What was found
FOUND DURING LETTER CHECK, FUSELAGE SKIN BULGED AND SKIN CRACKED EXTENDING FROM RIVET HOLES .0625 INCH 2 EA AT STA 530 AT FUSELAGE LAP JOINT STRINGER 26R. REPAIRED PER SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND DURING LETTER CHECK, FUSELAGE SKIN BULGED AND SKIN CRACKED EXTENDING FROM RIVET HOLES .0625 INCH 2 EA AT STA 530 AT FUSELAGE LAP JOINT STRINGER 26R. REPAIRED PER SRM 53-30-3.