What was found
INSPECTION TYPE:C+SI, STR 21 RT CRACKED AT FRAME ATTACH POINTS BS 380. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C+SI, STR 21 RT CRACKED AT FRAME ATTACH POINTS BS 380. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1.