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INTEGRA ARINC e-NAV 

DESCRIPTION, INSTALLATION, 

OPERATION MANUAL 

PAGE: 6 of 14 
REF.: DOC13033 
INDEX: B 
DATE: SEP 14/2016

 

 

© Orolia S.A.S.

 

4.  FIRST POWER UP PROCEDURE 

This  procedure  can  only  be  performed  by  the  installer,  as  it  requires  specific 
equipment such as a WS TECHNOLOGIES BT100 or any equivalent COSPAS-
SARSAT beacon decoder (AEROFLEX IFR 4000 opt1 for example) capable of 
being  connected  to  the  BNC  connector  of  the  ELT  in  order  to  decode  a 
COSPAS-SARSAT digital message at 406.037 MHz. 

4.1. Check of the ELT 

  Make sure that the ELT is programmed with a location protocol. 

4.2. Check of on board GPS equipment 

1.  Check that the RX ARINC link 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. Position Data Verification 

   CAUTION: Position  data verification  can  only  be checked if the ELT is 
activated. Never perform position data verification by checking the position 
data with the external antenna connected; in this case the 406 MHz would 
be  received  by  the  Cospas-Sarsat  Satellites  and  interpreted  as  a  real 
distress  message.  To  avoid  that,  connect  your  beacon  decoder  to  the 
external antenna output socket. 

4.3.1.   Tester Connection  

1.  Disconnect the antenna cable from the ELT antenna socket 
2.  Connect a Cospas-Sarsat tester to the antenna socket of the ELT as 

shown on figure 6 below: 

 

Figure 6: Beacon Tester Connection with ELT 

Summary of Contents for INTEGRA ARINC e-NAV

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 19: ......

Page 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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