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INTEGRA ARINC e-NAV 

DESCRIPTION, INSTALLATION, 

OPERATION MANUAL 

PAGE: 11 of 14 
REF.: DOC13033 
INDEX: B 
DATE: SEP 14/2016

 

 

© Orolia S.A.S.

 

6.3. Environmental Characteristics 

ENVIRONMENTAL CATEGORIES FORM FOR INTEGRA e-NAV ARINC 

Qualification 
Tests Title 

ED62A references 
(when applicable) 

DO-160F 
Section  

Category 

Temperature / Altitude 

ED-62A (SPECIAL) Class1  4.0 

As per ED-62A 

Low Temperature 

ED-62A (SPECIAL) -40°C  

4.5.1 

As per ED-62A 

High Temperature 
Activation 

ED-62A (SPECIAL) +55°C 

4.5.2 /3 

As per ED-62A 

In Flight Loss of Cooling 

N/A 

4.5.4 

Altitude 

ED-62A (SPECIAL) 50,000 
ft 

4.6.1 

As per ED-62A 

Decompression 

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 

 

Humidity 

 

Ops. shocks and crash 
safety 

ED-62A (SPECIAL) 

As per ED-62A 

Vibrations 

Fixed Wings 

R (C&C1)  

Helicopters 

U(G)

(1)

 

Explosion proofness 

N/A 

Waterproofness 

 

10 

Fluid susceptibility 

N/A 

11 

Sand and dust 

N/A 

12 

Fungus 

N/A 

13 

Salt spray 

 

14 

Magnetic effect 

 

15 

Power input 

 

16 

Voltage spike conducted 
susceptibility 

 

17 

Audio frequency 
conducted susceptibility 

 

18 

Induced signal 
susceptibility 

 

19 

ZC 

Radio frequency 
susceptibility 

 

20 

Conducted: T 
Radiated: L 

Radio frequency 
emission 

 

21 

Lightning transient 
susceptibility 

 

22 

A2G33 

Lightning direct effects 

N/A 

23 

Icing 

N/A 

24 

ESD 

 

25 

Fire, Flammability 

ED-62A (SPECIAL FLAME)  26 

As per ED-62A 

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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