Narrative:The DC-8 had been cleared for a runway 24L departure. Taxiing to the runway in thick fog, the crew ended up on runway 24R. Tower control gave directions and the crew then taxied to runway 24L. Just after lifting off the runway, the DC-8 stalled and crashed 300 m past the runway. The initial blood alcohol level of the captain was 298 mgs percent. A blood alcohol level of 100 mgs percent was considered to be legally intoxicating for drivers in the State of Alaska.
Probable Cause:
PROBABLE CAUSE: "A stall that resulted from the pilot's control inputs aggravated by airframe icing while the pilot was under the influence of alcohol. Contributing to the cause of this accident was the failure of the other flightcrew members to prevent the captain from attempting the flight."
Accident investigation:
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Investigating agency: | NTSB  |
Status: | Investigation completed |
Duration: | 2 years | Accident number: | NTSB/AAR-78-07 | Download report: | Final report
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Classification:
Flightcrew member's alcohol, drug usage
Loss of control
Sources:
» Flight International 05 February 1977 (267)
» NTSB-AAR-78-07
Follow-up / safety actions
NTSB issued 2 Safety Recommendations
Issued: 26-MAY-1977 | To: | A-77-34 |
ISSUE AN ADVISORY CIRCULAR TO ESTABLISH CRITERIA FOR THE DESIGN, INSTALLATION, AND USE OF LIVESTOCK RESTRAINING SYSTEMS AND TO INSURE THAT CARRIAGE OF LIVESTOCK WILL NOT ADVERSELY AFFECT THE OPERATION OF THE AIRCRAFT OR THE FUNCTION OF ITS CREWMEMBERS. (Closed - Acceptable Alternate Action) |
Issued: 26-MAY-1977 | To: | A-77-35 |
CONDUCT AN ENGINEERING ANALYSIS TO DETERMINE THE ADEQUACY OF LIVESTOCK RESTRAINING SYSTEMS WHICH ARE CURRENTLY APPROVED FOR USE. THE ANALYSIS SHOULD DETERMINE THE LOAD DISTRIBUTION AND MAXIMUM AMOUNT OF LOAD SHIFT THAT CAN BE PERMITTED WITHOUT CAUSING AN INTOLERABLE SHIFT OF THE AIRPLANE\'S CENTER OF GRAVITY AND ALSO SHOULD DETERMINE THAT THE PERMISSIBLE LIMITS WILL NOT ADVERSELY AFFECT THE AIRPLANE\'S STABILITY AND CONTROL CHARACTERISTICS OR INTRODUCE PHYSIOLOGICAL FACTORS WHICH COULD AFFECT CREW PERFORMANCE. (Closed - Acceptable Action) |
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Photos

accident date:
13-01-1977type: McDonnell Douglas DC-8-62AF
registration: JA8054

accident date:
13-01-1977type: McDonnell Douglas DC-8-62AF
registration: JA8054
Map
This map shows the airport of departure and the intended destination of the flight. The line between the airports does
not display the exact flight path.
Distance from Anchorage International Airport, AK to Tokyo-Haneda Airport as the crow flies is 5523 km (3452 miles).
This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.