FAA has issued AD 2011-17-09 applicable to TBM 700/850-001 thru 572, 574, 576. This AD requires that within 12 months or 100 hours (whichever comes first) of 15 Feb 2012 inspection of the aileron control cables in the wings per Socata Mandatory SB 70-191-27.

  EASA has issued EAD 2011-0235-E applicable to all serial number TBMs. This AD requires operators to a verify their the nose landing gear serial number within 5 flight cycles. If your gear is affected by this AD, it must be checked before each flight in accordance with SB 70-194-32. The affected gears also require maintenance action within 10 months of 13 December 2011.

  FAA has issued a letter recognizing SB70-190-27 amendment 1 as Alternative Method of Compliance (AMOC) for Airworthiness Directive (AD 2011-17-06) elevator trim tab actuators, for SOCATA TBM 700/850 SN 001-530

  FAA has issued AD 2011-17-06 applicable to all TBM 700/850-001 thru 530. This AD requires that within 12 months of 19 Sept 2011 elevator trim tab actuators be inspected in accordance with Socata Mandatory SB 70-190-27.

  EASA has issued AD 2011-0130 applicable to TBM 148, 434 to 572, 574 & 576. This AD requires within 6 months of 22 July 2011 that a protection fuse on the wire at the standby compass connector be installed in accordance with Socata SB 70-192-34.