What was found
LEFT WING OTBD FLAP, INBOARD FWD HINGE BRACKET LOWER OTBD MOUNT BORE CORRODED. EXCEED LIMITS IAW CMM 57-44-08. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806, PART 1, STEP 1C, AND STEP 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING OTBD FLAP, INBOARD FWD HINGE BRACKET LOWER OTBD MOUNT BORE CORRODED. EXCEED LIMITS IAW CMM 57-44-08. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806, PART 1, STEP 1C, AND STEP 1.