What was found
FUSELAGE SKIN CRACKED AT BS 340 BETWEEN STRINGERS 6L-7L. REMOVED DAMAGE, NDT'D AREA, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-30-03 PAGES 77-78D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACKED AT BS 340 BETWEEN STRINGERS 6L-7L. REMOVED DAMAGE, NDT'D AREA, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-30-03 PAGES 77-78D.