What was found
CRACK FOUND ON FUSELAGE FRAME 5 LOWER FLANGE CLOSE TO LT NLG WHEEL WELL. CRACK REMOVED AND REINFORCING ANGLE INSTALLED PER ATR REPAIR INSTRUCTIONS DO/TS-3825/06-7654. REF SRAS DO/TS-3825/06...3816. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND ON FUSELAGE FRAME 5 LOWER FLANGE CLOSE TO LT NLG WHEEL WELL. CRACK REMOVED AND REINFORCING ANGLE INSTALLED PER ATR REPAIR INSTRUCTIONS DO/TS-3825/06-7654. REF SRAS DO/TS-3825/06...3816. (M)