Casualties unknown

2007-08-18: Beech B36TC (N6750C) — Clearwater, FL

Clearwater, FL, US

On August 18, 2007, a Beech B36TC (registration N6750C) was involved in an aviation accident near Clearwater, FL. Investigators recorded the probable cause as: The pilot's improper rotation and climb during the takeoff which resulted in a stall/mush, a descent, and an impact with the ground. 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 reported that after a normal takeoff, the airplane yawed and then settled hard onto the runway. Witnesses observed wing rocking and porpoising. Post-crash examination of flight controls and engine revealed no anomalies.

Accident Description

A pilot reported a loss of control shortly after takeoff, leading to a hard landing. According to the pilot, the takeoff roll was uneventful, with rotation at 85 knots and full engine power. At about 60 feet above ground, he retracted the landing gear. Shortly after, the airplane yawed once to the right and once to the left, then settled straight down, landing hard and flat before skidding some distance. The pilot stated that the engine was producing good power and that the aircraft was within the weight and balance envelope, with 105 gallons of fuel and two normal-sized adults on board besides himself.

Pilot Statement

The owner of the accident airplane reported observing the takeoff and later spoke with the pilot while he was in the hospital. The pilot told the owner that after rotating at about 50 feet, the flight controls became mushy, and he lost elevator and rudder control. The pilot did not mention any problems during the takeoff roll.

Witness Accounts

Multiple witnesses stated that they saw the airplane lift off near the fuel farm, approximately 1,100 feet from the runway start. As the airplane climbed, its wings began to rock increasingly, and it started porpoising. The witnesses noted that the landing gear had been retracted at that point. They stated that the airplane appeared to simply cease flying. The engine sounded normal, and the propeller was rotating throughout the takeoff.

Post-Accident Examination

An FAA inspector conducted a post-crash examination of the airplane's flight controls, which functioned normally with no anomalies detected. Another FAA inspector, along with technicians from Teledyne Continental Motors, performed a detailed inspection of the engine and accessories and found no anomalies. No mechanical or control issues were identified.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20070823X01231. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.