1 fatality

1995-04-23: De Havilland DHC-6 Twin Otter (5N-AJQ) — Bristow Helicopters — Lagos-Murtala Muhammed, Nigeria

Lagos-Murtala Muhammed, NigeriaLanding (descent or approach)

On April 23, 1995, a De Havilland DHC-6 Twin Otter (registration 5N-AJQ) operated by Bristow Helicopters was involved in an aviation accident near Lagos-Murtala Muhammed, Nigeria during landing or approach. One person was killed. Investigators recorded the probable cause as: It was determined that the crew lost control of the airplane upon landing after the wind suddenly changed from 270° at 10 knots to 360° at 50 knots. Also, windshear was suspected. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781208069Data APIEditorial standards
Aircraft registered 5N-AJQ
Aircraft registered 5N-AJQ. Photo: Aeroprints.com / CC BY-SA 3.0, via Wikimedia Commons

A Twin Otter on approach to Lagos-Murtala Muhammed Airport in poor weather struck the runway nose-first, veered left, and collided with a parked Nigerian Air Force Fokker F27. One pilot died and eight others were injured; both aircraft destroyed.

Approach and Weather

During approach to Lagos-Murtala Muhammed Airport, the crew encountered poor weather conditions with heavy rainfall and strong winds.

Sequence of Events

The copilot was in command. The aircraft was too high on approach, so the captain assumed control and steepened the approach. Despite this, the aircraft remained too high over the threshold of runway 19L when it encountered a severe downdraft. The aircraft nosed down and struck the runway surface nose gear first. It bounced, veered off the runway to the left, rolled to the apron, and eventually collided with a parked Fokker F27 Friendship 200MP of the Nigerian Air Force, registered NAF908.

Damage and Occupants

Both the Twin Otter and the Fokker F27 were destroyed. One of the pilots on board the Twin Otter was killed, and all eight other occupants were injured.

Probable Cause

The probable cause, as determined by the investigation, is that the crew lost control of the airplane upon landing after the wind suddenly changed from 270° at 10 knots to 360° at 50 knots. Additionally, windshear was suspected.