96-12-03 R1
FR doc 97-25831 · 62 FR 51019AD 96-12-03 R1Published 1997-09-30Effective 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 document corrects the airworthiness directive (AD) number of an amendment that was published in the Federal Register on August 22, 1997 (62 FR 44535), and concerns Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B airplanes. The referenced amendment revises AD 96-12-03, but was inadvertently assigned the number of AD 97-17-07 instead of AD 96-12-03 R1. The 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 the aft lower fuselage wing attach fitting on both wings eliminates the repetitive inspection requirement of the AD. This action corrects the amendment to reflect the right AD number throughout the entire document.
More directives for Aviat/Pitts Special
- AD 96-12-03 R2 Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S... 1998-10-01
- AD 97-26-20 Airworthiness Directives; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2... 1997-12-30
- AD 97-17-07 Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S... 1997-08-22
- AD 96-09-08 R1 Airworthiness Directives; Aviat Aircraft Inc. Models S-2A, S-2B, and S-2... 1996-07-09
- AD 96-12-03 Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S... 1996-06-06
This is a correction notice. The AD it corrects is not in our index yet, so we are showing the correction alone rather than implying we hold the directive itself.
