AD 66-08-05

Active

Rudder Control System Rod

Key Information
66-08-05
Active
April 16, 1966
Not specified
Unknown
39-211
Applicability
["Aircraft"]
["Small Airplane"]
SOCATA - Groupe Aerospatiale
M.S. 760 (Paris I) M.S. 760.A (Paris IA) M.S. 760B (Paris II)
Regulatory Text

66-08-05 MORANE-SAULNIER: Amdt. 39-211 Part 39 Federal Register March 17, 1966. Applies to Models M.S. 760, M.S. 760 A, and M.S. 760B Airplanes.
Compliance required within the next 300 hours' time in service after the effective date of this AD unless already accomplished.
Replace aluminum alloy rudder control system rod, P/N 0176-27.1.191, located between Stations 5 and 10, with steel rod, P/N 0176-27.1.218.
(Morane-Saulnier Service Bulletin No. 45 pertains to this subject.)
This directive effective April 16, 1966.

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