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pdf GFA AD 621 Issue 1 Popular

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GFA AD 621 Issue 1.pdf

GFA AD 621 Issue 1

FLIGHT CONTROLS - ELEVATOR CONTROL SYSTEM

A Janus Ce suffered and in-flight failure of the elevator control circuit beneath the rear seat. Fortunately the aircraft was able to be safely landed by the use of trim. The LBA was issued AD D-2004-495 and D-2004-495R1 which was reissued to to correct an omission. Schempp-Hirth has issued a Technical Note 295-30 / 373-9 / 809-16 / 847-9 and an appendix which forms part of this AD.