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Accidents · NTSB ERA15FA353 · Final report

Aero Vodochody L39 accident near Oneida, Tennessee, September 12, 2015

On September 12, 2015 at about 8:25 pm local time, a 1983 Aero Vodochody L39, registered N139RT, was destroyed in an accident during initial climb near Oneida, Tennessee (Scott Muni airport). It was an air show or air race 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 failure to maintain airplane control following a partial loss of engine power during initial climb. The reason for the partial loss of engine power could not be determined due to extensive postimpact damage.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
September 12, 2015 · about 8:25 pm local time
Place
Oneida, Tennessee · Scott Muni · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Aero Vodochody L39 C, built 1983 · all L39s on the register
Registration
N139RT · no longer on the register · serial 332505
Damage
Destroyed
Flight
Air show or air race flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The pilot of the single-engine, high-performance, jet airplane was scheduled to be the final performer at an air show. Several witnesses who observed the airplane take off reported that the airplane seemed "slow" during climbout. A witness located near the end of the departure runway stated that the airplane did not appear to be climbing as quickly as other jet-powered airplanes he had previously observed. This witness reported that the airplane made a right turn and pitched -up to gain altitude, and then the engine lost power. The airplane subsequently descended nose first and impacted trees and terrain about 2 miles west of the airport. The wreckage was severely fragmented, scattered along a 325-ft debris path, and partially consumed by a postimpact fire. Examination of the airframe and engine did not reveal evidence of any preimpact mechanical malfunctions. Although bending of fan blades opposite the direction of rotation indicated that the engine was rotating at the time of impact, imprints of fan blade tips on the shrouds with no circumferential rub marks indicated that the engine had little rotational energy and was operating at low power. Extensive damage to the fuel control unit precluded a functional test for any anomalies that could have resulted in or contributed to a loss of engine power. Although one toxicology laboratory identified ethanol in the pilot's muscle tissue, a second laboratory did not, indicating that the ethanol was from postmortem production and did not play a role in the accident. In addition, metoprolol and diphenhydramine were identified in the pilot's muscle and brain tissue. Metoprolol, a medication for hypertension, is not impairing. Diphenhydramine is a significantly impairing sedating antihistamine; however, without a blood level, no determination could be made as to whether the pilot was impaired by the effects of diphenhydramine at the time of the accident.

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

  1. Loss of engine power (partial) during initial climb defining event
  2. Loss of control in flight during emergency descent
  3. Collision with terrain or object (not controlled flight into terrain) during emergency descent
  4. Fire/smoke (post-impact) during post (impact)

The NTSB's findings

  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained
  • cause Not determined › Not determined › (general) › (general) › Unknown/Not determined

Pilot

  • Certificate: airline transport pilot, private
  • Ratings: multi-engine land; single-engine land; single-engine sea; instrument: airplane
  • Flight time: 6,000 hours in all; 325 in this make and model
  • Last flight review: April 16, 2015
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: frt
  • Injury: fatal

The aircraft

  • Airframe total time: 1,550 hours
  • Last inspection: condition inspection, April 2, 2015; 15 hours since
  • Maximum gross weight: 10,360 lb
  • Seats: 2
  • Landing gear: retractable
  • Engine: Ivchenko AI-25TL (turbofan); 340 hours total
  • Fire on the ground

The flight

  • Departed from: SCX Oneida TN at 8:25 pm
  • Destination: SCX Oneida TN
  • Flight plan: none
  • Runway 23, 5,506 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: from 310° at 5 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 73°F (23°C), dew point 39°F (4°C)
  • Altimeter: 29.85 inHg
  • Observation at 8:35 pm from JAU, 24 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

10 documents, released by the NTSB on August 7, 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.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

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.