What was found
ON APPROACH TO NGF FLAPS LOCKED AT 20 DEGREES WITH FLAP HANDLE AT POSITION 30. PERFORMED FSEU BITE IAW FIM 27-51-00, FIG 104, STEP 4. NO FAULTS FOUND. PERFORMED T/E FLAP ADJUSTMENT AND TEST IAW AMM 27-51-00, PAGE 501. RAN FLAPS WITH HYDRAULICS AND ELECTRICALLY. NO FAULTS NOTED. AIRCRAFT OK FOR SERVICE.