Unapproved cable assemblies lead to Pegasus Quantum crash

Casualties unknown • Clench Common Airfield, near Marlborough, Wiltshire, GB

A microlight aircraft crashed into a barn in Wiltshire after improperly manufactured rigging cables failed during approach.

What happened

On 5 April 2006, a Pegasus Quantum 15-912, registration G-BYNO, was performing an air experience flight at Clench Common Airfield in Wiltshire. The flight, which was an instructional lesson for a passenger, proceeded normally until the aircraft was approximately 80 feet above the ground on final approach. During this phase, the aircraft encountered turbulence caused by nearby woodland.

Witnesses and the passenger reported hearing a loud noise, followed by the wing pitching up and the aircraft turning sharply to the right. A trailing wire was observed striking the propeller. The aircraft subsequently struck and penetrated the roof of a barn located near the landing threshold. The impact resulted in two serious injuries to the crew and passenger, and the aircraft was destroyed.

The investigation

Investigators examined the wreckage and found that all four rigging cable assemblies had failed. While the cables were made of the correct wire rope and were of the correct length, the metal ferrules used to secure the loops were not manufacturer-approved. These locally made assemblies had been installed approximately two weeks prior to the accident.

Laboratory analysis revealed that the ferrules used on G-BYNO had a thinner wall than factory-supplied parts. Furthermore, the copper used in these ferrules was significantly harder than the copper used in approved components. This increased hardness likely reduced the friction between the ferrule and the wire rope. Destructive testing confirmed that the cables failed because the wire rope pulled through the ferrules, rather than the wire itself snapping.

Findings

  • The primary cause of the accident was the use of non-approved, locally manufactured cable assemblies featuring incorrect ferrules.
  • The thinner wall thickness and increased hardness of the replacement ferrules resulted in insufficient grip on the wire rope.
  • The failure of the forward cables caused the wing to pitch up and the aircraft to turn right.
  • The decision to use unapproved parts instead of factory-supplied components was a critical link in the accident chain.

Probable cause

The accident was caused by the failure of rigging cable assemblies that were constructed using non-manufacturer-approved ferrules. These components lacked the necessary wall thickness and material properties to maintain a secure grip on the wire rope under flight loads, leading to the structural failure of the wing control frame.

Frequently asked questions

What happened in the 2006-04-05 Pegasus Quantum 15-912 accident near Clench Common Airfield, near Marlborough, Wiltshire, GB?

A microlight aircraft crashed into a barn in Wiltshire after improperly manufactured rigging cables failed during approach.

What aircraft was involved and where did it happen?

The accident on 2006-04-05 involved a Pegasus Quantum 15-912, registration G-BYNO, at Clench Common Airfield, near Marlborough, Wiltshire, GB.

What was the probable cause of the accident?

The accident was caused by the failure of rigging cable assemblies that were constructed using non-manufacturer-approved ferrules. These components lacked the necessary wall thickness and material properties to maintain a secure grip on the wire rope under flight loads, leading to the structural failure of the wing…

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