No fatalities

Left Main Landing Gear Partial Separation Following Bounced Takeoff (N3002T)

Haines, AK, US

On September 29, 2004, a Piper PA-28-181 (registration N3002T) operated by Lab was involved in an aviation accident near Haines, AK. No fatalities were reported. Investigators recorded the probable cause as: The pilot's inadequate compensation for wind conditions during the takeoff roll, which resulted in a premature liftoff and subsequent uncontrolled descent and collision with the runway. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 5 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

A commercial pilot on a VFR positioning flight experienced a bounced takeoff with premature lift-off and yaw. The left main landing gear partially separated, and the pilot returned for an emergency landing.

Incident Overview

A commercial pilot conducting a VFR positioning flight reported that during the takeoff roll, the airplane rapidly and prematurely became airborne and began to yaw to the right. The aircraft then descended rapidly while continuing to yaw. It bounced on the runway and became airborne again. The pilot climbed to approximately 1,200 feet, where damage to the top of the left wing was observed.

Pilot Actions

Despite the observed damage, the pilot elected to continue to the destination airport, where maintenance and other services were available. However, about 10 miles from the departure airport, the left main landing gear partially separated from the wing, remaining attached only by the hydraulic brake line. The pilot then returned to the departure airport and executed a landing.

Weather Conditions

The pilot reported that during the takeoff, winds were variable from 070 degrees to 130 degrees at 15–20 knots, with gusts from 25–30 knots.

Mechanical and Damage Assessment

According to the pilot, there were no known mechanical anomalies with the airplane prior to the accident. An FAA airworthiness inspector who examined the airplane determined that during the bounced takeoff, the left main landing gear attachments were sheared from the wing spar. Additionally, during the subsequent emergency landing, the outboard left wing section and aileron were damaged.

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Frequently asked questions

What happened in the 29 Sept 2004 Piper PA-28-181 accident near Haines, AK?

A commercial pilot on a VFR positioning flight experienced a bounced takeoff with premature lift-off and yaw. The left main landing gear partially separated, and the pilot returned for an emergency landing.

Were there any fatalities in the 29 Sept 2004 Piper PA-28-181 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 29 Sept 2004 involved a Piper PA-28-181, registration N3002T, operated by Lab, at Haines, AK.

What was the probable cause of the accident?

The pilot's inadequate compensation for wind conditions during the takeoff roll, which resulted in a premature liftoff and subsequent uncontrolled descent and collision with the runway.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20041122X01850. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.