What was found
CRACKED FITTING ON THE LT FLAP INTERNAL STRUCTURE XCW 65. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G, SRM 51-41-05-0G, AMM 20-00-02, AND AMM 20-50-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED FITTING ON THE LT FLAP INTERNAL STRUCTURE XCW 65. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G, SRM 51-41-05-0G, AMM 20-00-02, AND AMM 20-50-01.