What was found
DURING C4 CHECK FUSELAGE SECTION 43 SKIN DENT DAMAGE STRINGER CRACK, STA 720 S22L - S24L. REPAIR WAS PERFORMED WITH EWO 767-53-118.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C4 CHECK FUSELAGE SECTION 43 SKIN DENT DAMAGE STRINGER CRACK, STA 720 S22L - S24L. REPAIR WAS PERFORMED WITH EWO 767-53-118.