PIPER PA 28-180

Carroll, OH — November 8, 2017

Event Information

DateNovember 8, 2017
Event TypeACC
NTSB NumberCEN18LA036
Event ID20171122X13300
LocationCarroll, OH
CountryUSA
Coordinates39.75555, -82.65722
AirportFAIRFIELD COUNTY
Highest InjuryNONE

Aircraft

MakePIPER
ModelPA 28-180
CategoryAIR
FAR Part091
Aircraft DamageSUBS

Conditions

Light ConditionDAYL
WeatherVMC

Injuries

Fatal0
Serious0
Minor0
None1
Total Injured0

Event Location

Probable Cause

The total loss of engine power due to carburetor icing.

Full Narrative

On November 8, 2017, about 1230 eastern standard time, a Piper PA-28-180 airplane, N10GJ, was damaged during a forced landing following a loss of engine power near Carroll, Ohio. The pilot was not injured. The airplane received substantial damage to its left wing. The airplane was registered to and operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which was not on a flight plan. The local flight originated from the Fairfield County Airport(LHQ), Lancaster, Ohio, about 1200.

The pilot reported that he was performing takeoff and landing practice and while on the downwind leg of the airport traffic pattern he applied carburetor heat, 10° flaps, turned on the fuel pump, and reduced throttle to 1,500 rpm to set up for the base leg. He stated that the engine suddenly stopped producing power and was unresponsive to throttle input. He attempted to restart the engine without success. He turned the airplane onto a base leg but had insufficient altitude to make it back to the airport and landed in a field.

Subsequent examination of the airplane revealed that it had about 36 gallons of fuel remaining. A ground run of the engine was performed and the engine started and was run for several minutes at power setting from 1,500 to 1,700 rpm. Additional testing of the airplane's electric fuel boost pump and engine driven fuel pump revealed that both pumps were capable of pumping fuel. No anomalies were discovered that would explain the loss of engine power.

The temperature and dew point recorded at the accident airport about the time of the accident were 9° and 2° Celsius respectively. The recorded temperature and dew point were in the range of susceptibility for serious carburetor icing at any power setting. An article on carburetor icing published by Flight Safety Australia stated that if ice forms in the carburetor of a fixed pitch propeller aircraft, the restriction to the induction airflow will reduce power and force a drop in rpm, which might be accompanied or followed by rough running as the fuel/air mixture ratio is upset. Applying carburetor heat introduces less dense hot air which will cause a further drop in rpm.

About This NTSB Record

This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.

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