What was found
INSPECTION FOUND A .5 INCH CRACK (THREE EACH) IN L-1 DOOR AFT PAN AT NR 5, NR 6, AND NR 7 STOP FITTING ADJUSTMENT ACCESS HOLES. A DOUBLER REPAIR WAS INSTALLED AT EACH CRACK LOCATION IAW ECRA 5210-01941.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK (THREE EACH) IN L-1 DOOR AFT PAN AT NR 5, NR 6, AND NR 7 STOP FITTING ADJUSTMENT ACCESS HOLES. A DOUBLER REPAIR WAS INSTALLED AT EACH CRACK LOCATION IAW ECRA 5210-01941.