AD 2002-22-16

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model AS355N Helicopters

AD Number
2002-22-16
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2002-SW-32-AD
FR Citation
67 FR 68506

Applicability

TypeManufacturerModelDetails
aircraft Eurocopter France Model AS355N Airworthiness Directives; Eurocopter France Model AS355N Helicopters

Unsafe Condition

Excessive starter-generator (S-G) vibration could lead to separation of an engine exhaust pipe ejector, impact with the main or tail rotor, and subsequent loss of control of the helicopter.

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

Required Actions

Visually inspect the four engine exhaust pipe ejector attachment lugs, starter-generator attachment flange, and attachment half-clamps for cracks. Measure each starter-generator engine clamp torque and vibration level. Record the starter-generator vibration level on a component history card or equivalent record. If the starter-generator vibration level is equal to or higher than 0.5 inches per second (IPS), repair or replace the starter-generator as necessary.

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

Compliance Time

Before further flight

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

Affected Aircraft

Eurocopter France Model AS355N 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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