No fatalities

13 Nov 2019: Cessna 150 M (N704QJ) — Red Rock, AZ

Red Rock, AZ, United States

On 13 Nov 2019, a Cessna 150 M (registration N704QJ) was involved in an aviation accident near Red Rock, AZ. No fatalities were reported. Investigators recorded the probable cause as: A total loss of engine power due to carburetor icing. Contributing to the accident was the pilot’s improper use of carburetor heat. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On November 13, 2019, a Cessna 150 (N704QJ) experienced a total engine power loss during descent near Marana, Arizona, leading to a forced landing that collapsed the nose gear. The pilot was uninjured. Examination found a fuel drain handle extended and carburetor icing conditions.

Accident Details

On November 13, 2019, at 0015 mountain standard time, a Cessna 150 airplane, registration N704QJ, was substantially damaged when it was involved in an accident near Marana, Arizona. The private pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Pilot Report

The pilot reported that he recently purchased the airplane and the accident flight was a familiarization flight. After taking off, he conducted some maneuvers before proceeding to another airport to perform a touch-and-go landing. About 6 miles from the airport, he reduced the power setting to about 1,900 rpm and started the descent. About 1 mile from the airport, he reduced power to 1,500 rpm, and then to idle on final approach. He stated that he applied carburetor heat about halfway to reduce its effect on engine performance. During takeoff, the airplane started to shake, and about 1,500 ft above the ground, the engine lost total power. He performed a forced landing to a field, during which the nose landing gear collapsed.

Examination Findings

Examination of the engine by a Federal Aviation Administration (FAA) maintenance inspector revealed that the handle for the fuel strainer drain was extended about 1/2 inch. In addition, fuel streaking was found on the belly of the airplane extending from the drain port on the bottom of the cowling. The handle was manipulated by hand and operated normally. Engine compression and internal continuity was confirmed when the propeller was rotated by hand. A representative from Textron Aviation reported that when the carburetor heat control is pulled only halfway out, it will produce half the heat than when fully extended.

Weather Conditions

Weather about the time of the accident indicated a temperature of 14°C and a dewpoint of 0°C. According to FAA Special Airworthiness Information Bulletin (SAIB) CE 09-35, Carburetor Icing Prevention, this temperature/dew point was conducive to the development of icing at glide power settings. SAIB CE-09-35 noted that carburetor icing can occur at temperatures above freezing when there is visible moisture or high humidity, due to fuel vaporization and the Venturi effect causing sudden cooling. Carburetor ice can be detected by a drop in rpm in fixed pitch propeller airplanes and a drop in manifold pressure in constant speed propeller airplanes, often accompanied by roughness in engine operation.

Contributing factors

Effect on operationPilot