What was found
L/H AFT FUSELAGE EXTERIOR SKIN IS CRACKED STA 1654.5 BETWEEN STRINGER 3L-4L. REMOVED DAMAGE ON L/H AFT FUSELAGE SKIN AT STA 1554E PER B767 SRM 58-80-01 REPAIR 4. CAT A REPAIR NO OTHER ACTIONS REQ IAW B767SRM 51-00-06
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
L/H AFT FUSELAGE EXTERIOR SKIN IS CRACKED STA 1654.5 BETWEEN STRINGER 3L-4L. REMOVED DAMAGE ON L/H AFT FUSELAGE SKIN AT STA 1554E PER B767 SRM 58-80-01 REPAIR 4. CAT A REPAIR NO OTHER ACTIONS REQ IAW B767SRM 51-00-06