What was found
DURING INSP, A CANTED FRAME FWD ATTACH ANGLE WAS FOUND CRACKED AT STA 1121 BETWEEN LONG 17 AND 18R APPROX 6 INCHES. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-01, FIG 2 SHEET 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSP, A CANTED FRAME FWD ATTACH ANGLE WAS FOUND CRACKED AT STA 1121 BETWEEN LONG 17 AND 18R APPROX 6 INCHES. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-01, FIG 2 SHEET 4.