AD 78-13-03

Active

Elevator Control Assembly

Key Information
78-13-03
Active
July 05, 1978
Not specified
Unknown
39-3244
Applicability
["Aircraft"]
["Glider"]
GROB-WERKE GMBH & CO KG
G102 ASTIR CS
Regulatory Text

78-13-03 BURKHART GROB: Amendment 39-3244. Applies to Model G102 Astir CS gliders, Serial numbers, 1001 to 1234 and 1300 to 1315, certificated in all categories.

Compliance is required within the next 25 hours time in service after the effective date of this AD, unless already accomplished.

To reduce the possibility of elevator control failure due to possible loss of an elevator control pivot bolt, modify the elevator control assembly by installing a mechanical stop to the elevator control pivot (bearing) bolt, part no. 4205.06, in accordance with Burkhart Grob Technical Information TM102-4 dated August 16, 1976, or an equivalent, approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa and Middle East Region.

This amendment becomes effective July 5, 1978.

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