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Dossier Executive proposed rule 30-sep-2026 Comment closes · 16-nov-2026 · in 6 days
Draft regulation published for public comment — not yet in force.

Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters

Key claim: Operators of listed Airbus EC135 and EC635 helicopters must update their rotorcraft flight manuals with new emergency, malfunction, and normal procedures because the main-gearbox low-oil-pressure light may not come on if oil is lost.

Abstract

(Rule · Transportation Department, Federal Aviation Administration) The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Deutschland GmbH (AHD) Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3, and EC635T2+ helicopters. This AD was prompted by a determination that in cases of loss of oil from the main gearbox (MGB), the low pressure caution or warning light might not activate. This AD requires revising the existing rotorcraft flight manual (RFM) for the helicopter by incorporating updated emergency, malfunction, and normal procedures. The FAA is issuing this AD to address the unsafe condition on these products.

Why this matters

This AD addresses a cockpit-warning gap on a widely operated light twin helicopter — if main-gearbox oil is lost, the low-pressure light may not illuminate, leaving pilots without a primary cue of an impending gearbox failure. Flight-manual procedure updates are the FAA’s interim mitigation while the fleet continues to operate, and this pattern (procedure change rather than hardware fix) is common for warning-system defects on in-service rotorcraft.

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Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters
Stage: proposed rule · federal-register · 30-sep-2026

If you operate an affected Airbus EC135 or EC635, you would need to inspect yaw-actuator parts and replace any that fail the inspection.

The FAA would require operators of certain Airbus Helicopters EC135 and EC635 models to inspect yaw-actuator parts—and replace them if needed—after a broken control rod caused loss of tail-rotor control.

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External: fedreg:2026-19971

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