What was found
CRACK IN RIGHT WHEEL WELL PRESSURE DECK ADJACENT TO FUEL SHROUD SUPPORT ANGLE. INSTALLED DOUBLER PER SRM 53-01 FIGURE 2 SHEET 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN RIGHT WHEEL WELL PRESSURE DECK ADJACENT TO FUEL SHROUD SUPPORT ANGLE. INSTALLED DOUBLER PER SRM 53-01 FIGURE 2 SHEET 3.