Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (63)
Page 72 of 144
CHAPTER 63 – MAIN ROTOR DRIVE SYSTEM (63-00-00)

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:
6
Date: 13.08.26
63.5.15 Transmission Oil Jet No. 5
63.5.15.1 Removal
63.5.15.1.1
Remove screw (4, Figure 63-31).
63.5.15.1.2
Extract jet (3) with packings (1
and 2).
63.5.15.1.3
Discard packing (2 and 3).
63.5.15.1.4
Remove screw (5) and washers (6
and 7).
63.5.15.2 Cleaning
Refer to paragraph 63.5.10.2.
63.5.15.3 Inspection
Refer to paragraph 63.5.10.3.
63.5.15.4 Repair
Refer to paragraph 63.5.10.4.
63.5.15.5 Installation
MATERIALS REQUIRED
Refer to BHT-ALL-SPM for specification and
source.
NUMBER NOMENCLATURE
C-405 Lockwire
63.5.15.5.1
Install screw (5, Figure 63-31) with
washers (6 and 7) on jet (3).
63.5.15.5.2
Lubricate new packings (1 and 2)
with transmission oil (Chapter 12) and install in
grooves of jet.
63.5.15.5.3 Carefully insert jet (3) into
transmission case.
63.5.15.5.4
Install screw (4).
63.5.15.5.5
Secure screw (5) to screw (4) with
Iockwire (C-405).
63.5.15.5.6
Check for oil leaks at next
helicopter ground run.