What was found
NR 2 ENGINE T/R LOWER CLAM SHELL DENT AT 3RD RIB. LENGTH 5.2 WIDTH 2.8 DEPTH .033 D/X RATIO OF 84.8 FOUND TO BE WITHIN LIMITS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 ENGINE T/R LOWER CLAM SHELL DENT AT 3RD RIB. LENGTH 5.2 WIDTH 2.8 DEPTH .033 D/X RATIO OF 84.8 FOUND TO BE WITHIN LIMITS.