What was found
DURING C-CHECK INSPECTION, FOUND 1.5 INCH CRACK IN OUTER PAN BEHIND LOWER HINGE ARM MAIN CABIN ENTRY DOOR BETWEEN BEAMS 7 AND 8. REMOVED AND REPLACED PAN IAW SRM 52-01 AND 52-10-0 FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, FOUND 1.5 INCH CRACK IN OUTER PAN BEHIND LOWER HINGE ARM MAIN CABIN ENTRY DOOR BETWEEN BEAMS 7 AND 8. REMOVED AND REPLACED PAN IAW SRM 52-01 AND 52-10-0 FIGURE 1.