Summary
The FAA is superseding an existing airworthiness directive (AD) for Turbomeca Arrius 2F turboshaft engines. That AD currently requires removing from service certain serial number (SN) fuel control units (FCUs) or replacing the constant delta pressure (delta P) diaphragm in those FCUs. This AD requires replacing all FCUs not incorporating modification Tf 55 with FCUs that incorporate modification Tf 55. This AD results from the European Aviation Safety Agency (EASA) and Turbomeca expanding the applicability to the full population of FCUs installed on Arrius 2F turboshaft engines. FCUs not incorporating modification Tf 55 are susceptible to having an improperly assembled constant delta P diaphragm. We are issuing this AD to prevent an uncommanded engine in-flight shutdown on a single-engine helicopter, resulting in a forced autorotation landing or an accident.
Directive Details
AD Number
FAA-2005-22430
Document Number
E7-9721
Type
Rule
Publication Date
May 22, 2007
Effective Date
June 26, 2007
Affected Manufacturer
Turbomeca Arrius 2F Turboshaft
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2005-22430
Topics
Official Documents
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