Winchester

The Citation 550 was being repositioned for an air ambulance transportation flight, and was on approach to land on a 4,801-foot-long, grooved, asphalt runway. The airplane was being flown manually by the copilot, who reported that the landing approach speed (Vref) was 106 knots. The pilot-in-command (PIC) estimated that the airplane "broke out" of the clouds about two miles from the runway. Both pilots stated that the airplane continued to descend toward the runway, while on the glide slope and localizer. Neither pilot could recall the airplane's touchdown point on the runway, or the speed at touchdown. Witnesses observed the airplane, "high and fast" as it crossed over the runway threshold. The airplane touched down about halfway down the runway, and continued off the departure end. It then struck a wooden localizer antenna platform, and the airport perimeter fence, before crossing a road, and coming to rest about 400 feet from the end of the runway. Data downloaded from the airplane's Enhanced Ground Proximity Warning System (EGPWS) revealed that the airplane's groundspeed at touchdown was about 140 knots. Review of the cockpit voice recorder suggested that the PIC failed to activate the airplane's speed brake upon touchdown. Braking action was estimated to be "fair" at the time of the accident, with about 1/4 to 1/2 inches of loose, "fluffy" snow on the runway. The PIC reported that he thought the runway might be covered with an inch or two of snow, which did not concern him. The copilot reported encountering light snow during the approach. Both pilots stated that they were not aware of any mechanical failures, or system malfunctions during the accident; nor were any discovered during post accident examinations. According to the airplane flight manual, the conditions applicable to the accident flight prescribed a Vref of 110 knots, with a required landing distance on an uncontaminated runway of approximately 2,740 feet. The prescribed landing distance on a runway contaminated with 1-inch of snow, at a Vref of 110 knots was approximately 5,800 feet. At Vref + 10 knots, the required landing distance increased to about 7,750 feet.

While on approach at night, in VMC, the left engine lost power due to fuel starvation. The propeller was not feathered, the l/g was left down, and the aircraft drifted left of crs, struck trees, and then the ground. One gallon of fuel was drained from the right wing, engine and fuel line. No fuel was found in the left wing, engine and fuel line. The copilot said the fuel quantity system was erratic with the left side more erratic, and the right side reading about 10 gallons more than the left side. Testing found the right side indicated about 45 gallons more than was present while the left side was inoperative. There was no requirement for periodic recalibration of the fuel quantity system. The owner/pilot had operated the aircraft on 32 flights, over 23 hours, and refueled 23 times using partial fills, since he had full tanks. The pilot was checked out 17 months prior and the instructor said the pilot was fine, however, he was cautioned him to enroll in recurrent training. There was no record he did. The pilot had received an FAA checkride 19 months prior to the accident, which he passed.

The airplane departed Winchester Regional Airport under VFR mode and was completing a routine point-to-point flight to Newport News/Williamsburg International Airport (PHF), Virginia after conducting a flight inspection of the ILS at Winchester Regional Airport. After takeoff, while flying at an altitude of 2,000 feet, the crew requested permission to climb but this was denied by ATC due to traffic. Awaiting an IFR clearance, the aircraft struck the slope of Mt Knob located about 30 miles southwest from Winchester Airport. All three occupants were killed.

While spraying gypsy moths with dimilin over wooded/hilly terrain, the DC-3 collided with power lines in a valley area. Witnesses in an nearby observation aircraft reported the DC-3 entered a gradual climb, which continued until the DC-3 was in a steep nose high attitude. The pilot of the observation aircraft tried to communicate with the DC-3 pilots, but could not make radio contact. The observation pilot reported the DC-3 entered a stall/spin at about 1,200 feet agl, then crashed. An investigation revealed no evidence of a preimpact failure. The DC-3 was not equipped with a wire cutter kit. Both pilots were killed.

Shortly after departing from runway 15L at the Baltimore-Washington Intl Airport, the pilot transmitted that he had an emergency consisting of a fire under his side panel. He reported he was going to circle and land. According to witnesses, flames and smoke were in the cockpit area. The aircraft started a gradual descent during a left turn. Subsequently, it crashed into a house. An examination of the wreckage did not reveal the origin of the fire; however, a CB radio was found with evidence that it may have been wired to the aircraft electrical system. The owners stated that the CB was not installed in the aircraft prior to the pilot's use of the plane on that flight. The pilot, sole on board, was killed.

The manager of Blackhawk Airways had cleared the flight for a 1000 edt departure, but the actual takeoff time was not established. No record of a preflight weather briefing was found. However, during a telephone conversation prior to the flight, the pilot indicated to his manager that the clouds would be lower in the mountains. At approximately 1030, ground witnesses observed an aircraft, matching the description of N215W, circling beneath the clouds at Keyser, WV, then depart to the southwest. When the aircraft did not arrive at its destination, a search was begun. It was found where it had impacted rising terrain approximately 6 miles southwest of Keyser. The impact occurred on a 26° slope, at approximately the 3,000 feet level, just below a 3104 feet peak. The aircraft was climbing when it impacted wooded terrain. A pilot/mechanical, who operated an airport approximately 3 miles southeast of Keyser, reported there was fog in the morning hours with a ceiling of about 2,000 feet until midday and that the mountain tops in the vicinity of the crash site were obscured. The pilot, sole on board, was killed.

Crashed in unknown circumstances in a hilly terrain located about three miles northwest of Winchester. The aircraft was damaged beyond repair and all 13 crew members were rescued.

The crew was performing a local training mission from RAF Farnborough, consisting of asymmetric landing exercices. In flight, the crew lost control of the aircraft that crashed in a field in Winchester, about 27 miles southwest of RAF Farnborough. Both crew members were killed.
Crew:
F/Lt R. F. Smail, pilot,
W. N. Plews, flight engineer.