Casualties unknown

1996-03-07: Beech C24R (N6625P) — Robert W. Schmelzer — Philadelphia, PA

Philadelphia, PA, US

On March 7, 1996, a Beech C24R (registration N6625P) operated by Robert W. Schmelzer was involved in an aviation accident near Philadelphia, PA. Investigators recorded the probable cause as: the pilot's improper planning/decision, and his resultant flight into known icing conditions, which resulted in ice accumulation, loss of engine power, a forced landing, and subsequent collision with a residence and a vehicle. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A pilot made a forced landing in a residential area after encountering icing conditions, resulting in the aircraft striking a house and a car. Postaccident examination found no mechanical discrepancies.

Event Summary

A pilot received a preflight weather briefing that included warnings of occasional moderate mixed and rime icing, as well as isolated severe mixed and clear icing along the intended route. During the flight, the pilot encountered icing conditions and ice accretion on the aircraft. The manifold pressure began to decrease, and the pilot was unable to maintain altitude. Subsequently, a forced landing was executed in a residential area, where the airplane struck a house and a car.

Pilot Report

The pilot reported that at 5,000 feet, he expected to be above the freezing level due to a temperature inversion. This expectation held until reaching the Philadelphia area, where light mixed icing was encountered on the leading edges. Thereafter, the manifold pressure dropped to 21 inches, and altitude loss began. Although the pilot anticipated an increase in manifold pressure during descent, none occurred. At about 2,000 feet, the pilot determined that he could not reach a nearby airport and declared a mayday while maintaining 95 knots.

Postaccident Examination

A postaccident examination of the airplane included a functional check of the engine in a test cell. The engine operated rich below 1,800 RPM, and takeoff power was achieved. No mechanical discrepancies were noted with the airplane.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X05471. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.