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Airworthiness Directive

AD 98-06-13 63 FR 12605 Active

Federal Aviation Administration · 14 CFR part 39

Requires replacing the MLG axle assembly with an MLG axle assembly of improved design.

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

FR document
98-6452
Amendment
39-10391
Published
1998-03-16
Effective
1998-06-15
Models covered
1

Last live check: 2026-10-04

Printed from https://aircraftdirectives.com/ad/98-06-13 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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AD

98-06-13

FR doc 98-6452 · 63 FR 12605

AD 98-06-13Published 1998-03-16Effective 1998-06-15

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 replacing the MLG axle assembly with an MLG axle assembly of improved design.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Dornier Luftfahrt GmbH (Dornier) Models 228-100, 228- 101, 228-200, and 228-201 airplanes equipped with certain main landing gear (MLG). This action requires replacing the MLG axle assembly with an MLG axle assembly of improved design. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified in this AD are intended to prevent main landing gear failure, which, if not corrected, could result in loss of control of the airplane during landing operations.

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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