AD 2007-26-51
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Eurocopter | Deutschland GmbH Model EC135 | Airworthiness Directives; Eurocopter Deutschland GmbH Model EC135 Helicopters |
Unsafe Condition
Failure of the tail rotor control rod and adjoining ball pivot.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the tail rotor control rod and adjoining ball pivot within 5 hours time-in-service (TIS). Replace any unairworthy parts before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 5 hours time-in-service (TIS).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Eurocopter Deutschland GmbH Model EC135 helicopters.
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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