← My Government dashboard

Government Watch

Dossier Executive final rule 29-jun-2026 Takes effect · 03-aug-2026
Finalized regulation — legally enforceable once its effective date arrives.

Airworthiness Directives; Airbus Helicopters

Key claim: The FAA is superseding AD 2023-01-04 for specified Airbus Helicopters models to update tail rotor head inspection requirements by eliminating repetitive black paint index marking inspections and restricting installation of certain parts.

Abstract

(Rule · Transportation Department, Federal Aviation Administration) The FAA is superseding Airworthiness Directive (AD) 2023-01-04 for all Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters. AD 2023-01-04 required, for helicopters with certain part- numbered tail rotor head (TRH) spider pitch change units installed, inspecting the pitch change spider nut (nut) for correct installation; marking a 2 to 5 mm wide black paint index mark and repetitively inspecting the alignment of the marking; and performing additional inspections and corrective actions if necessary. Since the FAA issued AD 2023-01-04, new or more restrictive airworthiness limitations were issued, which terminated the requirement for the repetitive inspections of the black paint index marking. This AD requires the same actions as AD 2023-01-04, except for the repetitive black paint index marking inspections and prohibits installing certain parts unless certain requirements are met. The FAA is issuing this AD to address the unsafe condition on these products.

Why this matters

The FAA is superseding AD 2023-01-04 for specified Airbus Helicopters models to update tail rotor head inspection requirements by eliminating repetitive black paint index marking inspections and restricting installation of certain parts.

Source

Link

Briefing card

Airworthiness Directives; Airbus Helicopters
Stage: final rule · federal-register · 29-jun-2026

The FAA is issuing a new airworthiness directive requiring modification of window jettisoning system components on Airbus Helicopters Model H160-B helicopters due to self-locking nuts that could be loosened by hand from a cable kit non-conformity.

Cross-references (0)

None recorded — doctrine links and citations appear here as scans and citation sweeps find them.

External: fedreg:2026-13064

Ask about this finding

Replies are grounded in the abstract and metadata above. The model will quote directly when possible and say so if a question isn't covered.

Stages other doctrine resolution introduced proposed rule passed chamber executive action final rule enacted district opinion circuit opinion opinion

build build 392 · ea9c128-dirty · 2026-08-09