Goodland

According to the flight crew, they exited the clouds approximately 250 feet above ground level, slightly left of the runway centerline. The pilot not flying took control of the airplane and adjusted the course to the right. The airplane rolled hard to the right and when the pilot corrected to the left, the airplane rolled hard to the left. The airplane impacted the ground in a right wing low attitude, resulting in substantial damage. Further examination and testing revealed anomalies with the yaw damper and spoileron computer. According to the manufacturer, these anomalies would not have prevented control of the airplane. Greater control wheel displacement and force to achieve a desired roll rate when compared with an operative spoileron system would be required. The result would be a slightly higher workload for the pilot, particularly in turbulence or crosswind conditions. An examination of the remaining systems revealed no anomalies.

The flight was cleared for the ILS approach to runway 30. The flying pilot was the pilot-in-command. According to the cockpit voice recorder transcripts, the flying pilot had difficulty making a stabilized approach. During the initial descent the airplane entered an overspeed condition and the airplane flew through the localizer. During his attempt to re-establish the airplane on the localizer, the pilot allowed the airspeed to decrease to the point where the prestall 'stick-shaker' activated. The stick shaker continued until the airplane departed controlled flight and impacted terrain. No evidence of any preimpact mechanical anomalies were discovered during the investigation. All three occupants were killed.

The pilot received a weather briefing before takeoff, but did not file a flight plan. During the flight, the aircraft (Douglas A-26C, N4813E) crashed in mountainous terrain at an elevation of about 11,200 feet near Baldy Mountain. Scouting personnel, who were camped in the vicinity, reported the weather was poor with a low ceiling, restricted visibility, rain and hail. An examination of the crash site revealed the aircraft impacted in a steep, right wing low, nose low attitude. Much of the wreckage collapsed into the impact crater. The degree of destruction was consistent with a high speed impact. Chordwise scratch marks were found on the prop blades. Several tree branches and limbs at the crash site had smooth cuts. The pilot was type rated in the A-26, but his certificate had a limitation that restricted him to flying it in 'VFR only.' Neither the pilot nor the rated passenger held an instrument rating. The rated passenger did not have a type rating in the A-26, but the pilot possessed a waiver to fly N4813E as a single pilot airplane. Both occupants were killed.

The crew was performing a flight from Forbes AFB (Topeka) to Lowry AFB located near Aurora, Colorado. Enroute, while cruising in adverse weather conditions, the aircraft went out of control and crashed in a field located 4 miles north of Goodland. All 13 occupants were killed. It appears that at the time of the accident, weather conditions were poor with thunderstorm activity and electricity.

After takeoff from Goodland Airport, while climbing to a height of about 2,000 feet, the aircraft caught fire for unknown reasons. The pilot reduced his altitude and attempted an emergency landing when the airplane crashed in an open field, bursting into flames. All five occupants escaped with minor injuries and the aircraft was destroyed.

The pilot was approaching Goodland when he encountered poor weather conditions with a sandstorm. The airplane landed hard, overturned and came to rest upside down. All four occupants were injured and the aircraft was damaged beyond repair.