AD Amdt-39-19498
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Various | Airworthiness Directives; Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters |
Unsafe Condition
limited control of a tail rotor because of the binding of a bearing
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
modifying the floor and rod, inspecting the bearing for freedom of movement
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 100 hours TIS
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Model EC135 P1, P2, P2+, T1, T2, and T2+ helicopters, with bearing, part number (P/N) LN9367GE6N2; rod, P/N L671M5040205; lever, P/N L671M5040101; and floor, P/N L533M1014101, L533M1014102, L533M1014103, L533M1014104, L533M1014105 or L533M1014106, installed
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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