Eagle ICA-D212-725, Instructions Manual

Page: 192 / 729

ICA-D212-725 (28)
Page 43 of 48
CHAPTER 28 – FUEL SYSTEM (28-00-00)
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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
28.27.2.6 Install washer (15) and nut (14) on
union (16).
28.27.2.7 Connect fuel inlet lines to fittings on
bottom of fuel valve manifold (28).
28.27.2.8 Connect electrical connector to fuel
shutoff valve (10) and secure with lockwire (C-
405).
28.27.2.9 Connect fuel line to union (16).
Position shroud over fuel line fitting and secure
with clamp.
28.27.2.10 Turn battery switch ON, turn both boost
pump switches ON, move FUEL VALVE switch to
ON. Check all disturbed points for fuel leaks.
Observe that manual override handle on fuel shutoff
valve (10) moves to open position. Move FUEL
VALVE switch to OFF, observe that manual override
handle moves to closed position. Turn both boost
pump switches OFF. Turn battery switch OFF.
28.27.2.11 Close engine cowling and install access
panel on pylon island.