No fatalities

3 May 2020: AIRBUS HELICOPTERS AS350 B3 (N1WT) — MACNEIL AVIATION LLC — Clewiston, FL

Clewiston, FL, United States

On 3 May 2020, an AIRBUS HELICOPTERS AS350 B3 (registration N1WT) operated by MACNEIL AVIATION LLC was involved in an aviation accident near Clewiston, FL. No fatalities were reported. Investigators recorded the probable cause as: The seizure of the hydraulic pump pulley bearing caused by improper installation by the manufacturer, which led to the failure of the hydraulic pump belt and a partial loss of hydraulic assistance to the pedals. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A pilot performed an emergency landing at Airglades Airport after experiencing a hydraulic anomaly and smoke in the cockpit of an Airbus Helicopters AS350 B3.

What happened

On May 3, 2020, an Airbus Helicopters AS350 B3, registration N1WT, performed an emergency landing at Airglades Airport (2IS) in Clewiston, Florida. The flight, operated by MACNEIL AVISEATION LLC, originated from Fort Lauderdale Executive Airport (FXE) with a stop at Palm Beach County Park Airport (LNA) before proceeding to the destination.

While entering the left downwind for runway 13 at 2IS, the pilot experienced a sudden increase in pedal resistance, describing the pedals as feeling "rock hard." Simultaneously, the "HYD2" and "SERVO" caution lights illuminated on the warning panel. The pilot also observed light smoke and a burnt odor inside the cockpit, prompting him to open the window. The pilot executed a shallow approach and completed a run-on landing at the airport. There were no injuries and the helicopter sustained no substantial damage.

The investigation

Post-landing inspections of the aircraft revealed that the HYD2 belt had fractured, with significant wear noted on the belt grooves. Remnant belt material was found on the HYD2 pump pulley and the transmission deck. The pulley grooves showed signs of overheating, and the HYD2 pump pulley and its bearing could not be rotated freely by hand.

Components were sent to the Airbus Helicopters materials laboratory in France. Investigators found that the pulley bearing's visible surfaces were thermally discolored. Internal examination of the bearing revealed smearing damage on the pulley's inner diameter and longitudinal scratches on the bearing's inner ring. The bearing's internal components—including the rings, cage, and rolling elements—showed black residue from thermally degraded grease, as well as plastic deformation and cage material transfer.

Testing revealed that if the pulley is not heated to approximately 110° Celsius during installation, the bearing can be installed skewed. A test installation performed without preheating resulted in a skewed bearing and similar smearing damage to the pulley.

Probable cause

The seizure of the hydraulic pump pulley bearing caused by improper installation by the manufacturer, which led to the failure of the hydraulic pump belt and a partial loss of hydraulic assistance to the pedals.

Contributing factors

Pump, main — FailureIncorrect service/maintenance