N442JE

Substantial
None

ROBINSON HELICOPTER COMPANY R44 IIS/N: 10250

Accident Details

Date
Friday, July 22, 2022
NTSB Number
CEN22LA333
Location
Waterloo, IL
Event ID
20220725105560
Coordinates
38.335900, -90.149800
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The malfunction of the flight controls for undetermined reasons.

Aircraft Information

Registration
Make
ROBINSON HELICOPTER COMPANY
Serial Number
10250
Engine Type
Reciprocating
Year Built
2004
Model / ICAO
R44 IIR44
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
4
FAA Model
R44 II

Registered Owner (Current)

Name
CONCHO AVIATION LLC
Address
PO BOX 747
City
STERLING CITY
State / Zip Code
TX 76951-0747
Country
United States

Analysis

On July 22, 2022, about 0920 central daylight time, a Robinson R44 helicopter, N442JE, was substantially damaged when it was involved in an accident near Waterloo, Illinois. The pilot was not injured. The helicopter was operated under the provisions of Title 14 Code of Federal Regulations Part 137 as an aerial application flight.

The pilot reported that he was in a descent approaching a field to apply fungicide to a corn field. The collective flight control stiffened to a point that the pilot was unable to arrest the helicopter’s descent rate. The pilot attempted to use cyclic control to flare the helicopter and arrest the descent; however, the cyclic control was not responsive. The helicopter’s skids contacted the ground, which resulted 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 that the flight controls’ hydraulic assist system malfunctioned.

During the on-site inspection, no obvious anomalies were found with the flight control system. Collective, cyclic, and anti-torque pedals were all connected and appeared to be normal. Flight control continuity was confirmed from the cockpit to the main rotor swashplate linkages and main rotor blades. Flight control continuity was confirmed from the cockpit anti-torque pedals to the tail rotor gearbox and tail rotor linkages. The hydraulic components were removed for detailed examinations.

All 3 servos (2 forward and 1 aft) passed bench functionality tests. The hydraulic pump, reservoir, and fluids were normal. The forward right servo had a slightly bent piston shaft, but still was fully functional. The spool drives of the forward and aft servos exhibited signatures with normal operations. No anomalies were found that would preclude normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN22LA333