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Accidents · NTSB ERA23LA327 · Final report

Air Tractor AT502 accident near Leipsic, Ohio, August 4, 2023

On August 4, 2023 at about 11:30 pm local time, a 1998 Air Tractor AT502, registered N5048S, was substantially damaged in an accident during maneuvering (low-alt flying) near Leipsic, Ohio (Ruhe'S airport). 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

The incorrect assembly of the turbine engine’s reduction gear box second-stage ring gear, which resulted in an internal failure of multiple engine components and a total loss of power.

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

What the record shows

Date
August 4, 2023 · about 11:30 pm local time
Place
Leipsic, Ohio · Ruhe'S · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
visual conditions (good weather)
Aircraft
Air Tractor AT502 B, built 1998
Registration
N5048S · registry record · serial 502B-0495
Damage
Substantial damage
Flight
Aerial application (crop spraying) flight · agricultural flying rules (Part 137)

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

During the first aerial application flight of the day, the pilot noted no engine performance anomalies. After starting the second flight over the intended field, the pilot heard a “pop” and observed flames emitting from the engine exhaust ducts; then the engine sustained a total loss of power. He performed a forced landing to a field and the airplane sustained substantial damage to the left wing. About 8½ years before the accident, the engine was overhauled and reinstalled on the airplane. The records for the engine overhaul work order were no longer available. Since the overhaul, the airplane and engine received nine annual inspections and had accumulated 563.3 hours of service. Postaccident examination of the engine revealed that the reduction gear box (RGB) second-stage ring gear was assembled incorrectly in front of the retaining plates instead of the retaining plates being fixed within the dedicated slot on the ring gear. The incorrect assembly allowed the second-stage ring gear to migrate forward into the RGB front housing. This allowed reduction in the second-stage ring gear axial meshing spline engagement, to the point where the remaining contact surface could no longer sustain the ring gear load. The small overlapping region sheared off circumferentially, allowing the ring gear to spin freely and resulting in the decoupling of the power turbine (PT) disc from the propeller shaft. The reduced support by the second-stage ring gear resulted in an increase in movement of the second-stage carrier assembly. That movement then transmitted to the RGB first-stage carrier sun gear, where damage was observed on the mating teeth; the movement also resulted in excessive loads on the No. 3 bearing outer ring that resulted in its fracture. The loss of support from the No. 3 roller bearing resulted in an imbalance of the PT disc assembly that resulted in the blades fracturing. The PT vane previously had a repair performed that was not approved by the manufacturer; however, it likely did not influence the initial engine malfunction.

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. Fire/smoke (non-impact) during maneuvering (low-alt flying)
  2. Off-field or emergency landing during maneuvering (low-alt flying)
  3. Loss of engine power (total) during maneuvering (low-alt flying) defining event

The NTSB's findings

  • Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Reduction gear and shaft › Incorrect service/maintenance
  • Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Turbine section › Capability exceeded
  • Organizational issues › Support/oversight/monitoring › (general) › (general) › Maintenance provider

Pilot

  • Certificate: airline transport pilot, flight instructor
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
  • Flight time: 14,500 hours in all; 600 in this make and model; 100 in the last 90 days; 100 in the last 30 days; 11,500 as pilot in command; 1,200 on instruments
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: frt
  • Injury: no injuries

The aircraft

  • Airframe total time: 6,753.3 hours
  • Last inspection: annual inspection, May 1, 2023; 90 hours since
  • Maximum gross weight: 8,800 lb
  • Seats: 1
  • Landing gear: fixed
  • Engine: Pratt & Whitney Canada PT6A-34AG (turboprop); 8,347 hours total

The flight

  • Departed from: R47 Leipsic OH at 11:20 pm
  • Flight plan: none

Weather at the time

  • Light: dusk
  • Wind: from 020° at 4 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 79°F (26°C), dew point 57°F (14°C)
  • Altimeter: 29.99 inHg
  • Observation at 7:55 pm from OWX, 6 miles away

Weather report (METAR): KOWX 042355Z AUTO 02004KT 10SM CLR 26/14 A2999 RMK AO1

Injuries

FatalSeriousMinorNone
Flight crew1

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

13 documents, released by the NTSB on September 3, 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.

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.