No fatalities

2020-03-14: Hawker 800XP (N100AG) — Gemini Air Group — Scottsdale, United States of America

Scottsdale, United States of AmericaLanding (descent or approach)

On March 14, 2020, a Hawker 800XP (registration N100AG) operated by Gemini Air Group was involved in an aviation accident near Scottsdale, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s inability to maintain directional control during landing for undetermined reasons, which resulted in a runway excursion. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781190518Data APIEditorial standards

A pilot lost directional control during the landing roll, causing the airplane to veer off the runway and encounter rocks. The left nosewheel tire was underinflated and worn, but the cause of the loss of control could not be determined.

Incident Details

During landing, the airplane touched down on the runway centerline in light and variable wind conditions. The pilot reported that the touchdown felt normal. However, during the landing roll, the airplane began to veer to the right. Despite the pilot applying full left rudder, the airplane continued to veer off the runway surface and encountered large rocks located between the runway and taxiway.

Pilot's Report

The pilot stated that the landing roll deviation was unexpected and that the controls were not responding as anticipated. The full left rudder input was insufficient to correct the veering motion.

Aircraft Examination

A postaccident operational check of the nosewheel steering system revealed no mechanical malfunctions or anomalies that would have precluded normal operation. However, examination of the nosewheel tires revealed that the left nosewheel tire was not adequately inflated and was worn to the point at which the cord was exposed. The right nosewheel tire was within tolerances. Additionally, one-third of the rim was absent on the left nosewheel tire outer wheel half. The available evidence precluded a determination of whether the imbalance between the nosewheel tires contributed to the control problem on the runway. It could also not be determined whether the left nosewheel tire damage occurred before the touchdown or as a result of the accident sequence.

Probable Cause

The official probable cause was the pilot's inability to maintain directional control during landing for undetermined reasons, which resulted in a runway excursion.