CHI08LA171

NTSB accident investigation · Piper PA-28R-200 · Watseka, IL · June 22, 2008

Accident · Minor injuriesLimited investigationFinal report
Date
June 22, 2008, 12:50 local (17:50 UTC)
Place
Watseka, IL
Injuries
1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N6144JPiper PA-28R-200
Defining event
Enroute-descent: Loss of engine power (total)
Weather
Visual (VMC) · Day
Status
Completed · report March 5, 2009
Report
Approved by Office Director
Parties
FAA-Springfield FSDO
FAA report
20080622840729A
Case key
68479

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

The loss of engine power for undetermined reasons.

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Engine (reciprocating)Aircraft › Aircraft power plant · Not specifiedPiper PA-28R-200: 7 casesAll aircraft: 497 casesProbable cause
Not determinedNot determined › Not determined · Unknown/Not determinedPiper PA-28R-200: 16 casesAll aircraft: 2,247 cases

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

According to the pilot, the flight was cruising at 4,500 feet mean sea level (msl) when he initiated a descent in order to avoid some clouds. As the airplane descended through approximately 4,000 feet msl, the engine started to "sputter." The pilot switched fuel tanks, but he could not restore engine power. The pilot set up for a forced landing to a small road. The airplane touched down on the road, bounced, departed the left side of the road, and impacted an embankment. An examination of the airplane and engine revealed no preimpact mechanical anomalies.

Factual narrative

On June 22, 2008, about 1250 central daylight time, a Piper PA-28R-200 (Arrow II), N6144J, piloted by a private pilot, was substantially damaged during a forced landing following a loss of engine power near Watseka, Illinois. The pilot was receiving flight-following services at the time. The personal cross-country flight was being conducted under 14 CFR Part 91 without a flight plan. Visual meteorological conditions prevailed. The pilot was uninjured and the passenger sustained minor injuries. The flight departed French Lick Municipal Airport (FRH), French Lick, Indiana, about 1110. The intended destination was Lansing Municipal Airport (IGQ), Lansing, Illinois. The pilot stated the airplane was in cruise flight at the time of the loss of engine power. He noted that flight-following services were obtained after departure, and the flight diverted west of course to avoid weather. He added that the navigation instruments seemed to be inaccurate, and as a result, the flight got off course to an extent that the controller inquired about the intended route of flight. The controller subsequently provided a radar vector back on course. The flight was cruising at 4,500 feet mean sea level (msl). The pilot initiated a descent in order to avoid some clouds ahead. As the airplane descended through approximately 4,000 feet msl, the engine started to sputter. He switched fuel tanks, but could not restore engine power. He set up for a forced landing to a roadway. The airplane touched down on the road and bounced once. It subsequently departed the left side of the road where it impacted an embankment before coming to rest. According to the pilot, the airplane was topped off prior to the initial departure from IGQ, but it had not been fueled prior to the return flight. The airplane's fuel gauges indicated one-quarter full in one tank and full in the other tank. He noted that he had set the fuel flow at 11 gallons per hour (gph) during the flight. The airplane log sheet indicated that it had been flown 3.7 hours since departure from IGQ en route to FRH, the day before the accident. The airplane flight manual noted that the fuel consumption at 75-percent power was approximately 10.15 gph, with the engine properly leaned. The usable fuel capacity was 48 gallons. An examination of the airplane revealed no systems anomalies that could have contributed to the power loss or the accident.

Aircraft

Registration
N6144J
Reported as
Piper PA-28R-200
Category
Airplane
Serial number
28R-7635302
Engine
Lycoming IO-360-C1C, 200 hp, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Associated Air Activities
Airworthiness certificate
Standard, Normal
Departed
FRH · French Lick, IN
Destination
IGQ · Lansing, IL

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
46
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Without waivers/limitations
Last flight review
June 6, 2008
Seat
Left
Flight hours
290 total · 13 in this make and model · 237 as pilot in command · 5 in the last 90 days · 5 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
320° at 7 knots, gusting 17
Visibility
10 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 46 °F
Altimeter
29.89 inHg
Observed at
IKK, 19 nm away

FAA reports on this event · 1

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