AD 47-25-03

final rule

Airworthiness Directives; Culver Models V-1 to V-130

AD Number
47-25-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

Applicability

TypeManufacturerModelDetails
aircraft Superior Aircraft Company V Airworthiness Directives; Culver Models V-1 to V-130

Unsafe Condition

The nose gear drag link connection may not have the 3/4-inch diameter tube butted against the aft fitting, which could lead to structural failure of the nose gear assembly.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect the nose gear drag link connection. Replace the link or rework it if the 3/4-inch diameter tube does not butt the aft fitting.

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 Models V-1 to V-130, inclusive, serial numbers V-1 to V-130.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Nose Gear Drag Link

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_47-25-03.html
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Details
AD Number:
47-25-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Culver Models V-1 to V-130
Subject:
Nose Gear Drag Link
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Superseded AD: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Superseded By: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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 47-25-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-25-03

SUBJECT HEADING:   Airworthiness Directives; Culver Models V-1 to V-130

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   47-25-03 CULVER: (Was Mandatory Note 5 of AD-778-2.) Applies Only to Serial Numbers V-1 to V-130, Inclusive.

Compliance required prior to August 15, 1947.

Inspect the nose gear drag link for the type of connection used to attach the aft fitting. The 3/4-inch diameter tube must butt the aft fitting. If otherwise, replace the link or rework accordingly.

(Culver Service Bulletin No. 1 covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_47-25-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
47-25-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Culver Models V-1 to V-130
Subject:
Nose Gear Drag Link
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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 47-25-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-25-03

SUBJECT HEADING:   Airworthiness Directives; Culver Models V-1 to V-130

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   47-25-03 CULVER: (Was Mandatory Note 5 of AD-778-2.) Applies Only to Serial Numbers V-1 to V-130, Inclusive.

Compliance required prior to August 15, 1947.

Inspect the nose gear drag link for the type of connection used to attach the aft fitting. The 3/4-inch diameter tube must butt the aft fitting. If otherwise, replace the link or rework accordingly.

(Culver Service Bulletin No. 1 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.