What was found
FUSELAGE SKIN AT BS 660+10 BETWEEN STRINGERS 23R AND 24R DENTED. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-01 REPAIR 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN AT BS 660+10 BETWEEN STRINGERS 23R AND 24R DENTED. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-01 REPAIR 7.