CEN17LA284 · Air Tractor AT802 A
C & C Flying Service Air Tractor AT802 A · Accident while maneuvering
From Reyno, AR (private airstrip) to an unrecorded destination
Event
- NTSB case
- CEN17LA284
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- Unknown
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Air Tractor AT802 A
- Aircraft type
- Air Tractor AT802
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N816FF
- Operator
- C & C Flying Service
- Onboard fatalities
- Unknown
- Route
- From Reyno, AR (private airstrip)To not recorded
- Aircraft age
- Built the same year (2017)
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 137: Agricultural
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- Maneuvering · low-altitude flying
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Miscellaneous/other
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Aircraft › Aircraft propeller/rotor
- Personnel issues › Task performance
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The pilot was returning to the landing strip after an uneventful spray flight when he noticed a rapid increase in engine torque shortly after he made a power reduction. The pilot stated that he “looked at my levers and pushed the prop lever all the way forward.” According to the pilot, there was insufficient thrust to maintain altitude and he made a forced landing in an open field. The airplane’s left wing impacted the ground during landing and the airplane skidded sideways to a stop. The right wingtip, right aileron, and right elevator were substantially damaged.
Examination and bench testing revealed no evidence of a mechanical malfunction or failure that would have precluded normal engine operation. Engine control continuity was confirmed from the cockpit levers to their respective engine components, and the engine controls moved smoothly through their full range of motion.
An analysis of the airplane’s engine monitor data revealed that the pilot had mistakenly moved the cockpit propeller lever instead of the power lever while he maneuvered to land. When the pilot moved the propeller control aft it increased propeller pitch which, in turn, decreased propeller speed (Np). As Np decreased there was a corresponding increase in engine torque. The data analysis revealed that Np decreased to the point where the constant speed unit (CSU) feather valve dumped oil pressure, and the propeller feathered. Engine torque then rapidly increased above the 5,100 ft-lbs limitation. Shortly after the propeller feathered, there was a rapid increase in fuel flow and engine torque, consistent with the pilot moving the power lever full forward with the propeller still feathered. The gas generator speed (Ng) and fuel flow remained relatively constant and the engine torque remained above 6,600 ft-lbs until the engine was shut down after the accident.
Probable cause
The pilot’s inadvertent use of the propeller control, which caused the propeller to feather while in flight with the engine still operating, resulting in a loss of thrust and a subsequent forced landing.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record CEN17LA284
- Event ID
- 20170725X21326
- Case number
- CEN17LA284
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status, cause areas. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: 2b56659746bd736553650f44da8c05a056cf74bc4078aecd11fa2f457e4e7cf3; retrieved 2026-09-16T05:36:18.779Z.