What was found
CRACK IN AFT WHEEL WALL FRAME AT TOP OTBD END ABOVE FLAP BUS CABLE PULLEYS. INSTALLED REPAIR DOUBLER & -5 JAMB SECTION IAW SRM 51-70-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN AFT WHEEL WALL FRAME AT TOP OTBD END ABOVE FLAP BUS CABLE PULLEYS. INSTALLED REPAIR DOUBLER & -5 JAMB SECTION IAW SRM 51-70-05.