Airworthiness Directive

AD 97-17-07 62 FR 44535

Federal Aviation Administration · 14 CFR part 39

FR document
97-22046
Amendment
39-10109
Published
1997-08-22
Models covered
1
Last live check
2026-08-17
AD

97-17-07

FR doc 97-22046 · 62 FR 44535

AD 97-17-07Published 1997-08-22Effective 1997-10-03

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 revises AD 96-12-03, which applies to Aviat Aircraft, Inc. (Aviat) Models S-1S, S-1T, S-2, 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. That AD currently 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 both aft lower fuselage wing attach fittings eliminates the repetitive inspection requirement of AD 96-12-03. Aviat recently started incorporating modified aft lower fuselage wing attach fittings on newly manufactured airplanes. This AD retains the requirements of AD 96-12- 03, but exempts airplanes that had the modified aft lower fuselage wing attach fittings incorporated at manufacture. 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