What was found
COCKPIT FLOORBEAM ANGLE CORRODED AT BS 280. REMOVED AND REPLACED THE AFT SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001 A01, 51-42-11-001-001 A01 & DWG CC670-34095.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
COCKPIT FLOORBEAM ANGLE CORRODED AT BS 280. REMOVED AND REPLACED THE AFT SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001 A01, 51-42-11-001-001 A01 & DWG CC670-34095.