The method includes {HEAD ~ the steps} of: sensing whether the aircraft engine is operating near maximum power; upon sensing the condition, operating {TAIL ~ the jettison fuel pump} in fluid interconnection with the override fuel pump to deliver fuel to the fuel manifold; and upon sensing the cessation of the condition, deactivating the jettison fuel pump 
of operating
The method includes { HEAD ~ the steps } of : sensing whether the aircraft engine is operating near maximum power ; upon sensing the condition , operating { TAIL ~ the jettison fuel pump } in fluid interconnection with the override fuel pump to deliver fuel to the fuel manifold ; and upon sensing the cessation of the condition , deactivating the jettison fuel pump
OTH OTH OTH HEAD HEAD HEAD HEAD HEAD HEAD REL OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH REL TAIL TAIL TAIL TAIL TAIL TAIL TAIL TAIL OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH