Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (53)
Page 4 of 19
CHAPTER 53 – FUSELAGE (53-00-00)
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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
53.3.2 Crew Seat Tracks - Installation
53.3.2.1 Install right hand track assemblies (3,
Figure 53-3) as follows:
53.3.2.1.1 Make sure the mating surfaces are
clean.
53.3.2.1.2 Install the right hand track assembly
(3) with the screws (1) and the washers (2).
WARNING
MAKE SURE YOU INSTALL THE SPACERS (5)
ON THE LEFT HAND TRACK ASSEMBLY (6) AS
SHOWN. IF THE SPACERS ARE OMITTED,
THE SEAT CAN INTERFERE WITH
COLLECTIVE STICK TRAVEL.
53.3.2.2
Install the left hand track assemblies
(6) as follows:
53.3.2.2.1 Make sure the mating surfaces are
clean.
53.3.2.2.2 Install the left hand track assembly (6)
with the two screws (4) and spacers (5) in the
second hole position from the front of the track.
53.3.2.2.3 Install
the screws (1) and the washers
(2) in the remaining holes.
53.3.2.3 Install the applicable crew seat
(Chapter 25)
53.4 TENSION ROD ASSEMBLY
53.4.1 Tension Rod Assembly - Removal
53.4.1.1
Remove the nut (1, Figure 53-4),
bolt (3) and washers (2) from the aft end of the
tension rod assembly (4).
53.4.1.2 Remove the nut (1), bolt (3),
washers (2) and tension rod assembly (4) from
the bulkhead attachment point.
53.4.2 Tension Rod Assembly - Inspection
53.4.2.1
Examine the tension rod assembly
(4, Figure 53-4) for cracks, wear, mechanical
damage and corrosion damage (Figure 53-5).
Repair or replace as applicable.
53.4.3 Tension Rod Assembly - Installation
53.4.3.1
Install the tension rod assembly (4,
Figure 53-4) on the bulkhead attachment point
with the bolt (3), washers (2) and nut (1).
Tighten the nut.
53.4.3.2
Install the aft end of the tension rod
assembly (4) with the bolt (3), washer (2) and
nut (1). Tighten the nut.