NYC06LA064

NTSB accident investigation · Piper PA-28-161 · Smoketown, PA · January 28, 2006

Accident · Serious injuriesLimited investigationFinal report
Date
January 28, 2006, 17:45 local (22:45 UTC)
Place
Smoketown, PA
Injuries
1 serious, 1 minor, 2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N9183YPiper PA-28-161
Weather
Visual (VMC) · Dusk
Status
Completed · report October 3, 2006
Report
Approved by Office Director
Parties
Lycoming Engines, FAA/FSDO
FAA report
20060128012579A
Case key
63162

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

On this page

Probable cause

The pilot's improper pre-flight planning and improper fuel consumption calculations, which resulted in fuel exhaustion and a subsequent loss of engine power.

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 power(total) - nonmechanicalCruise
Fluid,fuel - exhaustion
Fuel consumption calculations - improperPilot in commandCause
Preflight planning/preparation - improperPilot in commandCause
Forced landingEmergency descent/landing
In flight collision with objectEmergency descent/landing
Object - building(nonresidential)

Analysis

The airplane was last fueled 1.4 hours prior to the accident flight. The pilot then flew for approximately 3 hours with the left fuel tank selected. When the airplane was approximately 12 miles from the destination airport, the airplane's engine lost power. The pilot attempted to restart the engine unsuccessfully, and then performed a forced landing to a field, during which the airplane impacted a barn. Examination of the airplane revealed the fuel tanks were ruptured, and no fuel was observed in the main fuel line from the firewall to the fuel pump, or the fuel line from the fuel pump to the carburetor. No mechanical anomalies were identified with the engine or airplane. According to the Piper PA-28-161 Pilot Operating Handbook, the airplane burned approximately 8.5 gallons per hour at a 75 percent power setting. The total fuel capacity was 48 useable gallons.

Factual narrative

On January 28, 2006, at 1745 eastern standard time, a Piper PA-28-161, N9183Y, was substantially damaged when it impacted a barn during a forced landing in Smoketown, Pennsylvania. The certificated private pilot received minor injuries, one passenger received serious injuries, and two other passengers were not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the flight that originated at the Cape May County Airport (WWD), Wildwood, New Jersey. The personal flight was conducted under 14 CFR Part 91.

According to the pilot, the flight originated at Lancaster Airport (LNS), Lancaster, Pennsylvania, at 1415. The pilot stated he departed with full fuel in the left tank and the right fuel tank was 3/4 full. He flew to Cape May, with the left fuel tank selected, arriving approximately 1545. He then departed Cape May at 1630, for the return flight to Lancaster. About 90 minutes later, at an altitude of 4,500 feet, the airplane's engine lost power. The pilot applied carburetor heat and switched the fuel selector to the right tank; however, the engine did not restart. He realized he would not be able to make it to Lancaster, and diverted to the Smoketown Airport (S37), Smoketown, Pennsylvania. Shortly thereafter, he realized he would not make it to Smoketown Airport, and prepared for a forced landing in a field. During the landing approach, the airplane impacted a barn.

A Federal Aviation Administration (FAA) inspector examined the airplane and engine after the accident. According to the inspector, the airplane's left and right wings were separated from the airplane and both fuel tanks were ruptured. The engine crankshaft was rotated by hand, and compression and valve train continuity was confirmed to all cylinders. Approximately 1 teaspoon of fuel was observed in the engine-driven fuel pump, and approximately 2 ounces of fuel were observed in the carburetor bowl. No fuel was observed in the main fuel line from the firewall to the fuel pump, or the fuel line from the fuel pump to the carburetor.

The data card from the Engine Data Management system, was extracted and sent to the manufacturer for download. Examination of the data correlated with values in the "normal" range for approximately 30 minutes, followed by an interruption of engine power, a momentary restart, and finally a total loss of engine power.

The pilot reported to the FAA inspector that he did not fuel the airplane at Lancaster or Cape May on the day of the accident.

Fuel records and flight logs provided by a fixed base operator at Lancaster indicated that the airplane was last fueled on January 28, 2006, at 1205, with 12.1 gallons of fuel. The airplane was then flown for 1.4 hours, prior to the accident flight.

According to the Piper PA-28-161 Pilot Operating Handbook, the airplane consumed approximately 8.5 gallons per hour at a 75 percent power setting, when leaned for best economy. The total fuel capacity was 48 useable gallons.

The pilot held a private pilot certificate with a rating for airplane single engine land, and reported 120 hours of total flight experience. His most recent FAA third-class medical certificate was issued on July 14, 2004.

Aircraft

Registration
N9183Y
Reported as
Piper PA-28-161
Category
Airplane
Serial number
288616016
Airframe hours
5,003
Engine
Lycoming O-360, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Advantage Aero Inc.
Registered owner
Murphy Air LLC
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · December 1, 2005 · 72 hours before
Departed
WWD · Wildwood, NJ
Destination
LNS · Lancaster, PA

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
51
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, With waivers/limitations
Last flight review
August 1, 2005
Seat
Left
Flight hours
120 total · 2 in this make and model · 55 as pilot in command · 5 in the last 90 days · 2 in the last 30 days

Weather

Conditions
Visual (VMC) · Dusk
Wind
240° at 4 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
50 °F, dew point 27 °F
Altimeter
30.17 inHg
Observed at
LNS, 6 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.