AD 2011-10-12

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model AS350B, B1, B2, B3, BA, and EC130 B4 Helicopters

AD Number
2011-10-12
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2010-1228
FR Citation
76 FR 28637

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; Eurocopter France Model AS350B, B1, B2, B3, BA, and EC130 B4 Helicopters

Unsafe Condition

Failure of the 41-tooth pinion in the engine accessory gearbox, caused by an inoperative torque damping system of the starter-generator due to incorrect adjustment, leading to bending stresses on the pinion. This failure causes the engine fuel pump to stop operating, resulting in an engine flameout.

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

Required Actions

Replace the cup springs and fan nut, functionally test the damping system, and mark '004' on the identification plate of the APC starter-generator. Comply with the requirements of this AD before installing an APC starter-generator with part numbers 150SG122Q or 200SGL130Q.

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

Compliance Time

Within 110 hours time-in-service (TIS) or 3 months, whichever occurs first.

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

Affected Aircraft

Eurocopter France Model AS350B, B1, B2, B3, BA, and EC130 B4 helicopters with ARRIEL engines and Aircraft Parts Corporation (APC) starter-generators, part numbers 150SG122Q or 200SGL130Q, without '004' marked on the identification plate.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.