Casualties unknown

Forced Landing After Carburetor Icing During Takeoff (N2908B)

San Manuel, AZ, US

On February 11, 1993, a Beech D35 (registration N2908B) operated by Lawrence H. Ray, Sr. was involved in an aviation accident near San Manuel, AZ. Investigators recorded the probable cause as: The pilot's failure to maintain adequate airspeed and apply preventive carburetor heat during takeoff in damp and cold conditions, which resulted in **carburetor icing** and subsequent loss of engine power. 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 2026-06-10Data APIEditorial standards

A pilot executed a forced landing after losing engine power during takeoff due to carburetor icing, regaining partial power before skidding off the runway.

What happened

During the initial climb phase following takeoff, the aircraft experienced a sudden loss of engine power. Recognizing the emergency, the pilot initiated a 180-degree turn to attempt a forced landing on the same runway from which they had just departed. As the aircraft descended for this maneuver, the pilot applied carburetor heat, which successfully restored partial engine power. Despite this intervention, the airplane failed to stop within the paved surface and skidded off the end of the runway during the landing roll.

The investigation

Post-incident analysis focused on the mechanical state of the aircraft and the environmental conditions at the time of the event. The pilot reported that the weather in the valley was damp and cold, conditions known to promote ice formation in carburetors. The application of carburetor heat resulting in partial power recovery confirmed that carburetor icing was the primary mechanical factor contributing to the power loss.

Findings

The sequence of events indicates a failure to maintain adequate airspeed or apply preventive measures against carburetor icing during the critical takeoff phase. The damp and cold atmospheric conditions provided the necessary environment for ice accumulation in the carburetor throat, restricting fuel-air mixture flow. While the pilot correctly identified the issue and applied heat, the timing of the intervention occurred after significant power had already been lost, limiting the ability to complete a safe landing on the available runway.

Probable cause

The pilot's failure to maintain adequate airspeed and apply preventive carburetor heat during takeoff in damp and cold conditions, which resulted in **carburetor icing** and subsequent loss of engine power.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X11855. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.