What was found
FUSELAGE SKIN WAS PUNCTURED AT BS 540 - 560, STRINGER 33 - 34R. INSTALLED A TEMP DOUBLER REPAIR IAW EO B747-5330-70630-A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN WAS PUNCTURED AT BS 540 - 560, STRINGER 33 - 34R. INSTALLED A TEMP DOUBLER REPAIR IAW EO B747-5330-70630-A.