No fatalities

Pilot Reports Stall on Approach, Collapse of Landing Gear

Sedona, AZ, United States

On September 20, 2019, a Piper PA60 601P was involved in an aviation accident near Sedona, AZ. No fatalities were reported. Investigators recorded the probable cause as: The pilot's exceedance of the airplane's critical angle of attack during landing in gusting crosswind conditions, which resulted in an aerodynamic stall. This summary draws on records from NTSB; 11 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 2026-08-03Data APIEditorial standards

During approach, a multi-engine airplane stalled aerodynamically, landed short of the runway threshold, bounced, veered right, and exited the runway, resulting in substantial damage to the fuselage and both wings.

Incident Overview

A pilot of a retractable-landing gear, multi-engine airplane reported an aerodynamic stall during the landing approach. The pilot stated that while on approach, he perceived the airplane was slightly slow and below the glide path. He corrected by adding power and reestablishing on the visual approach slope indicator (VASI) glide path before continuing the landing.

Sequence of Events

As the airplane reached the approach end of the runway, it aerodynamically stalled. The pilot lowered the nose, and the airplane landed approximately 15 feet before the threshold of the runway. Upon touchdown, the airplane bounced onto the runway, veered right, and exited the runway into an adjacent field. Subsequently, the landing gear collapsed.

Damage and Mechanical Condition

The airplane sustained substantial damage to the fuselage and both wings. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

Wind Conditions

The airport's automated weather observation station reported that, around the time of the accident, the wind was from 180° at 15 knots, gusting to 24 knots. The pilot reported the wind was from 210° at 15 to 25 knots, gusting 15 to 25 knots. The pilot was landing on runway 21.

Contributing factors

Capability exceededPilotEffect on operation