Beechcraft 200 Super King Air

Border Security Force (BSF) Beechcraft B200 Super King Air VT-EOA was engaged in a local flying (circuits and landings) at IGI Airport, Delhi on 27.8.92. There were two persons on board the aircraft including the commander. After two circuits and landings, the commander asked for full stop landing. However, after landing the commander asked the ATC about one more circuit to which the controller gave the consent and asked him to line up on runway 28 for take off. At this stage, the copilot on board was disembarked. The aircraft took-off without ATC clearance and turned left for circuit. Thereafter, it was seen going down in a nose down attitude and impacted the ground. The aircraft impacted the ground, caught fire and was destroyed. The pilot, who was the sole occupant on board, received fatal injuries.

Witnesses observed the airplane on a 'normal' final approach, then saw it drop 'low and slow, retract the gear and roll to the left into the trees.' Examination of the engines revealed that the left engine failed because of a fatigue failure of a compressor turbine blade. Examination of the right engine revealed no evidence of malfunction that would have prevented the use of full power. The aircrew was experienced and well trained. The radar data confirmed a drop in airspeed just before the airplane contacted the trees. All four occupants were killed.

While on a positioning flight, the twin engine aircraft crashed on approach to Epinal-Mirecourt Airport. The wreckage was found in a field 4 km short of runway threshold. Both pilots were killed.

While executing a VOR approach, on a dark, foggy night, depth perception and ground contact were lost when the landing lights were turned on short final. A hard landing resulted, before corrective action became effective, resulting in wing spar, engine mounting support and propeller damage. The runway, and entire airport was covered with about 3 inches of mirror smooth ice, causing considerable glare. All four occupants escaped uninjured.

While descending to Innsbruck-Kranebitten Airport, the crew encountered low clouds when the aircraft struck the slope of Mt Kellerjoch located 32 km east of the airport. The aircraft was destroyed and all three occupants were killed, among them the German entrepreneur Willy Korf (steel business).

While on approach to Halmstad Airport, the twin engine aircraft crashed in unknown circumstances 8 km short of runway. Both pilots were killed.

Following a wrong approach configuration, the twin engine aircraft landed too far down the runway 23 which is 1,600 meters long. After touchdown, the crew realized that the landing distance available was too short and decided to veer off runway. The aircraft rolled on a grassy area and came to rest. All 12 occupants evacuated safely while the aircraft was damaged beyond repair.

Before the flight, the pilots of 2 Beech 200 aircraft evaluated weather reports at a fixed base operation and made a computer weather inquiry. They departed Santa Monica, CA, on a positioning flight to Farmington, NM, without filing a flight plan. While en route, the lead aircraft was about 1 to 3 minutes ahead of the 2nd aircraft. The 2nd pilot reported they were at about 4,500 feet msl as they neared mountains and the clouds were about 1,000 feet above. As they continued eastward in a valley, the 2nd pilot heard the lead pilot report he was 'going up.' This was the last known transmission from the lead aircraft. The 2nd pilot continued his flight in VMC. Two days later, the lead aircraft was found, where it had crashed about 100 feet below the top of a 7,400 feet mountain ridge. Impact occurred on a heading of about 030°. The mountain ridge was oriented on headings of 060° 240°.

The aircraft was routinely flown to Pensacola to pickup a gulf power executive for a flight to Atlanta. The pax had 4 bags, 2 placed in the aft baggage area by the ground crew, the other 2 carried onboard by the pax. After takeoff the CVR recorded the pax stating that there was a fire. The fire in the aft cabin area was confirmed by the 1st officer. An emergency was declared to the personnel ATCT. Subsequently, the aircraft was seen descending out of the overcast streaming dark smoke behind it. The aircraft impacted an apartment complex and a post crash fire destroyed it. No evidence of a lightning strike, aircraft system malfunction, or incendiary device was found during the investigation. Forensic chemical tests showed traces of hydrochloric and sulphuric acid on pax articles but none on the cabin interior. Metallurgical exam of broken fuel line showed overload failure and post heat distress. The interior of the cockpit windows were severely sooted. The flight crew did not don available oxygen masks.

On approach to La Carlota-General Francisco de Miranda AFB, the crew was instructed to divert due to poor weather conditions at destination. While initiating a go-around procedure, the crew lost control of the aircraft that crashed in the backyard of a house, about 7,8 km short of runway. Both occupants were killed.