Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (52
)
Page 31 of 54
CHAPTER 52 – DOORS AND WINDOWS (52-00-00)

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
METAL SHALL BE REMOVED.
52.3.3.4.1 Abrade corrosion pits with aluminum
oxide cloth (C-406) or abrasive pad (C-407) and
MEK (C-309) in any sequence to reduce pit size to
acceptable limits.
52.3.3.4.2 After corrosion has been removed
repeat step 52.3.3.3.
52.3.4 Cargo Hinged Panels
The hinged panel (located forward of sliding door)
(Figure 52-9) provides a wider opening for cargo
loading.
52.3.4.1 Removal
52.3.4.1.1 Open sliding passenger/cargo door.
52.3.4.1.2
Operate latch handle of hinged panel
door to release pins from upper and lower
channels of door opening. Swing door open.
52.3.4.1.3 Disengage positioning spring (2,
Figure 52-9) from stud at top of opening.
52.3.4.1.4 Remove quick-release pins (1) from
hinges (4). Remove door panel.
52.3.4.1.5 Remove unserviceable parts in
latching mechanism as follows:
52.3.4.1.5.1 Remove screws (6) and remove
cover (5).
52.3.4.1.5.2 Remove screws (23) and remove
cover (22).
52.3.4.1.5.3 Remove eight screws and three
nuts (10) with washers to detach escutcheon (11).
Remove escutcheon and handle (13) as an
assembly.
52.3.4.1.5.4 Remove cotter pin and pin (14) to
detach tube (9) from spindle assembly (12). Pull
tube inboard until pin (7) is free of guide in panel.
Remove pin from tube and remove tube through
access opening at top of panel.
52.3.4.1.5.5 Remove cotter pin and pin (14) to
detach tube (15) from spindle assembly (12).
Pull tube inboard until pin (16) is free of guide in
panel. Remove pin from tube and remove tube
through access opening at bottom of panel.
52.3.4.1.5.6 To remove striker mechanism
from top or bottom of panel, remove screw (17),
washer, and nut. Remove striker guide (18),
shim (19), plate (20), and striker (21).
52.3.4.2 Repair or replacement
52.3.4.2.1 Replace unserviceable parts in
latching mechanism (paragraph 52.3.4.3).
52.3.4.2.2 Repair door structural damage.
Refer to BHT-MED-SRM-1 and to FAA
Publication AC 43.13-1B, Aircraft Inspection and
Repair Manual for structural maintenance.
52.3.4.2.3 Repair or replace damaged window
(paragraph 52.7.6).
52.3.4.2.4 Repair or replace damaged seal(s)
(paragraph 52.1.2).
52.3.4.3 Installation
52.3.4.3.1
Assemble latching mechanism as
follows:
52.3.4.3.1.1 Position
striker guide (18, Figure
52-9) on outside surface of panel and shim (19),
plate (20), and striker (21) on inside surface of
panel. Install two screws (17) with washers and
nuts.
52.3.4.3.1.2 Insert tube (9) through access
opening at top of hinged panel door. Install nut
(8) and pin (7) on tube. Insert pin through guide
at top of panel. Connect tube (9) to spindle
assembly (12) using pin (14) and cotter pin.
52.3.4.3.1.3 Insert tube (15) through access
opening at bottom of hinged panel door. Install