What was found
DEFORMATION OF STRINGER AT C65, P38 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DEFORMATION OF STRINGER AT C65, P38 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.