What was found
DURING COMPLIANCE WITH AD91-24-11, FOUND FITTING CRACKED AT FS 870 RT ROW 2 IN SECOND AND THIRD HOLES BELOW S-9R ROW 1 AT TOP HOLE AND ROW 2 AT 5TH HOLE BELOW S-9R. REPLACED BODY TERMINAL FITTING IAW S/B 727-53-0116 DWG 65C23231.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING COMPLIANCE WITH AD91-24-11, FOUND FITTING CRACKED AT FS 870 RT ROW 2 IN SECOND AND THIRD HOLES BELOW S-9R ROW 1 AT TOP HOLE AND ROW 2 AT 5TH HOLE BELOW S-9R. REPLACED BODY TERMINAL FITTING IAW S/B 727-53-0116 DWG 65C23231.