# Proposed AD FAA-2009-0883: Pratt & Whitney JT8D-209, -217, -217C, and -219 Turbofan Engines

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 97-17-04 R1
- Products: Pratt & Whitney
- Product type: Engine
- Action: Notice of proposed rulemaking (NPRM).
- Published: December 21, 2009, 74 FR 67831
- Comments due: February 19, 2010
- Became: [AD 97-17-04 R1](https://openairdocs.org/ad/97-17-04-R1)
- Docket: FAA-2009-0883 (https://www.regulations.gov/docket/FAA-2009-0883, where comments are filed)
- Project: 97-ANE-08
- FR document: E9-30221
- Official PDF: https://openairdocs.org/files/sha256/5e/54/5e5471d25ac915d80ecb1888676a2549f262a7edd9722e8d867d470173e39ca7 (from https://www.govinfo.gov/content/pkg/FR-2009-12-21/pdf/E9-30221.pdf)
- Federal Register: https://www.federalregister.gov/documents/2009/12/21/E9-30221/airworthiness-directives-pratt-and-whitney-jt8d-209--217--217c-and--219-turbofan-engines
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AF283B291922E65B86257693005656EF.0001
- Page: https://openairdocs.org/proposed/FAA-2009-0883

## Summary

The FAA proposes to revise an existing airworthiness directive (AD) for Pratt & Whitney JT8D-209, -217, -217C, and -219 turbofan engines with front compressor front hub (fan hub), part number (P/N) 5000501-01 installed. That AD currently requires cleaning the front compressor front hubs (fan hubs), initial and repetitive eddy current (ECI) and fluorescent penetrant inspections (FPI) of tierod and counterweight holes for cracks, removal of bushings, cleaning and ECI and FPI of bushed holes for cracks and, if necessary, replacement with serviceable parts. In addition, that AD currently requires reporting the findings of cracked fan hubs and monthly reports of the number of inspections completed. This proposed AD would require the same actions, except for the monthly reporting of the number of completed inspections. This proposed AD results from the FAA determining that it has collected a sufficient amount of data since issuing AD 97-17-04 and that therefore, it no longer needs the monthly reporting of the number of completed inspections. We are proposing this AD revision to prevent fan hub failure due to tierod, counterweight, or bushed hole cracking, which could result in an uncontained engine failure and damage to the airplane.

## Notices in this docket

- Dec 21, 2009: Notice of proposed rulemaking (NPRM). (first notice), FR document E9-30221, comments due Feb 19, 2010 (https://www.federalregister.gov/documents/2009/12/21/E9-30221/airworthiness-directives-pratt-and-whitney-jt8d-209--217--217c-and--219-turbofan-engines)

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