# Proposed AD 2001-NE-16-AD: Pratt & Whitney JT9D-7R4 Series Turbofan Engines

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2002-07-04
- Products: Pratt & Whitney
- Product type: Engine
- Action: Notice of proposed rulemaking (NPRM).
- Published: August 30, 2001, 66 FR 45789
- Comments due: October 29, 2001
- Became: [AD 2002-07-04](https://openairdocs.org/ad/2002-07-04)
- Docket: 2001-NE-16-AD
- FR document: 01-21895
- Official PDF: https://openairdocs.org/files/sha256/09/77/097739910582390630e25866151c2b36d956d73fa6e0098860aa348735fb05a0 (from https://www.govinfo.gov/content/pkg/FR-2001-08-30/pdf/01-21895.pdf)
- Federal Register: https://www.federalregister.gov/documents/2001/08/30/01-21895/airworthiness-directives-pratt-and-whitney-jt9d-7r4-series-turbofan-engines
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6A86DD5C4AD5C87186256AB8005D11DE.0001
- Page: https://openairdocs.org/proposed/2001-NE-16-AD

## Summary

The Federal Aviation Administration (FAA) proposes to adopt a new airworthiness directive (AD) that is applicable to Pratt & Whitney (PW) JT9D-7R4 series turbofan engines. This proposal would require a one-time inspection of low pressure turbine (LPT) 5th stage disks for evidence of blend repairs and mechanical damage, and replacement based on the extent of those repairs and damage. This proposal is prompted by a report of a PW JT9D-7R4G2 turbofan engine that experienced an uncontained failure of the LPT 5th stage disk. The actions specified by the proposed AD are intended to prevent uncontained failure of the LPT 5th stage disk, due to incomplete blend repairs, resulting in in-flight shutdown and damage to the airplane.

## Notices in this docket

- Aug 30, 2001: Notice of proposed rulemaking (NPRM). (first notice), FR document 01-21895, comments due Oct 29, 2001 (https://www.federalregister.gov/documents/2001/08/30/01-21895/airworthiness-directives-pratt-and-whitney-jt9d-7r4-series-turbofan-engines)

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