What was found
CRACK (2) ON SUPPORT ANGLE OF AFT SIDE FITTING (AFT LONGERON) AT RIGHT MAIN LANDING GEAR WHEEL WELL. REMOVED CRACKED ANGLE, FABRICATED, TREATED, PRIMED, AND INSTALLED NEW ANGLE PER SRM 53-53-01, 51-20-00, AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK (2) ON SUPPORT ANGLE OF AFT SIDE FITTING (AFT LONGERON) AT RIGHT MAIN LANDING GEAR WHEEL WELL. REMOVED CRACKED ANGLE, FABRICATED, TREATED, PRIMED, AND INSTALLED NEW ANGLE PER SRM 53-53-01, 51-20-00, AND 51-31-01.