What was found
NR 1 ENGINE NOSE COWL, 5 O'CLOCK POSITION SKIN IS PULLED UP 0.10 INCH BY 3 INCHES LONG, 0.5 INCH FORWARD WITH A 0.15 INCH CRACK IN UPPER EDGE. STOP DRILLED CRACK PER SRM 51-10-6. INSTALLED DOUBLER PER SRM 54-30-3 AND SRM 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE NOSE COWL, 5 O'CLOCK POSITION SKIN IS PULLED UP 0.10 INCH BY 3 INCHES LONG, 0.5 INCH FORWARD WITH A 0.15 INCH CRACK IN UPPER EDGE. STOP DRILLED CRACK PER SRM 51-10-6. INSTALLED DOUBLER PER SRM 54-30-3 AND SRM 51-10-2.