What was found
INSPECTION FOUND A 2.5 INCH CRACK IN FITTING AT STA 940, STRINGER 18A. A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2.5 INCH CRACK IN FITTING AT STA 940, STRINGER 18A. A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.