What was found
DURING A C CHECK INSPECTION, FOUND THE RT FUSELAGE SKIN AT FRAME 75, STRINGER 1R CRACKED. VERIFIED WITH NDT.SOP 5711. REPAIRED THE SKIN IAW SRM 53-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A C CHECK INSPECTION, FOUND THE RT FUSELAGE SKIN AT FRAME 75, STRINGER 1R CRACKED. VERIFIED WITH NDT.SOP 5711. REPAIRED THE SKIN IAW SRM 53-31-01.