# Airworthiness Directives; The New Piper Aircraft, Inc. PA24, PA28R, PA30, PA32R, PA34, and PA39 Series Airplanes; Correction
> **Rule** · Final rule; correction. · Published 1997-04-01 · Effective 1997-02-07 · 62 FR 15373
## Document
- **Document number:** 97-8250
- **Category:** airworthiness
- **Manufacturer:** The New Piper
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 62 FR 15373
- **Publication date:** 1997-04-01
- **Effective date:** 1997-02-07
- **FAA docket:** Docket No. 96-CE-09-AD
## Abstract

This document makes a correction to Airworthiness Directive (AD) 97-01-01, which was published in the Federal Register on January 2, 1997 (62 FR 10), and concerns The New Piper Aircraft, Inc. (Piper) PA24, PA28R, PA30, PA32R, PA34, and PA39 series airplanes. The amendment number in this AD is incorrectly referenced as Amendment 39- 9782 instead of 39-9872 in two places. All other reference is correct. The AD currently requires repetitively inspecting the main gear sidebrace studs for cracks, and replacing any main gear sidebrace stud found cracked. This action corrects the AD to reflect the right amendment number throughout the entire document.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1997/04/01/97-8250/airworthiness-directives-the-new-piper-aircraft-inc-pa24-pa28r-pa30-pa32r-pa34-and-pa39-series)
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