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INTEGRA ARINC e-NAV 

DESCRIPTION, INSTALLATION, 

OPERATION MANUAL 

PAGE: 12 of 14 
REF.: DOC13033 
INDEX: B 
DATE: SEP 14/2016

 

 

© Orolia S.A.S.

 

Environmental Categories 

  Fixed wings versions: RTCA DO-160G / EUROCAE ED14G chapters 4 to 

26 

-  [ED62A]X[ED62A]C[ED62A][R(C&C1)U(G)]XRXXXSAZAZ[ZC][TL]H[A

2G33]XXA[ED62A] 

  Helicopters versions: RTCA DO-160G / EUROCAE ED14G chapters 4 to 

26 

-  [ED62A]X[ED62A]C[ED62A][U(G)] 

XRXXXSAZAZ[ZC][TL]H[A2G33]XXA[ED62A] 

Storage temperature: -55 °C to +85 °C 

6.4. Temperatures Specifications 

  Operating: -40 °C to +55 °C (Class 1) 

  Storage: -55 °C to +85 °C 

6.5. Electrical Characteristics 

  Power supply: Ai28 VDC 

  Consumption: 7 mA typical, 12.5 mA max@28 V (established mode). 

                       300 mA max. (Power up). 

6.6. Compatibility List 

6.6.1.  ELT 

-  INTEGRA AP (ER-N):  

P/N S1850501-03 

-  INTEGRA AF (ER-N):  

P/N S1851501-03 

-  INTEGRA AF-H (ER-N):   P/N S1852501-03 
-  INTEGRA AP-H (ER-N):   P/N S1854501-03 

6.6.2.  Mounting Brackets 

-  Universal Mounting Bracket for INTEGRA ARINC e-NAV for ELT (AP):  

P/N S1850551- 01 

-  Universal Mounting Bracket  or INTEGRA ARINC e-NAV for ELT (AF): 

P/N S1850551 - 02 

6.6.3.  GPS 

-  All GPS compatible with ARINC 429 / 743 standards 
-  Data rate: 12.5 kbits/s or 100 kbits/s. 

 

 

 

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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