AD 2016-06-09

final rule
Data completeness: 70%

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

AD Number
2016-06-09
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2016-2701
FR Citation
81 FR 15154

Applicability

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

Unsafe Condition

Loosening of the nut attaching the swivel union to the engine power turbine module M04, leading to oil leakage from the low-pressure oil system and potential in-flight shutdown.

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

Required Actions

Tighten the nut, part number 9560130990, attaching the swivel union to the engine power turbine module M04 to 15 Newton-meters torque. Use a backup wrench to prevent the swivel union from rotating.

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

Compliance Time

Within 30 engine hours or 7 days after the effective date of this AD, whichever occurs first.

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

Affected Aircraft

All Turbomeca S.A. Makila 2A and 2A1 turboshaft engines that have incorporated Turbomeca S.A. Service Bulletin No. 298 79 2831, Version B, dated November 13, 2015, or earlier.

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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