Fukuoka

During the takeoff roll at Fukuoka-Itazuke Airport runway 16, at a speed of 158 knots, the captain started the rotation. During initial climb, at a height of about 3 metres, the right engine suffered a loss of power after a fan blade located on the 1st stage of the high pressure compressor disk separated. The N1 dropped to 23,7% and five seconds later, the flight engineer informed the crew about the failure of the engine n°1. The captain decided to abort the takeoff and landed back on runway. The aircraft contacted ground with a vertical acceleration of 2,1 g then thrust reversers were deployed and ground spoilers were extended. Unable to stop within the remaining distance, the aircraft overran, crossed a road, skidded for about 620 metres before coming to rest in an open field, bursting into flames. Three passengers were killed.

While cruising at a relative low altitude under VFR mode in IMC conditions (snow falls), the crew saw a mountain. To avoid a collision, the pilot increased engine power but the aircraft struck trees and crashed in a wooded area located on the Takami Peak, near Kawatana. Both pilots were injured and the aircraft was destroyed.

The twin engine aircraft registered JA8825 (MA825) departed Fukuoka Airport on a maritime patrol flight off the prefecture of Nagasaki. Shortly after takeoff, while climbing, the crew encountered poor visibility and low clouds when the airplane struck the slope of Mt Tachizawa located south of Fukuoka. The aircraft was destroyed upon impact and all five occupants were killed.

JAL Flight 350 took off from Fukuoka (FUK) runway 16 at 07:34 for a regular flight to Tokyo-Haneda (HND). The aircraft climbed to the cruising altitude of FL290. At 08:22 the crew started their descend to FL160. After reaching that altitude, they were cleared to descend down to 3000 feet. The aircraft was cleared for a runway 33R ILS approach and 5° of flaps were selected at 08:35, followed by 25 degrees of flaps one minute later. The landing gear was lowered at 08:39 and 50 degrees of flaps were selected two minutes after that. At 08:42 the aircraft descended through 1000 feet at an airspeed of 135 knots with wind from a direction of 360deg at 20 knots. The co-pilot called out "500 feet" at 08:43:25 but the captain did not make the "stabilized" call-out as specified by JAL operational regulations. The airspeed decreased to 133 knots as the aircraft descended through 300 feet at 08:43:50 and the co-pilot warned the captain that the aircraft was approaching the decision height. At 08:43:56 the radio altimeter warning sounded, followed by the flight engineer calling out "200 feet", which was the decision height, three seconds later . At 08:44:01 the aircraft descended through 164 feet at 130 KIAS. At that moment the captain cancelled autopilot, pushed his controls forward and retarded the throttles to idle. The co-pilot tried to regain control but the aircraft crashed into the shallow water of Tokyo Bay, 510 m short of the runway 33R threshold. The nose and the right hand wing separated from the fuselage. The captain had recently suffered a psychosomatic disorder; preliminary reports suggested that the captain experienced some form of a mental aberration. He had been off duty from November 1980 to November 1981 for these reasons.

En route from Fukuoka to Tokyo-Haneda Airport, the crew reported technical problems and decided to divert to Osaka-Itami Airport. The crew completed a wheels up landing and the airplane slid for several yards before coming to rest. All 64 occupants escaped uninjured while the aircraft was damaged beyond repair.

In unclear circumstances, the C-47 collided with a USAF North American F-100 Super Sabre over the city of Fukuoka. While the pilot of the fighter was able to land at Fukuoka-Itazuke Airport, the C-47 crashed onto two vacant houses. All three crew members were killed and there was no injuries on the ground.

Shortly after liftoff, while climbing at a height of 30 meters, the airplane stalled and crashed in flames onto a hangar. Four passengers were killed while 19 other occupants and eight people on the ground were injured.

Shortly after takeoff from runway 32, while in initial climb, the aircraft banked left and right, then nosed down and crashed in a paddy field. The aircraft was destroyed by impact forces and all 24 occupants, among them 3 civilians, were killed. The crew was completing a mail flight from Tachikawa AFB to Fukuoka with an intermediate stop in Osaka-Itami Airport. Weather conditions at the time of the accident were considered as marginal and it is believed that the left engine was not running at impact for reason that could not be determined with certainty.

Crash landed in Itazuke Airport. No casualties.

Shortly after liftoff from Fukuoka Airport, the twin engine airplane collided with the perimeter fence and crashed, bursting into flames. The pilot, the mechanic and four passengers were killed while five other occupants were injured.