N6536G

Substantial
None

CESSNA 150S/N: 15072036

Accident Details

Date
Saturday, February 18, 2023
NTSB Number
CEN23LA114
Location
Venus, TX
Event ID
20230222106757
Coordinates
32.360000, -97.030000
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The loss of engine power for undetermined reasons.

Aircraft Information

Registration
Make
CESSNA
Serial Number
15072036
Engine Type
Reciprocating
Model / ICAO
150C150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
150L

Registered Owner (Current)

Name
MESSERSMITH BRIAN W
Address
2002 BIRCHWOOD LN
City
GRAND PRAIRIE
State / Zip Code
TX 75050-2259
Country
United States

Analysis

On February 18, 2023, about 1100 central standard time, a Cessna 150L airplane, N6536G, was substantially damaged when it was involved in an accident near Venus, Texas. The flight instructor and student pilot were not injured. The airplane was operated under the provisions of Title 14 Code of Federal Regulations Part 91 as an instructional flight.

The flight instructor stated that while practicing power off stall recoveries, the student pilot had added engine power and was retracting the wing flaps when the engine began to lose power. The instructor took control of the airplane and scanned the engine instruments. He noted that oil temperature was in the green range and the oil pressure was 0 psi and blinking in the red. The engine lost total power and the flight instructor performed a forced landing to a field. During the landing roll out, the airplane nosed over and came to rest inverted. Substantial damage was sustained to the empennage and vertical stabilizer.

The airplane was recovered back to the flight school. An investigator from the National Transportation Safety Board traveled to the flight school and examined the airframe and engine. No preimpact anomalies were noted. The engine remained attached to the airframe and the investigator started the engine normally and idled the engine at 900 rpm for several minutes. Oil pressure was indicating in the normal operating range. The power was then advanced to 1,300 rpm with no discrepancies observed. Due to safety concerns, the engine power was not advanced further. When the investigator actuated the carburetor heat control, there was a drop in engine speed as expected. A magneto check was performed without any deficiencies noted.

A review of the Carburetor Icing Probability Chart located in the Federal Aviation Administration’s Special Airworthiness Information Bulletin CE-09-35, Carburetor Icing Prevention, dated June 30, 2009, found that the airplane was operating in conditions conducive to the formation of carburetor icing at glide and cruise power and serious icing at glider power. The instructor reported the use of carburetor heat during the stall training.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN23LA114