What was found
FUSELAGE EXTERIOR SKIN CRACKED AT CANTED FRAME, BS 1531 LT SIDE. REPAIRED IAW SRM 53-00-01, FIG 6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERIOR SKIN CRACKED AT CANTED FRAME, BS 1531 LT SIDE. REPAIRED IAW SRM 53-00-01, FIG 6.