What was found
DURING INSPECTION OUTBOARD CLOSING ANGLES FOUND TO BE CRACKED. 34848 CYC SINCE INSTALLATION OF ANGLES. ONE CRACK ON EACH ANGLE ONE P/N 8530016-015 2.5 INCHES AND P/N 8530016-113 1.0 INCHES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION OUTBOARD CLOSING ANGLES FOUND TO BE CRACKED. 34848 CYC SINCE INSTALLATION OF ANGLES. ONE CRACK ON EACH ANGLE ONE P/N 8530016-015 2.5 INCHES AND P/N 8530016-113 1.0 INCHES.