Landing Gear Tire Failure Leads to Brake System Malfunction

Casualties unknown • Houston, TX, US

A right nose gear tire tread separation during takeoff caused damage to the landing gear and triggered a faulty signal that disabled anti-skid brakes, forcing reliance on reverse thrust for stopping.

What happened

During the takeoff roll, the tread of the right nose landing gear tire separated from the casing. This mechanical failure inflicted significant damage to several surrounding components, including the ground shift mechanism, the nose gear door, the taxi light assembly, and the equipment compartment door. The flight crew elected to return to the departure airport for a safe landing.

Upon touchdown, the aircraft's anti-skid system was engaged. However, no braking action was available from the main wheel brakes. The pilot successfully brought the aircraft to a halt using reverse thrust alone.

The investigation

A thorough examination of the aircraft revealed that the damaged ground shift mechanism had sent an erroneous signal to the anti-skid control unit. This faulty input caused the system to incorrectly interpret the aircraft's status as airborne, thereby placing the brake system into an "airborne" mode where braking is disabled.

Inspection of the failed tire showed that a liner repair had been stitched over a cut area. Evidence indicated that the cut originated from a puncture wound in the tire structure.

Findings

The investigation determined that the root cause was the improper repair of the tire. Aviation guidance AC145-4, which covers the inspection and repair of aircraft tires, generally advises against attempting to repair cuts extending through more than 40% of the ply. Crucially, it explicitly states that tires with punctures are non-repairable. The presence of a stitched liner over a puncture site violated these safety standards.

The mechanical damage caused by the tire failure led to a secondary system failure in the braking controls. The combination of an unrepairable tire and the resulting false signal to the anti-skid system created a hazardous situation where primary braking means were unavailable during landing.

Probable cause

The pilot's decision to use a tire with a puncture that had been improperly repaired, which resulted in tread separation and a subsequent faulty signal to the anti-skid system that disabled the brakes.

Frequently asked questions

What happened in the 1982-10-18 Douglas DC-9-30 accident near Houston, TX?

A right nose gear tire tread separation during takeoff caused damage to the landing gear and triggered a faulty signal that disabled anti-skid brakes, forcing reliance on reverse thrust for stopping.

What aircraft was involved and where did it happen?

The accident on 1982-10-18 involved a Douglas DC-9-30, registration N536TX, operated by Texas International, at Houston, TX.

What was the probable cause of the accident?

The pilot's decision to use a tire with a puncture that had been improperly repaired, which resulted in tread separation and a subsequent faulty signal to the anti-skid system that disabled the brakes.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020917X04495. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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