Casualties unknown

2005-09-30: Bellanca 7GCBC (N113AW) — Longmont, CO

Longmont, CO, US

On September 30, 2005, a Bellanca 7GCBC (registration N113AW) was involved in an aviation accident near Longmont, CO. Investigators recorded the probable cause as: The left rudder cable failed due to wear damage caused by interference from a seatback support bar extension resulting from a repair to the seat frame. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

During landing roll, a student pilot's left rudder input was unresponsive due to a failed cable. The airplane departed the runway, resulting in substantial damage. Investigation revealed cable wear from a seat frame repair.

Incident Overview

A flight instructor reported that during the landing roll, a student pilot attempted to correct the airplane from drifting to the right by applying left rudder. The rudder input was unresponsive, and the airplane continued to drift to the right, departing the runway. The airplane then looped to the right and came to rest on the right side of the runway, sustaining substantial damage.

Examination Findings

Examination of the airplane revealed that the left rudder cable had failed. Detailed optical examination of the fractured individual wire ends and strands adjacent to the fracture showed significant wear damage. At the cable separation point on the left side of the fuselage, wear marks were found on the upper, outboard seatback support bar.

Seat Frame Repair

The seat was removed from the airplane, revealing that the seat frame had been repaired on the left side. The weld extended the seatback support bar down and aft, preventing it from aligning with the lower seat support bar. This extension entered the travel path of the left rudder cable.

Additional Systems Check

An examination of the remaining airplane systems revealed no anomalies.

Probable cause

The left rudder cable failed due to wear damage caused by interference from a seatback support bar extension resulting from a repair to the seat frame.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20051007X01602. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.