N8843L

Substantial
None

PIPER PA-25-235S/N: 25-5354

Accident Details

Date
Saturday, June 3, 2023
NTSB Number
CEN23LA233
Location
Carrington, ND
Event ID
20230608192334
Coordinates
47.442983, -99.142824
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A total loss of engine power as a result of carburetor ice that formed while the engine was operating at a low power setting for an extended period of time before departure.

Aircraft Information

Registration
Make
PIPER
Serial Number
25-5354
Engine Type
Reciprocating
Model / ICAO
PA-25-235PA25
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
PA-25-235

Registered Owner (Current)

Name
POLRIES LARRY J
Address
1226 41ST ST NW
City
JAMESTOWN
State / Zip Code
ND 58401-1810
Country
United States

Analysis

On June 3, 2023, about 0900 central daylight time, a Piper PA-25-235 airplane, N8843L, was substantially damaged when it was involved in an accident near Carrington, North Dakota. The pilot was uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 137 aerial application flight.

According to the pilot, after engine start, he taxied to the end of the runway to perform an engine run-up and allow the oil temperature to rise. During the run-up, the pilot checked the magnetos and turned on the carburetor heat. During the carburetor heat check, he noted an expected drop in rpm and then turned off the carburetor heat. He stated that he remained on the ground about 10 minutes at idle power waiting for a rise in oil temperature and reduction in oil pressure since it was the first flight of the day and the engine was cold.

The pilot stated that shortly after departure while turning onto the crosswind leg of the traffic pattern, the engine lost power, and he executed a forced landing to a gravel road. During landing, the airplane impacted a drainage ditch, which resulted in substantial damage to both wings.

During a postaccident examination, no preimpact mechanical malfunctions or failures were discovered that would have precluded normal operation.

The temperature (75°F) and dewpoint (62°F) about the time of the accident were plotted on a carburetor icing probability chart, which showed that the airplane was operating in an environment conducive for serious carburetor icing at a glide power setting. (See figure.)

Figure. Carburetor Icing Probability Chart. Reference: FAA Special Airworthiness Information Bulletin CE-09-35

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN23LA233