MD Helicopters MD Explorer - Page 874

CSP−900RMM−2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 604
Revision 1
28-10-00
(18). Reinstall panels and retest.
(19). If test is successful, slowly release air
pressure from fuel cell, disconnect the
air supply and U-tube manometer
(T2014-4) hose from the fuel transfer
hose.
(20). Reconnect vent hose to vent tube and
secure with lockwire (C702).
(21). Reconnect fuel transfer hose to elbow
fitting. Torque fitting (Ref. CSP-SPM).
(22). Reinstall aft left main fuel tank
vent/rollover valve access panel AL230
(Ref. Section 53-20-00).
(23). Reinstall baggage floor panels (Ref.
Section 53-20-00).
BL
0.00
FS
235.532
1
2 (2PL)
3
9G28-075
1. VENT HOSE
2. LOCKWIRE
3. VENT TUBE
Figure 601. Supplemental Fuel Tank Leak/Pressure Test Method 1 (Sheet 1 of 2)