EASA Regulations for Cessna U206F

2 airworthiness directives and regulations affecting Cessna U206F.

EASA SIB 2013-17

Cessna U206F Aeroplanes — Elevator Trim Tab Actuator Corrosion

EASA Safety Information Bulletin SIB No: 2013-17 addresses corrosion concerns in the elevator trim tab actuator of Cessna U206F aeroplanes. The bulletin references Transport Canada Civil Aviation Safety Alert CASA 2011-06 and Cessna Single-Engine Service Letter SE73-25, highlighting a safety issue involving the failure of the threaded rod end of the elevator trim tab actuator leading to elevator jamming and tailplane damage. This information bulletin is intended to inform owners, operators, and maintainers of affected aircraft registered in EASA Member States.

Oct 14, 2013

Safety Information BulletinMaintenanceSafety MgmtCessna U206F

EASA SIB CE-09-39

Cessna (T)U206 aeroplanes with Wing Tip Tanks - STC SA4366WE

The Special Airworthiness Information Bulletin FAA Aircraft Certification Service SAIB CE-09-39 addresses the maximum landing gross weight limitation for Cessna U206F, U206G, TU206F, and TU206G series airplanes equipped with Flint Aero wing tip tanks installed under Supplemental Type Certificate SA4366WE. It clarifies the maximum landing weight as documented in Flint Aero Airplane Flight Manual Supplement Revision B. This bulletin provides safety information but does not mandate regulatory action.

Jul 31, 2009

Safety Information BulletinSafety MgmtCessna U206FCessna U206GCessna TU206FCessna TU206G