Casualties unknown

Rudder Cable Failure During Landing Flare (N369AE)

Austin, TX, US

On February 27, 1995, a Fairchild SA227-AC (registration N369AE) operated by Conquest Airlines was involved in an aviation accident near Austin, TX. Investigators recorded the probable cause as: Improper routing of the left rudder control cable during scheduled replacement in compliance with an Airworthiness Directive, which resulted in cable separation during landing. 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

A rudder cable severed during the flare phase due to improper routing from a scheduled maintenance task, yet the crew maintained control and landed safely.

What happened

The aircraft was in the final stages of approach, flaring for landing when a mechanical failure occurred. The flight crew reported hearing a distinct popping sound, immediately followed by the rudder pedal deflecting fully to its stop. Despite this sudden loss of rudder authority, the pilot successfully maintained directional control throughout the remainder of the flare and executed a normal landing without incident.

The investigation

Post-accident examination revealed that the cable controlling the left rudder had severed completely. The root cause was traced to improper routing of the control cables. This error occurred during a scheduled replacement of the control cables, which was being performed in compliance with an Airworthiness Directive. The incorrect installation path led to excessive stress or interference that caused the cable to fail during the high-load phase of landing.

Findings

The failure was not due to material fatigue or manufacturing defects but rather a procedural error during maintenance. The improper routing compromised the structural integrity of the cable under operational loads. The crew's ability to maintain control highlights effective handling skills despite the sudden loss of primary flight control surface functionality.

Probable cause

Improper routing of the left rudder control cable during scheduled replacement in compliance with an Airworthiness Directive, which resulted in cable separation during landing.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001207X02957. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.