No fatalities

22 Jul 2022: ROBINSON HELICOPTER COMPANY R44 II (N442JE) — CONCHO AVIATION LLC — Waterloo, IL

Waterloo, IL, United States

On 22 Jul 2022, a ROBINSON HELICOPTER COMPANY R44 II (registration N442JE) operated by CONCHO AVIATION LLC was involved in an aviation accident near Waterloo, IL. No fatalities were reported. Investigators recorded the probable cause as: The malfunction of the flight controls for undetermined reasons. This summary draws on records from NTSB; 13 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A Robinson R44 helicopter, N442JE, was substantially damaged in a rollover near Waterloo, Illinois, after the pilot reported stiff flight controls during a descent for aerial application.

Accident Overview

On July 22, 2022, about 0920 central daylight time, a Robinson R44 helicopter, registration N442JE, sustained substantial damage in an accident near Waterloo, Illinois. The helicopter was operated under Title 14 Code of Federal Regulations Part 137 as an aerial application flight. The pilot was not injured.

Pilot Report

The pilot reported that during a descent to apply fungicide to a corn field, the collective flight control stiffened to the point that he was unable to arrest the helicopter’s descent rate. Attempts to use cyclic control to flare and arrest the descent were unsuccessful, as the cyclic was not responsive. The helicopter’s skids contacted the ground, resulting in a rollover and cartwheel as the main rotors impacted the ground. The helicopter sustained substantial damage to the tail boom, fuselage, and main rotor system. The pilot stated that he suspected the flight controls’ hydraulic assist system had malfunctioned.

Examination Findings

During an on-site inspection, no obvious anomalies were found with the flight control system. The collective, cyclic, and anti-torque pedals were all connected and appeared normal. Flight control continuity was confirmed from the cockpit to the main rotor swashplate linkages and main rotor blades. Continuity was also confirmed from the cockpit anti-torque pedals to the tail rotor gearbox and tail rotor linkages. The hydraulic components were removed for detailed examination. All three servos (two forward and one aft) passed bench functionality tests. The hydraulic pump, reservoir, and fluids were normal. The forward right servo had a slightly bent piston shaft but remained fully functional. The spool drives of the forward and aft servos exhibited signatures consistent with normal operations. No anomalies were found that would preclude normal operation.

Contributing factors

Malfunction