What was found
HFEC INSPECTION FOUND 01EA CRACK ON LT BS883.5 FRAME INNER CHORD SURFACE AND TRANSITION RADIUS PER W/C 5311-01195-03 STEP 5 AND REPAIRED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HFEC INSPECTION FOUND 01EA CRACK ON LT BS883.5 FRAME INNER CHORD SURFACE AND TRANSITION RADIUS PER W/C 5311-01195-03 STEP 5 AND REPAIRED.