AD 44-04-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Rankin, Joe | CP-65 | Joe Rankin Model CP-65 Airplanes |
Unsafe Condition
The wings may separate from the airplane during flight due to failure of the wing-to-fuselage attachment bolts.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the wing-to-fuselage attachment bolts for proper installation and torque. Replace any bolts that do not meet the specified torque requirements.
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Compliance Time
within 100 flight hours after the effective date of this AD
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Affected Aircraft
Joe Rankin Model CP-65 airplanes, all serial numbers
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Federal Register Abstract
Wings
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - 44-04-03.pdf Copy URL Document Versions Feedback DetailsAttachments/Public Comments AD Number: 44-04-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Joe Rankin Model CP-65 Airplanes Subject: Wings Status: Current Citation: Citation Publish Date: Effective Date: Make: Rankin, Joe Model: CP-65 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Originally posted to RGL on 9/6/2012 Automatic Zoom Actual Size Page Fit Page Width 50% 75% 100% 125% 150% 200% 300% 400% 125% of 2
Document Text
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AD Final Rules - 44-04-03.pdf Copy URL Document Versions Feedback DetailsAttachments/Public Comments AD Number: 44-04-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Joe Rankin Model CP-65 Airplanes Subject: Wings Status: Current Citation: Citation Publish Date: Effective Date: Make: Rankin, Joe Model: CP-65 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Originally posted to RGL on 9/6/2012 Automatic Zoom Actual Size Page Fit Page Width 50% 75% 100% 125% 150% 200% 300% 400% 125% of 2
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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