What was found
MAJOR REPAIR. LOWER FUSELAGE SKIN AT STA.1440, STRINGER 29L HAS A BULDGE BETWEEN STRINGER ATTACH RIVETS. DOT 8-001. APPLIED CIC AT NEW STRINGER I.A.W. AMM 51-00-59. VERIFIED ALL WORK COMPLETE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAJOR REPAIR. LOWER FUSELAGE SKIN AT STA.1440, STRINGER 29L HAS A BULDGE BETWEEN STRINGER ATTACH RIVETS. DOT 8-001. APPLIED CIC AT NEW STRINGER I.A.W. AMM 51-00-59. VERIFIED ALL WORK COMPLETE.