What was found
DURING ENGINE CHANGE PRE-INSTALL INSPECTION, FOUND .25 INCH CRACK AT FASTENER HOLE IN NR 3 NACELLE OUTBD SKIN AT NAC STA 41, AFT OF OUTBD UPPER ENG MOUNT POINT. REPAIRED PER SRM 54-2-1, FIG 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ENGINE CHANGE PRE-INSTALL INSPECTION, FOUND .25 INCH CRACK AT FASTENER HOLE IN NR 3 NACELLE OUTBD SKIN AT NAC STA 41, AFT OF OUTBD UPPER ENG MOUNT POINT. REPAIRED PER SRM 54-2-1, FIG 3.