No fatalities

Tailwheel Failure and Substantial Damage in De Havilland DHC-2 Off-Airport Landing in Alaska (N723DR)

Northway, AK, United States

On August 3, 2011, a DEHAVILLAND DHC-2 MK. I(L20A) (registration N723DR) operated by COPPER VALLEY AIR SERVICE LLC was involved in an aviation accident near Northway, AK. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to identify unsuitable terrain for landing and subsequent contact with a dirt mound, resulting in the separation of the tailwheel from the airframe. This summary draws on records from NTSB; 16 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 2026-08-03Data APIEditorial standards

On August 3, 2011, a de Havilland DHC-2 (N723DR) sustained substantial damage during an off-airport landing near Northway, Alaska, after the tailwheel casting broke. The pilot and four passengers were uninjured.

Accident Overview

On August 3, 2011, at approximately 0950 Alaska daylight time, a de Havilland DHC-2 airplane, registration N723DR, sustained substantial damage during an off-airport landing about 40 miles south of Northway, Alaska. The aircraft was operated by Copper Valley Air Service, LLC, of Glennallen, Alaska, under 14 Code of Federal Regulations Part 135 as an on-demand air taxi flight, under contract to the U.S. National Park Service (NPS). The pilot and four passengers were not injured. Visual meteorological conditions prevailed, and company flight following procedures were in effect.

Flight Information

The flight originated from Gulkana Airport in Glennallen, Alaska, at about 0830. Its purpose was to transport NPS employees to a remote site for water sampling and a site survey. The pilot reported that during the landing, as the airplane came to a stop, he noticed a problem with the tailwheel. After unloading the passengers, he found that the tailwheel casting had broken, and the tailwheel spindle and fork had separated from the airframe. He inspected the landing area and observed that the aircraft had struck a small, 4-inch bank of dirt in the grass that he had not seen during the landing.

Damage Assessment

A postaccident examination by a Federal Aviation Administration (FAA) airworthiness inspector revealed substantial damage to the aft fuselage bulkhead. The aircraft was substantially damaged but no other details about the extent of damage were specified.

Probable Cause

The investigation did not state a probable cause for the accident.

Contributing factors

Causes

Damaged/degradedPilot

Other contributing factors

Effect on equipment