What was found
INSPECTION FOUND A 3/4" CRACK IN FUSELAGE SKIN FORWARD OF L-2 DOOR FUSELAGE TORQUE TUBE ACCESS PANEL AT STA 947 BETWEEN STRINGER 10 AND 11L. THE CRACKED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-60-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3/4" CRACK IN FUSELAGE SKIN FORWARD OF L-2 DOOR FUSELAGE TORQUE TUBE ACCESS PANEL AT STA 947 BETWEEN STRINGER 10 AND 11L. THE CRACKED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-60-01.