Amateur-built KITFOX 4 1200 accident near Canandaigua, New York, August 20, 2016
On August 20, 2016 at about 2:00 pm local time, a 2000 amateur-built KITFOX 4 1200, registered N51TM, was substantially damaged in an accident during landing near Canandaigua, New York (Canandaigua airport). It was a personal flight under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The failure of the right rudder pedal torque tube due to fatigue, which resulted in a loss of directional control during landing. Also causal to the accident was the airplane owner/builder's failure to install a rudder torque tube reinforcement or replacement in accordance with the kit manufacturer's recommendation.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- August 20, 2016 · about 2:00 pm local time
- Place
- Canandaigua, New York · Canandaigua · map
- Type
- Accident
- Injuries
- No one was hurt; 1 person was on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built KITFOX 4 1200 IV, built 2000
- Registration
- N51TM · registry record · serial C9406-0031
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The private pilot, who was also the owner/builder of the experimental, amateur-built, tailwheel-equipped airplane, was conducting a cross-country personal flight. He reported that, during landing, a rudder pedal torque tube separated, which resulted in a loss of directional control and the airplane departing the right side of the runway. Metallurgical examination revealed that the vertical torque tube for the right rudder pedal had fractured at a fillet welded intersection where it attached to a horizontal torque tube. The fracture surface exhibited a small thumbnail-like fatigue region followed by an overstress region. The pilot had assembled the airplane about 16 years before the accident, and it had accrued about 551 hours of operation. The actual kit model was manufactured 22 years before the accident, and 1 year later, the kit manufacturer published a service letter (SL) applicable to the accident airplane model, which advised owners that the company had recently noticed signs of fatigue in rudder pedal torque tubes. The SL instructed owners to inspect the areas for fatigue and offered a reinforcement kit. Further, 6 years later, the kit manufacturer redesigned the rudder pedal torque tubes for subsequent models to include a reinforcement similar to the reinforcement that had previously been offered in the reinforcement kit. The accident airplane was not equipped with the reinforcement kit recommended in the SL nor was it equipped with the newer rudder torque tube design.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Sys/Comp malf/fail (non-power) during landing defining event
- Loss of control on ground during landing
- Runway excursion during landing
- Collision with terrain or object (not controlled flight into terrain) during landing
The NTSB's findings
- cause Aircraft › Aircraft systems › Flight control system › Rudder control system › Fatigue/wear/corrosion
- cause Aircraft › Aircraft systems › Flight control system › Rudder control system › Failure
- cause Personnel issues › Task performance › Maintenance › (general) › Owner/builder
- cause Personnel issues › Action/decision › Action › Lack of action › Owner/builder
Pilot
- Certificate: private
- Ratings: single-engine land; single-engine sea
- Flight time: 1,667 hours in all; 600 in this make and model
- Last flight review: April 22, 2015
- Medical certificate: Sport Pilot
- Seat: left
- Injury: no injuries
The aircraft
- Airframe total time: 551 hours
- Last inspection: condition inspection, August 8, 2016; 3 hours since
- Maximum gross weight: 1,200 lb
- Seats: 2
- Landing gear: fixed
- Engine: Jabiru 2200 (piston); 551 hours total
The flight
- Departed from: B16 Weedsport NY at 1:20 pm
- Destination: D38 Canandaigua NY
- Flight plan: none
- Runway 31, 950 ft by 25 ft
Weather at the time
- Light: daylight
- Wind: from 190° at 7 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 79°F (26°C), dew point 63°F (17°C)
- Altimeter: 29.90 inHg
- Observation at 1:53 pm from PEO, 15 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
8 documents, released by the NTSB on August 21, 2017. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Materials Laboratory Factual Report | PDF, 3 pages | View Download |
| 2 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 9 pages | View Download |
| 3 | Interview Summary | PDF, 1 page | View Download |
| 4 | Kit Manufacturer Service Letter | PDF, 2 pages | View Download |
| 5 | Kit Manufacturer Rudder Pedal Redesign | PDF, 1 page | View Download |
| 6 | Weather Report | PDF, 1 page | View Download |
| 7 | Evidence Control Form | PDF, 1 page | View Download |
| 8 | Photo Array (Courtesy of FAA) | PDF, 2 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Other NTSB records under N51TM the same tail number, which may have belonged to a different aircraft at the time
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
