What was found
NR 2 ENGINE HOSE COLLAR AFT FLANGE IS CRACKED IN 2 LOCATIONS, BOTH 1" LONG LOCATED 3.5" TO LT OF CENTER BOTH VERTICAL ROWS OF RIVETS. R & R RIVETS AND DAMAGED RADIUS IAW RD8-54-3774.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 ENGINE HOSE COLLAR AFT FLANGE IS CRACKED IN 2 LOCATIONS, BOTH 1" LONG LOCATED 3.5" TO LT OF CENTER BOTH VERTICAL ROWS OF RIVETS. R & R RIVETS AND DAMAGED RADIUS IAW RD8-54-3774.