AD 2012-07-09

final rule
Data completeness: 70%

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

AD Number
2012-07-09
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2009-0330
FR Citation
77 FR 23380

Applicability

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

Unsafe Condition

The P3 air pipe (first section) and the RH rear half-wall could rub each other. Rubbing between the pipe and the RH rear half-wall may lead to rupture of the P3 air pipe (first section), which could cause an uncommanded power loss to flight idle.

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

Required Actions

Inspect the clearance between the P3 air pipe (first section) and the RH rear half-wall for sufficient clearance (0.5 mm or more). Replace damaged parts before further flight. Replace the RH rear half-wall if contact is found but no damage. Repeat inspections as specified for certain engine installations or re-installations. Installation of RH rear half-wall, P/N 0 319 99 008 0, is terminating action.

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

Compliance Time

Within 100 engine hours after the effective date of this AD.

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

Affected Aircraft

Turbomeca S.A. Arrius 2F turboshaft engines with right-hand (RH) rear half-wall, part number (P/N) 0319 99 824 0, installed.

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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