ASN Wikibase Occurrence # 330322
Date: | Tuesday 28 November 1972 |
Time: | 19:51 |
Type: | McDonnell Douglas DC-8-62 |
Owner/operator: | Japan Air Lines - JAL |
Registration: | JA8040 |
MSN: | 46057/474 |
Year of manufacture: | 1969 |
Engine model: | Pratt & Whitney JT3D- |
Fatalities: | Fatalities: 61 / Occupants: 76 |
Aircraft damage: | Destroyed, written off |
Category: | Accident |
Location: | Moskva-Sheremetyevo Airport (SVO) -
Russia
|
Phase: | Initial climb |
Nature: | Passenger - Scheduled |
Departure airport: | Moskva-Sheremetyevo Airport (SVO/UUEE) |
Destination airport: | Tokyo-Haneda Airport (HND/RJTT) |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:A McDonnell Douglas DC-8-62 passenger plane, JA8040, was destroyed when it crashed on takeoff from Moscow's -Sheremetyevo Airport (SVO), Russia.
Five of the 14 crew members and ten of the 62 passengers survived the accident.
JAL flight JL446 was a scheduled international flight from Copenhagen (CPH), Denmark to Tokyo-Haneda (HND), Japan with an en route stop in Moscow.
The flight to Moscow was uneventful and the airplane landed at 18:17. After servicing of the aircraft startup and taxi clearance was received at 19:38. JL446 was cleared for takeoff from runway 25 at 19:49.
On takeoff the DC-8 climbed to 100 m with a supercritical angle of attack and lost height abruptly. It hit the ground and burst into flames.
PROBABLE CAUSE:
The cause of the disaster to aircraft DC-8-62 JA-8040 resided in the fact that during take-off and following attainment of the safety speed V2, the crew put the aircraft into a supercritical angle of attack which resulted in loss of speed and altitude.
The aircraft's assumption of supercritical angles of attack was the consequence of one of the following circumstances:
a) inadvertent extension of the spoilers in flight, leading to a fall in the maximum value of the lift ratio and an increase in drag;
b) loss of control of the aircraft by the crew in conditions associated with malfunctioning of the No. 1 or No. 2 engine consequent upon possible ice formation on the engine intake at a time when the de-icing system was switched off.
The anomalies in the functioning of the engines observed by the crew and other witnesses may have arisen after the aircraft had assumed a supercritical angle of attack with the spoilers extended.
Sources:
Flight International 05 November 1977 (1342)
ICAO Circular 132-AN/93 (22-26)
Location
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