AD 74-13-06
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | McCauley | 180J | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| aircraft | Cessna Aircraft Company | McCauley | 210L | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| aircraft | Cessna Aircraft Company | McCauley | A185F | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| aircraft | Cessna Aircraft Company | McCauley | T210L | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| aircraft | Cessna Aircraft Company | McCauley | TU206F | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| aircraft | Cessna Aircraft Company | McCauley | U206F | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| aircraft | Cessna Aircraft Company | McCauley | Main Wheel Assemblies | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| appliance | Cessna Aircraft Company | McCauley | 180J | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| appliance | Cessna Aircraft Company | McCauley | 210L | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| appliance | Cessna Aircraft Company | McCauley | A185F | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| appliance | Cessna Aircraft Company | McCauley | T210L | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| appliance | Cessna Aircraft Company | McCauley | TU206F | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| appliance | Cessna Aircraft Company | McCauley | U206F | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
| appliance | Cessna Aircraft Company | McCauley | Main Wheel Assemblies | Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 |
Unsafe Condition
Possible wheel failures due to breakage of the wheel flange attaching bolts.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify main wheel assemblies per McCauley Service Bulletin WB-1-A or FAA-approved method within 25 hours' time in service. For 1973 Cessna Models 180J and A185F, also inspect bolts every 25 hours' time in service until modified. Record compliance in aircraft logbook.
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 (for modification) and within 25 hours' time in service after effective date (for inspection), with subsequent inspections not exceeding 25 hours' time in service until modification is done.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
McCauley Main Wheel Assemblies P/N D-30063-1, -2, -4, S/N 720000 thru 739999, installed on Cessna Models 180J, A185F, U206F, TU206F, 210L, T210L.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Main Wheel Assemblies
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_74-13-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 74-13-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, ...Show more Subject: Main Wheel Assemblies Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 06/24/1974 Make: Cessna Aircraft Company | McCauley Model: 180J | 210L | A185F | T210L | TU206F | U206F | Main 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: 74-13-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1878 AD NUMBER: 74-13-06 SUBJECT HEADING: Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 ACTION: SUMMARY: DATES: Effective June 24, 1974. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 74-13-06 McCAULEY: Amendment 39-1878. Applies to main wheel assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 typically used on, but not limited to, Cessna Aircraft Models 180J, A185F, U206F, TU206F, 210L and T210L. Compliance required as indicated unless already accomplished. To prevent possible wheel failures due to breakage of the wheel flange attaching bolts, accomplish the following: (a) For main wheel assemblies used on the Cessna Aircraft Models 180J, A185F, U206F, TU206F, 210L, and T210L manufactured in the Model Year 1974 and any other aircraft with these main wheel assemblies installed, within the next 25 hours' time in service, modify main wheel assemblies in accordance with the instructions contained in McCauley Industrial Corporation Service Bulletin WB-1-A dated June 10, 1974, or subsequent Federal Aviation Administration approved revisions. Equivalent methods of compliance with this Airworthiness Directive must be approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration Great Lakes Region, Des Plaines, Illinois. (b) For main wheel assemblies used on Cessna Aircraft Models 180J and A185F, manufactured in the Model Year 1973; within 25 hours' time in service after the effective date of this Airworthiness Directive and thereafter, at intervals not to exceed 25 hours' time in service visually inspect the 1/4" bolts attaching the wheel flanges for broken bolts until compliance with the modification in Paragraph (a) above is accomplished. If indications of broken bolts exist modify wheels in accordance with Paragraph (a). (c) Upon completion of the modification in Paragraph (a), record compliance with this particular part of the Airworthiness Directive in the aircraft logbook. NOTE: Cessna Service Letter SE 74-8 or subsequent revisions pertains to the same subject. The McCauley wheels may additionally be marked with Cessna P/N's C163002-0102, -0103 or -0104. This amendment becomes effective June 24, 1974. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_74-13-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 74-13-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, ...Show more Subject: Main Wheel Assemblies Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 06/24/1974 Make: Cessna Aircraft Company | McCauley Model: 180J | 210L | A185F | T210L | TU206F | U206F | Main 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: 74-13-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1878 AD NUMBER: 74-13-06 SUBJECT HEADING: Airworthiness Directives; McCAULEY: Applies to Main Wheel Assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 ACTION: SUMMARY: DATES: Effective June 24, 1974. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 74-13-06 McCAULEY: Amendment 39-1878. Applies to main wheel assemblies P/N's D-30063-1, -2, and -4, S/N's 720000 thru 739999 typically used on, but not limited to, Cessna Aircraft Models 180J, A185F, U206F, TU206F, 210L and T210L. Compliance required as indicated unless already accomplished. To prevent possible wheel failures due to breakage of the wheel flange attaching bolts, accomplish the following: (a) For main wheel assemblies used on the Cessna Aircraft Models 180J, A185F, U206F, TU206F, 210L, and T210L manufactured in the Model Year 1974 and any other aircraft with these main wheel assemblies installed, within the next 25 hours' time in service, modify main wheel assemblies in accordance with the instructions contained in McCauley Industrial Corporation Service Bulletin WB-1-A dated June 10, 1974, or subsequent Federal Aviation Administration approved revisions. Equivalent methods of compliance with this Airworthiness Directive must be approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration Great Lakes Region, Des Plaines, Illinois. (b) For main wheel assemblies used on Cessna Aircraft Models 180J and A185F, manufactured in the Model Year 1973; within 25 hours' time in service after the effective date of this Airworthiness Directive and thereafter, at intervals not to exceed 25 hours' time in service visually inspect the 1/4" bolts attaching the wheel flanges for broken bolts until compliance with the modification in Paragraph (a) above is accomplished. If indications of broken bolts exist modify wheels in accordance with Paragraph (a). (c) Upon completion of the modification in Paragraph (a), record compliance with this particular part of the Airworthiness Directive in the aircraft logbook. NOTE: Cessna Service Letter SE 74-8 or subsequent revisions pertains to the same subject. The McCauley wheels may additionally be marked with Cessna P/N's C163002-0102, -0103 or -0104. This amendment becomes effective June 24, 1974. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.