What was found
DURING CHECK-C MAINT, FOUND A 2 INCH CRACK IN PRESSURE WEB, RT MLG WHEEL WELL AT STA 940, RBL 55. CONFIRMED CRACK WITH HIGH FREQ EDDY CURRENT. INSTALLED REPAIR DOUBLER PER BOEING PRINT 65-89360, AND AD 92-19-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT, FOUND A 2 INCH CRACK IN PRESSURE WEB, RT MLG WHEEL WELL AT STA 940, RBL 55. CONFIRMED CRACK WITH HIGH FREQ EDDY CURRENT. INSTALLED REPAIR DOUBLER PER BOEING PRINT 65-89360, AND AD 92-19-11.