Accident McDonnell Douglas DC-8-61 JA8061, Tuesday 9 February 1982
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Date:Tuesday 9 February 1982
Time:08:44
Type:Silhouette image of generic DC86 model; specific model in this crash may look slightly different    
McDonnell Douglas DC-8-61
Owner/operator:Japan Air Lines - JAL
Registration: JA8061
MSN: 45889/291
Year of manufacture:1967
Total airframe hrs:36955 hours
Engine model:Pratt & Whitney JT3D-3B
Fatalities:Fatalities: 24 / Occupants: 174
Other fatalities:0
Aircraft damage: Destroyed, written off
Category:Accident
Location:Tokyo-Haneda Airport (HND) -   Japan
Phase: Approach
Nature:Passenger - Scheduled
Departure airport:Fukuoka Airport (FUK/RJFF)
Destination airport:Tokyo-Haneda Airport (HND/RJTT)
Investigating agency: AAIC
Narrative:
JAL Flight 350, a McDonnell Douglas DC-8-61, 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 5deg 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 130KIAS. 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.

Accident investigation:
cover
  
Investigating agency: AAIC
Report number: mrt-58
Status: Investigation completed
Duration: 1 year and 3 months
Download report: Final report

Sources:

Aircraft Accident in Japan by SAKUMA Mitsuo

Statistics

  • 21st worst accident in 1982
  • 9th worst accident of this aircraft type
  • 6th worst accident of this aircraft type at the time

Location

Revision history:

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