Active Aero Charter

Beechcraft E18

The pilot was conducting his initial revenue and solo flight for this company, in this type of airplane. The weather for takeoff included fog and low ceilings. The airplane was equipped with a primary (left) attitude indicator which was electrically operated via an independent switch. This aircraft was the only such airplane operated by this company, with an independent switch configuration for the primary attitude indicator. The airplane collided with the terrain on the airport, just after takeoff. Subsequent examination revealed no anomalies with the engines or airframe. The primary attitude indicator was located. On examination it was found to have a malfunctioning on/off flag which gave the indication of being operative regardless of power to the unit. No rotational damage was noted within the gyro housing. The pilot, sole on board, was killed.

Beechcraft E18

N3281T was attempting an instrument departure when it crashed left of the extended centerline of runway 18. The flight was observed climbing through 200 feet prior to descending to the ground. Prior to taxiing to takeoff the pilot failed to deice the airframe. Airplanes on the parking ramp around N3281T deiced prior to takeoff. Weather reports indicated that temp/dew point were 26 and 23° respectively. The surface observation also reported fog as a restriction to visibility. According to the airplane's handbook that tests prove that a coat of frost on a wing can destroy its lift. The pilot, sole on board, was killed.

Beechcraft E18

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.