EASA SIB CE-17-25
Textron Aviation Inc. (formerly Cessna, Reims) 172, 175, 180, 182, 185, 188, and 208 Aeroplanes - Elevator Torque Tube — Inspections for Cracks and Corrosion
Summary
The Textron Aviation Inc. (formerly Cessna, Reims) 172, 175, 180, 182, 185, 188, and 208 Aeroplanes - Elevator Torque Tube — Inspections for Cracks and Corrosion is a Safety Information Bulletin focused on airworthiness. It addresses the need for inspections of the elevator torque tube on specified Textron Aviation aircraft models to detect cracks and corrosion that could affect flight safety.
What Changed
This Safety Information Bulletin introduces inspection requirements for the elevator torque tube on the listed Textron Aviation aircraft models. It emphasizes the identification of cracks and corrosion that were not previously mandated for routine inspection, aiming to enhance safety measures.
Why It Matters
This bulletin is important for aviation professionals because cracks or corrosion in the elevator torque tube can compromise the control surfaces, potentially leading to unsafe flight conditions. Operators, maintenance organizations, and compliance teams need to be aware of these inspection requirements to maintain aircraft airworthiness and prevent in-service failures.
What To Do
Affected operators and maintenance personnel should conduct thorough inspections of the elevator torque tube on Textron Aviation 172, 175, 180, 182, 185, 188, and 208 aeroplanes for any signs of cracks or corrosion. They must follow the inspection procedures outlined in the bulletin and address any findings promptly. No specific compliance deadlines are stated in the document.