N7810N

Substantial
None

Piper PA-28-180S/N: 28-5261

Accident Details

Date
Tuesday, March 7, 2006
NTSB Number
CHI06CA098
Location
Holly, MI
Event ID
20060322X00328
Coordinates
42.665279, -83.418609
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A loss of engine power due to undetermined reasons. Factors associated with the accident were the guard rail and the ditch which the airplane contacted during the forced landing.

Aircraft Information

Registration
N7810N
Make
PIPER
Serial Number
28-5261
Engine Type
Reciprocating
Year Built
1968
Model / ICAO
PA-28-180P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
LAKEFIELD FLYERS LIMITED
Address
PO BOX 54
Status
Deregistered
City
COLDWATER
State / Zip Code
OH 45828-0054
Country
United States

Analysis

The airplane contacted a guard rail and a ditch during a forced landing on an interstate highway following a total loss of engine power. The pilot reported he initially flew past his intended destination airport and was turning back to the airport when loss of power occurred. He stated they were at 3,000 feet mean sea level (msl) when the engine started to sputter intermittently. He reported that he immediately checked the engine gauges which looked normal, and he switched fuel tanks. The pilot reported that upon reaching an altitude of about 2,000 msl, the engine stopped producing power. The pilot reported he applied carburetor heat and since he had the mixture leaned, he moved the mixture control to full rich. The pilot stated he attempted to restart the engine to no avail. The pilot reported his choices of a place to land included a small field, a gravel pit, or the highway. He chose the highway. He reported that he intentionally kept his speed between 75 and 80 miles per hour during the landing to match the speed of the traffic on the highway. The pilot reported that during the landing the airplane bounced and contacted a guard rail. The airplane then spun around and contacted a ditch prior to coming to rest. Following the accident the airplane was secured on a flat bed trailer and an engine test run was conducted using an alternate fuel supply. According to the Federal Aviation Administration inspector who over saw the test, the engine started and ran smooth up to 1,900 rpm. No mechanical failure/malfunction was found which would have resulted in the loss of engine 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# CHI06CA098