Airworthiness Directives; Twin Commander Aircraft Corporation 500, 600, and 700 Series Airplanes
airworthiness · Rule · Final rule. · Published 1998-04-17 · Effective 1998-05-18 · 63 FR 19170
Document
Document number
98-9874
Federal Register citation
63 FR 19170
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Twin Commander
Publication date
1998-04-17
Effective date
1998-05-18
FAA docket
Docket No. 95-CE-92-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that applies to all Twin Commander Aircraft Corporation (Twin Commander) 500, 600, and 700 series airplanes. This AD requires installing access holes in both wing leading edges and repetitively inspecting the forward attach brackets and straps for cracks. Reports of cracks in the wing to fuselage attachment brackets and straps, wing station (WS) 24, and fuselage frames prompted this action. The actions specified by this AD are intended to detect cracks at the wing to fuselage attach points, which, if not detected and corrected, could cause structural failure and loss of control of the airplane.