- 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.
On this page
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.
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.