EASA Regulations for EADS SOCATA TBM 850

2 airworthiness directives and regulations affecting EADS SOCATA TBM 850.

EASA SIB 2007-27

WITHDRAWN: REPLACED BY EASA AD 2009-0214

EASA Safety Information Notice No. 2007-27 N is a safety communication regarding EADS SOCATA TBM 700 aircraft main landing gear wheel axles. It addresses a safety issue involving partially unscrewed wheel attaching nuts on TBM 850 aircraft, caused by machining defects in certain wheel axle production batches. This notice informs operators about the DGAC France Emergency Airworthiness Directive UF-2007-015 related to this issue.

Sep 20, 2007

Safety Information BulletinMaintenanceSafety MgmtEADS SOCATA TBM 700EADS SOCATA TBM 850

EASA SIB 2007-19

EADS SOCATA TBM 700 C and TBM 850 aeroplanes Main Landing Gear - Wheel Axle - Inspection/Modification DGAC France Emergency AD (CN) No. UF-2007-007

EASA Safety Information Notice No. 2007-19 is an advisory document regarding the DGAC France Emergency Airworthiness Directive No. UF-2007-007. It concerns EADS SOCATA TBM 700 C and TBM 850 aeroplanes up to serial number 408 with specific main landing gear wheel axle batch numbers CZ52790, CZ62189, CZ64034, or CZ66207. The notice addresses inspection and modification requirements for the main landing gear wheel axle to ensure continued airworthiness and safety.

Aug 2, 2007

Airworthiness DirectiveMaintenanceSafety MgmtEADS SOCATA TBM 700 CEADS SOCATA TBM 850