# Airworthiness Directives; Pratt & Whitney JT8D Series Turbofan Engines
> **Rule** · Final rule. · Published 1998-06-09 · Effective 1998-08-10 · 63 FR 31340
## Document
- **Document number:** 98-15086
- **Category:** airworthiness
- **Manufacturer:** Pratt & Whitney JT8D Series Turbofan
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 63 FR 31340
- **Publication date:** 1998-06-09
- **Effective date:** 1998-08-10
- **FAA docket:** Docket No. 97-ANE-05
## Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to Pratt & Whitney JT8D series engines, that currently requires a determination of the utilization rate and coating type of the 7th, 8th, 9th, 10th, 11th, and 12th stage high pressure compressor (HPC) disks, and removal, inspection for corrosion, and recoating of those HPC disks based on utilization rate. This amendment shortens the inspection interval for certain low utilization disks. This amendment is prompted by reports of an additional uncontained 9th stage HPC disk failure due to corrosion pitting. The actions specified by this AD are intended to prevent fracture of the HPC disks, which can result in uncontained release of engine fragments, inflight engine shutdown, and airframe damage.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/06/09/98-15086/airworthiness-directives-pratt-and-whitney-jt8d-series-turbofan-engines)
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