Takeoff (climb)

Shortly after takeoff from Mezhdurechensky Airport, while on a forest patrol flight to Uray, the engine did not have sufficient power and the aircraft was unable to gain sufficient height. It struck power cables, stalled and crashed 2 km from the airfield. All 25 occupants were injured, four of them seriously, and the aircraft was damaged beyond repair.

Shortly after takeoff from Madrid-Barajas Airport, while climbing, the crew lost control of the aircraft that crashed near a warehouse located in Paracuellos del Jarama, about 3 km east of the airport. The aircraft was destroyed and both pilots were seriously injured.

After takeoff from Johannesburg-Rand Airport, while in initial climb, the single engine aircraft nosed up and stalled. It collided with power cables and crashed, bursting into flames. The aircraft was totally destroyed and all three occupants were killed.

Shortly after takeoff from Karimui Airfield, while in initial climb, the left engine failed. The aircraft rolled to the left and crashed near the runway end. Both occupants were killed.

During the takeoff roll from runway 13, the twin engine aircraft went out of control, veered off runway and crashed in a banana plantation. One of the pilot was killed while few other occupants were injured, some seriously. The aircraft was written off.

Shortly after takeoff from Alotau Airport, while in initial climb, the aircraft caught fire and suffered an explosion. It entered an uncontrolled descent and crashed in shallow water about 2 km offshore. The aircraft was totally destroyed by impact forces and all 15 occupants were killed.

On July 10, 1995, about 1430 eastern daylight time, an Aero Commander 500, N89M, registered to Candy Yellow Apple, Inc., leased to and operated by Palm Beach Aviation, experienced separation of a propeller blade during the ground roll to takeoff from the Treasure Cay Airport, Treasure Cay, Bahamas. The nonscheduled, international, passenger flight was operating under 14 CFR Part 135. Visual meteorological conditions prevailed at the time and a VFR flight plan was filed for the flight. The airplane was substantially damaged and the airline transport- rated pilot and five passengers were not injured. One passenger was fatally injured. The flight was originating at the time of the accident.

Crashed in unknown circumstances shortly after takeoff from Pine Lake, killing all five occupants.

On a crop spraying flight for the sovkhoz (state farm) Sry-Altyn (Kanlykul district of Karakalpakstan) when the engine lost power shortly after take off from an airstrip located some 43 km northwest from Nukus. At a height of some 15-20 metres, the crew attempted a forced landing in a field when the left main gear struck a 2.5 metres high dam and the aircraft suffered substantial damage. Both pilots escaped unhurt.

This was the first flight of the Grumman G-21 in two years. Also, the pilot had not flown the G-21 for two years. Before taking off, the pilot reported that three takeoffs and landings would be needed for purposes of becoming current. After takeoff, he flew the airplane approximately one hour and made two full stop landings. During the third takeoff, the airplane was described as lifting off in a short distance and going into a nose high attitude below an altitude of 100 feet. The airplane then rolled left, struck the ground in a steep descent, and burned. Witnesses reported that the engines were providing power until impact; the engines and propellers had evidence of rotational damage. The flap actuators were found extended to a position that equated with 30° of flaps (half flaps). Four G-21 pilots were interviewed. According to them, flaps were not normally used for takeoff in this airplane. They reported that the turboprop engines had substantial power for the weight of the airplane, especially when the plane was not loaded, and that the G-21 would tend to become airborne quickly with flaps extended. No pre impact mechanical problem was noted during the investigation.