Casualties unknown

1993-10-06: Cessna 310I (N8090M) — Southlake, TX

Southlake, TX, US

On October 6, 1993, a Cessna 310I (registration N8090M) was involved in an aviation accident near Southlake, TX. Investigators recorded the probable cause as: AIRCRAFT CONTROL NOT MAINTAINED BY THE PRIVATE PILOT RECEIVING INSTRUCTION. FACTORS WERE ROUGH RUNWAY, RUNWAY EDGE LIGHTS INOPERATIVE, DARK NIGHT CONDITIONS, BRAKES RESTRICTED DUE TO AN OUT OF RIG RUDDER SYSTEM, AND INADEQUATE CFI SUPERVISION. 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

A training aircraft veered off the runway during night operations, striking a pole and hangar. Investigation revealed that full right rudder input by the instructor caused the right brake pedal to contact the firewall, preventing effective braking.

What happened

The accident occurred during a night flight operation involving a private pilot receiving dual instruction from a certified flight instructor (CFI). The pilot was seated in the left seat while the instructor occupied the right seat. At the time of the incident, twelve out of thirty-three runway edge lights were inoperative, resulting in reduced visibility and situational awareness on the dark night.

During the ground maneuver, the aircraft encountered a bump on the runway surface. This disturbance caused the airplane to veer to the left. Both occupants reported applying right rudder and braking inputs simultaneously in an attempt to correct the trajectory. Despite these efforts, the aircraft continued its leftward deviation, striking a runway light fixture, a nearby pole, and finally a hangar.

The investigation

Following the collision, a mechanic conducted a detailed examination of the aircraft's control systems, specifically focusing on the rudder and brake mechanisms. The inspection revealed a critical mechanical interference issue within the cockpit layout.

When the pilot in the right seat applied full right rudder input, the physical movement of the controls caused the right brake pedal to contact the firewall. This contact prevented the right brake from being fully applied by either the instructor or the student pilot. Consequently, the braking capability was significantly compromised at a critical moment when maximum deceleration and directional control were required.

Findings

The investigation identified several contributing factors to the accident sequence:

  • Mechanical interference: The right brake pedal contacting the firewall during full right rudder application prevented full right brake application.
  • Inoperative lighting: Twelve of thirty-three runway edge lights were not functioning, reducing visual cues during night operations.
  • Runway surface irregularity: A bump on the runway triggered the initial veer that necessitated immediate corrective action.

The combination of reduced visual references and the mechanical failure to apply full braking force contributed to the loss of directional control. The aircraft's inability to stop or correct its path in time led to the collision with stationary objects.

Safety message

This incident highlights the importance of verifying control system functionality during pre-flight inspections, particularly regarding potential interference between pedal movements. Pilots operating in low-visibility conditions must remain aware of runway lighting status and exercise increased caution during ground maneuvers.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X13561. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.