# Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes (Formerly Known as Pitts Models S- 1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes); Correction
> **Rule** · Final rule; correction. · Published 1997-09-30 · Effective 1997-10-03 · 62 FR 51019
## Document
- **Document number:** 97-25831
- **Category:** airworthiness
- **Manufacturer:** Aviat
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 62 FR 51019
- **Publication date:** 1997-09-30
- **Effective date:** 1997-10-03
- **FAA docket:** Docket No. 96-CE-23-AD
## 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.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1997/09/30/97-25831/airworthiness-directives-aviat-aircraft-inc-models-s-1s-s-1t-s-2-s-2a-s-2s-and-s-2b-airplanes)
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