# NTSB MIA01LA026: J and J Tukan, Hayesville, NC, November 11, 2000 - Type: NTSB accident investigation - Classification: Accident · Fatal · Limited investigation · Final report - Date: November 11, 2000, 16:30 local (21:30 UTC) - Place: Hayesville, NC - Coordinates: 35.040271, -83.810836 (estimated) - Nearby events: https://openairdocs.org/map.md?lat=35.0403&lon=-83.8108&mi=10 - Phase of flight: [Unknown](https://openairdocs.org/ntsb-phases/990) (OpenAirDocs' grouping) - Highest injury: Fatal - Injuries: 1 fatal - Status: Completed, report July 2, 2001 - Report: Approved by Office Director - NTSB case key (mKey): 51246 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=MIA01LA026 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/51246/pdf - Page: https://openairdocs.org/ntsb/MIA01LA026 ## Probable cause The ultralight pilot's in-flight loss of control for unknown reasons resulting in an in-flight collision with the terrain. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - Loss of control - in flight, unknown - reason for occurrence undetermined - In flight collision with terrain/water, descent - uncontrolled - terrain condition - grass ## Analysis No witnesses saw the ultralight depart the grass field, nor did anyone witness the crash. A heavy equipment operator saw the ultralight taxi, thought it was too windy to fly, and didn't think any more about the craft until he saw the wreckage over a fence, and called 911. Examination of the wreckage by the sheriff department investigator and the airstrip owner revealed the 'trike', movable wing configured ultralight sustained no obvious mechanical failures of the structure, rigging, or engine. The airstrip owner and a USUA instructor stated that the pilot had sustained numerous landing crashes since purchasing the ultralight. The accident flight was the first attempt by the pilot to fly with sandbag ballast in the rear seat and a runway crosswind condition. ## Factual narrative On November 11, 2000, about 1630 eastern standard time, an unregistered, J and J Toucan ultralight "trike" aircraft, operating as a Title 14 CFR Part 91 personal flight, crashed near a private airstrip in the vicinity of Hayesville, North Carolina. Visual meteorological conditions prevailed and no flight plan was filed. The airplane was destroyed and the U.S. Ultralight Association, (USUA) registered pilot, the sole occupant, received fatal injuries. The flight originated from the airstrip at an unknown time. No person actually witnessed the ultralight's departure or the accident. According to the owner of the airstrip where the ultralight was kept, a person operating heavy equipment adjacent to the airstrip saw the craft taxiing, but thought that conditions were too windy to fly. The heavy equipment operator, at some later time, discovered the wreckage over a fence and called 911. According to a Clay County Sheriff Department investigator responding to the 911 call, examination of the wreckage revealed no aircraft registration markings, a two-seat tandem configuration with sand bags strapped to the rear seat, and a 4- to 5-gallon fuel tank. The ballistic recovery system was deployed, but examination revealed it had not blossomed, and may have deployed in the collision sequence. Examination of the wreckage site revealed the ultralight impacted nose wheel first in a nose down and slight left wing down attitude, and rolled over once. According to USUA Headquarters, the pilot did not hold a USUA exemption or waiver to fly the dual-seat configured ultralight in a solo configuration. Wreckage examination was conducted by the Clay County Sheriff's Department, who provided wreckage information as well as digital photographs of the wreckage to the NTSB. Additionally, the airstrip owner provided wreckage examination statements, and background on the pilot. Examination of the wire cable rigging and all fittings and connections revealed no structural failures or malfunctions. Damage to the propeller revealed low rpm at the time of the ground/propeller strike. According to the airstrip owner, the wing and propeller had been recently replaced as a result of a previous landing accident by the pilot. The airstrip owner added that his observation of the winds at the estimated time of the accident was about 8 to 15 mph from an easterly direction, which represented a crosswind to the north-south oriented runway. He thought the accident would have been the first time the pilot flew the ultralight with the weight of the added sandbags and the wind conditions. According to a statement by a USUA flight instructor, the accident pilot sought him out about 3 months prior to the accident for additional instruction after he had been certified a USUA ultralight pilot by the facility where he bought the "trike" because he was having trouble with landings. The instructor stated that the accident pilot bought the ultralight in March 2000, and suffered a crash during initial flight instruction, as well as "multiple crashes" since receiving his ultralight pilot license. The flight instructor's statement is an attachment to this report. ## Aircraft - Registration: UNREG (not matched to a registry record) - Reported make and model: J and J TUKAN - Category: Airplane - Airframe hours: 500 - Engines: Rotax 447 40 horsepower reciprocating - Damage: Destroyed - Flight: Personal, Part 91 - Registered owner: Yves Vernier - Last inspection: Unknown, March 30, 2000, 50 hours before ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 53; seat: front; toxicology performed ## Weather - Conditions: Visual (VMC), Day - Wind: 60° at 11 knots - Visibility: 10 statute miles - Lowest ceiling: none - Temperature: 54 °F, dew point 34 °F - Altimeter: 30.00 inHg - Observed at: TYS, 46 nm away From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.