Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (63)
Page 82 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
63.5.20 Oil Pressure Transmitter
63.5.20.1 Removal
63.5.20.1.1
Disconnect electrical connector (5,
Figure 63-37).
63.5.20.1.2
Remove pressure transmitter (4)
with packing (3). Discard packing.
63.5.20.1.3
Cap or plug exposed cavity in
manifold (2).
63.5.20.2 Inspection
Inspect transmitter (4, Figure 63-37) and electrical
connector for bent pins, damaged threads, dents,
or other mechanical damage rendering transmitter
unserviceable.
63.5.20.3 Installation
MATERIALS REQUIRED
Refer to BHT-ALL-SPM for specification and
source.
NUMBER NOMENCLATURE
C-405 Lockwire
63.5.20.3.1
Lubricate packing (3, Figure 63-
37) with transmission oil (Chapter 12).
63.5.20.3.2
Install packing (3) on transmitter
(4).
63.5.20.3.3
Install transmitter (4) in manifold
(2). Apply lockwire (C-405) to transmitter.
63.5.20.3.4
Install electrical connector (5).
63.5.20.3.5 Perform functional check of
pressure transmitter (Chapter 96) and check for oil
leaks at next helicopter ground run.