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