Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (71)
Page 28 of 28
CHAPTER 71 – POWER PLANT SYSTEM (71-00-00)
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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: 5
Date: 12.06.20
adapter located at top of engine, forward of the
combustion chamber. Route the hose assembly
aft and downward across the combustion
chamber. Secure hose to combustion chamber
section using engine supplied hardware and
clamps.
71.4.3.19.6
Connect engine breather hose,
end fitting to engine breather port union fitting,
located at lower right side of engine compressor
section.
71.4.3.19.7
Connect tank to engine oil inlet
hose, to union fitting in inlet port of engine oil
pump located at lower right side of the
compressor section of engine.
71.4.3.19.8
Connect engine oil outlet hose,
to the elbow fitting in the outlet port of the engine
oil pump located at lower side of the engine
compressor section. Torque hose-to-fitting
locking nut 750 to 850 inch-pounds. Position
shroud over connection and secure with clamp.
71.4.3.19.9
Connect fuel inlet hose elbow
fitting to fuel inlet port union fitting of fuel control.
Position shroud over connection and secure with
clamp.
71.4.3.19.10
Connect tailpipe drain hose to
lower fitting of tailpipe.
71.4.3.20
Install electrical harness as
follows: The electrical harness is installed as
per the Installation Instructions IIN-D212-725.
71.4.3.21
Install output driveshaft adapter.
(Refer to Chapter 66)