AD 75-22-15
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | SOCATA | MS 880B | Airworthiness Directives; Models MS880B, MS885, MS892A150, MS893A, and MS894A Airplanes |
| aircraft | SOCATA | MS 885 | Airworthiness Directives; Models MS880B, MS885, MS892A150, MS893A, and MS894A Airplanes |
| aircraft | SOCATA | MS 892A-150 | Airworthiness Directives; Models MS880B, MS885, MS892A150, MS893A, and MS894A Airplanes |
| aircraft | SOCATA | MS 893A | Airworthiness Directives; Models MS880B, MS885, MS892A150, MS893A, and MS894A Airplanes |
| aircraft | SOCATA | MS 894A | Airworthiness Directives; Models MS880B, MS885, MS892A150, MS893A, and MS894A Airplanes |
Unsafe Condition
Possible interference between the control stick and floor section.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the floor adjacent to the control stick by increasing the clearance between the floor and control stick in accordance with Socata Service Bulletin No. 104 GR-27-09, dated September 1972, or an FAA-approved equivalent.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 25 hours' time in service after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
SOCATA models MS880B and MS885 airplanes except serial numbers 1962 and subsequent; MS892A150, MS893A, and MS894A airplanes except serial numbers 11993 and subsequent.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Floor and Control Stick
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_75-22-15.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 75-22-15 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Models MS880B, MS885, MS892A150, MS893A, and MS894A Airplanes Subject: Floor and Control Stick Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/04/1975 Make: SOCATA Model: MS 880B | MS 885 | MS 892A-150 | MS 893A | MS 894A Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 75-22-15 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2405 AD NUMBER: 75-22-15 SUBJECT HEADING: Airworthiness Directives; Models MS880B, MS885, MS892A150, MS893A, and MS894A Airplanes ACTION: SUMMARY: DATES: Effective November 4, 1975. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-22-15 MORANE SAULNIER (SOCATA) RALLYE: Amendment 39-2405. Applies to MS880B and MS885 airplanes, certificated in all categories, except serial numbers 1962 and subsequent; and MS892A150, MS893A, and MS894A airplanes, certificated in all categories, except serial numbers 11993 and subsequent. Compliance is required within the next 25 hours' time in service after the effective date of this AD, unless already accomplished. To prevent possible interference between the control stick and floor hat section, accomplish the following: Modify the floor adjacent to the control stick by increasing the clearance between the floor and control stick in accordance with the "Description" paragraph in Socata Service Bulletin No. 104 GR-27-09, dated September, 1972, or an FAA-approved equivalent. This amendment becomes effective November 4, 1975. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_75-22-15.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 75-22-15 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Models MS880B, MS885, MS892A150, MS893A, and MS894A Airplanes Subject: Floor and Control Stick Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/04/1975 Make: SOCATA Model: MS 880B | MS 885 | MS 892A-150 | MS 893A | MS 894A 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: 75-22-15 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2405 AD NUMBER: 75-22-15 SUBJECT HEADING: Airworthiness Directives; Models MS880B, MS885, MS892A150, MS893A, and MS894A Airplanes ACTION: SUMMARY: DATES: Effective November 4, 1975. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-22-15 MORANE SAULNIER (SOCATA) RALLYE: Amendment 39-2405. Applies to MS880B and MS885 airplanes, certificated in all categories, except serial numbers 1962 and subsequent; and MS892A150, MS893A, and MS894A airplanes, certificated in all categories, except serial numbers 11993 and subsequent. Compliance is required within the next 25 hours' time in service after the effective date of this AD, unless already accomplished. To prevent possible interference between the control stick and floor hat section, accomplish the following: Modify the floor adjacent to the control stick by increasing the clearance between the floor and control stick in accordance with the "Description" paragraph in Socata Service Bulletin No. 104 GR-27-09, dated September, 1972, or an FAA-approved equivalent. This amendment becomes effective November 4, 1975. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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