What was found
INSPECTION TYPE:2C FUSELAGE MAIN FRAME IS CRACKED AT STA 469.173 AND X=-60. REPAIRED CRACKED FUSELAGE MAIN FRAME AT STA 469.173 AND X= -60 IAW EA 011-5310-01-A8355 REV I/R AND EO MD11-5310-76977-A. (MAJOR)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:2C FUSELAGE MAIN FRAME IS CRACKED AT STA 469.173 AND X=-60. REPAIRED CRACKED FUSELAGE MAIN FRAME AT STA 469.173 AND X= -60 IAW EA 011-5310-01-A8355 REV I/R AND EO MD11-5310-76977-A. (MAJOR)