Airworthiness Directive

AD 96-12-03 61 FR 28730

Federal Aviation Administration · 14 CFR part 39

FR document
96-14051
Amendment
39-9645
Published
1996-06-06
Models covered
1
Last live check
2026-08-17
AD

96-12-03

FR doc 96-14051 · 61 FR 28730

AD 96-12-03Published 1996-06-06Effective 1996-06-24

Requires repetitively inspecting the aft lower fuselage wing attach fitting on both wings for cracks and modifying any cracked aft lower fuselage wing attach fitting.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Aviat Aircraft, Inc. (Aviat) Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B airplanes that are equipped with aft lower fuselage wing attach fittings incorporating either part number (P/N) 76090, 2-2107-1, or 1-210-102. This action requires repetitively inspecting the aft lower fuselage wing attach fitting on both wings for cracks and modifying any cracked aft lower fuselage wing attach fitting. Modifying the aft lower fuselage wing attach fitting on both wings eliminates the repetitive inspection requirement of the AD. Several reports of cracked fuselage wing attach fittings on the affected airplanes prompted this action. The actions specified by this AD are intended to prevent possible in-flight separation of the wing from the airplane caused by a cracked fuselage wing attach fitting.

Applies to 1 model in our index