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Airworthiness Directive

AD 2007-02-13 72 FR 3355 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect the landing gear carbon brake assembly.

Superseded by AD 2021-19-06Federal Register (opens in a new tab)

FR document
E7-900
Amendment
39-14900
Published
2007-01-25
Effective
2007-03-01
Models covered
1

Last live check: 2026-10-04

Printed from https://aircraftdirectives.com/ad/2007-02-13 · 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

2007-02-13

FR doc E7-900 · 72 FR 3355

AD 2007-02-13Published 2007-01-25Effective 2007-03-01

Superseded by 2021-19-06

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 you to inspect the landing gear carbon brake assembly.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for DORNIER LUFTFAHRT GmbH Model 228-212 airplanes. This AD requires you to inspect the landing gear carbon brake assembly. This AD results from mandatory continuing airworthiness information (MCAI) issued by the European Aviation Safety Agency (EASA), which is the airworthiness authority for the European Union. We are issuing this AD to inspect the landing gear carbon brake assembly to detect and replace loose bolts or self-locking nuts, which could result in the brake assembly detaching and malfunctioning, degrade brake performance and potentially cause loss of control of the aircraft during landing and roll-out.

More directives for Dornier 228

  1. AD 2021-19-06 Airworthiness Directives; RUAG Aerospace Services GmbH (Type Certificate... Effective 2021-10-15
  2. AD 2016-17-05 Airworthiness Directives; RUAG Aerospace Services GmbH Airplanes Effective 2016-09-30
  3. AD 2014-10-02 Airworthiness Directives; Dornier Luftfahrt GmbH Airplanes Effective 2014-07-28
  4. AD 2014-04-02 Airworthiness Directives; DORNIER LUFTFAHRT GmbH Airplanes Effective 2014-04-01
  5. AD 2011-03-05 Airworthiness Directives; Dornier Luftfahrt GmbH Models Dornier 228-100,... Effective 2011-03-14

All Dornier 228 directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2007-02-13 (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