Airworthiness Directive

AD 2004-08-13 69 FR 21402 Active

Federal Aviation Administration · 14 CFR part 39

FR document
04-8794
Amendment
39-13582
Published
2004-04-21
Effective
2004-06-04
Models covered
1
Last live check
2026-10-01
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AD

2004-08-13

FR doc 04-8794 · 69 FR 21402

AD 2004-08-13Published 2004-04-21Effective 2004-06-04

Superseded by 2005-26-12

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 replace the center of gravity (CG) release hook attachment brackets with brackets of improved design.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for certain BURKHARDT GROB LUFT-UND RAUMFAHRT GmbH & CO KG (Grob) Models G103 Twin ASTIR, G103 TWIN II, G103 TWIN III ACRO, and G103 C Twin III SL sailplanes. This AD requires you to replace the center of gravity (CG) release hook attachment brackets with brackets of improved design. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent abnormal or uncontrolled sailplane release due to cracked CG release hook attachment brackets. This condition could result in reduced or loss of sailplane control.

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Applies to 1 model in our index