What was found
INSPECTION FOUND A 2 INCH CRACK ON ANGLE BRACKET AT FUSELAGE STA 540, STRINGER 23L. A NEW PART WAS INSTALLED IAW SRM 51-70-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK ON ANGLE BRACKET AT FUSELAGE STA 540, STRINGER 23L. A NEW PART WAS INSTALLED IAW SRM 51-70-11.