N4470X

Substantial
Minor

PIPER PA 28-140S/N: 28-7625040

Accident Details

Date
Wednesday, September 21, 2016
NTSB Number
CEN16LA382
Location
Wooster, OH
Event ID
20160926X94927
Coordinates
40.873054, -81.942779
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
1
Total Aboard
2

Probable Cause and Findings

A total loss of engine power for reasons that could not be determined because postaccident examination of the engine revealed no mechanical malfunctions or failures that would have precluded normal operation.

Aircraft Information

Registration
N4470X
Make
PIPER
Serial Number
28-7625040
Engine Type
Turbo-shaft
Model / ICAO
PA 28-140M600
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Status
Deregistered
Country
United States

Analysis

On September 21, 2016 at 1236 eastern daylight time, a Piper PA-28-140, N4470X, nosed over during an off-airport landing in near Wooster, Ohio, following a loss of engine power. The private pilot received a minor injury and the passenger was not injured. The airplane was substantially damaged. The aircraft was registered to and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which was not operating on a flight plan. The flight originated from the Norwalk-Huron County Airport (5A1), Norwalk, Ohio, with an intended destination of the Carrol County-Tolson Airport (TSO), Carrollton, Ohio.The pilot reported the airplane operated normally during the first part of the flight. About 30 to 40 minutes into the flight, at an altitude of 3,500 ft, the engine suddenly lost all power. The pilot turned on the fuel boost pump, adjusted the mixture, and switched fuel tank to restart the engine. The propeller rotated, but the engine did not start. The pilot subsequently landed the airplane in a soybean field. Upon touching down, the nose gear dug into the dirt and the airplane nosed over. The pilot and passenger kicked out the windscreen and exited the airplane.

A postaccident examination of the airplane was conducted by a Federal Aviation Administration inspector. The inspector reported he verified there was fuel going to the engine, the magnetos sparked, compression on all cylinders, and continuity throughout the engine. The inspector reported the air intake duct was crushed, which most likely occurred during the accident sequence. The examination did not reveal any preimpact anomalies that would have resulted in the loss of engine power. The temperature and dewpoint were not conducive to carburetor icing at cruise 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# CEN16LA382