# Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) AE 3007 Series Turbofan Engines
> **Rule** · Final rule. · Published 2001-12-19 · Effective 2002-01-23 · 66 FR 65427
## Document
- **Document number:** 01-30952
- **Category:** airworthiness
- **Manufacturer:** Rolls-Royce Corporation (Formerly Allison
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 66 FR 65427
- **Publication date:** 2001-12-19
- **Effective date:** 2002-01-23
- **FAA docket:** Docket No. 99-NE-46-AD
## Abstract

This amendment supersedes an existing airworthiness directive (AD), that is applicable to Rolls-Royce Corporation (formerly Allison Engine Company) AE 3007 series turbofan engines. That AD currently requires removal of certain compressor cone shafts from service before exceeding new cyclic life limits and replacement with serviceable parts. This amendment requires increasing the cyclic life limit for certain serial numbers of new compressor cone shafts, part number (P/N) 23070729, that are used on AE3007A1/3 and AE3007A1P engines. This amendment is prompted by recent approved changes in engineering and manufacturing processes for new compressor cone shafts P/N 23070729. The actions specified by this AD are intended to prevent low-cycle fatigue (LCF) failure of cone shafts, which could result in an uncontained engine failure and damage to the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2001/12/19/01-30952/airworthiness-directives-rolls-royce-corporation-formerly-allison-engine-company-ae-3007-series)
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