AD 2000-13-08

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter Deutschland GmbH Model EC 135 Helicopters

AD Number
2000-13-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 98-SW-74-AD
FR Citation
65 FR 41326

Applicability

TypeManufacturerModelDetails
aircraft Eurocopter Deutschland GmbH Model EC 135 Airworthiness Directives; Eurocopter Deutschland GmbH Model EC 135 Helicopters

Unsafe Condition

Misaligned or cracked bearing supports and loose bearing attachment bolts can lead to loss of drive to the 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

Conduct a tail rotor drive shaft vibration survey and install a Fenestron Shaft Retrofit Kit. Install double bearing supports and struts. Inspect bearing supports for cracks and replace if cracked. Inspect bearing attach hardware lock plates for bent-open tabs and slippage marks, and replace loose hardware. Perform inspections at intervals not exceeding 50 hours time-in-service.

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 Deutschland GmbH Model EC 135 helicopters, certificated in any category.

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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