AD Amdt-39-19529
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Eurocopter Deutschland GmbH | Various | Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters (Type Certificate Previously Held by Eurocopter Deutschland GmbH) |
| aircraft | Airbus | Helicopters Deutschland GmbH | Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters (Type Certificate Previously Held by Eurocopter Deutschland GmbH) |
Unsafe Condition
bearings were detected which had not been correctly fixed, which may cause the affected control lever to shift in the axial direction and contact the helicopter structure, possibly resulting in reduced helicopter control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
install bushings and washers, retrofitting bushings on the levers to prevent movement of the bearings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 100 hours TIS or at the next annual inspection, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Helicopters Deutschland GmbH (Type Certificate previously held by Eurocopter Deutschland GmbH) Model EC135 P1, P2, P2+, T1, T2, and T2+ helicopters, serial number 0005 through 00829, and Model MBB-BK 117C-2 helicopters, serial number 9004 through 9310.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.