What was found
CRACKED UPPER PAN AT RT, FWD OVERWING EMERGENCY EXIT DOOR JAMB. CRACK WAS STOPPED IAW 53-20-15, FIG 201, REP 8. NEW DOUBLER WAS DRILLED IAW 51-40-08. NEW DOUBLER WAS INSTALLED IAW 51-40-02. LENGTH CRACK .265".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED UPPER PAN AT RT, FWD OVERWING EMERGENCY EXIT DOOR JAMB. CRACK WAS STOPPED IAW 53-20-15, FIG 201, REP 8. NEW DOUBLER WAS DRILLED IAW 51-40-08. NEW DOUBLER WAS INSTALLED IAW 51-40-02. LENGTH CRACK .265".