AD 2005-17-15

final rule
Data completeness: 70%

Airworthiness Directives; Turbomeca Arrius 2F Turboshaft Engines

AD Number
2005-17-15
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2005-21924
FR Citation
70 FR 50168

Applicability

TypeManufacturerModelDetails
engine Turbomeca Arrius 2F Airworthiness Directives; Turbomeca Arrius 2F Turboshaft Engines

Unsafe Condition

Incorrect positioning of the FCU filter that could limit the fuel flow downstream of the filter.

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

Required Actions

Remove and inspect the fuel filter-holder assembly to determine that the FCU filter is dimensionally correct. Update the Engine Maintenance Manuals to include a dimensional check of the fuel filter-holder assembly every time the FCU filter element is removed.

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

Compliance Time

Within the compliance times specified in the AD 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 S.A. Arrius 2F turboshaft engines installed on, but not limited to, Eurocopter EC120 helicopters.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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