What was found
ALL THREE STIFFENERS UNDER THRESHOLD FLOOR PANEL CRACKED. REMOVED AND REPLACED STIFFENERS (2 EA) 45A33606-005 AND (1 EA) 45A33606-006, IAW SRM 51-41-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ALL THREE STIFFENERS UNDER THRESHOLD FLOOR PANEL CRACKED. REMOVED AND REPLACED STIFFENERS (2 EA) 45A33606-005 AND (1 EA) 45A33606-006, IAW SRM 51-41-00.