AD 75-26-14

Active

Elevator Control

Key Information
75-26-14
Active
December 29, 1975
Not specified
Unknown
39-2463
Applicability
["Aircraft"]
["Glider"]
Scheibe-Flugzeugbau GmbH
Bergfalke-III Bergfalke-II/55
Regulatory Text

75-26-14 SCHEIBE FLUGZEUGBAU GmbH: Amendment 39-2463. Applies to Model Bergfalke II/55 and III gliders, certificated in all categories, equipped with loose connecting bolt between the elevator push-pull rod and elevator control lever.

Compliance is required as indicated, unless already accomplished.

To ensure a reliable elevator control connection, within the next 10 hours' time in service after the effective date of this AD, replace the safety pin (Fokker needle) at the connecting bolt between the elevator push-pull rod and the elevator control lever with an aviation quality washer and cotter pin.

This supersedes Amendment 39-2334 (49 FR 33008), AD 75-17-29.

This amendment becomes effective December 29, 1975.

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References
This information is not available.
--- - Part 39
FAA Documents