AD 66-08-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | SOCATA - Groupe Aerospatiale | M.S. 760 (Paris I) | Airworthiness Directives; Morane-Saulnier Models M.S. 760, M.S. 760 A, and M.S. 760B Airplanes |
| aircraft | SOCATA - Groupe Aerospatiale | M.S. 760.A (Paris IA) | Airworthiness Directives; Morane-Saulnier Models M.S. 760, M.S. 760 A, and M.S. 760B Airplanes |
| aircraft | SOCATA - Groupe Aerospatiale | M.S. 760B (Paris II) | Airworthiness Directives; Morane-Saulnier Models M.S. 760, M.S. 760 A, and M.S. 760B Airplanes |
Unsafe Condition
Failure of the aluminum alloy rudder control system rod (P/N 0176-27.1.191) between Stations 5 and 10 could result in loss of rudder control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the aluminum alloy rudder control system rod (P/N 0176-27.1.191) with a steel rod (P/N 0176-27.1.218) located between Stations 5 and 10.
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Compliance Time
within the next 300 hours' time in service after the effective date of this AD unless already accomplished
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Affected Aircraft
Morane-Saulnier Models M.S. 760, M.S. 760 A, and M.S. 760B Airplanes
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Rudder Control System Rod
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_66-08-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 66-08-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Morane-Saulnier Models M.S. 760, M.S. 760 A, and M.S. 760B Airplanes Subject: Rudder Control System Rod Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/16/1966 Make: SOCATA - Groupe Aerospatiale Model: M.S. 760 (Paris I) | M.S. 760.A (Paris IA) | M.S. 760B (Paris II) Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 66-08-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-211 AD NUMBER: 66-08-05 SUBJECT HEADING: Airworthiness Directives; Morane-Saulnier Models M.S. 760, M.S. 760 A, and M.S. 760B Airplanes ACTION: SUMMARY: DATES: Effective April 16, 1966. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: 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. FOOTER:
Document Text
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AD Final Rules - DRS_66-08-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 66-08-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Morane-Saulnier Models M.S. 760, M.S. 760 A, and M.S. 760B Airplanes Subject: Rudder Control System Rod Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/16/1966 Make: SOCATA - Groupe Aerospatiale Model: M.S. 760 (Paris I) | M.S. 760.A (Paris IA) | M.S. 760B (Paris II) Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 66-08-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-211 AD NUMBER: 66-08-05 SUBJECT HEADING: Airworthiness Directives; Morane-Saulnier Models M.S. 760, M.S. 760 A, and M.S. 760B Airplanes ACTION: SUMMARY: DATES: Effective April 16, 1966. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: 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. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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