AD 2026-02-12

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

AD Number
2026-02-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2026-0731
FR Citation
91 FR 4006

Applicability

TypeManufacturerModelDetails
aircraft Airbus Various Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

Unsafe Condition

excessive wear on the bearing bolts connecting the cardan ring and the control ring assembly

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

Required Actions

initial and repetitive inspections of the swashplate for vertical and radial play, and depending on the results of the inspections, replacing any affected bolts

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

Compliance Time

within 830 hours time-in-service (TIS) since new accumulated by the bearing bolt, or within 10 hours TIS after the effective date of this AD, whichever occurs later

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

Affected Aircraft

Airbus Helicopters Deutschland GmbH (AHD) Model MBB-BK117 D-3 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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