What was found
FOUND 2 CRACKS (13MM AND 6MM,LT SIDE) AND 1 CRACK (5MM RT SIDE) ON C 12 A STIFFENER FITTING. REPAIR PERFORMED BY MODIFICATION OF STRUCTURE IAW SB A300-53-6137, APPROVED BY EO 6-5340-7-5002 PART 5600.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND 2 CRACKS (13MM AND 6MM,LT SIDE) AND 1 CRACK (5MM RT SIDE) ON C 12 A STIFFENER FITTING. REPAIR PERFORMED BY MODIFICATION OF STRUCTURE IAW SB A300-53-6137, APPROVED BY EO 6-5340-7-5002 PART 5600.