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Airworthiness Directives; Airbus Helicopters

airworthiness · Rule · Final rule. · Published 2025-09-18 · Effective 2025-10-23 · 90 FR 44962

Document

Document number
2025-18083
Federal Register citation
90 FR 44962
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2025-09-18
Effective date
2025-10-23
FAA docket
Docket No. FAA-2025-1108

Abstract

The FAA is superseding Airworthiness Directive (AD) 2020-24-07 for certain Airbus Helicopters Model AS350B3, EC130B4, and EC130T2 helicopters. AD 2020-24-07 required modifying and inspecting the throttle twist grip (twist grip). Since the FAA issued AD 2020-24-07, there have been reports of the engine remaining in idle when the twist grip was turned to the "FLIGHT" mode. This AD retains the actions required by AD 2020-24-07 and adds a modification that constitutes terminating action for the repetitive inspections. This AD also expands the helicopter applicability, provides additional requirements for certain helicopters, and prohibits installing affected microswitches or an affected twist grip with the affected microswitch. The FAA is issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown