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Accidents · NTSB ERA24LA375 · Final report

Air Tractor INC AT-802 accident near Hickory Valley, Tennessee, September 10, 2024

On September 10, 2024 at about 1:43 pm local time, a 2015 Air Tractor INC AT-802, registered N802JF, was substantially damaged in an accident during maneuvering (low-alt flying) near Hickory Valley, Tennessee. It was an aerial application (crop spraying) flight under agricultural flying rules (Part 137). 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

A partial loss of engine power due to a leak in the fuel control unit bellows, which resulted in the fuel valve moving to minimum fuel flow.

Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.

What the record shows

Date
September 10, 2024 · about 1:43 pm local time
Place
Hickory Valley, Tennessee · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
visual conditions (good weather)
Aircraft
Air Tractor INC AT-802, built 2015 · all AT-802s on the register
Registration
N802JF · registry record · serial 802-0623
Damage
Substantial damage
Flight
Aerial application (crop spraying) flight · agricultural flying rules (Part 137)

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

The pilot of the aerial application airplane reported that he departed his base airport to spray fields about 6 miles away. He had made multiple passes over the target fields when he noticed the turboprop engine’s fuel flow was lower than he had set. He pushed the power lever forward and the engine began to lose power. The pilot then pushed the power and condition levers to the forward stops in an attempt to regain power, but the engine continued to “roll back.” He jettisoned the aerial application payload in the hopper and initiated a forced landing. The airplane impacted a hay field and bounced on a slight uphill section before coming to rest. The airplane’s fuselage and engine mounts were substantially damaged during the off-airport landing. Review of data downloaded from the engine monitoring system showed that about 10 minutes after takeoff, the fuel flow began to decrease from about 82 gallons per hour to about 11 gallons per hour over 24 seconds. Examination of the engine’s fuel control unit (FCU) found the bellows exhibited corrosion and was leaking between the bellows and end cap. A review of maintenance records showed that a service bulletin (SB) was issued by the FCU manufacturer that called for the replacement of the bellows due to its age; however, the SB was not required by FAA airworthiness directive and was not complied with at overhaul or during any subsequent repair. The engine manufacturer reported that a leak in the bellows would have allowed the bellows to expand, subsequently moving the FCU fuel valve to the minimum fuel flow output as observed in the engine data recorded and as described by the pilot, preventing further power modulation. Had the actions prescribed by the SB been complied with, it is likely that the bellows would have been replaced before they began leaking and the loss of engine power occurred. The operator reported that the airplane was mainly used for spraying and fertilizing. It is possible that the corrosive chemicals used during those operations contributed to the corrosion of the bellows.

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. Collision with terrain or object (not controlled flight into terrain) during maneuvering (low-alt flying)
  2. Loss of engine power (partial) during maneuvering (low-alt flying) defining event

The NTSB's findings

  • Aircraft › Aircraft power plant › Engine fuel and control › Fuel controlling system › Fatigue/wear/corrosion
  • Aircraft › Aircraft power plant › Engine fuel and control › Fuel controlling system › Inadequate inspection
  • Aircraft › Aircraft power plant › Engine fuel and control › Fuel controlling system › Not serviced/maintained
  • Environmental issues › Operating environment › (general) › (general) › Effect on equipment
  • Personnel issues › Task performance › Maintenance › Repair › Maintenance personnel
  • Personnel issues › Action/decision › Action › Lack of action › Maintenance personnel

Pilot

  • Certificate: airline transport pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane; rotorcraft: helicopter
  • Flight time: 10,351 hours in all; 3,068 in this make and model
  • Last flight review: March 19, 2024
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: frt
  • Injury: no injuries

The aircraft

  • Airframe total time: 5,325.1 hours
  • Last inspection: 100-hour inspection, July 2, 2024; 68 hours since
  • Maximum gross weight: 16,000 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: P&W Canada PT6A-65AG (turboprop); 5,325 hours total
  • Operator: Miles Flying Service INC

The flight

  • Departed from: M08 Bolivar TN at 12:18 pm
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 75°F (24°C), dew point 63°F (17°C)
  • Altimeter: 30.11 inHg
  • Observation at 9:55 am from M08, 3 miles away

Weather report (METAR): KM08 101455Z AUTO VRB03KT 10SM CLR 24/17 A3011 RMK A01

Injuries

FatalSeriousMinorNone
Flight crew1

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

16 documents, released by the NTSB on October 22, 2025. 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.

About this page

Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The documents and photographs are the NTSB's docket, the folder of records gathered during the investigation, shown as the NTSB released them (the NTSB redacts some personal details first) and listed under the NTSB's own titles. This site's own text never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number ERA24LA375.