NPRM FAA-2026-4656

Comment period closed

Proposed airworthiness directive · Airbus Helicopters Deutschland EC135P1, EC135P2, EC135P2+ and 6 more

Published
June 29, 2026 · 91 FR 39043
Comments due
August 13, 2026
Action
Notice of proposed rulemaking (NPRM)
Docket
FAA-2026-4656
Project
MCAI-2026-00214-R
FR document
2026-13034
Products
Aircraft
Models
EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3, EC635T2+

A proposal is not in force. If adopted, it becomes an AD, usually with changes. Only the Federal Register edition is official.

Summary

The FAA proposes to adopt 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 proposed AD was prompted by a report of a separated tail rotor blade (TRB) assembly due to a crack caused by intergranular corrosion. This proposed AD would require repetitively inspecting a certain TRB assembly for cracks and, depending on the results, removing any cracked TRB assembly from service and replacing an affected part as terminating action for the repetitive inspections. This proposed AD would also prohibit installing a certain TRB assembly on any helicopter unless certain requirements are met. The FAA is proposing this AD to address the unsafe condition on these products.

Notices in this docket · 1