ATL06CA015

NTSB accident investigation · Piper PA-32-260 · Bryson City, NC · November 14, 2005

Accident · Minor injuriesData collectionFinal report
Date
November 13, 2005, 21:45 local (Nov 14, 2005, 02:45 UTC)
Place
Bryson City, NC
Injuries
1 minor, 3 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N1186XPiper PA-32-260
Weather
Visual (VMC) · Day
Status
Completed · report February 28, 2006
Report
Approved by Office Director
Parties
Charlotte FSDO
FAA report
20051113027019A
Case key
62881

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 due to carburetor icing, and the pilot's failure to use carburetor heat.

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(partial) - nonmechanicalCruise
Weather condition - carburetor icing conditionsCause
Carburetor heat - not usedPilot in commandFactor
Fuel system,carburetor - iceCause
Forced landingEmergency descent/landing
In flight collision with objectEmergency descent/landing
Object - tree(s)Cause

Analysis

According to the pilot, approximately 30 minutes into the instrument flight after reaching a cruise altitude of 7,000 feet in the clouds the engine surged, and began to lose power. The pilot switched fuel tanks, and turned on the electric fuel pump. No fuel pressure was noted on the fuel gauge, and the engine did not regain full power. The pilot reported that he did not apply carburetor heat during the loss of engine power. The pilot radioed air traffic control, and declared an emergency. During the emergency landing the airplane collided with trees. Post-accident examination of the airplane revealed the fuselage was buckled; both wing assemblies were separated from the fuselage. Post-accident examination of the airplane revealed no mechanical or flight control anomalies. Review of Advisory Circular 20-113 item 7.A-8 states: "If induction system ice is suspected of causing a power loss, apply full heat or alternate air. Do not disturb the throttle until improvement is noted. Expect a further power loss momentarily and then a rise in power as the ice is melted."

Factual narrative

According to the pilot, approximately 30 minutes into the instrument flight after reaching a cruise altitude of 7,000 feet in the clouds the engine surged, and began to lose power. The pilot switched fuel tanks, and turned on the electric fuel pump. No fuel pressure was noted on the fuel gauge, and the engine did not regain full power. The pilot reported that he did not apply carburetor heat during the loss of engine power. The pilot radioed air traffic control, and declared an emergency. During the emergency landing the airplane collided with trees. Post-accident examination of the airplane revealed the fuselage was buckled; both wing assemblies were separated from the fuselage. Post-accident examination of the airplane revealed no mechanical or flight control anomalies. Review of Advisory Circular 20-113 item 7.A-8 states: If induction system ice is suspected of causing a power loss, apply full heat or alternate air. Do not disturb the throttle until improvement is noted. Expect a further power loss momentarily and then a rise in power as the ice is melted.

Aircraft

Registration
N1186X
Reported as
Piper PA-32-260
Category
Airplane
Serial number
32-7500041
Airframe hours
2,766
Engine
Lycoming O-540, 250 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Stephen W. Beazley
Airworthiness certificate
Standard, Normal
Last inspection
Annual · May 1, 2005 · 40 hours before
Departed
GKT · Sevierville, TN
Destination
Sevierville, TN
Flight plan
IFR
Airport
GKT · Gatlinburg-Pigeon Forge

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
36
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Without waivers/limitations
Last flight review
June 1, 2005
Seat
Left
Flight hours
240 total · 35 in this make and model · 25 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 9 knots
Visibility
10 statute miles
Lowest ceiling
8,500 ft overcast
Temperature
64 °F, dew point 57 °F
Altimeter
30.25 inHg
Observed at
TYS, 23 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.