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Airworthiness Directive

AD 2005-26-14 70 FR 76676 Active

Federal Aviation Administration · 14 CFR part 39

FR document
05-24478
Amendment
39-14435
Published
2005-12-28
Effective
2006-02-06
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/2005-26-14 · 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

2005-26-14

FR doc 05-24478 · 70 FR 76676

AD 2005-26-14Published 2005-12-28Effective 2006-02-06

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 elevator lever, part number (P/N) 103-3521, with an improved design part, P/N 103-3523.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for all BURKHARDT GROB LUFT-UND RAUMFAHRT GmbH & CO KG (Burkhardt Grob) Model G103 TWIN ASTIR sailplanes. This AD requires you to replace the elevator lever, part number (P/N) 103-3521, with an improved design part, P/N 103-3523. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent cracks in the elevator lever, which could cause the elevator lever to fail. This failure could result in loss of control of the sailplane.

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View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index