 7.37 kHz at 60 dB bandwidth Adjacent channel rejection (mode 2)  Better than 44dB to get a BER better than 1.10-3 Co-channel interference (mode 2)  Co-channel interference ratio better than 20dB to get a BER better than 1.10-3 Dynamic Range (mode 2)  From -98dBm up to -7dBm to get a BER better than 1.10-3Strong Signals within the VHF range (mode 2) Better than -27dBm to get a BER better than 1.10-3 Cross modulation  Unwanted signal level (1 kHz/50%) to obtain – 10 dB referred to a signal of –87 dBm (1 kHz/50%):   - at   ±   25 kHz > – 20 dBm   - at   ±   50 kHz > – 15 dBm   - at   ±   100 kHz > – 10 dBm AGC regulation  Within 3 dB (-93 dBm to -13 dBm input); no more than 6 dB (-101 dBm to +1 dBm) Audio output  10 mW (adjustable from 5 mW to 40 mW) into 600 ohms (± 20%) resistive load for -53 dBm signal modulated 30% at 1000 Hz Audio output frequency response  Within 6 dB from 300 Hz to 2500 Hz better than -20 dB at 3750 Hz Audio output harmonic distortion  Not to exceed < 3% for -53 dBm signal modulated 30% at 1000 Hz Undesired responses  < 80 dB Intermodulation (FM immunity)  as per ARINC 716 section 3.6.7.5   Output level  0.5 Vrms (min.) into 600 ohms (± 20%) resistive load Selcal/Data Output Frequency response Selcal (mode Voice): < 3 dB from 312 Hz to 1200 Hz AM-MSK (mode data) < ± 6 dB from 300 Hz to 6600 Hz   Distortion  < 3% for a signal of -53 dBm, modulated 30% at 1000 Hz (cont’d)
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A and EVR750-03-0100A   23-12-30 Page 72003/03/01  CHARACTERISTICS SPECIFICATIONS TRANSMITTER  ED-23B/DO-186A  Class 3 and 5  ED-92 Class 7 Output power  > 25 W Output power (mode 2)  > 15 W Harmonics H2 < -16 dBm Hn < -26 dBm (n≥ 3) AF response  Within 6 dB from 300 Hz to 2500 Hz Audio distortion  < 10% Modulation level  > 80 % for 0.25 Vrms at 1000 Hz Spectrum mask (8.33 kHz)  For an audio frequency from 300 Hz to 10 kHz and an audio level attenuated by 10 dB/octave from 800 Hz to 10 kHz, referred to 70% modulation level < -45 dBc from ± 3.2 kHz to ± 5 kHz < -60 dBc from ± 5 kHz to ± 7 kHz < -70 dBc for frequency shift greater than ± 7 kHz  Modulation ratio > 80% for a frequency of 1000 Hz at -10 dBm Data Input  Frequency response Within 6 dB from 600 Hz to 6600 Hz   Distortion  < 10% for 80% modulation ratio over frequency range from 600 Hz to 6600 Hz RF Power rise time  < 190µs RF Power release time  < 190µs Symbol constellation error  Error vector Magnitude (EVM) < 6% Adjacent channel power  1st  ACP : < -18dBm 2nd ACP : < -28dBm 3rd ACP : < -38dBm Wide band noise  < -53dBm Certification  Pour EVR716-01-xxxxx et EVR750-03-xxxxx : DO160C/A2D1/YBA/BCMN/XXXXXXABAZZUZ/A2E2/XX Pour EVR750-04-xxxxx : DO160D Env.Cat.[(A2)(D1)Y]BAB[SMBC]XXXXXXAAAZZUZ[A2E2]XXA  QAC1  NOTE:  ”Nominal” relates to Standard Conditions. The first and last selectable 25 kHz channels are respectively: −  118.000 (F0 = 118.0000 MHz) −  136.975 (F0 = 136.9750 MHz)
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 82003/03/01  The first and last selectable 8.33 kHz channels are respectively: −  118.005 (F0 = 118.0000 MHz) −  136.990 (F0 = 136.9917 MHz)
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A and EVR750-03-0100A   23-12-30 Page 92003/03/01 (2) Environmental Certification The EVR716/750 Transceiver meets the environmental conditions of the Radio Technical Commission for Aeronautics (RTCA) document number DO-160C, ”Environmental Conditions and Test Procedures for Airline Electronic/electrical Equipment and Instruments”.(DO-160D for EVR750-04-xxxxx).    A2 D1 /BAB /SMBC /X X X X X X A A A Z Z U Z /A2E2 /X  XEXPLOSIONWATERPROOFNESSHYDRAULIC FLUIDSAND AND DUSTFUNGUS RESISTANCESALT SPRAYVIBRATIONHUMIDITYTEMPERATUREAND ALTITUDELOSS OF COOLINGSYSTEMTEMPERATUREVARIATIONICINGLIGHTNING INDIRECTEFFECTLIGHTNING DIRECTEFFECTEMISSION OF RADIOFREQUENCY ENERGYRADIO FREQUENCYSUSCEPTIBILITYINDUCED SIGNALSUSCEPTIBILITYAUDIO FREQUENCYCONDUCTEDSUSCEPTIBILITYVOLTAGE SPIKESPOWER UNITMAGNETIC EFFECTNOTAPPLICABLE/AELECTROSTATICDISCHARGE     Figure 2 - Environmental Certification Categories
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 102003/03/01 B. Description See Figure 3. The EVR716/750 appears as a 3 MCU form box. The EVR716/750 transceiver has the operating subassemblies (SRU) below: −  a receiver module −  a transmitter module −  a power supply module −  a Data Processing unit (DPU module) −  an HIRF module −  a power storage module (behind the rear panel) −  a wired chassis The EVR716/750 transceiver is built with a center chassis which holds (See Figure 4): −  a front panel assembly which hold the LED type indicators, a pushbutton for the triggered test and the headset and microphone connectors. The six indicators are: ⋅  ”FAIL LRU” (red) ⋅  ”FAIL IN” (red) ⋅ ”PASS” (green) ⋅ ”VSWR” (red) ⋅ ”Tx” (green) ⋅  ”Rx” (green)  −  on left side, the receiver module, −  on right side, the DPU module, −  on the center part, the Power Supply module and the Transmitter module. −  a rear panel with power supply, antenna input, inputs/outputs (discretes, ARINC buses) and ATE (Automatic Test Equipment) interface. The rear connector has the three parts below: −  the 60-way Middle Part (MP) with all the transceiver inputs (discretes, ARINC buses), −  the 60-way Top Part (TP) with the contacts used for the ATE, −  the Bottom Part (BP) with the power supply contacts and the antenna coaxial connector.
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A and EVR750-03-0100A   23-12-30 Page 112003/03/01 (1) Electrical interfaces NOTE:  Hi = High Lo = Low LS = Low Speed HS = High Speed (a)  Middle Part connector CONNECTOR/PIN SIGNAL NAME MPA1 MPB1 MPC1 MPD1 Mike Input  Hi  “  Lo  “  PTT Key Event MPA2 MPB2 MPC2 MPD2 Max Trans cutoff Mike Input (Ground) Data Loader Input  A  “  B MPA3 MPB3 MPC3 MPD3 Optional Hi (Remote Squelch)  ARM    Lo (GND) DC Ground MPA4 MPB4 MPC4 MPD4 Self Test Discrete Audio Ground (Ground) Data Loader Output  A  “  B MPA5 MPB5 MPC5 MPD5 Data Link Input  HI  ”  Lo Reserved for ARNIC 716 compatibility 8.33 kHz program for ARINC 716 compatibility MPA6 MPB6 MPC6 MPD6 Data from OMS/CFDS # 1 input Port A  A  LS  ”  ”  ”  B Data from OMS/CFDS# 2 input Port B  A  LS  ”  ”  ”  B MPA7 MPB7 MPC7 MPD7 Freq./Func: Select    A  LS Data I/P Port B    B Voice/Data Select Data key line (cont’d)   MPA8 MPB8 MPC8 MPD8 Reserved Data loader enable Reserved Return (DC Ground) MPA9  SDI code input HS HS
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 122003/03/01 CONNECTOR/PIN SIGNAL NAME MPB9 MPC9 MPD9 SDI code input Ground Reserved for AGC MPA10 MPB10 MPC10 MPD10 Program common Reserved Data to both CMUs Output port    A  HS  ”  ”  ”    B MPA11 MPB11 MPC11 MPD11 Freq./Funct. Select Data I/P Port A    A  LS  ”  ”  ”    B Maintenance interface software pin programming Data select discrete MPA12 MPB12 MPC12 MPD12 Data from CMU#1 Input Port A  A  HS   ”             ”            ”  B Data from CMU#2 Input Port B  A  LS   ”             ”            ”  B MPA13 MPB13 MPC13 MPD13 Selcal audio and Data output  HI   ”             ”            ”  Lo Squelch disable Squelch disable return (Ground) MPA14 MPB14 MPC14 MPD14 Maintenance interface software pin programming Ground/air discrete Data to OMS or CFDS Output port    A  LS  ”  ”  ”    B MPA15 MPB15 MPC15 MPD15 Audio/sidetone output  HI  ”  Lo Muting output Muting return (Ground)
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A and EVR750-03-0100A   23-12-30 Page 132003/03/01 (b)  Top Part connector CONNECTOR/PIN  SIGNAL NAME TPA1 TPB1 TPC1 TPD1 MANUFACTURER IDENTIFIER MANUFACTURER  RESERVED RESERVED TPA2 TPB2 TPC2 TPD2   COMMON NOT USED TPA3 TPB3 TPC3 TPD3 NOT USED NOT USED NOT USED NOT USED TPA4 TPB4 TPC4 TPD4 NOT USED NOT USED NOT USED NOT USED TPA5 TPB5 TPC5 TPD5 SELECT MODE ATE TX 232A  DC GROUND RX 232A TPA6 TPB6 TPC6 TPD6 LED A1 LED A2 LED A3 LED A4 TPA7 TPB7 TPC7 TPD7 LED A5 RESERVED FOR AGC RESERVED WRITTEN TPA8 TPB8 TPC8 TPD8 P5VT P15VT M15VT NOT USED TPA9 TPB9 TPC9 TPD9 RESPUATE1 RESPUATE2 NOT USED NOT USED TPA10 TPB10 TPC10 TPD10 BLOSQLT CANOCT COMPRESSOR-ON/OFF-INPUT RESERVED  TPA11 TO TPD15  NOT USED
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 142003/03/01 (c)  Bottom Part connector CONNECTOR/PIN  SIGNAL NAME BP1 BP2 BP3 BP4 BP5 ANTENNA RF POWER INPUT + 28 VDC SPARE POWER INPUT GROUND NOT USED  (d)  Pin programming for maintenance software selection −  P/N EVR 716/750 with BOEING maintenance interface by default:  EVR7xx-0x-0200A. −  P/N EVR716750 with AIRBUS maintenance interface by default:  EVR7xx-0x-0100A.  Pin Programming for maintenance software selection Maintenance Software selected MC11 MA14   0 0 Airbus 0 1* Boeing 1* 0 Airbus 1* 1* Default  * or not wired.
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A and EVR750-03-0100A   23-12-30 Page 152003/03/01     Figure 3 - SRU Location
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 162003/03/01  Figure 4 - Rear and Front Panels
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A and EVR750-03-0100A   23-12-30 Page 172003/03/01 INTLET AREA3 MAX114.3 MINI26756.763.9 MAX2 MAX194318   1+319323.7 MAX0.4  BCENTEROF GRAVITY0.5  W45.250 MAXOUTLETAREA3 MAX51 MAX53.50.53.6 Figure 5 – Dimensions
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 182003/03/01 3. Operation A. General The primary function of the EVR716/750 transceiver is to provide voice and data communications for Air Transport Aircraft, in the aeronautical band (118 MHz to 137 MHz). The EVR716/750  transceiver operates in the voice and data modes given in the ARINC 716/750 specifications, that is for the voice modes: Amplitude Modulation with Double Side Bands, with the channels 25 kHz (0A mode) or 8.33 kHz (0B mode) apart; and in data mode: ACARS mode with an external modem. (internal modem for EVR-750) and VDL Mode 2 (D8PSK). MODE CHARACTERISTICS 0A  Analog voice transmission 25 kHz 0B  Analog voice transmission 8.33 kHz 1A  Data, 25 kHz channel AM-MSK modulation (2.4 kb/sec.) External modem, CSMA access ACARS protocol (analog interface for digital interface with ATSU/CMU for EVR-750). 1C  Data, 25 kHz channel AM-MSK modulation (2.4 kb/sec.) Internal modem, ACARS protocol (analog interface with ATSU/CMU). 2  Data, 25 kHz channel D8PSK modulation (bit rate 31.5kb/sec, symbol rate 10.5 kbauds) Access to the channel :CSMA non adaptive p-persistent Interface with ATSU/CMU through link ARINC 429 high speed. Table 2 - Modes of Operation
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A and EVR750-03-0100A   23-12-30 Page 192003/03/01   The EVR716/750 transceiver has seven subassemblies (SRU) which can be replaced in a maintenance shop. These are: Name Short name WIRED CHASSIS  CHC HIRF module  HIRF RECEIVER Module  REC TRANSMITTER Module  EME DPU Module  DPU POWER SUPPLIES Module  ALM POWER STORAGE module  PST Table 3 - SRU of EVR716/750 The primary functions of an SRU are known as the Design Functions (DF). Each function of a design function is known as a Technical Function (TF). An TF is a set of components related to a primary component. The functions are identified by the short name (mnemonic) of SRU and the short names of the design function and technical function. Example: SRU_DF_TF HIRF_HIRF_RECIN SRUDESIGN FUNCTION (DF)DESIGN FUNCTION (DF)DESIGN FUNCTION (DF)DESIGN FUNCTION (DF)TECHNICAL FUNCTION (TF)TECHNICAL FUNCTION (TF)TECHNICAL FUNCTION (TF)TECHNICAL FUNCTION (TF)TECHNICAL FUNCTION (TF)TECHNICAL FUNCTION (TF)TECHNICAL FUNCTION (TF)TECHNICAL FUNCTION (TF)TECHNICAL FUNCTION (TF)
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 202003/03/01 Figure 6 - Organization of Functions
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A and EVR750-03-0100A   23-12-30 Page 212003/03/01 The next block diagrams show the connections between all the subassemblies of the EVR716/750:FRONT PANELPower SuppliesModule+28V NetworkREAR CONNECTORALMPP5VReceiverModuleRECPP5VR_SYN_P (10 MHz)PP15VPM15VPP21VPP16VPRESETPPOW_1PPOW_2PPOWINTTransmitterModuleEMEDPUModuleGSTPP28VPM15VPP15VPP5VPP21VPRESETPPOW_1PPOW_2PPOWINTA1Z-SA-EHIRFModuleHIRFPower StorageModulePSTPP50VPP28VPAPP28VPSPP5VTPP15VTPM15VT Figure 7 - Power Supply Connections
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 222003/03/01 FRONT PANELRAGCFSTREAR CONNECTOR + HIRFReceiverModuleRECTransmitterModuleEMEDPUModuleDPURAGCWBFRSQLFMIKINFDTINRDTOUTRVOOUTRLO2LEVRANTENLED_ATEMTX232AFRX232AFMODEAFWRITENFOT-IDFSDIFSLFTSTFSLTDTFMNTID2FMNTID1FDATSELFAIRGROFDATLODFTXCUTOFVODATFDLRFCMC2FCMC1FCMU2FCMU1FDFS2FDFS1FDATKEYFPTTKEYMCMUMCMCMDLMMUTINGMKEVENTD_LF2D_LF1Receiver ModuleMALT_TXMALT_RXMPROTECMTST_TXMTST_RXMNB_WBMAN_D8MVO_DATMCLKSERMDATSERMSTRORHEARBLOSQLRCANOCLogic testsREXT-LO-HICMIK (R/T LF)RSQL-OBMLEDsCPUSHB (Push-button)RSYNDPUR-LF3R-LF4Logic testsTLFREC (LF)TSIDETONETVHFT_RR_SYN_TMTST_TXMTST_RXMVO_DATMAM_D8MNB_WBMSTRO_TMDATSERMCLKSERMPROTECMALT_TX222222222252322222112(Audio Side tone)464A2Z-SA-ECPTTRAGCIFRCANOCRBLOSQLCMIK22RHEAFCOMP Figure 8 - Signal Connections
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A and EVR750-03-0100A   23-12-30 Page 232003/03/01 B.  Wired Chassis Assembly (CHC) The wired chassis assembly does the functions below (without the mechanical functions): −  electrical interface between the internal functions of the equipment, −  dissipation of the heat caused by the operation of the electrical subassemblies, −  control of a serviceability test using six LEDs. Ribbon cables connect the cards and the rear connector. The wired chassis assembly has one Design Function (DF): Name Short name Front Panel  CHC_FAV Table 4 - Wired Chassis Design Function CHCFront PanelCHC_FAV+5VLO_MICRO_FACE_AVHI_MICRO_FACE_AVTriggered Test (PB)HI_HEADPHONE_FACE_AVLEDs ControlLO_HEADPHONE_FACE_AV6B1Z-SA-EAlternat phonie Figure 9 - Wired Chassis (CHC) Block Diagram This DF has one TF: Name Short name Front Panel  CHC_FAV_FAV Table 5 - Front Panel Technical Function This TF is the front panel of the EVR716/750 transceiver. It has six LED type indicators, one ”TEST” pushbutton to trigger the tests. There are also two jack type sockets, one for the headset and the other for the microphone (See Figure 4).
 COMPONENT MAINTENANCE MANUAL P/N EVR716-01-0100A, EVR750-03-0100A and EVR750-04-0100A  LIST OF EFFECTIVE PAGES  23-12-30 INTRO - Page 242003/03/01 The six indicators are: −  ”FAIL LRU” (red):  lights  on  when  the  continuous or/and triggered tests (init or pushbutton) find a malfunction in the transceiver and not in the inputs (discrete or ARINC 429 bus). −  ”FAIL IN” (red):  lights on when the EVR716/750 transceiver finds a malfunction in the inputs (DFS ARINC 429 bus). −  ”PASS” (green):  lights on when the continuous or/and triggered tests (init or pushbutton) do not find any malfunctions. −  ”VSWR” (red):  lights on when the transceiver measures an VSWR larger than 2:1. −  ”Tx” (green):  lights on when the transceiver transmits. −  ”Rx” (green):  lights on when the transceiver is in receive mode.  The front panel connections are as follows:  Signal Input/Output SRU_DF_TF LED Tx control  I  DPU_G/M_AFFAV LED Tx control  I  DPU_G/M_AFFAV LED VSWR control  I  DPU_G/M_AFFAV LED PASS control  I  DPU_G/M_AFFAV LED FAIL LRU control  I  DPU_G/M_AFFAV LED FAIL IN control  I  DPU_G/M_AFFAV Front Panel Test (PB)  O  DPU_G/M_DECTEST +5V voltage  I  REC_ALM_+ 5V HI_CASQUE_FACE_AV (RHEA_H)  I  REC_AIGUI_BFAUDIO LO_CASQUE_FACE_AV (RHEA_L)  I  REC_AIGUI_BFAUDIO HI_MICRO_FACE_AV (CMIK_H)  O  REC_AIGUI_AUDIOIN LO_MICRO_FACE_AV (CMIK_L)  O  REC_AIGUI_AUDIOIN Alternat phonie (CPTT)  I

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