N66748

Substantial
None

CESSNA 150MS/N: 15076249

Accident Details

Date
Wednesday, August 11, 2021
NTSB Number
CEN21LA381
Location
Wadsworth, OH
Event ID
20210824103745
Coordinates
41.030000, -81.800000
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A partial loss of engine power due to carburetor icing and the pilot’s failure to apply carburetor heat when the power loss occurred.

Aircraft Information

Registration
Make
CESSNA
Serial Number
15076249
Engine Type
4-cycle
Year Built
1974
Model / ICAO
150MC150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
150M

Registered Owner (Current)

Name
SKYPARK INC
Address
PO BOX 420
City
WADSWORTH
State / Zip Code
OH 44281-0420
Country
United States

Analysis

On August 10, 2021, about 1000 eastern daylight time, a Cessna 150, N66748, sustained substantial damage when it was involved in an accident near Wadsworth Municipal Airport, Wadsworth, Ohio. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that, after she taxied to runway 21, she used the airplane’s checklist to perform an engine run-up, which included checking the magnetos and carburetor heat. Afterward, she taxied the airplane into position on the runway, held the brakes, and advanced the throttle to full power before releasing the brakes to initiate the takeoff. The pilot stated that, shortly after takeoff, she noticed that the airplane was not climbing normally and heard the stall warning horn. She then noticed the that the engine speed had rapidly decreased from 2,500 to 1,500 rpm and was continuing to decrease. The pilot stated that, due to the airplane’s low altitude, she had time only to establish the airplane’s best glide speed and prepare for forced landing to a corn field. After touchdown, the airplane nosed over, resulting in substantial damage to the fuselage, vertical stabilizer, and rudder. The airplane remained inverted in the field for about 4 days prior to recovery.

Postaccident examination of the engine revealed low compression on the No.1 cylinder. Further examination with a borescope found a small amount of carbon and lead fouling on the piston and valves. The valve cover was removed, and all valves were observed moving without restriction. After staking the valves, compression increased from 12/80 to 60/80 with no leaking past the valves. (At the time of the engine’s most recent 100hour and annual inspection, which was 4 days before the accident, the compression in the No.1 cylinder was 78/80.) All spark plugs were removed and tested; all produced a strong blue spark.

When the temperature (20°C) and dew point (17°C) that were present in the area surrounding the accident site were entered into a carburetor icing probability chart, the result was in the “moderate icing – cruise power” and “serious icing – descent power” category, as shown in the figure below. The Cessna 150 pilot’s operating handbook stated, “carburetor ice, as evidenced by an unexplained drop in RPM, can be removed by application of full carburetor heat.”

Figure . Carburetor icing probability chart (Source: AAIB).

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN21LA381