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Printed page xii. PDF page 15.
NTSB Aircraft Accident Report When the main landing gear and the aft fuselage struck the seawall, the tail of the airplane broke off at the aft pressure bulkhead. The airplane slid along the runway, lifted partially into theOpen final report at PDF page 15NTSB AAR-14/01: Asiana Airlines 214
Printed page 34. PDF page 52.
Wreckage and Impact Information Examination of the accident site showed that the airplane's main landing gear and the underside of the aft fuselage struck the seawall. The main landing gear, the first part of the airplane to hit the seawall,Open final report at PDF page 52NTSB AAR-14/01: Asiana Airlines 214
Printed page 66. PDF page 84.
phases of flight. For flight on final approach (1,500 ft agl), gear down, thrust set to maintain a 3� glidepath, flaps 30, and speed Vref plus 10 knots (142 knots for flight 214), at a landing weight of 450,000 lbs,Open final report at PDF page 84NTSB AAR-14/01: Asiana Airlines 214
Printed page 77. PDF page 79.
gear) was found to the east of the site and the lighter debris to the west. Outside the main area of 600 metres by 200 metres, a rear left fuselage panel containing eleven windows and around seven metres long wasOpen official document at PDF page 79Final Report: Accident on 1st June 2009 to the Airbus A330-203 registered F-GZCP operated by Air France flight AF 447