Eagle ICA-D212-725, Инструкция по эксплуатации

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ICA-D212-725 (52
)
Page 38 of 54
CHAPTER 52 – DOORS AND WINDOWS (52-00-00)
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COPYRIGHT

2007 BY DART AEROSPACE LTD.

THIS DOCUMENT IS PRIVATE AND CONFIDENTIAL AND IS SUPPLIED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED FOR ANY PURPOSE OR COPIED OR COMMUNICATED TO
ANY OTHER PERSON WITHOUT WRITTEN PERMISSION FROM DART AEROSPACE LTD.
Revision: 4
Date: 11.06.01
52.5.1.2 Inspection
52.5.1.2.1 Inspect hinges for cracks and
distortion.
52.5.1.2.2 Inspect latches for operation and
security.
52.5.1.2.3 Inspect door for structural damage.
52.5.1.2.4 Inspect seal for secure bonding and
for deterioration.
52.5.1.3 Repair
52.5.1.3.1 Replace unserviceable parts in nose
access doors.
52.5.1.3.2 Repair door structural damage. Refer
to BHT-MED-SRM-1 and FAA Publication AC
43.13-1B, Aircraft Inspection and Repair Manual
52.5.1.3.3 Replace damaged seals (paragraph
52.1.2).
52.5.1.4 Installation
52.5.1.4.1 Position upper door to structure and
align attachment holes at top of door with holes in
hinges.
52.5.1.4.2 Install screws and engage latches or
install attaching studs.
52.5.1.4.3 Install lower door hinges to fittings on
structure.
52.5.1.4.4 Close door and install attaching studs.
52.5.2 Electrical and Equipment
Compartment Access Doors
Access to forward fuselage section compartments,
other than the crew area, is obtained by use of
hinged doors.
52.5.2.1 Removal
52.5.2.1.1 Release spring loaded latches and
hold door open.
52.5.2.1.2 Remove hinge pins attaching doors
to structure and remove door.
52.5.2.2 Inspection and repair
Inspect and repair electrical compartment
access door in accordance with procedures in
paragraphs 52.5.1.2 and 52.5.1.3.
52.5.2.3 Installation
52.5.2.3.1 Position door in opening and insert
attaching hinge pin.
52.5.2.3.2 Close door firmly, forcing spring
loaded latch to lock.
52.5.3 Miscellaneous Access Doors
Doors and panels are provided at various
locations on the fuselage for access to interior
areas. Three types of construction are used:
Honeycomb with sheet metal and fiberglass
faces; honeycomb with both faces of fiberglass;
and contoured flat sheet metal. Screws or twist
type fasteners retain doors in place.
52.5.3.1 Removal
Remove screws or disengage fasteners, as
applicable, and remove door, panel, or fairing.
52.5.3.2 Inspection and repair
Inspect and repair electrical compartment
access door in accordance with procedures in
paragraphs 52.5.1.2 and 52.5.1.3.