What was found
INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 861-864 JUST BELOW S22L ON THE BONDED DOUBLER LINE. THE CRACKED AREA OF STRINGER WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, REPAIR 31, PAGE 201-209.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 861-864 JUST BELOW S22L ON THE BONDED DOUBLER LINE. THE CRACKED AREA OF STRINGER WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, REPAIR 31, PAGE 201-209.