Piper PA-28 Cadet — Other Documents

This document is an accident report from the AAIB concerning the Piper PA-28-161 Cadet, registration G-TLET, which experienced a sudden loss of engine power shortly after takeoff on July 21, 2012. The report details the circumstances of the accident, including the nature of the flight, the engine type, and the subsequent investigation into the cause of the power loss. It highlights the failure of a Wiggins clamp in the engine's turbocharger system, which led to a significant reduction in power and resulted in a forced landing. The report also discusses maintenance practices and safety recommendations to prevent similar incidents in the future.

• Aircraft Model: Piper PA-28-161 Cadet
• Engine Type: Thielert TAE 125-02-99 diesel engine
• Last Maintenance Check: 150-hour check completed 2 days before the accident
• Wiggins Clamp Inspection: Required every 300 hours, replacement every 1,200 hours
• Safety Recommendations: Addressed to Technify Motors GmbH regarding clamp inspection and maintenance practices.