ERA10CA194

NTSB accident investigation · Piper PA-28-180 · Palermo, NY · March 28, 2010

Accident · Serious injuriesData collectionFinal report
Date
March 28, 2010, 15:25 local (19:25 UTC)
Place
Palermo, NY
Injuries
1 serious, 1 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N3442RPiper PA-28-180
Defining event
Enroute-cruise: Fuel exhaustion
Weather
Visual (VMC) · Day
Status
Completed · report March 16, 2011
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20100328030449A
Case key
75598

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 fuel exhaustion as a result of the pilot's inadequate fuel planning.

Findings · 3

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.

Fluids: fuelAircraft › Fluids/misc hardware · Fluid managementPiper PA-28-180: 32 casesAll aircraft: 1,695 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

Prior to departure the pilot obtained a standard preflight weather briefing. Based on the pilot's input pertaining to flight performance parameters, the flight's duration was calculated to be about 3 hours, with an estimated fuel consumption of 29.3 gallons; this fuel consumption rate was based on the pilot's historical experience of 10.0 gallons per hour. The pilot stated that the flight departed with 34 gallons of usable fuel on board. After takeoff, the pilot obtained visual-flight-rules flight following and proceeded toward the destination airport. The engine experienced a total loss of power and, approximately 3 hours 7 minutes after takeoff, the pilot advised the controller that she had exhausted the airplane's fuel supply. The pilot maneuvered the airplane toward a field and the airplane collided with a tree during the descent. Inspection of the accident site and wreckage by a Federal Aviation Administration inspector revealed the left wing was separated. No fuel was found in either main fuel tank and there was no evidence of leakage from either fuel filler cap or sump drain. A total of 1.5 ounces of fuel were drained from the carburetor bowl. Inspection of the engine revealed no evidence of preimpact failure or malfunction.

Factual narrative

The pilot obtained a standard preflight weather briefing with Lockheed Martin Automated Flight Service Station and also Data Transformation Corporation (DTC) direct user access terminal (DUAT) before departure. The estimated flight duration calculated by "DUAT.COM Flight Planner" based on pilot input pertaining to flight performance parameters, and winds aloft forecasts was 2 hours 59 minutes, with an estimated fuel consumption of 29.3 gallons. The trip fuel consumption was based on the pilot's historical experience of 10.0 gallons-per-hour (gph). The pilot stated that the flight departed with 34 gallons usable fuel on-board; the time of departure based on a witness account was 1215. After takeoff, the pilot obtained visual flight rules (VFR) flight following, and proceeded towards the destination airport. At 1522:48, or approximately 3 hours 7 minutes after takeoff, the pilot advised the controller, "mayday uh four two romeo's uh out of fuel." The controller advised the pilot of a nearby airport but the pilot advised she was unable to land there. The pilot stated that she maneuvered the airplane towards a field and during the descent she heard the sound of tree contact then recalls nothing further. Inspection of the accident site and wreckage by a Federal Aviation Administration inspector revealed the left wing was separated. No fuel was found in either main fuel tank, and there was no evidence of leakage from either fuel filler cap or sump drain. A total of 1.5 ounces of fuel were drained from the carburetor bowl. Inspection of the engine revealed no evidence of preimpact failure or malfunction.

Aircraft

Registration
N3442R
Reported as
Piper PA-28-180
Category
Airplane
Serial number
28-5681
Airframe hours
5,023
Engine
Lycoming O-360-A4A, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Williamson Flying Club
Registered owner
Williamson Flying Club
Airworthiness certificate
Standard, Utility; Standard, Normal
Last inspection
Annual · December 5, 2009 · 38 hours before
Departed
LCI · Laconia, NH
Destination
SDC · Williamson/Sodu, NY

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
56
Injuries
Serious
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, With waivers/limitations
Last flight review
August 10, 2008
Seat
Left
Flight hours
289 total · 47 in this make and model · 243 as pilot in command · 21 in the last 90 days · 13 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
160° at 10 knots
Visibility
10 statute miles
Lowest ceiling
3,500 ft overcast
Temperature
46 °F, dew point 32 °F
Altimeter
29.95 inHg
Observed at
FZY, 3 nm away

Docket · 10

The files NTSB released with the investigation on October 8, 2010, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.7 MB in all.

FAA reports on this event · 1

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