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Airworthiness Directives; SOCATAGroupe Aerospatiale Model TBM 700 Airplanes

airworthiness · Rule · Final rule. · Published 1998-11-24 · Effective 1998-12-28 · 63 FR 64844

Document

Document number
98-31010
Federal Register citation
63 FR 64844
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
SOCATAGroupe Aerospatiale Model TBM 700
Publication date
1998-11-24
Effective date
1998-12-28
FAA docket
Docket No. 95-CE-65-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain SOCATA--Groupe AEROSPATIALE (SOCATA) Model TBM 700 airplanes. This AD requires repetitively inspecting (using visual methods) the web of the left and right flap carriage for cracks, and replacing any cracked flap carriage with one of improved design. The proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by this AD are intended to detect and correct cracks in a flap carriage, which could result in loss of the flap function with consequent reduced and/or loss of airplane control.

Source

Authoritative
Federal Register document
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