Airworthiness Directives; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2S Airplanes (Formerly Pitts Models S-2A, S-2B, and S-2S Airplanes)
airworthiness · Rule · Final rule; request for comments. · Published 1996-05-02 · Effective 1996-05-20 · 61 FR 19540
Document
Document number
96-10477
Federal Register citation
61 FR 19540
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Aviat
Publication date
1996-05-02
Effective date
1996-05-20
FAA docket
Docket No. 95-CE-101-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to Aviat Aircraft Inc., Models S-2A, S-2B, and S-2S airplanes (formerly Pitts Models S-2A, S-2B, and S-2S airplanes). This action requires inspecting the longerons aft of the rear cabane struts for cracks, and if cracked, prior to further flight, repairing the cracks. Reports of longeron failure caused by fatigue aft of the rear cabane struts prompted this action. The actions specified by this AD are intended to prevent cracking and subsequent failure of the longerons resulting in possible loss of control of the airplane.