AD 2007-11-06

final rule
Data completeness: 80%

Airworthiness Directives; Turbomeca Arrius 2F Turboshaft Engines

AD Number
2007-11-06
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2005-22430
FR Citation
72 FR 28589

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; Turbomeca Arrius 2F Turboshaft Engines
engine Turbomeca Arrius 2F Airworthiness Directives; Turbomeca Arrius 2F Turboshaft Engines

Unsafe Condition

FCUs not incorporating modification Tf 55 are susceptible to having an improperly assembled constant delta pressure (delta P) diaphragm, which could lead to an uncommanded engine in-flight shutdown on a single-engine helicopter.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Replace all FCUs not incorporating modification Tf 55 with FCUs that incorporate modification Tf 55.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

No later than July 31, 2007, unless the actions have already been done.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Turbomeca Arrius 2F turboshaft engines with fuel control units (FCUs) not incorporating modification Tf 55, installed on, but not limited to, Eurocopter EC120B helicopters.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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