What was found
FOUND EVIDENCE OF A CRACK STARTING AT A FASTENER HOLE ON THE RIGHT EXTERNAL SIDE OF THE FUSELAGE SKIN BETWEEN STRINGER 21R & STRINGER 22R & FRAMES 40 TO 41. BLENDED AREA IN REF TO SRM 51-74-10. ORIGINAL MATERIAL THICKNESS 0.061 IAW SRM 53-14-12. MATERIAL REMOVED WAS 0.002. MATERIAL REMAINING IS 0.059. FOUND TO BE WITHIN LIMITS IAW SRM 53-10-12; DIA 0.112. ACCOMPLISHED HFEC INSPECTION PER NTM PART 6; 51-10-8; NO CRACK NOTED. ALODINED IAW SRM 51-21-10. PRIMED & TOP COATED IN REF TO AMM 51-23-10-0.