2. An identification of the Firmware version on the cover of the housing. 3. A LED to indicate the INTEGRA ARINC e-NAV status. 4. A 19 Pin male socket to connect the INTEGRA ARINC e-NAV to the ELT, A/C +28V DC and on board GPS.
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DESCRIPTION, INSTALLATION, DATE: SEP 14/2016 OPERATION MANUAL The INTEGRA ARINC e-NAV is to be mounted on a 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 ...
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 meter using a torque driver with a 2.5 mm Allen bit.
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 ...
PAGE: 6 of 14 INTEGRA ARINC e-NAV REF.: DOC13033 INDEX: B DESCRIPTION, INSTALLATION, DATE: SEP 14/2016 OPERATION MANUAL 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-...
SELF TEST 1. Switch the ELT from OFF to ARM. 2. 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 Frame is not valid.
National 4 seconds Administration Location NOTE (1): These protocols are not available by default in Kannad e-Prog Software 6. Switch the ELT to OFF. 7. Disconnect the Cospas-Sarsat tester. 8. Connect the antenna cable to the antenna socket of the ELT.
If the ELT switch is on ARM position, perform 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, ...
Dimensions: 85 x 74 x 40 mm (3.346 x 2.913 x 1.574 in) Weight: 176 g. (0.388 lbs) typical 6.2. ARINC Frames Specifications The format of frames accepted by INTEGRA ARINC e-NAV are as follows: ARINC Bits 31->30 29->9...
PAGE: 13 of 14 INTEGRA ARINC e-NAV REF.: DOC13033 INDEX: B DESCRIPTION, INSTALLATION, DATE: SEP 14/2016 OPERATION MANUAL 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.