AD 47-25-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Superior Aircraft Company | V | Airworthiness Directives; Culver Model V Aircraft |
Unsafe Condition
The absence of wing fillets at the junction of the fuselage and wing trailing edge could lead to airflow separation and adverse aerodynamic effects.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install wing fillets, Culver P/N 10477, at the junction of fuselage and wing trailing edge using 6 x 1/4 PK screws (12) or equivalent.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
prior to August 15, 1947
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Culver Model V Aircraft, all serial numbers.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Wing Fillets
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_47-25-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 47-25-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Culver Model V Aircraft Subject: Wing Fillets Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Superior Aircraft Company Model: V Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 47-25-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 47-25-02 SUBJECT HEADING: Airworthiness Directives; Culver Model V Aircraft ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 47-25-02 CULVER: (Was Mandatory Note 4 of AD-778-2.) Applies to All Model V Aircraft. Compliance required prior to August 15, 1947. Install wing fillets, Culver P/N 10477, at junction of fuselage and wing trailing edge. Attach with 6 x 1/4 PK screws (12) or equivalent. (Culver Service Bulletin No. 13 covers this same subject.) FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_47-25-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 47-25-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Culver Model V Aircraft Subject: Wing Fillets Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Superior Aircraft Company Model: V 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: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 47-25-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 47-25-02 SUBJECT HEADING: Airworthiness Directives; Culver Model V Aircraft ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 47-25-02 CULVER: (Was Mandatory Note 4 of AD-778-2.) Applies to All Model V Aircraft. Compliance required prior to August 15, 1947. Install wing fillets, Culver P/N 10477, at junction of fuselage and wing trailing edge. Attach with 6 x 1/4 PK screws (12) or equivalent. (Culver Service Bulletin No. 13 covers this same subject.) 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.
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