Casualties unknown

Wing Struts Damaged During Aborted Landing at Private Airport (N50340)

Krum, TX, US

On September 7, 2006, a Bellanca 7GCBC (registration N50340) operated by Marcair was involved in an aviation accident near Krum, TX. Investigators recorded the probable cause as: The CFI's and ATP's inflight decision to land halfway down the runway and the ATP's delayed decision to abort the landing. A factor was the ATP's excessive airspeed on final. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

An FAA inspector and flight instructor practicing takeoffs and landings in a tail-wheel airplane experienced a wing strut collision with a T-bar and fence post after an aborted landing due to excessive speed, downhill runway slope, and brake issues.

Accident Overview

A 1,800-hour flight instructor and a 4,500-hour airline transport pilot (ATP), who was also an FAA inspector, were conducting recurrency training in a tail-wheel equipped single-engine airplane. The ATP had rented the aircraft under the FAA's 4040.9D Flight Management Program. Prior to departure, the inspector noted excessive travel in the left brake pedal, but the instructor reported no prior brake issues.

Flight Details

The pair flew to a private airport with a 3,501-foot-long, 250-foot-wide turf runway, which the inspector had never visited. On the first approach, large birds on the runway prompted a go-around; the birds dispersed. On the next approach, birds had returned. The instructor suggested landing beyond the birds, approximately halfway down the runway.

The inspector maintained an approach speed of 85 mph, later admitting this was about 30 mph too fast. Upon touchdown, he realized the runway sloped downhill and that the available stopping distance was insufficient. Additionally, the left brake was not functioning properly. He aborted the landing by adding full power and initiating a climb.

Collision and Damage

During the climb, the right wing strut struck a metal T-bar and a wooden fence post that were obscured by bushes. The pilot maintained directional control and elected to return to the private airport for landing. Post-flight examination revealed damage to both left and right wing struts, with the right wing's wood spar split about 2 to 3 inches.

The ATP later stated that the airplane required at least 2,000 feet of runway to stop safely under the conditions.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20060928X01413. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.