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Accidents · NTSB ERA21FA232 · Final report

Gulfstream American CORP AA-5A accident near Crossville, Tennessee, May 25, 2021

On May 25, 2021 at about 12:30 pm local time, a 1979 Gulfstream American CORP AA-5A, registered N26889, was destroyed in an accident during enroute near Crossville, Tennessee. It was an instructional 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

A partial loss of engine power due to carburetor icing, which resulted in a descent and impact with terrain. Contributing to the accident was the pilot’s failure to apply carburetor heat following the initial loss of engine power.

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

What the record shows

Date
May 25, 2021 · about 12:30 pm local time
Place
Crossville, Tennessee · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Gulfstream American CORP AA-5A, built 1979 · all AA-5As on the register
Registration
N26889 · no longer on the register · serial AA5A0792
Damage
Destroyed
Flight
Instructional flight · general aviation rules (Part 91)

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

The student pilot was on a multi-leg, solo cross-country flight in atmospheric conditions conducive to serious carburetor icing at descent power. Track data and interviews with the pilot’s instructor revealed that the airplane entered a gradual descent over a 5-minute span that included a 450° descending right turn. Shortly thereafter, the pilot called his instructor via cell phone and reported that the airplane’s engine was producing only partial power. The instructor stated that the pilot’s demeanor was calm, and as such, the discussion felt conversational and that there was time to discuss fuel state, engine control positions, landing at the nearest airport, or selecting a forced landing site. When asked, the pilot reported he was “40 to 50 miles” from his departure airport; however, track data revealed that the airplane was about 8 miles south of the departure airport. The instructor suggested the pilot make an “emergency landing in a field,” but the pilot reported that there were trees and mountains ahead of him before the sounds of impact were heard. The airplane was consumed by postcrash fire. Control continuity to all flight control surfaces was confirmed; examination of the engine revealed the accessories were destroyed by fire and that the core exhibited no preimpact anomalies. The fracture surfaces on a separated carburetor heat control revealed signatures consistent with overstress due to impact and high temperatures. Based on the lack of mechanical anomalies and the partial loss of engine power as reported by the pilot, it is likely that the engine lost partial power as the result of carburetor ice accumulation, which resulted in descent into terrain. It is likely that the pilot’s prompt application and use of carburetor heat in accordance with the airplane’s operating handbook would have restored engine power.

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 enroute
  2. Fuel related during enroute defining event
  3. Collision with terrain or object (not controlled flight into terrain) during emergency descent

The NTSB's findings

  • Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › Conducive to carburetor icing › Effect on equipment
  • Personnel issues › Action/decision › Action › Lack of action › Pilot
  • Aircraft › Aircraft systems › Ice/rain protection system › Intake anti › ice, deice › Not used/operated

Pilot

  • Certificate: student
  • Flight time: 44 hours in all; 44 in this make and model; 44 in the last 30 days
  • Medical certificate: Class 3 (without waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 5,419.1 hours
  • Last inspection: 100-hour inspection, May 19, 2021
  • Maximum gross weight: 2,400 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Lycoming O320-E2G (piston); 5,321 hours total
  • Fire on the ground

The flight

  • Departed from: CSV Crossville TN at 12:15 pm
  • Destination: RZR Cleveland TN
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Visibility: 9 statute miles
  • Sky: clear
  • Temperature: 72°F (22°C), dew point 63°F (17°C)
  • Altimeter: 30.26 inHg
  • Observation at 7:53 am from CSV, 8 miles away

Weather report (METAR): KCSV 251253Z AUTO 00000KT 9SM CLR 22/17 A3026 RMK AO2 SLP229 T02170167

Injuries

FatalSeriousMinorNone
Flight crew1

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

11 documents, released by the NTSB on June 8, 2023. 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.