# Proposed AD 2004-NE-10-AD: Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) (RRC) 250-B and 250-C Series Turboshaft and Turboprop Engines

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2004-24-09
- Products: Rolls-Royce
- Product type: Engine
- Action: Notice of proposed rulemaking (NPRM).
- Published: October 18, 2005, 70 FR 60453
- Comments due: December 19, 2005
- Became: [AD 2004-24-09](https://openairdocs.org/ad/2004-24-09)
- Docket: 2004-NE-10-AD
- FR document: 05-20779
- Official PDF: https://openairdocs.org/files/sha256/9b/71/9b715874df045c5f21a113178ce71fc5823ebe933415ae09125f190b8b8959ed (from https://www.govinfo.gov/content/pkg/FR-2005-10-18/pdf/05-20779.pdf)
- Federal Register: https://www.federalregister.gov/documents/2005/10/18/05-20779/airworthiness-directives-rolls-royce-corporation-formerly-allison-engine-company-allison-gas-turbine
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9C3704F1974BF91C8625709E0058524E.0001
- Page: https://openairdocs.org/proposed/2004-NE-10-AD

## Summary

The FAA proposes to supersede an existing airworthiness directive (AD) for certain RRC 250-B and 250-C series turboshaft and turboprop engines. That AD currently requires a onetime inspection of the fuel nozzle screen for contamination, and if contamination is found, inspection and cleaning of the entire aircraft fuel system before further flight. That AD also requires replacing the fuel nozzle with a new design fuel nozzle, at the next fuel nozzle overhaul or by June 30, 2006, whichever occurs first. This proposed AD would require the same actions, but would add additional part numbers (P/Ns) to the list of affected fuel nozzles. This proposed AD would also explain that the existing AD, as worded, allows certain part number (P/N) fuel nozzles back into service. Those fuel nozzles must not be allowed back into service. This proposed AD results from the discovery that several P/Ns of fuel nozzles were inadvertently left out of AD 2004-24-09. We are proposing this AD to minimizethe risk of sudden loss of engine power and uncommanded shutdown of the engine due to fuel contamination and collapse of the screen in the fuel nozzle.

## Notices in this docket

- May 7, 2004: Notice of proposed rulemaking (NPRM). (first notice), FR document 04-10385, comments due Jul 6, 2004 (https://www.federalregister.gov/documents/2004/05/07/04-10385/airworthiness-directives-rolls-royce-corporation-formerly-allison-engine-company-allison-gas-turbine)
- Oct 18, 2005: Notice of proposed rulemaking (NPRM)., FR document 05-20779, comments due Dec 19, 2005 (https://www.federalregister.gov/documents/2005/10/18/05-20779/airworthiness-directives-rolls-royce-corporation-formerly-allison-engine-company-allison-gas-turbine)

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