- Date
- February 14, 2001, 12:30 local (20:30 UTC)
- Place
- Petaluma, CA
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Landing
- Aircraft
- N8286PPiper PA-24-250
- Weather
- Visual (VMC) · Day
- Status
- Completed · report November 6, 2001
- Report
- Approved by Office Director
- Parties
- FEDERAL AVIATION ADMINISTRATION
- FAA report
- 20010214003459A
- Case key
- 51734
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
Failure of non-airframe and powerplant mechanic/certificated owners to properly install a new mixture cable that became entangled in the nose landing gear during its extension for landing, resulting in a loss of engine power.
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
During landing, the engine lost power. The airplane collided with trees, and made a hard landing in an open dirt field in the ensuing forced landing. On the downwind leg for landing, the pilot lowered the landing gear, and the engine began to run rough. He noted that the landing gear stopped about halfway down. He attempted to add power, but did not receive a corresponding power increase, and set up for an emergency landing. A visual external examination of the engine revealed that the mixture cable was entangled in the nose landing gear. When the landing gear was lowered the mixture cable was pulled out of its sleeve, which allowed the engine to be in a full lean position. Mixture, throttle, and propeller cables were recently installed by the pilot and his two partners. The pilot and his partners were not certificated A & P mechanics, and a certified mechanic had not returned the airplane to service after the cable installation. The last entry in the logbook was made 6 months prior to the accident,.
Factual narrative
On February 14, 2001, at 1230 hours Pacific standard time, a Piper PA-24-250, N8286P, experienced a loss of power during landing at the Petaluma Muni Airport, Petaluma, California. The airplane collided with a tree and impacted the ground 100 yards short of the runway. The airplane was owned and operated by the private pilot under the provisions of 14 CFR Part 91 as a personal flight, and sustained substantial damage. The pilot was not injured. Visual meteorological conditions prevailed. No flight plan had been filed. The flight departed the Sonoma County Airport, Santa Rosa, California, at 1145, and was scheduled to terminate at the Petaluma airport.
An inspector from the Federal Aviation Administration (FAA) interviewed the pilot. The pilot stated that he conducted the prelanding checklist on downwind for runway 11, which included reducing power and lowering the landing gear. He saw the instrument panel flex forward and the engine began to run rough. He attempted to add power, but there was not a corresponding power increase. The pilot stated that he set the airplane up for best glide and continued the flight to the airport. About 300 yards from the end of runway 29 the airplane struck a tree. The airplane continued over a street and fence, where it came to rest about 150 yards from the departure end of runway 29.
In the pilot's written statement to the Safety Board he indicated that the landing gear stopped about halfway down and then he felt a "severe" vibration. After the engine quit he continued in the pattern to set up for an emergency landing in an open field on airport property.
The airplane was inspected on scene by an FAA inspector. He visually inspected the fuel tanks. Each outboard fuel tank had half a tank of fuel, and the main fuel tanks were full.
During the inspection of the airplane, the FAA inspector noted that the mixture cable was entangled in the nose landing gear. When the landing gear was lowered, it pulled the mixture cable "out of its holder," which allowed the engine to be in a full lean position.
The pilot informed the FAA inspector that he and his two partners had recently installed the mixture, throttle, and propeller cables. The FAA inspector reported that the pilot and his partners were not certified airframe and power plant (A & P) mechanics. He further noted that a certificated A & P mechanic had not returned the airplane to service.
A review of the airplane logbook by the Safety Board investigator disclosed that the last entry was made on September 18, 2000.
Aircraft
- Registration
- N8286P
- Reported as
- Piper PA-24-250
- Category
- Airplane
- Serial number
- 24-3538
- Airframe hours
- 2,339
- Engine
- Lycoming O-540-A1D5, 250 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Registered owner
- Thomas A. Conroy
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · March 3, 2000
- Departed
- STS · Santa Rosa, CA
- Destination
- O69 · Petaluma, CA
- Airport
- O69 · Petaluma Muni, runway 11, 3,600 × 75 ft, asphalt
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
- 38
- Injuries
- None
- Certificate
- Private
- Airplane ratings
- Single-engine land
- Medical
- Class 3, Valid Medical--no waivers/lim.
- Last flight review
- March 18, 2000
- Seat
- Left
- Flight hours
- 331 total · 241 in this make and model · 294 as pilot in command · 3 in the last 90 days · 1 in the last 30 days
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 200° at 5 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 54 °F, dew point 32 °F
- Altimeter
- 30.05 inHg
- Observed at
- STS, 22 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.