What was found
DENT ON FUSELAGE SKIN STA 33.45 BETWEEN S-21L TO S-22L. FOUND OUT TO BE OUT OF LIMIT IAW SRM 53-00-01, PG 101. DETAIL IV HFEC ON CUT- OUT & INITIAL FUSELAGE HOLES IAW NTM 51-00-19PT 6, NO CRACK NOTED. FABRICATED DOUBLER AND FILLER IAW SRM 53-00-01 PG 201, TABLE I. INSTALLED DOUBLER & FILLER IAW SRM 51-40-02 AND SRM 53-00-01 PG 201, FIG 201, REPAIR 2, CAT B REPAIR ZONE A, THRESHOLD INSP 37,500 FLIGHT CYCLE, INTERVAL 6,000 FLIGHT CYCLE, HFEC, NDT PT6 51-00-01. MAJOR REPAIR.