SAIB CE-06-59
Current · Issued 08/11/2006 · Schempp-Hirth Flugzeugbau Discus-2T | Discus-2cT | Ventus-2cT · FAA DRS
SAIB CE-06-59 — Open on drs.faa.gov ↗
The FAA-published PDF is the authoritative source.
Bulletin text · verbatim from the FAA PDF · 14 paragraphs · 233 words
CE-06-59 August 11, 2006 http://www.faa.gov/aircraft/safety/alerts/ This is information only. Recommendations aren’t mandatory.
Introduction
This Special Airworthiness Information Bulletin advises you of an airworthiness concern on the following Schempp-Hirth sailplanes:
Model Serial Number Discus-2T 1 through 40 Discus-2cT 1 through 30 Ventus-2cT 1 through 179
Background
During an inspection, cracks were found in the steel tubes next to the welding seams of the engine pylon assembly. The European Aviation Safety Agency (EASA) has issued Emergency Airworthiness Directive number 2006-0227-E, dated July 26, 2006, to mandate corrective actions for owner/operators in the Agency’s member states.
Schempp-Hirth Technical Note Numbers 825- 38 (Ventus-2cT) and 863-13 (Discus-2T and Discus-2cT) provide instructions for inspection and modification of the engine pylon assembly.
Note: The Discus-2T, Discus-2cT, and Ventus-2cT are not type certificated in the United States and therefore do not meet the criteria for mandatory action. We do not issue ADs for sailplanes without U.S. type certification. However, these models are currently operating in the United States with an experimental airworthiness certificate.
Recommendation
We recommend you do the actions stated in the Technical Notes.
For Further Information Contact
Gregory Davison, Glider Program Manager FAA Small Airplane Directorate 901 Locust Street, Room 301 Kansas City, Missouri 64106 Phone: (816) 329-4130 Fax: (816) 329-4090 Email: [email protected]
SCHEMPP-HIRTH Flugzeugbau GmbH Krebenstraße 25 D-73230 Kirchheim/Teck Germany Phone: 49 7021 7298-0 Fax: 49 7021 7298-199 Email: [email protected]
Technical Note information is available at: http://www.schempp-hirth.com/