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AD/TBM 700/38	Flap Carriage Roller Pins	3/2005

Applicability:	All Model TBM 700 aircraft that have accumulated more than 2,500 landings.
Requirement:	Action in accordance with EADS Socata TBM 700 Service Bulletin No. SB 70-122, dated November 2004, or later EASA approved revision.Note: DGAC AD F-2005-017 refers.
Compliance:	At the next scheduled 100 hour inspection after 17 March 2005. Repeat thereafter at each 100 hour inspection.
	This Airworthiness Directive becomes effective on 17 March 2005.
Background:	Reports were received of two fatigue failures of flap carriage roller pins on in-service aircraft.

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David Punshon
Delegate of the Civil Aviation Safety Authority

4 February 2005

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