Compressor Stall
Just a simple question..
A scenario:
After encountering a compressor stall on takeoff in a B737, the checklist items of reducing the thrust lever to idle etc are conducted. Now if the engine continues to operates normally, the thrust lever can be advanced to an intermediate position so as to keep the engine from stalling again. With the thrust lever now in an intermediate position my question is what flaps should be selected for landing back? Full Normal Landing Flaps or Single Engine Non Normal Flaps 15?
Thanks