Installation Maintenance Manual
FMHPA 82166
6-6
Jul 2008
©
THALES AVIONICS Ltd. This document and any
information included are the property of Thales Avionics.
They cannot be reproduced, disclosed or utilized without the
company’s prior written approval
b.
The part numbers (see section 2) of the LRU being installed (FMHPA)
should be placed into the aircraft operator‚ appropriate aircraft
Illustrated Parts Catalogue (IPC).
c.
Wiring connection information contained in this manual (see sections 2
and 3) should be placed into the aircraft operator‚ appropriate Wiring
Diagram Manual.
d.
The FMHPA maintenance is considered as an ‚ “On-condition”‚ and as
such no additional maintenance is required other than a check for
security and operation at normal inspection intervals.
e.
If a system LRU is inoperative remove the specific unit, secure cables
and wiring, collar applicable switches and circuit breakers, and placard
them inoperative. Revise equipment list and weight and balance as
applicable prior to flight and make a log book entry that the unit was
removed (refer to section 91.213 of the FAR or the aircraft‚ Minimum
Equipment List (MEL).
f.
FMHPA can be repaired by an Approved Maintenance Organization or
an appropriately rated FAA Part 145 repair station.
g.
Once repaired, reinstall the LRU in the aircraft in accordance with the
original Form 337 approved data or instructions in this manual. Perform
a Return to Service test of the system and approve it for return to service
with a logbook entry required by section FAR Part 145 Section 43.9.
h.
Once repaired, install the LRU in the aircraft in accordance with the
original Form 337 approved data or instructions in this manual. Do a
Return to Service test of the system and approve it for return to service
with a log book entry in accordance with the requirements specified in
FAR Part 145 Section 43.9.
