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Crash of a Dornier DO.128 Skyservant near Warri: 6 killed

Date & Time: Oct 26, 2000
Type of aircraft:
Operator:
Registration:
NAF018
Flight Type:
Survivors:
No
Schedule:
Benin City – Warri
MSN:
6018
YOM:
1985
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
While approaching Warri Airport runway 06 following an uneventful flight from Benin City, the twin engine aircraft entered an uncontrolled descent and crashed near a refinery located near Jeddo, about 11 km west of the airport. All six occupants were killed, among them five Nigerian Army Officers.

Crash of a Cessna 208 Caravan I in Warri

Date & Time: Nov 27, 1998 at 1025 LT
Type of aircraft:
Operator:
Registration:
5N-PAN
Survivors:
Yes
Schedule:
Lagos – Lekki – Warri
MSN:
208-0200
YOM:
1991
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
4613
Circumstances:
A float-equipped Cessna Caravan, 5N-PAN, departed Lagos (LOS) on a chartered flight to Warri with a scheduled stop-over at Lekki. The aircraft was airborne at 07:34 hours UTC and was cleared to 1,000 feet by Lagos Tower and landed at Lekki at 07:42 hours UTC. At 08:20 hours UTC, the aircraft departed Lekki and called Lagos Approach which cleared it to 3,500 feet with further instructions for the aircraft to report at TMA. The aircraft reported at TMA and continued its normal flight at 3,500 feet. On contact with Escravos Tower, it requested for a descent from 3,500 feet to 700 feet in order to overfly the Chevron facility at Opuekaba for an aerial inspection. After the inspection, the aircraft was cleared to 2,500 feet to resume its normal flight to Warri. The pilot made an outbound turn to line up for the final approach to runway 03. At about five nm DME from Warri the pilot chose to reduce speed to 120 knots and he selected gear down with flap 15°. At three nautical miles out, the aircraft was about 900 feet high above the approach path, and cleared to land. The aircraft was now configured for landing with flap at 30° and the pilot reduced the speed to between 85 and 90 knots. At about 1.5 miles out, the aircraft was between 350 - 400 feet high, gliding with 400 lb of torque, the pilot felt a small shudder from the engine which was instantaneously followed by a need for power input, so he advanced the throttle but there was no response from the engine. He quickly retracted the flaps and feathered the propeller. Then the pilot re-selected flap 30° and also unfeathered the propeller which restored the engine to full torque. The pilot decided to abandon the approach mainly because of the a building structure ahead, close to the runway threshold. The pilot chose to veer the airplane to the left of the approach path centerline and ditched into the swampy terrain, cutting through some scattered trees and shrubbery.
Probable cause:
The probable cause of the accident was the little old fractured cotter pin which lodged itself in the orifice and caused the BOV to malfunction at the very critical instance when more power output was demanded from the powerplant. The engine did not completely flameout, because of the position of the BOV valve in partially/fully open position which, could only sustain idle running of the engine.

Crash of a De Havilland DHC-6 Twin Otter 300 in Lagos: 1 killed

Date & Time: Apr 23, 1995 at 1240 LT
Operator:
Registration:
5N-AJQ
Survivors:
Yes
Schedule:
Port Harcourt – Warri – Lagos
MSN:
607
YOM:
1979
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
On approach to Lagos-Murtala Muhammed Airport, the crew encountered poor weather conditions with heavy rain falls and strong winds. The copilot was in command and the airplane was too high on approach so the captain took over controls and steeped the approach. Nevertheless, the aircraft was still too high over runway 19L threshold when it encountered severe downdraft. It nosed down and struck the runway surface nose gear first. It bounced, veered off 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. Both aircraft were destroyed and one of the pilot on board the Twin Otter was killed, all eight other occupants were injured.
Probable cause:
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.

Crash of a De Havilland DHC-2 Beaver in Warri: 3 killed

Date & Time: Nov 14, 1968
Type of aircraft:
Operator:
Registration:
5N-ACW
Survivors:
No
Schedule:
Warri - Warri
MSN:
864
YOM:
1956
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The aircraft was leased to J. Ray McDermott Construction Company and flying a regular route from Lagos to the various construction sites up country. On the day of the accident the amphibious float-equipped aircraft took off from Warri Airstrip for a three-minute flight to the river with wheels extended and on landing flipped over and came to rest inverted. Initially the occupants were-seen trying to escape but two large containers of Red Lead oxide burst open on impact and hindered the escape by possibly blinding or suffocating the pilot and two passengers. It is believed the occupants did not survive the accident.
Probable cause:
The pilot failed to raise the wheels after takeoff from Warri Airport.