What was found
NR 1 ENGINE NOSE COWL AT 12 O'CLOCK POSITION BETWEEN NOSE COWL LEADING EDGE AND ACOUSTIC PANEL HAS A CRACK. INSTALLED REPAIR DOUBLER PER SRM 54-11-00 FIG 1A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE NOSE COWL AT 12 O'CLOCK POSITION BETWEEN NOSE COWL LEADING EDGE AND ACOUSTIC PANEL HAS A CRACK. INSTALLED REPAIR DOUBLER PER SRM 54-11-00 FIG 1A.