No fatalities

7 Jul 2019: Piper PA32 260 — Seldovia, AK

Seldovia, AK, United States

On 7 Jul 2019, a Piper PA32 260 was involved in an aviation accident near Seldovia, AK. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to attain a sufficient climb following a short-field takeoff, which resulted in collision with trees. 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 reported that during a short-field takeoff from a 1,800ft gravel runway, the climb performance degraded, leading to a collision with treetops and subsequent impact with a lake. The airplane sustained substantial stabilator damage.

Accident Summary

A single-engine airplane, while performing a short-field takeoff from an 1,800-foot gravel surface, collided with treetops approximately 1,000 feet from the departure end of the runway. After the collision, the aircraft descended and impacted a lake, becoming submerged. The airplane sustained substantial damage to the stabilator.

Pilot Report

The pilot reported that the airplane's takeoff gross weight was 300 pounds less than the maximum allowable. He executed a short-field takeoff, and the initial climb proceeded as expected. However, the climb performance subsequently degraded and became insufficient to clear 80-foot-tall trees located near the departure end.

Aircraft Performance Guidelines

The manufacturer's Pilot Operating Handbook (POH) stated that for short-field takeoffs requiring obstacle clearance, the procedure after breaking ground is to accelerate to the best angle of climb speed (95 MPH) and climb past obstacles. The POH also indicated that the minimum runway distance required to take off over a 50-foot barrier was 1,360 feet, based on a hard surface runway. Additionally, the POH specified a soft-field obstacle clearance takeoff procedure using 25° flaps, accelerating just above the ground to best angle of climb speed, then continuing to climb while accelerating to best rate of climb speed (105 MPH) and slowly retracting flaps.

Outcome

The pilot reported no preaccident mechanical failures or malfunctions that would have precluded normal operation.

Contributing factors

PilotEffect on operationClimb rate — Not attained/maintained