What was found
DURING A C CHECK, FOUND THE LT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 1L TO 2L, VERIFIED BY SOP 5711, NDT. REPAIRED 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, FOUND THE LT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 1L TO 2L, VERIFIED BY SOP 5711, NDT. REPAIRED IAW SRM 53-31-01.