AD 2014-12-05

final rule
Data completeness: 70%

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

AD Number
2014-12-05
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2006-23809
FR Citation
79 FR 36634

Applicability

TypeManufacturerModelDetails
engine Turbomeca S Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

Unsafe Condition

failure of the HMU drive gear shaft, which could lead to damage to the engine and damage to the aircraft.

Required Actions

inspect the high-pressure (HP) pump drive gear shaft splines and coupling shaft assembly splines. Use paragraph 2.B.(1)(b) of Turbomeca S.A. Mandatory Service Bulletin (MSB) No. 292 73 2812, Version G, dated June 24, 2013, to do your inspection.

Compliance Time

within 25 HMU operating hours from the effective date of this AD, for Arriel 2B and 2B1 engines with 500 or more operating hours since new or since last overhaul.

Affected Aircraft

all Turbomeca S.A. Arriel 2B, 2B1, 2C, 2C1, 2C2, 2S1, and 2S2 turboshaft engines.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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