Czech Sport Aircraft As Piper Sport accident near Spring Hill, Florida, May 7, 2011
On May 7, 2011 at about 3:28 am local time, a Czech Sport Aircraft As Piper Sport, registered N420PS, was substantially damaged in an accident during enroute (cruise) near Spring Hill, Florida. It was a positioning flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's inadvertent application of control inputs that resulted in rapid, right-rolling, negative g-forces during night cruise flight and his subsequent ejection from the airplane. Contributing to the accident was the pilot's decision to fly at night in an airplane not approved for night flight, his unbuckling of the seat belt portion of the restraint harness, and the inadvertent opening of the airplane’s canopy.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- May 7, 2011 · about 3:28 am local time
- Place
- Spring Hill, Florida · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Czech Sport Aircraft As Piper Sport · all Piper Sports on the register
- Registration
- N420PS · no longer on the register · serial P1001009
- Damage
- Substantial damage
- Flight
- Positioning flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot, who had previously provided flight instruction in the light sport airplane to its two principal owners, was flying it at night from Florida to Illinois. The pilot had flown commercially from Illinois to Florida earlier that day and had been offered lodging by the owners on several occasions but declined. The airplane was not approved for night operations due, in part, to a lack of interior lighting. For over an hour after takeoff, on a clear, dark night, the airplane was headed northbound in straight and level flight at 6,500 feet. The pilot, who had been in contact with an air traffic control facility, had been told to switch to a new radio frequency; afterward radar contact was lost and there were no distress calls from the pilot. The airplane impacted wooded terrain and was mostly consumed by post-impact fire. All flight control surfaces were accounted for at the scene and no preexisting mechanical anomalies were found. There was no evidence of an in-flight fire and no evidence of the pilot attempting to use the whole-airplane ballistic parachute system. The pilot was found about 1/3 mile away from the wreckage, about 600 feet to the right of the airplane's radar track. Numerous personal items were also located to the right of the airplane's radar track, with heavier items generally closer to the track than the lighter items. Shards of bubble-canopy glass and the canopy frame were found at the airplane's impact site, but no shards were noted in the vicinity of where the pilot or the personal items were found, indicating that the canopy was likely unlatched and open when the pilot and the other items exited the airplane. Each seat of the two-seat airplane was equipped with a four-point restraint harness, with each harness having four identical belt adjusting mechanisms: two for the risers and two for the seatbelt portion of the harness. Except for a number of small pieces, both harnesses were almost entirely burned. One surviving piece, for adjusting either a riser or a seat belt portion of the harness, had distorted metal and pulled material, consistent with sudden, forceful loading. The top of the pilot's shoulders also exhibited bruising, indicative of a sudden loading while the harness risers were loosely in place. There were no marks on the pilot's frontal area to indicate that the seat belt portion of the harness was buckled at the time of the loading. Ground testing revealed that access to the back shelf behind the seats would have been difficult to reach if the pilot had not unbuckled the seat belt portion of his restraint harness and loosened the risers. Thus, it is likely that the pilot tried to reach something on the back shelf. Then, at some point afterward, the canopy T-handle likely became unlatched, possibly having been caught by a loose right harness riser or a looped headset wire that plugged in next to the canopy handle. With a dark, noisy cockpit, the pilot likely then inadvertently applied rapid control inputs that resulted right-rolling, negative g-forces of sufficient intensity to eject him and the other personal items.
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
- Loss of control in flight during enroute (cruise) defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- factor Aircraft › Aircraft structures › Windows › windshield system › (general) › Unintentional use/operation
- cause Personnel issues › Action/decision › Action › Incorrect action performance › Pilot
- Environmental issues › Conditions/weather/phenomena › Light condition › Dark › Effect on operation
- Aircraft › Aircraft systems › Equipment/furnishings › Flight compartment equipment › Not used/operated
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained
- factor Aircraft › Aircraft systems › Equipment/furnishings › Flight compartment equipment › Not used/operated
- factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
Pilot
- Certificate: commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instrument: airplane
- Flight time: 2,350 hours in all
- Medical certificate: Class 1 (without waivers/limitations)
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 100 hours
- Last inspection: annual inspection, April 14, 2011
- Maximum gross weight: 1,320 lb
- Seats: 2
- Landing gear: fixed
- Engine: Rotax 912ULS (piston); 0 hours total
- Fire on the ground
The flight
- Departed from: FMY Fort Myers FL at 2:13 am
- Destination: JOT Joliet IL
- Flight plan: none
Weather at the time
- Light: night
- Visibility: 7 statute miles
- Sky: clear
- Temperature: 61°F (16°C), dew point 57°F (14°C)
- Altimeter: 30.03 inHg
- Observation at 3:53 am from BKV, 1 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
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.
