CHI06CA098

NTSB accident investigation · Piper PA-28-180 · Holly, MI · March 7, 2006

Accident · No injuriesData collectionFinal report
Date
March 7, 2006, 16:00 local (21:00 UTC)
Place
Holly, MI
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N7810NPiper PA-28-180
Weather
Visual (VMC) · Day
Status
Completed · report May 30, 2006
Report
Approved by Office Director
Parties
Detroit, MI FSDO
FAA report
20060307004269A
Case key
63323

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

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.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine powerCruise - normal
Reason for occurrence undeterminedCause
Forced landingEmergency descent/landing
On ground/water collision with objectEmergency landing
Object - wall/barricadeFactor
On ground/water encounter with terrain/waterEmergency landing
Terrain condition - ditchFactor

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 that 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. 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.

Factual narrative

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.

Aircraft

Registration
N7810N
Reported as
Piper PA-28-180
Category
Airplane
Serial number
28-5261
Engine
Lycoming O-360-A4A, 180 hp, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Mark U. Heinl
Registered owner
Lakefield Flyers Limited
Airworthiness certificate
Standard, Normal
Departed
CQA · Celina, OH
Destination
Y47 · New Hudson, MI

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
45
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3
Flight hours
114 total · 114 in this make and model · 55 as pilot in command · 4 in the last 90 days · 2 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
350° at 3 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
43 °F, dew point 10 °F
Altimeter
30.25 inHg
Observed at
PTK

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.