Positioning

Shortly after takeoff from Mindelheim-Mattsies Airport, while in initial climb, the pilot informed ATC about problems and elected to return. While completing a sharp turn to the right at a relative low altitude, the aircraft stalled and crashed in a field located less than 2 km from the airfield. The aircraft was destroyed and the pilot, sole on board, was killed. The aircraft was operated by Burkhart Grob Luft-und-Raumfahrt later renamed Grob Aerospace.

En route from Los Roques to Caracas, the crew encountered engine problems and declared an emergency. He was cleared to divert to Caracas-Maiquetía-Simón Bolívar Airport. Upon landing, the crew encountered strong cross winds and the twin engine aircraft went out of control and crashed in a drainage ditch located 45 metres from the runway. Both pilots were injured and the aircraft was destroyed.

The crew was completing a positioning flight from Veracruz. After touchdown, the crew encountered difficulties to stop the aircraft within the remaining distance (runway 13/31 is 1,300 metres long). It overran and eventually crashed past the runway end. The aircraft was destroyed and both pilots were killed.

The flightcrew had completed a 14 cfr part 135 charter flight and had landed in the harbor at Key West, Florida. They had moored the seaplane and departed. About an hour later, they reboarded the seaplane to fly it to an airport for refueling, then to return to the harbor to board the passengers. During takeoff, the seaplane was observed to pitch nose up, roll left, and crash nose down in the harbor. Due to the damage done by tidal flow and recovery attempts, the exact condition of the aft bilge drain plugs was unknown. During a check of the CVR recording, the crew was not heard to call out the bilge pumps during the before-takeoff checklist. After lift-off, both pilots made comments about keeping the nose down due to water in the aft portion of the aircraft. Both pilots were killed.

While on approach at night, in VMC, the left engine lost power due to fuel starvation. The propeller was not feathered, the l/g was left down, and the aircraft drifted left of crs, struck trees, and then the ground. One gallon of fuel was drained from the right wing, engine and fuel line. No fuel was found in the left wing, engine and fuel line. The copilot said the fuel quantity system was erratic with the left side more erratic, and the right side reading about 10 gallons more than the left side. Testing found the right side indicated about 45 gallons more than was present while the left side was inoperative. There was no requirement for periodic recalibration of the fuel quantity system. The owner/pilot had operated the aircraft on 32 flights, over 23 hours, and refueled 23 times using partial fills, since he had full tanks. The pilot was checked out 17 months prior and the instructor said the pilot was fine, however, he was cautioned him to enroll in recurrent training. There was no record he did. The pilot had received an FAA checkride 19 months prior to the accident, which he passed.

Following a night takeoff from Ngara Airstrip, the twin engine aircraft struck obstacles with its left wing, lost height and crashed, bursting into flames. The pilot, sole on board, was slightly injured and the aircraft was destroyed by a post crash fire.

The privately owned Israel Aircraft Industries (IAI) Westwind II aircraft was en route from the Edmonton Municipal Airport, Alberta, to the Meadow Lake aerodrome, Saskatchewan. Low ceilings and reduced visibility were reported in the vicinity of the destination aerodrome. The crew completed a straight-in instrument approach to runway 08 at Meadow Lake, and began a circling procedure to the south of the aerodrome in order to set up to land on runway 26. The aircraft passed overhead the aerodrome at an altitude of approximately 400 feet above ground level (agl). It then turned and proceeded in level flight towards the southeast. Approximately two and one-half miles from the aerodrome, the aircraft entered a number of steep-banked rolling manoeuvres. Immediately following these manoeuvres, the aircraft descended and struck the ground in a nose-high, slightly right-wing-low attitude. The ground-strike produced very high deceleration forces. The aircraft broke into several sections, internal fuel tanks ruptured, and fuel was sprayed forward and outward from the initial impact point. A severe post-crash fire erupted and engulfed the entire wreckage trail. Emergency medical service and firefighting crews responded from the town of Meadow Lake and were on the scene within minutes of the accident. Both pilots died in the crash.

On final approach to Santa Elena Airfield, Entre Ríos, the crew heard a loud bang apparently coming from the undercarriage. Pilots initiated a go-around procedure and while climbing, elected to retract the landing gear but without success. Flaps remained blocked in an inappropriate angle while the hydraulic pressure dropped. Decision was taken to return to Paraná Airport where the landing gear collapsed upon landing. The aircraft slid on its belly and came to rest. Both pilots evacuated safely while the aircraft was damaged beyond repair.

The crew was cleared for a night visual approach to Kinshasa-N'Djili Airport. Weather conditions were good with a visibility over 10 km. On approach, ATC asked the crew to turn on the approach lights. Shortly later, the aircraft struck the ground and crashed 20 km short of runway 24 threshold. Both pilots were killed.

En route from Morlaix on a positioning flight to Dijon, while cruising at FL230, the twin engine aircraft entered a left turn then an uncontrolled descent. It partially disintegrated in the air and eventually crashed in an open field located near Saint-Broladre. The pilot, sole on board, was killed, and debris were found on more than 8 km. The pilot did not send any distress call prior to the loss of control.