What was found
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 2 INCH CRACK IN THE AFT ENTRY DOOR PAN, LOWER CENTER BEAM ATTACH ANGLE AND VERTICAL ANGLE. REPAIRED PER EA 96-100274.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 2 INCH CRACK IN THE AFT ENTRY DOOR PAN, LOWER CENTER BEAM ATTACH ANGLE AND VERTICAL ANGLE. REPAIRED PER EA 96-100274.