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Airworthiness Directive

AD 2021-26-09 86 FR 71134 Active

Federal Aviation Administration · 14 CFR part 39

Requires repetitive inspections of the T/R hub and depending on the results, removing the T/R hub from service.

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FR document
2021-27052
Amendment
39-21868
Published
2021-12-15
Effective
2022-01-19
Models covered
1

Last live check: 2026-10-04

Printed from https://aircraftdirectives.com/ad/2021-26-09 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2021-26-09

FR doc 2021-27052 · 86 FR 71134

AD 2021-26-09Published 2021-12-15Effective 2022-01-19

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires repetitive inspections of the T/R hub and depending on the results, removing the T/R hub from service.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Brantly Helicopters Industries U.S.A. Co., Ltd., Model 305 helicopters and Brantly International, Inc., Model B-2, B-2A, and B-2B helicopters. This AD was prompted by a report of a crack in the tail rotor (T/R) hub. This AD requires repetitive inspections of the T/R hub and depending on the results, removing the T/R hub from service. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for Brantly B-2 / 305

  1. AD 2014-20-16 Airworthiness Directives; Brantly International, Inc. Helicopters Effective 2014-11-12
  2. AD 2006-08-07 Airworthiness Directives; Brantly International, Inc. Model B-2, B-2A, a... Effective 2006-05-02

All Brantly B-2 / 305 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index