Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (52
)
Page 20 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
52.2.2.1.5
Disassemble ejection mechanism as
follows:
52.2.2.1.5.1 Remove cotter pins and two pins
(14) to detach upper and lower hinge pins (17 and
23) from plate (25) and link (13).
52.2.2.1.5.2 Remove bolt (26) with nut, washers,
and spacer (24) to separate plate and link from
support (16).
52.2.2.1.6
Remove ejection cable as follows:
52.2.2.1.6.1 Disconnect aft end fork of cable (9)
from latch striker (1) by removing cotter pin and
pin (3).
52.2.2.1.6.2 Pull cable aft out of flex tube (7)
leaving tube in place.
52.2.2.2 Installation
52.2.2.2.1
Check ends of jettison cable flex
tube for proper installation:
52.2.2.2.1.1 Aft end of flex tube (7, Figure 52-5)
should be positioned vertically at F.S. 68.96 in
door post, secured between clamp (4) and spacer
(5) attached to bracket (6) on structure with two
screws, washers, and nuts. End of tube should
extend 0.10 in. (2.54 mm) above clamp.
52.2.2.2.1.2 Forward end of flex tube should
pass up through grommet (12) in nose structure
forward of door opening, and be secured between
clamp (10) and spacer (11) attached to structure
with two screws, washers, and nuts. End of tube
should extend 0.10 in. (2.54 mm) above horizontal
angle at W.L. 30.
52.2.2.2.2
Thread plain end of ejection cable
(9) through flex tube (8) from aft end.
NOTE
Forward end of cable will be attached during
installation of jettison mechanism.
52.2.2.2.3
Attach cable fork terminal on aft end
of latch striker (1) with pin (3) secured by cotter
pin. Verify spring (2) is attached between striker
and bracket in door post.
52.2.2.2.4 Install jettison mechanism as
follows:
52.2.2.2.4.1 Insert spacer (24) through pivot
holes of plate (25) and link (13).
52.2.2.2.4.2 Place standard steel washer on
bolt (26), and insert bolt from plate side through
spacer.
52.2.2.2.4.3 Place thin aluminum washer on
bolt next to spacer, and insert bolt (26) through
support (16).
52.2.2.2.4.4 Install nut (15) and aluminum
washer on outboard end of bolt and torque 50 to
70 in-Lbs. (5.65 to 7.91 Nm).
52.2.2.2.4.5 Position
slotted ends of hinge pins
(17 and 23) between plate (25) and link (13),
align holes, and install pins (14) secured by
cotter pins.
52.2.2.2.4.6
Position assembly in nose
structure, with hinge pins inserted in hinge
bushings and support (16) resting on horizontal
structural member at W.L. 30.
52.2.2.2.4.7 Align support (16) to holes with
plate nuts, and install two bolts (18) with
aluminum washers. Torque bolts 20 to 25 in-
Lbs. (2.26 to 2.82 Nm).
52.2.2.2.4.8 Position handle (30) with tube (28)
inserted through grommet (27) at W.L. 35.56.
Align clamps (29) to mounting holes in angle
and attach with two screws, washers, and nuts.
52.2.2.2.4.9 Connect fork terminal of cable
(22) to forward end of plate (25) with pin (21),
washer, and cotter pin.
52.2.2.2.5 Connect
cable (9) with swivel (8)
to hole with bushing in middle of plate (25).
Adjust cable length to remove slack with hinge
pins extended and latch striker (1) held down in