What was found
AFTER BUSHING REMOVAL, RIGHT WING INBOARD FLAP VANE INBOARD TEE FITTING BORE FOUND CORRODED. RIGHT WING INBOARD FLAP VANE INBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27-50-22-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER BUSHING REMOVAL, RIGHT WING INBOARD FLAP VANE INBOARD TEE FITTING BORE FOUND CORRODED. RIGHT WING INBOARD FLAP VANE INBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27-50-22-4.