# Airworthiness Directives; Pilatus Britten-Norman Ltd. BN-2A and BN-2A Mk 111 Series Airplanes; Correction
> **Rule** · Final rule; correction. · Published 1997-07-11 · Effective 1997-08-18 · 62 FR 37130
## Document
- **Document number:** 97-18139
- **Category:** airworthiness
- **Manufacturer:** Pilatus Britten-Norman Ltd. BN-2A and BN-2A Mk 111 Series
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 62 FR 37130
- **Publication date:** 1997-07-11
- **Effective date:** 1997-08-18
- **FAA docket:** Docket No. 96-CE-24-AD
## Abstract

This document makes a correction to Airworthiness Directive (AD) 97-14-01, which was published in the Federal Register on July 2, 1997 (62 FR 35670), and is applicable to Pilatus Britten-Norman Ltd. (PBN) BN-2A and BN-2A Mk 111 series airplanes. This AD currently has an issue date and effective date of August 18, 1997. The AD currently requires inspecting the LH rudder bar assembly for wall thickness of the slider tube unit and modifying the rudder bar assembly by replacing the LH slider tube with a new strengthened slider tube unit. This action changes the issue date of this AD to June 24, 1997 and leaves the effective date at August 18, 1997.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1997/07/11/97-18139/airworthiness-directives-pilatus-britten-norman-ltd-bn-2a-and-bn-2a-mk-111-series-airplanes)
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