What was found
DURING A C CHECK INSPECTION, THE REAR FUSELAGE SKIN WAS FOUND CRACKED AT FRAME 75, NEAR STRINGERS 2L & 3L. MAINTENANCE PERFORMED TYPICAL DOUBLER REPAIR 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, THE REAR FUSELAGE SKIN WAS FOUND CRACKED AT FRAME 75, NEAR STRINGERS 2L & 3L. MAINTENANCE PERFORMED TYPICAL DOUBLER REPAIR IAW SRM 53-31-01.