Cagatay CGT-50 Drone Wing Separated Mid-Flight at Radnor Range
Summary
The UK AAIB published a field investigation bulletin regarding a Cagatay CGT-50 unmanned aircraft accident at Radnor Range, Powys on 5 October 2023. The investigation found that the right wing separated in-flight due to wing joiners that were shorter than design specification, combined with asymmetrical installation and inadequate quality control during manufacturing. The manufacturer implemented corrective actions including dimensional tolerances, quality checks on components, serial numbering for wing joiners, and revised assembly procedures.
What changed
The AAIB investigation determined that wing assembly components (wing joiners) were shorter than design specification and installed asymmetrically, creating uneven bending load distribution that caused the wing to separate mid-flight. The UAS operated under a CAA operational authorisation in the specific category and was not required to meet recognised design/build/test standards.
Affected parties include UAS manufacturers operating in the specific category who should review their component quality control procedures, assembly verification processes, and dimensional tolerance specifications. Range operators should also review operational communication and hazard management protocols.
What to do next
- Monitor for updates to AAIB guidance on UAS manufacturing quality standards
Archived snapshot
Apr 16, 2026GovPing captured this document from the original source. If the source has since changed or been removed, this is the text as it existed at that time.
AAIB investigation to Cagatay CGT-50, (UAS registration n/a)
Right wing separated from airframe in-flight, Radnor Range, Powys, 5 October 2023
From: Air Accidents Investigation Branch Published 16 April 2026 Category: Unmanned Aircraft Systems (UAS) Report type: Bulletin - Field investigation Date of occurrence: 5 October 2023 Aircraft type: Cagatay CGT-50 Location: Radnor Range, Powys Registration: n/a While conducting a demonstration flight at Radnor Range the right wing separated from the unmanned aircraft. The remainder of the aircraft descended rapidly, out of control and struck the ground close to personnel who were standing under the flight path.
The investigation found that the wing assembly on the accident aircraft did not have sufficient structural strength to carry the wing bending loads encountered in 1 g straight and level flight. Structural components known as wing joiners, which attached the wings to the fuselage, were shorter than the design specification. Together with a wing design that allowed movement of the joiner position and an absence of procedures to ensure the wing joiners were installed symmetrically during aircraft assembly, this created a condition where there was an uneven bending load distribution on the forward wing joiner.
The investigation determined that it was likely that old stock wing joiners from an earlier aircraft development model were inadvertently fitted to the aircraft at the production facility.
The UAS was operating in the specific category under a CAA operational authorisation (OA). The CGT-50 was not designed, built or tested to any recognised standards, nor was it required to be for operation in the specific category.
The manufacturer took several safety actions to improve quality and component control in its production facility. These included introducing dimensional tolerances on design drawings, introducing quality checks on supplied components, introducing serial numbers for wing joiners, modifying the design and production process and introducing wing joiner assembly procedures.
The range reviewed its safety plan and indicated its intention to make several improvements to operational communication and hazard management.
Download the report:
Cagatay CGT-50, UAS registration N/A 05-26
Download glossary of abbreviations:
Published 16 April 2026
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