Airworthiness Directive

AD 2006-02-12 71 FR 5584 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to modify or replace the complete rudder mount assembly and ensure that the securing washer, castellated nut, and new split pins are installed.

FR document
06-735
Amendment
39-14464
Published
2006-02-02
Effective
2006-03-15
Models covered
1

Last live check: 2026-08-19

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AD

2006-02-12

FR doc 06-735 · 71 FR 5584

AD 2006-02-12Published 2006-02-02Effective 2006-03-15

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 you to modify or replace the complete rudder mount assembly and ensure that the securing washer, castellated nut, and new split pins are installed.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for all Glaser-Dirks Flugzeugbau GmbH Models DG-100 and DG-400 sailplanes and certain DG Flugzeugbau GmbH Models DG-500 Elan Series and DG-500M sailplanes. This AD requires you to modify or replace the complete rudder mount assembly and ensure that the securing washer, castellated nut, and new split pins are installed. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent the universal bearing of the lower rudder mounting from slipping out of the bearing support. The universal bearing slipping out could result in the rudder separating from its support. This failure could lead to loss of sailplane control during flight operations.

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Applies to 1 model in our index