Rudder Control Failure During Taxi at Edinburgh Airport

Casualties unknown • EGSS, PL

A SprintAir S.A. Saab-340 experienced a loss of rudder control functionality following the release of the gust lock during taxiing at Edinburgh Airport.

What happened

On November 21, 2017, a Saab-3arm-340, registration SP-KPZ, operated by SprintAir S.A., was taxiing for takeoff at Edinburgh Airport (EGPH) for a non-scheduled commercial flight. As the crew approached runway 22, they disengaged the gust lock mechanism. Shortly after the lock was released, an audible bang was heard within the cockpit, followed by a complete lack of response from the rudder pedals.

Following the loss of rudder control, the crew immediately aborted the takeoff attempt and taxied the aircraft back to the parking stand.

The investigation

Technical personnel were dispatched from Warsaw to inspect the aircraft. The investigation established that a clevis pin located in the rear fuselage, which tensioned the right-hand rudder control cable, had fractured. This failure also caused damage to the bulkhead through which the control cable passed.

Following consultation with the aircraft manufacturer, the damaged clevis pin was replaced, and a thorough inspection of the rear fuselage area was conducted. The aircraft was subsequently ferried to Warsaw under a Permit to Fly (PTF) to facilitate repairs to the damaged bulkhead.

Probable cause

The incident was caused by the **fracture of a clevis pin** in the rear fuselage, which resulted in the loss of tension in the right rudder control cable.

Frequently asked questions

What happened in the 2017-11-21 SAAB, 340 accident near EGSS, PL?

A SprintAir S.A. Saab-340 experienced a loss of rudder control functionality following the release of the gust lock during taxiing at Edinburgh Airport.

What aircraft was involved and where did it happen?

The accident on 2017-11-21 involved a SAAB, 340, registration SP-KPZ, at EGSS, PL.

What was the probable cause of the accident?

The incident was caused by the **fracture of a clevis pin** in the rear fuselage, which resulted in the loss of tension in the right rudder control cable.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2017-3126/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.

Loading the flight search…