CSP−900RMM−2MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 603
Revision 34
28-00-00
(9). Examine the fuel cell longitudinal
baffle for separation where the metal
baffle connects to the rubber.
(a). No separation is permitted.
(10). Inspect the installation of the fuel cell
frangible valves.
(a). Repair or replace components as
necessary.
(11). Inspect the fuel supply hoses for
deterioration, collapsed or kinked
hoses.
(a). No damage is permitted.
(12). Examine the the fuel supply hose
clamps for installation and deteriora
tion.
(a). Repair or replace components as
necessary.
(13). Examine the installation of the fuel
quantity probes.
(a). Repair or replace components as
necessary.
(14). Install the fuel cell access covers (ref.
Section 28-00-00, Removal/Installa
tion)
(15). Install access panels AL155, AR155,
A160, AL165, AR165, A170, A217,
AL230, and AR230 (ref. Section
53-20-00).
NOTE:
Use installation tool (T801) through hole
in the cabin floor panel to lift the top of
the fuel cell for installation of screws to
support the fuel cell to floor panel. Install
the vapor seal plug in the floor panel hole
(ref. Section 53-20-00).
As an alternate method use high-grade
steel all thread rods with large surface
flat washers and nuts. Insert threaded
rods through the cabin floor panel and
threaded hole in the fuel access panel.
Place large surface flat washers over the
floor panel and threaded rods. With nuts
installed on threaded rods, turn the nuts
down evenly until the fuel cell is located
in the correct position to the cabin floor
panel.
(16). Do the Fuel Cell Leak Check/Pressure
Test (ref. Procedure 4.).
(17). Fuel the rotorcraft (ref. Section
12-00-00)
(18). Install the carpet, if applicable (ref.
Section 25-20-00).
(19). Install the cabin seats, if applicable
(ref. Section 25-20-00).
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