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INTEGRA ARINC e-NAV 

DESCRIPTION, INSTALLATION, 

OPERATION MANUAL 

PAGE: 5 of 14 
REF.: DOC13033 
INDEX: B 
DATE: SEP 14/2016

 

 

© Orolia S.A.S.

 

3.  INTEGRA ARINC e-NAV CONNECTION 

3.1. Connectors and Cables 

3 separate shielded cables have to be wired to the plug connected to the 19 
Pin male socket. 

  A 2-Wire cable to connect INTEGRA ARINC e-NAV to the On Board 28 V 

DC power supply. 

  A 2-Wire cable to connect INTEGRA ARINC e-NAV to the On Board GPS 

equipment 

  A 6-Wire cable to connect INTEGRA ARINC e-NAV to the ELT 

Wires of AWG24 gauge should be preferred. 

A 19 Pin female plug reference SOURIAU 851 06 R 14 19 S 50 shall be used 
to connect the INTEGRA ARINC e-NAV (this plug is not provided) 

 

Figure 5: 19 Pin female plug, View from Back Face of Inserts 

3.2. Connection to On Board 28V DC Power Supply 

Refer to Section 7, Connecting Diagram

 

3.3. Connection to On Board GPS Equipment 

Refer to Section 7, Connecting Diagram

 

3.4. Connection to INTEGRA (ER-N) ELT 

  Fabricate a 6-wire cable long enough to reach the INTEGRA (ER-N) ELT. 

  On the ELT side, connect a DIN-12 connector, P/N S1820514-03 (Not 

supplied). 

IMPORTANT: It is not possible to use a programming dongle in this 
cable.

 

Refer to Section 7, Connecting Diagram

 

 

Содержание INTEGRA ARINC e-NAV

Страница 1: ...520 GUIDEL FRANCE Telephone 33 0 2 97 02 49 49 Fax 33 0 2 97 65 00 20 Web http www mcmurdogroup com E mail info mcmurdogroup com REF DOC13033 INDEX B DATE SEP 14 2016 INTEGRA ARINC e NAV DESCRIPTION I...

Страница 2: ...S A S Users are kindly requested to notify Orolia S A S of any discrepancy omission or error found in this manual Please report to our customer support E mail support mcmurdogroup com Tel 33 0 2 97 0...

Страница 3: ...4 Connection to INTEGRA ER N ELT 5 4 FIRST POWER UP PROCEDURE 6 4 1 Check of the ELT 6 4 2 Check of on board GPS equipment 6 4 3 Position Data Verification 6 4 3 1 Tester Connection 6 4 3 2 Test prep...

Страница 4: ...IGURES Figure 1 INTEGRA ARINC e NAV Overview 1 Figure 2 Example of INTEGRA ARINC e NAV installed on Mounting Bracket 2 Figure 3 INTEGRA ARINC e NAV Concept 3 Figure 4 INTEGRA ARINC e NAV Installation...

Страница 5: ...the 406 MHz distress message as soon as the ELT is activated This manual contains information to install and operate the INTEGRA ARINC e NAV Part Number S1850581 01 1 2 INTEGRA ARINC e NAV Presentati...

Страница 6: ...specific INTEGRA ELT mounting bracket Bracket Universal for INTEGRA ARINC e NAV for ELT AP P N S1850551 01 when connect to an AP INTEGRA ER N or AP H INTEGRA ER N ELT or Bracket Universal for INTEGRA...

Страница 7: ...olia S A S 1 3 Concept The 19 Pin male socket has to be connected to 3 separate cables On Board 28 VDC power supply ARINC frames of the On Board GPS equipment DIN 12 plug of the ELT In addition the EL...

Страница 8: ...s supports either with its connector on the left side or on the right side 2 Fix the INTEGRA ARINC e NAV onto the mounting bracket with the 2 captive screws and tighten to a torque of 1 4 Newton per m...

Страница 9: ...e ELT Wires of AWG24 gauge should be preferred A 19 Pin female plug reference SOURIAU 851 06 R 14 19 S 50 shall be used to connect the INTEGRA ARINC e NAV this plug is not provided Figure 5 19 Pin fem...

Страница 10: ...nk of the aircraft GPS equipment is activated refer to the GPS equipment relevant manual 2 Switch the GPS equipment to ON 3 Wait for the acquisition of a GPS valid position on the GPS equipment 4 3 Po...

Страница 11: ...LT in aluminum or copper foil 4 3 3 Validation Procedure NOTE For ELT operation refer to the relevant ELT Operation Manual 1 After having performed all wiring tasks as indicated in Section 3 INTEGRA A...

Страница 12: ...ata Protocols Unique ELT Serial Number 4 minutes User Location 1 4 seconds Standard Location Aircraft Operator Designator Serial Number 4 minutes User Location 1 4 seconds Standard Location Aircraft 2...

Страница 13: ...m a self Test by switching ELT to OFF then to ARM After 5 seconds the LED of INTEGRA ARINC e NAV switches ON GREEN 28V DC is correct and ARINC Frame is valid Red 28V DC is not correct and or ARINC Fra...

Страница 14: ...d longitude are encoded on 21 bits and use both Data field bits 29 11 and SDI field 10 and 9 bits Parity bit can be checked or not by INTEGRA ARINC e NAV ARINC RX1 ARINC positive input ARINC RX2 ARINC...

Страница 15: ...ompression ED 62A SPECIAL 4 6 2 As per ED 62A Overpressure 4 4 3 ED 62A 4 6 3 As per ED 62A Temperature variation 5 B Humidity 6 C Ops shocks and crash safety ED 62A SPECIAL 7 As per ED 62A Vibrations...

Страница 16: ...ratures Specifications Operating 40 C to 55 C Class 1 Storage 55 C to 85 C 6 5 Electrical Characteristics Power supply Aircraft 28 VDC Consumption 7 mA typical 12 5 mA max 28 V established mode 300 mA...

Страница 17: ...2016 Orolia S A S 7 CONNECTING DIAGRAM NOTE RCP mating connectors and relevant RCP pin out inputs are defined in the INTEGRA ELT initial installation Manual supplied with the ELT For complete instruct...

Страница 18: ...TEGRA ARINC e NAV DESCRIPTION INSTALLATION OPERATION MANUAL PAGE 14 of 14 REF DOC13033 INDEX B DATE SEP 14 2016 Orolia S A S 8 SERVICING Maintenance is on demand only No periodic inspection is require...

Страница 19: ......

Страница 20: ...Orolia S A S Orolia S A S Z I des Cinq Chemins CS10028 56520 GUIDEL FRANCE Phone 33 0 2 97 02 49 49 Fax 33 0 2 97 02 65 00 20 Website www mcmurdogroup com Email info mcmurdogroup com DOC13033B...

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