What was found
TPA - DURING CX-1 CHECK, FOUND TWO EACH 1 INCH LONG CRACKS IN FITTING AT BS 727 COMPRESSION CHORD, ONE AT RBL 25 AND ONE AT RBL 45. INSTALLED REPAIR PER TYPICAL REPAIR 53-10-03A. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TPA - DURING CX-1 CHECK, FOUND TWO EACH 1 INCH LONG CRACKS IN FITTING AT BS 727 COMPRESSION CHORD, ONE AT RBL 25 AND ONE AT RBL 45. INSTALLED REPAIR PER TYPICAL REPAIR 53-10-03A. (M)