AD 2005-13-25

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Turbomeca S.A. Arriel 2B Turboshaft Engines

AD Number
2005-13-25
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2005-21624
FR Citation
70 FR 36480

Applicability

TypeManufacturerModelDetails
engine Turbomeca S Airworthiness Directives; Turbomeca S.A. Arriel 2B Turboshaft Engines

Unsafe Condition

Hydromechanical unit (HMU) acceleration controller axle sticking, leading to loss of control of engine fuel flow in manual or mixed control mode, resulting in engine overspeed and in-flight engine shutdown, or uncommanded in-flight engine shutdown.

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

Required Actions

Inspect, clean, lubricate, and check for proper operation of the HMU acceleration controller axle using Turbomeca Alert Mandatory Service Bulletin No. A292 73 2814, Update No. 1, dated January 11, 2005. Initial inspection must be completed within 20 operating hours after the effective date, followed by repetitive inspections as specified.

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

Compliance Time

Within 20 operating hours after the effective date

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

Affected Aircraft

Turbomeca S.A. Arriel 2B turboshaft engines with Modification TU62A incorporated, installed on, but not limited to, Eurocopter AS350B3 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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