Takeoff (climb)

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.

As ValuJet Flight 597 began its takeoff roll, a 'loud Bang' was heard by the occupants, the right engine fire warning light illuminated, the crew of a following airplane reported to the ValuJet crew that the right engine was on fire, and the takeoff was rejected. Shrapnel from the right engine penetrated the fuselage and the right engine main fuel line, and a cabin fire erupted. The airplane was stopped on the runway, and the captain ordered evacuation of the airplane. A flight attendant (F/A) received serious puncture wounds from shrapnel and thermal injuries; another F/A and 5 passengers received minor injuries. Investigation revealed that an uncontained failure of the right engine had occurred due to fatigue failure of its 7th stage high compressor disc. The fatigue originated at a stress redistribution hole in the disc. Analysis of fatigue striation measurements indicated that the fatigue crack had originated before the disc was last overhauled at a repair station (Turk Hava Yollari) in 1991, but was not detected. Also, investigation of the repair station revealed evidence concerning a lack of adequate recordkeeping and a failure to use 'process sheets' to document the step-by-step overhaul/inspection procedures.

Shortly after takeoff from a field located in Lake Grassmere, while completing the 8th sortie of the morning, the pilot lost control of the airplane that crashed on hilly terrain. The aircraft was destroyed and the pilot was killed.

The twin engine aircraft departed Hohenems-Dornbirn Airport on a local skydiving mission, carrying 23 skydivers and one pilot. After takeoff from runway 05, while climbing to a height of about 50 metres, the pilot encountered difficulties to gain height and elected to make an emergency landing when the right wing struck a tree. The aircraft stalled and crashed in an open field located 500 metres from the runway end. Four occupants, including the pilot, were injured. All 20 other occupants escaped uninjured. The aircraft was damaged beyond repair.