AD 75-05-05
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | Goodyear | DC-10-30 | Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2 |
| aircraft | The Boeing Company | Goodyear | DC-10-30F (KC-10A, KDC-10) | Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2 |
| aircraft | The Boeing Company | Goodyear | DC-10-40 | Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2 |
| aircraft | The Boeing Company | Goodyear | DC-10-40F | Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2 |
| aircraft | The Boeing Company | Goodyear | Aerospace Corp Wheel Assemblies | Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2 |
| appliance | The Boeing Company | Goodyear | DC-10-30 | Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2 |
| appliance | The Boeing Company | Goodyear | DC-10-30F (KC-10A, KDC-10) | Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2 |
| appliance | The Boeing Company | Goodyear | DC-10-40 | Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2 |
| appliance | The Boeing Company | Goodyear | DC-10-40F | Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2 |
| appliance | The Boeing Company | Goodyear | Aerospace Corp Wheel Assemblies | Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2 |
Unsafe Condition
Failures of the MS 21250-10060 bolts attaching the wheel halves due to cracks or damaged threads.
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Required Actions
Perform magnetic-particle inspection for cracks of all wheel-half attaching bolts, paying particular attention to the radius under the bolt head and to the threads. Replace cracked bolts and those with stripped, crossed, or damaged threads. No reworking of bolts is permitted; defective bolts must be scrapped.
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Compliance Time
At the next tire change or wheel re-assembly after the effective date of this Airworthiness Directive, unless already accomplished, and thereafter at each tire change or wheel re-assembly or during replacement of any wheel half attaching bolts in a tire/wheel assembly.
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Affected Aircraft
Goodyear Aerospace Corporation Main Wheel Assemblies P/N 5000757-1 and -2, typically used on McDonnell-Douglas DC-10-30, DC-10-40 series aircraft including DC-10-30F (KC-10A, KDC-10), DC-10-40F.
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Federal Register Abstract
Wheel Assemblies
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_75-05-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 75-05-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5...Show more Subject: Wheel Assemblies Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/26/1975 Make: The Boeing Company | Goodyear Model: DC-10-30 | DC-10-30F (KC-10A, KDC-10) | DC-10-40 | DC-10-40F | Aerospace Corp Wheel Assemblies Product Type: Appliance Product Subtype: Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 75-05-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2101 AD NUMBER: 75-05-05 SUBJECT HEADING: Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2 ACTION: SUMMARY: DATES: Effective March 26, 1975. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-05-05 GOODYEAR AEROSPACE CORPORATION: Amendment 39-2101. Applies to main wheel assemblies P/N's 5000757-1 and -2 typically used on, but their use is not limited to, McDonnell-Douglas DC-10-30 and DC-10-40 series aircraft. Compliance is required at the next tire change or wheel re-assembly after the effective date of this Airworthiness Directive, unless already accomplished, and thereafter at each tire change or wheel re-assembly or during replacement of any wheel half attaching bolts in a tire/wheel assembly. New wheels or spare wheel assemblies with previously magnetic-particle inspected bolts are exempt only from the initial inspection. To prevent failures of the MS 21250-10060 bolts attaching the wheel halves, accomplish the following: (a) Perform magnetic-particle inspection for cracks of all wheel-half attaching bolts, paying particular attention to the radius under the bolt head and to the threads. Replace cracked bolts and those having stripped, crossed or damaged threads. No reworking of wheel bolts is permitted. Defective bolts shall be scrapped. This amendment becomes effective March 26, 1975. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_75-05-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 75-05-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5...Show more Subject: Wheel Assemblies Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/26/1975 Make: The Boeing Company | Goodyear Model: DC-10-30 | DC-10-30F (KC-10A, KDC-10) | DC-10-40 | DC-10-40F | Aerospace Corp Wheel Assemblies Product Type: Appliance Product Subtype: Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 75-05-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2101 AD NUMBER: 75-05-05 SUBJECT HEADING: Airworthiness Directives; GOODYEAR AEROSPACE CORPORATION: Applies To Main Wheel Assemblies P/N's 5000757-1 and -2 ACTION: SUMMARY: DATES: Effective March 26, 1975. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-05-05 GOODYEAR AEROSPACE CORPORATION: Amendment 39-2101. Applies to main wheel assemblies P/N's 5000757-1 and -2 typically used on, but their use is not limited to, McDonnell-Douglas DC-10-30 and DC-10-40 series aircraft. Compliance is required at the next tire change or wheel re-assembly after the effective date of this Airworthiness Directive, unless already accomplished, and thereafter at each tire change or wheel re-assembly or during replacement of any wheel half attaching bolts in a tire/wheel assembly. New wheels or spare wheel assemblies with previously magnetic-particle inspected bolts are exempt only from the initial inspection. To prevent failures of the MS 21250-10060 bolts attaching the wheel halves, accomplish the following: (a) Perform magnetic-particle inspection for cracks of all wheel-half attaching bolts, paying particular attention to the radius under the bolt head and to the threads. Replace cracked bolts and those having stripped, crossed or damaged threads. No reworking of wheel bolts is permitted. Defective bolts shall be scrapped. This amendment becomes effective March 26, 1975. FOOTER:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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