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Airworthiness Directive

AD 2001-25-09 66 FR 66730 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect the brake housing subassembly for cracks, nicks, or corrosion (referred to as damage).

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FR document
01-31297
Amendment
39-12562
Published
2001-12-27
Effective
2002-01-18
Models covered
1

Last live check: 2026-10-04

Printed from https://aircraftdirectives.com/ad/2001-25-09 · 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

2001-25-09

FR doc 01-31297 · 66 FR 66730

AD 2001-25-09Published 2001-12-27Effective 2002-01-18

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 brake housing subassembly for cracks, nicks, or corrosion (referred to as damage).

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Dornier Luftfahrt GmbH (Dornier) Model 228-212 airplanes that have a certain brake assembly installed. This AD requires you to inspect the brake housing subassembly for cracks, nicks, or corrosion (referred to as damage). This AD also requires you to replace damaged brake housing assemblies and modify the torque take-out cavity. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to detect and correct damage to the brake housing assembly, which could result in failure of this assembly. Such failure could lead to loss of braking action on landing and possible loss of control of the airplane.

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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