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 {TAIL ~ the fuel manifold}; and upon sensing {HEAD ~ the cessation} of 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 { TAIL ~ the fuel manifold } ; and upon sensing { HEAD ~ the cessation } of the condition , deactivating the jettison fuel pump
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