Delaware

According to a witness, prior to arriving in the run-up area the pilot lowered the airplane's flaps. After the right flap fully extended, the flap key on the drive shaft inside the 90-degree drive assembly adapter fractured, in overload, in the direction of flap extension. Before takeoff, the pilot raised the flaps; however, with the fractured key, the right flap would have remained fully extended. The pilot could have identified this condition prior to takeoff, either visually or by means of the flap indicator, which received its input from the right flap actuator. The pilot subsequently took off, and the airplane turned left, but it is unknown at what point the pilot would have noted a control problem. The pilot climbed the airplane to 250 to 300 feet and allowed the airspeed to bleed off to where the airplane stalled and subsequently spun into the ground. Airplane manufacturer calculations revealed that the pilot should have been able to maintain control of the airplane at airspeeds over 70 knots. According to the pilot's operating handbook, the best two-engine angle of climb airspeed was 99 knots and the best two-engine rate of climb airspeed was 120 knots.

The four engine aircraft departed Dover AFB at 0621LT on a flight to Kuwait City with an intermediate stop at Ramstein Airbase, Germany, carrying 17 people, three passengers and 14 crew members. Ten minutes into the flight, the copilot informed ATC about technical problems and was cleared for an immediate return. On final approach to runway 32, the aircraft descended below the glide and impacted ground few hundred metres short of runway. It came to rest in a prairie, broken in three. All 17 occupants were injured.

During a VOR runway 22 approach, the instrument rated pilot sighted the runway and cancelled his IFR flight plan. As he was circling to land, the airplane stalled and collided with terrain. Witnesses stated that the airplane made a steep left banking turn about 250 feet above the ground. According to witnesses, upon roll out of the turn, the airplane's wings rocked back and forth, the nose and right wing dropped below the horizon, and the airplane fell to the ground. Instrument meteorological conditions existed at the time of the accident and witnesses stated that the ceiling was about 400 to 500 feet above the ground. Weather facilities in the area were forecasting about 1,000 foot ceilings throughout the area. All three occupants were killed.

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.

The aircraft impacted trees during a VOR approach and descended to ground impact. The pilot flew the approach with the autopilot coupled. The altitude hold and alert were set for the MDA. When visual contact with the airport environment was established, the pilot disconnected the altitude hold and began lowering full flaps. At this time the electric trim pitched the nose of the aircraft down and the aircraft impacted trees. Both occupants escaped unhurt.

After lift-off a flock of birds approached from left to right at about 400 feet. The pilot maneuvered the aircraft behind and above the birds in an attempt to avoid them. Both engines flamed out and the aircraft made a forced landing on a road. Ground witnesses described the climbout as '...very steep...' and '...a steep angle, between 40° 45°.' There was some bird residue on the engines. Both pilots escaped uninjured.

The pilot was involved in a local spraying mission on behalf of Joseph R. Hudson, aircraft's owner. During the takeoff roll, an engine failed. For unknown reason, the pilot delayed action in aborting takeoff and failed to maintain directional control. The aircraft veered off runway and came to rest. While the pilot aged 28 was uninjured, the aircraft was damaged beyond repair.

Shortly after takeoff from Middletown-Summit Airpark, while in initial climb, the twin engine aircraft banked left and crashed in a huge explosion. Both occupants were killed and the aircraft was destroyed.

The crew was engaged in a special cargo flight on behalf of the US Air Force. Shortly after takeoff from Dover AFB, while climbing, a false engine fire warning caused the propeller to feather. The crew elected to return for a safe landing but was unable to lower the landing gear that could bot be locked due to a hydraulic pressure leak in the windshield wiper. The captain decided to complete a belly landing in a field located few dozen yards short of runway. The airplane came to rest and was damaged beyond repair while all three crew members were slightly injured.

The four engine aircraft left Dover AFB runway 32 at 0828LT on a local training flight. Fifteen minutes later, while cruising at a relative low altitude of 2,000 feet, the airplane went out of control, dove into the ground and crashed in flames in a dense wooded area located near Ellendale. The airplane was destroyed by impact forces and all four crew members were killed.
Crew:
Cpt Raymond R. Bern, pilot,
1st Lt Herbert T. Palisch, copilot,
T/Sgts Marvin A. Aust, flight engineer,
T/Sgt Edward L. McKinley Jr., flight engineer.