AD 2010-16-51

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model SA330J Helicopters

AD Number
2010-16-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2010-0825
FR Citation
75 FR 53857

Applicability

TypeManufacturerModelDetails
aircraft Eurocopter France Model SA330J Airworthiness Directives; Eurocopter France Model SA330J Helicopters

Unsafe Condition

Internal degradation of the bearings of the fan rotor shaft can cause interference between the fan rotor blade and the upper area of the guide vane bearing housing, leading to fan rotor blade separation and puncture holes in the transmission deck.

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

Required Actions

Within 10 hours time-in-service (TIS), inspect for a gap between the main gearbox (MGB) oil cooling fan assembly rotor blade and the upper section of the guide vane bearing housing using a 0.2 mm feeler gauge attached to a rigid rod. If the feeler gauge cannot be inserted, replace the two fan rotor shaft bearings with airworthy bearings. After replacement, reinspect to ensure sufficient clearance.

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

Compliance Time

Within 10 hours time-in-service (TIS)

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

Affected Aircraft

Eurocopter France Model SA330J 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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