What was found
INSPECTION FOUND A .5 INCH CRACK IN SECOND DOOR FRAME FROM TOP OF MAIN CABIN DOOR. REPAIRED IAW SRM 52-05, FIGURE 31.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN SECOND DOOR FRAME FROM TOP OF MAIN CABIN DOOR. REPAIRED IAW SRM 52-05, FIGURE 31.