N9681K

Substantial
Minor

PIPER PA 28-181S/N: 28-7690274

Accident Details

Date
Sunday, July 13, 2014
NTSB Number
CEN14LA443
Location
Waukesha, WI
Event ID
20140821X03930
Coordinates
43.041110, -88.236946
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The loss of engine power for reasons that could not be determined because no anomalies were identified during postaccident examination.

Aircraft Information

Registration
N9681K
Make
PIPER
Serial Number
28-7690274
Engine Type
Turbo-shaft
Year Built
1976
Model / ICAO
PA 28-181M600
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BEEGLES AIRCRAFT SERVICE INC
Address
635 AIRPORT RD
Status
Deregistered
City
GREELEY
State / Zip Code
CO 80631
Country
United States

Analysis

On July 13, 2014, about 1300 central daylight time, a Piper PA 28-181 airplane, N9681K, impacted trees and terrain during a forced landing following a loss of engine power while on approach to land at the Waukesha County Airport, Waukesha, Wisconsin. The pilot and passenger received minor injuries. The airplane was substantially damaged. The airplane was registered to and operated by Wisconsin Fox River Flyers, Inc., 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 on a flight plan. The flight originated from the Watertown Municipal Airport, Watertown, Wisconsin, about 1220.The pilot reported that he had entered the airport traffic pattern for landing. When the airplane was abeam the approach end of the runway, he reduced power, applied carburetor heat, and confirmed that the auxiliary fuel pump was on. When the airplane was on the base leg of the traffic pattern, the pilot attempted to increase engine power but the engine did not respond. He stated that even full throttle did not result in an increase in power. He attempted moving the engine and carburetor heat controls to no avail. While attempting the remedial actions he had turned toward the runway and declared an emergency. The airplane impacted trees and terrain short of the runway resulting in substantial damage to the wings and fuselage. A postaccident examination of the airplane confirmed that fuel was present. The engine was rotated and compression was verified on all cylinders. The magnetos showed spark that was confirmed at all of the spark plug leads. No mechanical reason for the loss of engine power was found. At the time of the accident the temperature and dew point were 24 degrees C and 17 degrees C respectively. According to a carburetor icing probability chart, the temperature and dew point were in a range of susceptibility for moderate icing at cruise power settings and serious icing at descent power settings.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN14LA443