AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2021-19-06 86 FR 54032 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspecting certain carbon brake assemblies and corrective actions if necessary.

Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
2021-21097
Amendment
39-21724
Published
2021-09-30
Effective
2021-10-15
Models covered
1

Last live check: 2026-10-04

Printed from https://aircraftdirectives.com/ad/2021-19-06 · 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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

2021-19-06

FR doc 2021-21097 · 86 FR 54032

AD 2021-19-06Published 2021-09-30Effective 2021-10-15

Supersedes 2007-02-13

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 inspecting certain carbon brake assemblies and corrective actions if necessary.

Full official abstract

The FAA is superseding Airworthiness Directive (AD) 2007-02- 13, which applied to certain Dornier Luftfahrt GmbH (type certificate currently held by RUAG Aerospace Services GmbH) Model Dornier 228-212 airplanes. AD 2007-02-13 required inspecting the landing gear carbon brake assembly. This AD requires inspecting certain carbon brake assemblies and corrective actions if necessary. This AD was prompted by mandatory continuing airworthiness information (MCAI) issued by the European Union Aviation Safety Agency (EASA) to correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as loose bolts and nuts on the landing gear carbon brake assembly. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for Dornier 228

  1. AD 2016-17-05 Airworthiness Directives; RUAG Aerospace Services GmbH Airplanes Effective 2016-09-30
  2. AD 2014-10-02 Airworthiness Directives; Dornier Luftfahrt GmbH Airplanes Effective 2014-07-28
  3. AD 2014-04-02 Airworthiness Directives; DORNIER LUFTFAHRT GmbH Airplanes Effective 2014-04-01
  4. AD 2011-03-05 Airworthiness Directives; Dornier Luftfahrt GmbH Models Dornier 228-100,... Effective 2011-03-14
  5. AD 2009-20-07 Airworthiness Directives; DORNIER LUFTAHRT GmbH Models Dornier 228-100, ... Effective 2009-11-03

All Dornier 228 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