AD 2006-10-19

final rule
Data completeness: 90%

Airworthiness Directives; Eurocopter France Model EC130 B4 Helicopters

AD Number
2006-10-19
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2006-24807
FR Citation
71 FR 33598

Applicability

TypeManufacturerModelDetails
aircraft Eurocopter France Model EC130 B4 Airworthiness Directives; Eurocopter France Model EC130 B4 Helicopters

Unsafe Condition

Jamming of the throttle twist grip assembly in the 'IDLE' position, which could keep the engine from operating above idle speed and result in loss of control of engine power.

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

Required Actions

Inspect the throttle twist grip assembly for foreign bodies (chips or debris), any rotating micro-switch, and any micro-switch roller that does not move freely. Correct any unairworthy condition found before further flight.

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

Compliance Time

Within 30 hours time-in-service (TIS), unless accomplished during the previous 100-hour TIS or annual inspection.

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

Affected Aircraft

Eurocopter France Model EC130 B4 helicopters with twist grip assembly part numbers 350A27-5209-00, 350A27-5209-01, or 350A27-5209-02, before embodiment of MOD 073773.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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