# Airworthiness Directives; Pratt & Whitney JT9D Series Turbofan Engines
> **Rule** · Final rule. · Published 1999-07-16 · Effective 1999-08-16 · 64 FR 38299
## Document
- **Document number:** 99-17555
- **Category:** airworthiness
- **Manufacturer:** Pratt & Whitney JT9D Series Turbofan
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 64 FR 38299
- **Publication date:** 1999-07-16
- **Effective date:** 1999-08-16
- **FAA docket:** Docket No. 98-ANE-31-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Pratt & Whitney (PW) JT9D series turbofan engines, that requires initial and repetitive in-shop eddy current and on-wing ultrasonic inspections of the Combustion Chamber Outer Casing (CCOC) forward flange (L-flange) fillet radius for cracking, and replacing cracked L-flanges with serviceable parts. Replacement with an improved L-flange constitutes terminating action to the repetitive inspections. This amendment is prompted by reports of CCOC rupture due to cracking in the L-flange fillet radius. The actions specified by the proposed AD are intended to prevent CCOC rupture due to cracking, which could result in an uncontained engine failure and damage to the aircraft.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1999/07/16/99-17555/airworthiness-directives-pratt-and-whitney-jt9d-series-turbofan-engines)
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