Beechcraft 200 Super King Air

The twin-engine airplane was damaged during a precautionary landing following a reported loss of power to the right engine on takeoff. The pilot reported that the right engine lost power as the landing gear was retracting after takeoff. He stated that he elected to land the airplane on the remaining runway and selected gear down. The pilot stated, "I then flew the aircraft maintaining directional control and landed on runway 24 however due to the short time between selecting gear down and landing the landing gear had not extended and the aircraft landed gear up." No anomalies were found with respect to the right engine or fuel controls during the on-scene or follow-up examination. Examination of the right propeller indicated that it was not in the feather position. The pilot reported that the autofeather system did not engage. The airplane came to rest on the runway with approximately 2000 feet of the runway surface remaining.

The aircraft was refuelled to capacity at Polokwane Airport, South Africa on 28 June 2004 with 1750 litres of Jet A1 fuel where after it flew to São Sebastião, near Vilanculos, Mozambique. Later the day on 28 June 2004 the crew attempted to take off on a non-scheduled flight from Sao Sebastiao (near Vilanculos) to Vilanculos Airport (VNX). The purpose of the fight was to airlift an injured man to a hospital at an unknown destination. The crew did not use the full runway length available but attempted the takeoff run with only 870ft (265 m) of runway available. The aircraft failed to become airborne and overran the runway, colliding with a sandbank, the perimeter fence and trees and erupted in fire. Calculations, using the takeoff performance graphs in the POH (Pilot Operating Handbook), showed that the aircraft would have required a ground roll distance of 2000 ft (610 m) with 40° flap and 2100 ft (640 m) with no flap selected.

An IFR flight plan and slot reservation were filed for the planned flight over mountainous terrain. The flightcrew intended to reposition to an airport about 30 miles southeast of the departure airport, pick up passengers, and then complete a revenue flight to another airport. The airplane departed VFR, and the flightcrew never activated the flight plan. A debris path was located, consistent with straight and level flight, near the peak of a mountain at 3,475 feet msl. Examination of the wreckage did not reveal any pre-impact mechanical malfunctions. Instrument meteorological conditions prevailed near the accident site, about the time of the accident. Further investigation revealed the aircraft operator was involved in two prior weather related accidents, both of which resulted in fatalities. A third accident went unreported, and the weather at the time of that accident was unknown. Over a period of 14 years, the same FAA principal operations inspector was assigned to the operator during all four accidents; however, no actions were ever initiated as a result of any of the accidents.

The aircraft departed Papeete-Faaa on a local post maintenance flight with one engineer and one pilot on board. Shortly after takeoff, while in initial climb, the pilot informed ATC about control problems and elected to return. Unable to maintain control, he decided to ditch the aircraft few hundred metres offshore. The aircraft sank by a depth of 21 metres and both occupants were able to swim to shore.

The twin engine aircraft departed Skopje on an official flight to Mostar, carrying two pilots and seven passengers, among them Boris Trajkovski, President of the Republic of Macedonia. He was flying to Mostar with members of his government to take part to an economic conference. On approach by night and limited visibility due to marginal weather conditions, the aircraft struck the slope of a mountain located near Berkovići, about 32 km southeast of the airport. The aircraft was destroyed by impact forces and a post crash fire and all nine occupants were killed.

Upon arriving at the destination airport, the controller cleared the flight for localizer 32 approach and informed the pilot that radar service was terminated and a frequency change was approved, report canceling IFR this frequency. The pilot acknowledged the clearance. A review of radar data revealed that the airplane was on course and lined up with the runway when the airplane collided with trees and the ground one mile south of runway 32. A review of information on file with Southeastern Air Charter, Inc., the operator of the accident airplane, found that the pilot's most recent Airman Competency/Proficiency Check was conducted in a Cessna 210. There were no records to indicate the pilot had undergone a flight-check in the Beech 200, as outlined in the Corporations FAA Approved Operational Specifications. Examination of the airframe and engines found no pre-existing discrepancies that would have precluded the airplane from operating properly prior to impact. Surface Weather Observations reported near the time of the accident. was visibility 1 to 1¼ miles; ceiling 200 feet overcast. A review of the approach plate found the minimum descent altitude for the approach to be 325 AGL and visibility 1 mile.