- Date
- September 30, 1999, 07:00 local (13:00 UTC)
- Place
- Hermosa, SD
- Injuries
- 1 minor, 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Enroute
- Aircraft
- N3889FPiper PA-28-181
- Weather
- Visual (VMC) · Dawn
- Status
- Completed · report March 2, 2001
- Report
- Approved by Office Director
- FAA report
- 19990930030749A
- Case key
- 47467
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 fuel management, improper in-flight decision and the precautionary landing. Factors relating to this accident were the pilot's inadequate preflight planning and the fence post.
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
While en route to Rapid City, South Dakota, the airplane's engine started to lose power. The pilot said he discovered the fuel selector in the off position. The pilot switched the fuel selector to the left wing tank, and switched the ferry tank to 'off'. The engine began to run normally. Approximately 15 minutes later, the engine began to lose power again. The pilot turned the fuel selector to the right wing tank, turned on the electric fuel pump, and selected carburetor heat. The pilot said that none of these actions had any effect. The pilot performed a precautionary landing to a dirt road. After touching down on the dirt road, the airplane's right wing tip struck a wood fence post. The pilot said the impact tore off the right wing and the airplane spun around 180 degrees before coming to a stop. Examination of the airplane revealed fuel in the wing tanks. No fuel was found in the ferry tank. Examination of the engine and other airplane systems revealed no anomalies.
Factual narrative
On September 30, 1999, at 0700 mountain daylight time (mdt), a Piper PA-28-181, N3889F, operated by a commercial pilot, sustained substantial damage when the airplane's right wing struck a fence post, during a precautionary landing on a dirt road, 10 miles southwest of Hermosa, South Dakota. Preceding the precautionary landing, the airplane experienced an intermittent loss of engine power while in cruise flight. Visual meteorological conditions prevailed at the time of the accident. The ferry flight was being conducted under 14 CFR Part 91. There was no flight plan on file. The pilot reported no injuries. A pilot-rated passenger, on board, received minor injuries. The cross-country flight originated at Casper, Wyoming, and was en route to Rapid City, South Dakota.
In his written statement, the pilot said that while en route to Rapid City, the airplane's engine started to lose power. "After an emergency flow check, I discovered the fuel selector was in the off position. I then realized that I did not switch the ferry tank valve to the off position before taking off from Casper." The pilot switched the fuel selector to the left wing tank, and switched the ferry tank to "off". The engine began to run normally. The pilot said that 15 minutes later, the engine began to lose power again. The pilot turned the fuel selector to the right wing tank, turned on the electric fuel pump, and selected carburetor heat. None of these actions had any effect on the situation. The pilot decided to perform an emergency landing to a dirt road. After touching down on the dirt road, the airplane's right wing tip struck a wood fence post. The impact tore off the right wing and the airplane spun around 180 degrees before coming to a stop.
A Federal Aviation Administration (FAA) inspector examined the airplane at the accident site. The airplane rested upright on a dirt road flanked by fences on both sides. The airplane's right wing was broken off at the wing root. The bottom of the fuselage and the elevator showed scrapes and buckles. The propeller blades were bent aft. Examination of the airplane's fuel tanks revealed fuel in the wing tanks and no fuel in the ferry tank. Flight control continuity was confirmed. Examination of the engine, engine controls and other airplane systems revealed no anomalies.
Aircraft
- Registration
- N3889F
- Reported as
- Piper PA-28-181
- Category
- Airplane
- Serial number
- 28-7690455
- Airframe hours
- 2,457
- Engine
- Lycoming O-360-A4M, 180 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Ferry · Part 91
- Operator
- Klaas-Jaap Broek
- Registered owner
- Helease, Incorporated
- Airworthiness certificate
- Special, Special flight (Special)
- Last inspection
- Annual · May 18, 1999 · 29 hours before
- Departed
- CPR · Casper, WY
- Destination
- RAP · Rapid City, SD
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
- 26
- Certificate
- Commercial
- Airplane ratings
- Single-engine land, Multi-engine land
- Instrument ratings
- Airplane
- Medical
- Class 1, Valid Medical--no waivers/lim.
- Seat
- Left
- Flight hours
- 820 total · 80 in this make and model · 800 as pilot in command · 230 in the last 90 days · 11 in the last 30 days · 8 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Dawn
- Wind
- 320° at 6 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 39 °F, dew point 34 °F
- Altimeter
- 30.00 inHg
- Observed at
- RAP, 25 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.