N72129

Substantial
Serious

CESSNA 140S/N: 9296

Accident Details

Date
Monday, July 26, 2021
NTSB Number
ERA21LA300
Location
Murfreesboro, TN
Event ID
20210726103553
Coordinates
35.887134, -86.370303
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A total loss of engine power as a result of carburetor icing.

Aircraft Information

Registration
N72129
Make
CESSNA
Serial Number
9296
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
140C140
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
6000 DOUGLAS DR N
Status
Deregistered
City
CRYSTAL
State / Zip Code
MN 55429-2314
Country
United States

Analysis

On July 26, 2021, about 0900 central daylight time, a Cessna 140, N72129, was substantially damaged when it was involved in an accident near Murfreesboro Municipal Airport (MBT), Murfreesboro, Tennessee. The airline transport pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot completed a preflight inspection with no anomalies noted, and reported that the airplane contained about 14 gallons of fuel. After flying for about half an hour, the pilot entered the MBT traffic pattern. During the initial climb after the second touch-and-go landing, about 100 ft above ground level, the engine “sputtered,” lost total power, and the propeller continued to windmill. The pilot performed a forced landing onto a road, during which the airplane struck a wire, pitched downward, and impacted the road. The airplane slid about 300 ft and came to rest upright, resulting in substantial damage to the fuselage and wing struts.

The pilot reported that during landing, he typically had the carburetor heat ON until the airplane was on short final. Then, he would turn the carburetor heat OFF and perform the landing. He stated that he had a “similar” situation occur previously, during which the engine lost total power during an idle check while on the ground. After the power loss, he was able to restart the engine, and subsequently had the engine examined with no anomalies noted. Since that issue could not be duplicated, he “concluded it was carb[uretor] icing.”

An examination of the engine was performed by a mechanic under the supervision of an Federal Aviation Administration (FAA) inspector. There were no mechanical malfunctions or failures found that would have precluded normal engine operation.

The reported weather about the time of the accident included a temperature of 27°C and a dew point of 23°C. The calculated relative humidity was 80 percent. Review of the carburetor icing probability chart contained within FAA Special Airworthiness Information Bulletin CE-09-35 revealed the atmospheric conditions at the time of the accident were "conducive to serious icing at glide [idle] power."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA21LA300