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FAA
Federal Aviation Administration Department of Transportation
Aviation Safety
AIRWORTHINESS DIRECTIVE
Generated by Aircraft-logs.com — March 22, 2026

AD 66-08-05 ACTIVE

Rudder Control System Rod
Key Information
AD Number 66-08-05 Status Active
Effective Date April 16, 1966 Issue Date Not specified
Docket Number Unknown Amendment 39-211
Product Type ["Aircraft"] Product Subtype ["Small Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) SOCATA - Groupe Aerospatiale
Model(s) 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.

AD 66-08-05 — Rudder Control System Rod
Printed from Aircraft-logs.com — 03/22/2026