What was found
LT FUSELAGE SKIN 2 EACH DENTS AT BS 887 APPROX 6 INCHES ABOVE STRINGER L20 JUST FWD AND AFT OF OF 887 L FRAME. REMOVED DAMAGE AND INSTALLED REPAIR REF SRM 53-00-01 REPAIR 31 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT FUSELAGE SKIN 2 EACH DENTS AT BS 887 APPROX 6 INCHES ABOVE STRINGER L20 JUST FWD AND AFT OF OF 887 L FRAME. REMOVED DAMAGE AND INSTALLED REPAIR REF SRM 53-00-01 REPAIR 31 FIG 201.