Quincy-Baldwin Field

The Beechcraft 1900C, N87GL, was in its landing roll on runway 13, and the Beechcraft A90, N1127D, was in its takeoff roll on runway 04. The collision occurred at the intersection of the two runways. The flight crew of the Beechcraft 1900C had made appropriate efforts to coordinate the approach and landing through radio communications and visual monitoring; however they mistook a Cherokee pilot's transmission (that he was holding for departure on runway 04) as a response from the Beechcraft A90 to their request for the Beechcraft A90's intentions, and therefore mistakenly believed that the Beechcraft A90 was not planning to take off until after the Beechcraft 1900C had cleared the runway. The failure of the Beechcraft A90 pilot to announce over the common traffic advisory frequency his intention to take off created a potential for collision between the two airplanes.

The Beechcraft 1900C, N87GL, was in its landing roll on runway 13, and the Beechcraft A90, N1127D, was in its takeoff roll on runway 04. The collision occurred at the intersection of the two runways. The flight crew of the Beechcraft 1900C had made appropriate efforts to coordinate the approach and landing through radio communications and visual monitoring; however they mistook a Cherokee pilot's transmission (that he was holding for departure on runway 04) as a response from the Beechcraft A90 to their request for the Beechcraft A90's intentions, and therefore mistakenly believed that the Beechcraft A90 was not planning to take off until after the Beechcraft 1900C had cleared the runway. The failure of the Beechcraft A90 pilot to announce over the common traffic advisory frequency his intention to take off created a potential for collision between the two airplanes.

The aircraft, at near gross weight (cg unknown), was on initial climb after takeoff. A witness reported that engines sounded normal. At about 400 feet agl the aircraft was reported to pitch up about 10°, then level off and entered a left turn. The aircraft made another left turn to the south-southwest. The pilot reported that he was returning to the field, but did not state problem. The witness said the aircraft was in a 30° left bank, turning toward the airport, when the aircraft stalled and descended to the ground in a vertical nose down attitude. Fire/explosion after impact. Left propeller found in feathered position. No engine problem found. On 1/28/87, left engine lost power after takeoff; no problem found; unable to duplicate. Pilot had two engine-out experiences in airplane previously, both when at low weight. Surrounding terrain suitable for off-airport landing. Both occupants were killed.

The aircraft was a Beech TC-45J that had been modified into a Hamilton Turboliner under STC SA-1821-WE. During arrival, the pilot reported that he encountered moderate icing at 4,000 feet. He made a localizer-only approach to runway 35. An ATC specialist stated that they saw the aircraft break out of the clouds over the approach end of the runway. At about that time, the pilot transmitted that he was going to enter a left base turn for runway 35 and that he had the runway in sight. He started a turn, and shortly thereafter, the aircraft enter a steep nose down attitude. The aircraft impacted in a railroad yard in a relatively level attitude with the landing gear extended and the wing flaps retracted. However, during impact, it was still descending at a steep angle (estimated approximately 30°). It was destroyed by impact and ground fire. No preimpact, mechanical failure or malfunction was found. The minimum ceiling and visibility for a straight-in approach were 500 feet and one mile, and for a circling approach, the minimums were 700 feet and one mile. The pilot, sole on board, was killed.