Takeoff (climb)

After takeoff from Ocumare del Tuy Airport, while climbing, the pilot encountered engine problems and elected to make an emergency landing in a city center's avenue. Just prior to landing, the single engine aircraft collided with a telephone line and crashed on an autobus. The pilot, the bus driver and a bus passenger were killed. The pilot departed Ocumare del Tuy Airport on a cargo flight to Puerto Ayacucho.

Witnesses said that it appeared that the left engine sustained a loss of power just after rotation and liftoff. The airplane initially had a positive rate of climb, but then immediately yawed to the left as it cleared 30-foot-high power lines that were perpendicular across the flight path. The airport is at the east end of a lake in a mountain valley; the airplane departed to the west and was flying over the lake. The airplane was about 2 miles from the runway when witnesses observed dark smoke coming from the left engine, and the smoke increased significantly as the flight continued. The airplane banked hard left with the wings perpendicular to the ground, and then nosed in vertically. The landing gear remained down throughout the accident sequence. On site examination revealed that the top spark plugs for the left engine were black and sooty. A detailed examination revealed that the left turbocharger turbine wheel shaft fractured and separated. Extreme oxidation of the fracture surfaces prevented identification of the failure mode; however, the oxidation was the result of high temperature exposure indicating that the fracture occurred while the turbocharger was at elevated temperature during operation. The multiple planes exhibited by the fracture also were not consistent with a ductile torsional failure as would be expected from a sudden stoppage of either rotor. No evidence of a mechanical malfunction was noted to the right engine. The Cessna Owners Manual for the airplane notes that the most critical time for an engine failure is a 2-3 second period late in the takeoff while the airplane is accelerating from the minimum single-engine control speed of 87 KIAS to a safe single-engine speed of 106 KIAS. Although the airplane is controllable at the minimum control speed, the airplane's performance is so far below optimum that continued flight near the ground is improbable. Once 106 KIAS is achieved, altitude can more easily be maintained while the pilot retracts the landing gear and feathers the propeller. The best single-engine rate-of-climb is 108 KIAS with flaps up below 18,000 feet msl. Section VI of the manual provides operational data for single-engine climb capability. The data was only valid for the following conditions: gear and flaps retracted, inoperative propeller feathered, wing banked 5 degrees toward the operating engine, 39.5 inches of manifold pressure if below 18,000 feet, and mixture at recommended fuel flow.

The pilot departed his home airport at 0502 and landed at another airport where he picked up employees of a marketing company to fly them to an out of state meeting. The accident occurred at 2003 shortly after taking off on the return trip to fly the employees back home. Shortly before departure a fourth passenger was added to the flight after his commercial flight was cancelled. A person who worked for the fixed base operator at the departure airport stated the pilot looked tired or just ready to go home. The pilot received his clearance for the IFR flight prior to takeoff. The pilot misread the clearance back to the controlled and was corrected. Radar data showed the pilot initially flew the assigned south-southwest heading prior to the airplane turning right to a westerly heading. The controller queried the pilot and issued a heading to intercept the VOR. The pilot corrected the heading and shortly thereafter the airplane once again began a right turn back toward the west. The airplane continued to climb throughout the heading changes. Radar data showed the airplane then began another left turn during which time it entered a spiraling rapid descent. According to weather data, the airplane was in instrument meteorological conditions when this occurred. The airplane impacted the terrain in an open cornfield. Weight and balance calculations indicate the airplane was at least 383 pounds over gross weight. Post accident inspection of the airplane and engines did not reveal any preexisting failure/malfunction.

Shortly after takeoff from Rottnest Island Airport, while in initial climb, the twin engine aircraft suffered a bird strike and crashed in a salt lake located near the airport. The aircraft was destroyed upon impact and all six occupants were injured.

Shortly after takeoff from Nakhon Sawan-Takhli AFB, while climbing to a height of about 150 feet, the pilot contacted ATC and declared an emergency following a loss of engine power. He elected to return for an emergency landing when the aircraft went out of control and crashed onto a hangar located near the airport, bursting into flames. All seven occupants were killed, among them two photographers and one mechanic who were taking part to a reconnaissance mission in view to prepare an incoming air race in Thailand.

The B737-200 aircraft which night-stopped at Calabar on Saturday the 28th of October, 2006, departed for Lagos in the morning of the 29th of October, 2006, and landed in Lagos at 0825 hrs. While on ground in Lagos, it uplifted some fuel. There was only cabin crew change. The aircraft departed Lagos on scheduled passenger service as ADK 063 at 0929 hrs and landed in Abuja at 1020 hrs. The aircraft uplifted 5000 litres of fuel and had 11000kg fuel for departure as ADK 053, a scheduled service to Sokoto. After boarding, it started raining and this compelled the crew to close the aircraft doors. Shortly after the rain had subsided, the doors were opened for the ground personnel to disembark. The crew then requested for start-up clearance. At 1115 hrs the aircraft was given a start up clearance for Sokoto. At 1121 hrs, the aircraft was given taxi clearance to holding position Runway 22. The pilot immediately requested for the wind, which was given as “210 variable at 8 kts”. Shortly after, the Control Tower transmitted the wind as south-westerly at 15 kts. While taxiing, the control tower advised Flight ADK 053 of gusty wind. The wind was initially given as 35 kts and then changed to 28 kts within 1 minute. At 1125 hrs while the aircraft was at the holding point, the crew was again advised of South-Westerly wind at 15 kts. At this juncture, the pilot of Virgin Nigeria 042 was heard on the radio saying “it looks like 35 kts to me” and then stated that he was going to wait for improvement in the weather, which he did. Thereafter, the ADK 053 crew requested for takeoff clearance and was cleared with right turn-out on course. Flight ADK 053 was airborne at 1129 hrs and was transferred to the Approach Control on 119.8MHZ but there was no acknowledgement from the crew. After three unsuccessful attempts to contact the aircraft, the Tower advised the Approach Control to call ADK 053. Other aircraft on the apron (Virgin Nigeria 042 and Trade Wings 2401), which were on that frequency were also asked to assist in contacting the aircraft but all attempts were unsuccessful. Kano and Lagos Area Controls were requested to contact ADK 053, but there was no response from the aircraft. Abuja Flight Communication Centre was then advised to inform National Emergency Management Agency (NEMA) in Kano about the loss of contact with the aircraft. At 1138 hrs, Flight Communication Centre called the Control Tower that someone came from a nearby village (Tungar Madaki) near the radar site and reported that a plane had crashed in their village. A search party from the airport was dispatched and they found and confirmed that the plane had crashed shortly after takeoff. The accident resulted in 96 fatalities out of 105 persons on board (POB). The accident occured at latitude N 08 59.691’ longitude E 007 14.772’ on an elevation of 1123 ft (ASL). The time of the accident was 1130 hrs during daylight and in rain.

The twin engine aircraft was performing an on-demand taxi flight from Toliara to the capital city Antananarivo with 4 pax and a two pilots on behalf of the company Magrama (Marbres & Granites de Madagascar). Less than two minutes after takeoff, while in initial climb, the aircraft suffered an engine failure and crashed about 1,500 metres from the runway end, bursting into flames. All 6 occupants were killed, among them 4 Italians and 2 Madagascar citizens.

The twin engine aircraft was engaged in an ambulance flight from Besançon to Amiens with 2 surgeons, one pilot and one operator agent. Following a course of 950 metres on runway 23 at Besançon-La Vèze Airport by night, the aircraft lifted off. With a low climb gradient, the aircraft collided with trees and crashed in a wooded area located 250 metres past the runway end, bursting into flames. The aircraft was totally destroyed and all four occupants were killed. Both surgeons were en route to Amiens in order to a lever harvesting.

Shortly after takeoff from Bukavu-Kavumu Airport, the single engine aircraft lost height and crashed, bursting into flames. All five occupants were rescued, among them two were injured.

A first attempt to take off from El Obeid Airport failed. During the second attempt, an engine caught fire and the aircraft crashed. There were no casualties but the aircraft was damaged beyond repair.