What was found
DURING C1 CHECK INSPECTION WAS FOUND A CRACK AT FUSELAGE SKIN STA 1725.5 STRINGER 7 RT. DAMAGE WILL BE REPAIRED IAW EWO 767-53-016 AND SRM 53-80-01. THIS REPAIR CONSTITUTES A MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C1 CHECK INSPECTION WAS FOUND A CRACK AT FUSELAGE SKIN STA 1725.5 STRINGER 7 RT. DAMAGE WILL BE REPAIRED IAW EWO 767-53-016 AND SRM 53-80-01. THIS REPAIR CONSTITUTES A MAJOR REPAIR.