# Airworthiness Directives; Boeing Model 757 Series Airplanes Equipped With Pratt & Whitney Engines
> **Rule** · Final rule; request for comments. · Published 1997-09-02 · Effective 1997-09-17 · 62 FR 46186
## Document
- **Document number:** 97-23176
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 757 Series
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 62 FR 46186
- **Publication date:** 1997-09-02
- **Effective date:** 1997-09-17
- **FAA docket:** Docket No. 97-NM-130-AD
## Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Boeing Model 757 series airplanes, that currently requires repetitive inspections to detect cracking in the midspar fuse pins; replacement with new or refinished fuse pins, if necessary; and repetitive inspections of newly installed fuse pins. This AD requires earlier initial inspections and replacements; more frequent repetitive inspections of certain fuse pins; and replacement with new fuse pins, if necessary. This amendment is prompted by reports of fatigue cracking of the midspar fuse pins and by fatigue test data indicating that current inspection thresholds and intervals for repetitive inspections are inadequate to detect fatigue cracking in a timely manner. The actions specified in this AD are intended to detect and correct such fatigue cracking, which could lead to separation of the strut and engine from the wing of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1997/09/02/97-23176/airworthiness-directives-boeing-model-757-series-airplanes-equipped-with-pratt-and-whitney-engines)
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