Loss of climb performance during takeoff at airport

No fatalities • Grand Canyon-National Park, United States of America • Takeoff (climb)

An aircraft failed to maintain altitude during its initial climb, resulting in a collision with trees and terrain near the runway departure end.

What happened

During the takeoff phase, an aircraft failed to gain sufficient altitude following liftoff. While the pilot had received a weather briefing indicating favorable conditions, the aircraft encountered difficulties immediately after departing runway 21. The pilot noted that the plane had ceased climbing and requested updated wind information from the tower. In an attempt to avoid approaching trees, the pilot maneuvered the aircraft toward a clearing; however, the left wing struck a tree, causing the aircraft to descend into the ground.

At the time of the accident, the aircraft's gross weight was 6,000 pounds, and the density altitude was calculated at 9,481 feet. Although the pilot reported no mechanical issues with the engines or airframe, performance charts for the aircraft type indicated that the plane should have maintained a positive rate of climb of approximately 1,100 feet per minute under the recorded atmospheric conditions.

Findings

Investigation of the airport's wind recording system revealed significant fluctuations in wind speed and direction during the departure. While the initial wind reported was 300 degrees at 10 knots, subsequent data samples showed a rapid shift. Specifically, the sensor at the departure end of the runway recorded a 10-knot increase in wind speed, while the approach end sensor recorded a shift from a headwind to a tailwind of 10 knots.

Analysis of these meteorological conditions suggests that the aircraft encountered wind shear caused by developing convection over the runway. This increasing tailwind event significantly degraded the takeoff and climb performance of the aircraft.

Probable cause

The aircraft encountered wind shear characterized by an increasing tailwind due to developing convection, which prevented the aircraft from maintaining a positive rate of climb.

Frequently asked questions

What happened in the 2003-05-28 Rockwell Aero Commander 500 accident near Grand Canyon-National Park, United States of America?

An aircraft failed to maintain altitude during its initial climb, resulting in a collision with trees and terrain near the runway departure end.

Were there any fatalities in the 2003-05-28 Rockwell Aero Commander 500 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 2003-05-28 involved a Rockwell Aero Commander 500, registration N64TS, operated by Joseph L. Ciabattoni, at Grand Canyon-National Park, United States of America.

What was the probable cause of the accident?

The aircraft encountered wind shear characterized by an increasing tailwind due to developing convection, which prevented the aircraft from maintaining a positive rate of climb.

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