# Proposed AD 2003-CE-56-AD: Valentin GmbH & Co. Taifun 17E Sailplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2004-20-10
- Products: Valentin
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: April 22, 2004, 69 FR 21771
- Comments due: May 27, 2004
- Became: [AD 2004-20-10](https://openairdocs.org/ad/2004-20-10)
- Docket: 2003-CE-56-AD
- FR document: 04-9113
- Official PDF: https://openairdocs.org/files/sha256/7d/df/7ddfa2d5914398294ca93cb1bd4cbe8df6f60ec14956f19a9380de7a5988cbc0 (from https://www.govinfo.gov/content/pkg/FR-2004-04-22/pdf/04-9113.pdf)
- Federal Register: https://www.federalregister.gov/documents/2004/04/22/04-9113/airworthiness-directives-valentin-gmbh-and-co-taifun-17e-sailplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F5FC06884FE546A786256E7E004EE208.0001
- Page: https://openairdocs.org/proposed/2003-CE-56-AD

## Summary

The FAA proposes to adopt a new airworthiness directive (AD) for all Valentin GmbH & Co. Taifun 17E sailplanes. This proposed AD would require you to do an operational check of the front wing-locking mechanism left and right, inspect stop key movement, inspect wing and fuselage side root ribs, inspect the wing side shear force fittings, and take any corrective actions that may be required. This proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this proposed AD to detect and correct malfunction of wing-locking mechanism, which could result in failure of the wing-locking mechanism disengagement. This failure could lead to unlocking of wing in flight and consequent loss of control of the sailplane.

## Notices in this docket

- Apr 22, 2004: Notice of proposed rulemaking (NPRM). (first notice), FR document 04-9113, comments due May 27, 2004 (https://www.federalregister.gov/documents/2004/04/22/04-9113/airworthiness-directives-valentin-gmbh-and-co-taifun-17e-sailplanes)

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