What was found
DURING CHECK-C MAINT ON THE NOSE LANDING GEAR, THE RT NOSE LANDING GEAR WHEEL WELL DOOR HAD CORROSION AND TORN METAL ON LEADING EDGE. REMOVED DAMAGE BY BLENDING PER SRM 52-01 FIG 1. REMOVED CORROSION PER SPM 6-80-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT ON THE NOSE LANDING GEAR, THE RT NOSE LANDING GEAR WHEEL WELL DOOR HAD CORROSION AND TORN METAL ON LEADING EDGE. REMOVED DAMAGE BY BLENDING PER SRM 52-01 FIG 1. REMOVED CORROSION PER SPM 6-80-01.