What was found
CRACK ON RT UPPER FWD WINDOW RING PAN AT STA Y=886, AND Y=946 AT CABIN FUSELAGE STRUCTURE. RING PAN WERE REPAIRED IAW SRM 53-05, PAR 139, FIG 122, 51-30-02, 51-30-05, ERA 487747-14MA, REV A AND 493648-14MA, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON RT UPPER FWD WINDOW RING PAN AT STA Y=886, AND Y=946 AT CABIN FUSELAGE STRUCTURE. RING PAN WERE REPAIRED IAW SRM 53-05, PAR 139, FIG 122, 51-30-02, 51-30-05, ERA 487747-14MA, REV A AND 493648-14MA, REV A.