What was found
DURING CHECK-C MAINT, FOUND CRACK AT RIVET HEAD ON LT O/B SIDE OF THE NUMBER 2 ENGINE INLET, 17 INCHES UP FROM THE FUSELAGE AND 28 ICHES AFT OF THE INLET L/E. FABRICATED REPAIR PER SRM 54-30-3 AND INSTALLED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT, FOUND CRACK AT RIVET HEAD ON LT O/B SIDE OF THE NUMBER 2 ENGINE INLET, 17 INCHES UP FROM THE FUSELAGE AND 28 ICHES AFT OF THE INLET L/E. FABRICATED REPAIR PER SRM 54-30-3 AND INSTALLED.