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FARE Pump Failure During Ground FARE Refueling Operation
HYDRAULIC COMPARTMENTS CHECKS

TM-1-1520-240-CL Army CH-47D Heilcopter (EIC:RCD) Manual
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TM 1-1520-240-CL P-1 DETAILED PROCEDURES ERFS II For each installed ERFS II Tank Assembly. 1.  Tank restraint assembly — Check location and security. 2.  Cavity overboard drain — Check connection and security of drain in use. Check drain not in use is capped. 3.  Grounding cable — Check connection security. 4.  Vent   hose   assembly   —   Check   connection security.      Ensure   dust   cover   is   secure   on retention   strap   and   connection   to   dust   cap stowage connector. O 5.   Fuel     transfer     hose     assembly     —     Check connection security; all Unisex valves OPEN. O 6.   Single point pressure refueling hose assembly — Check connection security; Unisex valve at ERFS II Tank CLOSED. 7.  Electrical Harness — Check connection security of J1. 8.  Fuel quantity sensing wiring harness — Check connection security of J2. 9.  Fuel/defuel vent valve — Check in the CLOSED position. 10.  ERFS II tank sump fuel sample — Check before first flight of the day. 11.  Filler cap — Check in place, closed, and locked. 12.  ERFS II Fuel Control Panel — Check or set as follows: a.   Electrical harness - Helicopter receptacles to fuel control panel — Check connection security of J5. b.   Electrical  harness  -  Fuel  control  panel  to tank     assembly     —     Check     connection security of J1, J2, and J3.







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