Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (29)
Page 38 of 50
CHAPTER 29 – HYDRAULIC SYSTEM (29-00-00)
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COPYRIGHT

2007 BY DART AEROSPACE LTD.
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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:
6
Date: 13.08.26
Figure 29-8. Hydraulic cylinder boot
29.3.8.2.2.6 Remove bolt attaching lower or end
bearing (19) to support (20) and ensure no side
loads have been induced into lower piston rod. If
necessary, loosen and retighten bearing and
jamnuts (11 and 12) to assure proper cylinder
alignment in airframe.
29.3.8.3 Installation
MATERIALS REQUIRED
NUMBER NOMENCLATURE
C-101 Corrosion Compound Preventive
C-104 Corrosion Compound Preventive
C-308 Sealant
C-405 Lockwire
29.3.8.3.1 Coat threads of clevis (8, Figure 29-
7) with corrosion preventive compound (C- 101).
29.3.8.3.2 Assemble jam nut and lock on clevis
and install in end of cylinder (13) to 1.75 in.
(44.45 mm) between end of cylinder rod and
center of hole in clevis. Torque jamnut 660 to
780 in-Lbs. (74.57 to 88.12 Nm).
29.3.8.3.3 Secure jam nut with Iockwire (C-
405). Apply sealant (C-308) around nut, lock,
and threads on clevis.
29.3.8.3.4 Attach clevis (8) to universal (7) with
bolt, using washers under bolt head and nut.
Torque nut 100 to 140 in.lbs. (11.30 to 15.82
Nm). Install cotter pin.