- Date
- March 18, 2006, 15:45 local (20:45 UTC)
- Place
- Easley, SC
- Injuries
- 1 minor
- Damage
- Substantial damage
- Phase of flight
- Enroute
- Aircraft
- N2133TPiper PA28-180F
- Weather
- Visual (VMC) · Day
- Status
- Completed · report July 31, 2006
- Report
- Approved by Office Director
- Parties
- Columbia FSDO
- FAA report
- 20060318004849A
- Case key
- 63362
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
Loss of engine power for undetermined reasons which resulted in a forced landing and subsequent in-flight collision with non-suitable terrain.
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, following takeoff, he made a left standard pattern and turned to the north and climbed to about 3,000 feet. Upon reaching altitude, he leveled off and retarded the throttle to cruise power and turned off the fuel pump. At that time, the engine began running rough like a "magneto failure". He immediately turned the fuel pump back on, made a left standard turn back toward the runway. The engine continued to lose power and he could get no response from the throttle. He tried to glide to the runway, but then realized he was going to be short. He elected to land in a road intersection. He saw two sets of power wires in his path and went over the first set and had to go under the second set. Unable to regain altitude, he impacted the ground thirty yards short of the road and slid through the intersection. Damage consisted of the left wing, left main landing gear, nose gear, engine mount, firewall, and tearing of the bottom right wing lower skin. Examination of the engine by the FAA found fuel in the gascolator and carburetor bowl with a small amount of water in both. The throttle cable was attached and functioning. There were no obstructions observed in the intake manifold. The magnetos, spark plugs and compression were all within normal limits, and valve and valve train continuity was established through to the accessory section. The engine was not run due to the collapsed nose gear. The FAA further stated that all systems inspected appeared normal and that he suspected an intermittent fuel supply problem.
Factual narrative
On March 18, 2006, at 1545 eastern standard time, a Piper PA28-180F, N2133T, registered to and operated by a private individual, as a 14 CFR Part 91 personal flight, lost engine power in cruise flight and collided with the ground during a forced landing, in Easley, South Carolina. Visual meteorological conditions prevailed and no flight plan was filed. The private pilot reported minor injuries and the airplane received substantial damage. The flight originated from the Williamsport Airpark, Easley, South Carolina, on March 18, 2006, at 1530.
According to the pilot, following takeoff, he made a left standard pattern and turned to the north and climbed to about 3,000 feet. Upon reaching altitude, he leveled and retarded the throttle to cruise power and turned off the fuel pump. At that time, the engine began running rough like a "magneto failure". He immediately turned the fuel pump back on, made a left standard turn back toward the runway. The engine continued to lose power and he could get no response from the throttle. He tried to glide to the runway then realized he was going to be short. He elected to land in a road intersection. He saw two sets of power wires in his path and went over the first set and had to go under the second set. Unable to regain altitude, he impacted the ground thirty yards short of the road and slid through the intersection. Damage consisted of the left wing, left main landing gear, nose gear, engine mount, firewall, and tearing of the bottom right wing lower skin.
Examination of the engine by the FAA found fuel in the gascolator and carburetor bowl. The FAA inspector further stated, "Found small amount of water in both but not significant." The throttle cable was attached and functioning. There were no obstructions observed in the intake manifold. The magnetos, spark plugs and compression were all within normal limits, and valve and valve train continuity was established through to the accessory section. The inspector stated, "All systems inspected appeared normal. Suspect intermittent fuel supply problem, and that he was, "Unable to run engine due to collapsed nose gear."
Aircraft
- Registration
- N2133T
- Reported as
- Piper PA28-180F
- Category
- Airplane
- Serial number
- 28-7105 158
- Airframe hours
- 6,840.36
- Engine
- Lycoming O-360-A4A, 180 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Registered owner
- Richard C. Swillen
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · October 1, 2005 · 4 hours before
- Departed
- SC86 · Easley, SC
- Destination
- SC86 · Easley, SC
- Airport
- SC86 · Williams Port
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
- 55
- Injuries
- Minor
- Certificate
- Private
- Airplane ratings
- Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 3, With waivers/limitations
- Last flight review
- December 1, 2005
- Seat
- Left
- Flight hours
- 500 total · 255 in this make and model · 400 as pilot in command · 5 in the last 90 days · 2 in the last 30 days
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- Variable at 7 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 63 °F, dew point 37 °F
- Altimeter
- 30.07 inHg
- Observed at
- GMU, 10 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.
Other investigations on N2133T · 1
Matched to the same aircraft by N-number and date.