Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (28)
Page 46 of 48
CHAPTER 28 – FUEL SYSTEM (28-00-00)
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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: 6
Date: 13.08.26
28.28.1 Removal
28.28.1.1
Open engine cowling on the left side.
28.28.1.2 Disconnect fuel hose from outlet fitting
(1, Figure 28-14) on filter head (4). Drain fuel from
filter by opening drain valve (6) located under filter
head (4).
28.28.1.3
Remove filter element (10) as follows:
NOTE
Change fuel filter element when fuel filter caution
light illuminates.
28.28.1.3.1 Open V-band clamp (8).
28.28.1.3.2 Remove filter body (11) and element
(10), from filter head (4).
28.28.1.3.3 Separate element (10) and packings
(9) from filter body (11).
28.28.1.3.4 The filter head (4) will normally
remain in place but can be removed when
necessary by disconnecting electrical cable plug
(3), fuel line (2), drain line (5), pressure transmitter
line (13), and removing four bolts (7).
28.28.2 Installation
28.28.2.1 If removed, reinstall filter head (4,
Figure 28-9), secure to firewall with bolts (7) and
washers. Secure bolt (7) heads with lockwire (C-
405). Connect fuel line tube (2), filter outlet fitting
(1), and drain line (5) to drain valve (6) at bottom
of filter head (4). Connect and secure electrical
cable plug (3) with lockwire (C-405). Connect fuel
pressure transmitter line (13) to filter head (4) and
to pressure transmitter (12).
28.28.2.2 Install
filter element (10) and filter
body (11).
28.28.2.2.1 Place packing (9) on boss in bottom
of filter body (11).
28.28.2.2.2 Place clean filter element (10) in
body, seated firmly on boss.
28.28.2.2.3 Install packing (9) around upper lip of
filter body (11), next to flange.
28.28.2.2.4 Place packing (9) around center boss
in (C-405).
28.28.2.2.5 Install body assembly into filter head
(4), pressing firmly to seat.
28.28.2.2.6 Install V-band clamp (8) around
mating flanges of filter head (4) and filter body (11).
Torque nut on clamp (8) 50 inch-pounds.
28.28.2.3
Connect hose from engine fuel control
inlet to outlet fitting on filter.
28.28.2.4
During next ground run-up, check fuel
filter and connections for leaks. Also check that
FUEL FILTER light on caution panel does not come
on.
28.29 PRESSURE TRANSMITTER
One electrical transmitter of the fuel pressure gage
system, mounted on left rear side of the forward
engine firewall, is connected to main fuel filter.
28.29.1 Removal
MATERIALS REQUIRED
NUMBER NOMENCLATURE
C-428 Caps and/or Plugs
28.29.1.1
Disconnect electrical power
28.29.1.2 Open engine cowling for access to rear
left side of aft cabin bulkhead.
28.29.1.3 Disconnect electrical connector (1,
Figure 28-15) from pressure transmitter (4).
28.29.1.4
Disconnect tube (12) from union (11).
28.29.1.5 Remove union (11) and packing (10).
Discard packing.