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CEN26LA259 · Robinson Helicopter R44

18 Jul 2026 · Adair, IA, United States

Helicrop Robinson Helicopter R44 · Accident: system/component malfunction/failure (non-power) while maneuvering

From Menlo, IA to Menlo, IA

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Event

NTSB case
CEN26LA259
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
Ongoing
API-reported fatalities
0 · all aircraft and ground
Ground fatalities
0
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

Robinson Helicopter R44

Aircraft type
Robinson R44
Category
Helicopter
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
N484AT
Operator
Helicrop
Onboard fatalities
Unknown
Route
From Menlo, IATo Menlo, IA
Aircraft age
About 33 years (built 1993)
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
System/component malfunction/failure (non-power)
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

No findings designated as a cause are recorded in the NTSB data yet.

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

On July 18, 2026, about 1440 central daylight time, a Robinson Helicopter Company R44, N484AT, was substantially damaged when it was involved in an accident near Adair, Iowa. The pilot was not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 137 aerial application flight. The pilot stated that he was recently hired by the owner to complete agricultural spraying operations. He spoke with the pilot who flew the helicopter on the previous day and reported that the engine governor was slow to respond and that he should watch it during subsequent flights. The accident pilot decided to load the helicopter with water and complete a test flight to ensure normal operations and no governor malfunctions. The test flight was completed with no anomalies noted, and the governor was working normally. The pilot completed about 5 hours of flight time and sprayed about 600 acres without incident. Shortly before the accident, the pilot landed the helicopter on the refueler truck and added 1 quart of oil to the engine, then continued to spray another field. The pilot had completed 2 to 3 spray passes and climbed out of the field to turn around for another pass. During the turn, the low rotor rpm horn sounded so the pilot lowered the collective and increased the throttle, which increased the rotor rpm and the horn turned off. The pilot continued another spray pass and the low rotor rpm horn sounded again. He attempted to increase the throttle beyond the governor limitation, but the horn continued. The helicopter was flying about 60 mph and was about 15 to 20 ft above the field, so he executed an autorotation and landed in the mature corn. The helicopter slid in the field and rolled left, then came to rest upright. The responding FAA inspector reported that the helicopter sustained substantial damage to the main rotor blades, fuselage, and tailcone. Postaccident examination revealed that the governor control unit was not secured to its mounting location but was still connected to the airframe main wiring harness. The owner and company mechanic stated that the helicopter was recently purchased for the agricultural business and discovered that the previous owner had removed the governor control unit. They acquired another governor control unit and helicopter underwent an overhaul. When the helicopter was put back into service, the governor control unit was not secured to its mounting location. The helicopter was retained for further examination.

Verbatim NTSB factual narrative from the NTSB dataset

Sources

NTSB record CEN26LA259
Event ID
20260720203426
Case number
CEN26LA259
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, coordinates. 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: ff693be24de12f5e8839354e2f3d256a82a67c5471d63d38ec561945e7d6786d; retrieved 2026-09-17T05:17:13.376Z.