AD 77-15-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | SOCATA - Groupe Aerospatiale | M.S. 760 (Paris I) | Airworthiness Directives; Morane Saulnier (Socata) Model MS 760 (Paris 1) and MS 760A (Paris 1A) Airplanes |
| aircraft | SOCATA - Groupe Aerospatiale | M.S. 760.A (Paris IA) | Airworthiness Directives; Morane Saulnier (Socata) Model MS 760 (Paris 1) and MS 760A (Paris 1A) Airplanes |
Unsafe Condition
Cracks in the landing gear wheels, P/N 3760-A, could lead to wheel failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect each ERAM wheel, P/N 3760-A, using a dye penetrant procedure per ERAM Service Bulletin No. 32-01 (Dec 1970, Oct 1973 revision) or FAA-approved equivalent. Replace wheels with more than one crack per stud or any crack exceeding 14 mm in length.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 50 hours time in service after the effective date of this AD, unless already accomplished within the preceding 50 hours time in service, and thereafter at intervals not to exceed 100 hours time in service from the last inspection.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Morane Saulnier (Socata) Model MS 760 (Paris 1) and MS 760A (Paris 1A) airplanes, all serial numbers, equipped with ERAM wheels, P/N 3760-A.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Landing Gear Wheels
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_77-15-14.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 77-15-14 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Morane Saulnier (Socata) Model MS 760 (Paris 1) and MS 760A (Paris 1A) Airplanes Subject: Landing Gear Wheels Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/29/1977 Make: SOCATA - Groupe Aerospatiale Model: M.S. 760 (Paris I) | M.S. 760.A (Paris IA) Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 77-15-14 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2985 AD NUMBER: 77-15-14 SUBJECT HEADING: Airworthiness Directives; Morane Saulnier (Socata) Model MS 760 (Paris 1) and MS 760A (Paris 1A) Airplanes ACTION: SUMMARY: DATES: Effective August 29, 1977. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 77-15-14 MORANE SAULNIER (SOCATA): Amendment 39-2985. Applies to Model MS 760 (Paris 1) and MS 760A (Paris 1A) airplanes, all serial numbers, certificated in all categories, that are equipped with ERAM wheels, P/N 3760-A. Compliance is required within the next 50 hours time in service after the effective date of this AD, unless already accomplished within the preceding 50 hours time in service, and thereafter, at intervals not to exceed 100 hours time in service from the last inspection. To detect cracks in the landing gear wheels and prevent possible wheel failure, accomplish the following: (a) Visually inspect, using a dye penetrant procedure, each ERAM wheel, P/N 3760-A, in accordance with paragraph 2 of ERAM Service Bulletin No. 32-01, dated December 1970, as revised October 1973, or an FAA-approved equivalent. (b) If, during an inspection required by this AD, a wheel is found to have more than one crack per stud or any crack exceeding 14 mm in length, replace that wheel with a serviceable wheel of the same part number or an FAA-approved equivalent. This amendment becomes effective August 29, 1977. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_77-15-14.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 77-15-14 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Morane Saulnier (Socata) Model MS 760 (Paris 1) and MS 760A (Paris 1A) Airplanes Subject: Landing Gear Wheels Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/29/1977 Make: SOCATA - Groupe Aerospatiale Model: M.S. 760 (Paris I) | M.S. 760.A (Paris IA) 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: 77-15-14 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2985 AD NUMBER: 77-15-14 SUBJECT HEADING: Airworthiness Directives; Morane Saulnier (Socata) Model MS 760 (Paris 1) and MS 760A (Paris 1A) Airplanes ACTION: SUMMARY: DATES: Effective August 29, 1977. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 77-15-14 MORANE SAULNIER (SOCATA): Amendment 39-2985. Applies to Model MS 760 (Paris 1) and MS 760A (Paris 1A) airplanes, all serial numbers, certificated in all categories, that are equipped with ERAM wheels, P/N 3760-A. Compliance is required within the next 50 hours time in service after the effective date of this AD, unless already accomplished within the preceding 50 hours time in service, and thereafter, at intervals not to exceed 100 hours time in service from the last inspection. To detect cracks in the landing gear wheels and prevent possible wheel failure, accomplish the following: (a) Visually inspect, using a dye penetrant procedure, each ERAM wheel, P/N 3760-A, in accordance with paragraph 2 of ERAM Service Bulletin No. 32-01, dated December 1970, as revised October 1973, or an FAA-approved equivalent. (b) If, during an inspection required by this AD, a wheel is found to have more than one crack per stud or any crack exceeding 14 mm in length, replace that wheel with a serviceable wheel of the same part number or an FAA-approved equivalent. This amendment becomes effective August 29, 1977. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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