# Proposed AD 2002-NE-39-AD: Turbomeca S.A. Arrius-2F Turboshaft Engines

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2003-11-10
- Products: Turbomeca
- Product type: Engine
- Action: Notice of proposed rulemaking (NPRM).
- Published: February 5, 2003, 68 FR 5856
- Comments due: April 7, 2003
- Became: [AD 2003-11-10](https://openairdocs.org/ad/2003-11-10)
- Docket: 2002-NE-39-AD
- FR document: 03-2633
- Official PDF: https://openairdocs.org/files/sha256/2b/f3/2bf36ab51b64d53e9667f27fccb8dc8bbaf80743805f48f25093735d489f75cd (from https://www.govinfo.gov/content/pkg/FR-2003-02-05/pdf/03-2633.pdf)
- Federal Register: https://www.federalregister.gov/documents/2003/02/05/03-2633/airworthiness-directives-turbomeca-sa-arrius-2f-turboshaft-engines
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AF239848A4536E2686256CC4005EAA1B.0001
- Page: https://openairdocs.org/proposed/2002-NE-39-AD

## Summary

The Federal Aviation Administration (FAA) proposes to adopt a new airworthiness directive (AD) that is applicable to Turbomeca S.A. Arrius-2F turboshaft engines with certain serial number (SN) Fuel Control Units (FCU's). This proposal would require adjusting the FCU maximum fuel flow mechanical stop position to a higher fuel flow setting. This proposal is prompted by an FCU discovered to have a maximum fuel flow limit adjusted below the maximum required setting. The actions specified by the proposed AD are intended to prevent reduced maximum available power during takeoff, landing, or an emergency, which could significantly affect helicopter performance and result in loss of the helicopter.

## Notices in this docket

- Feb 5, 2003: Notice of proposed rulemaking (NPRM). (first notice), FR document 03-2633, comments due Apr 7, 2003 (https://www.federalregister.gov/documents/2003/02/05/03-2633/airworthiness-directives-turbomeca-sa-arrius-2f-turboshaft-engines)

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