AD 46-04-01

final rule

Airworthiness Directives; Culver Models LCA and LFA Aircraft

AD Number
46-04-01
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 LCA Airworthiness Directives; Culver Models LCA and LFA Aircraft
aircraft Superior Aircraft Company LFA Airworthiness Directives; Culver Models LCA and LFA Aircraft

Unsafe Condition

Failure of the landing gear throttle stop mechanism could result in improper clearance during operation, leading to potential landing gear malfunction.

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

Required Actions

Inspect the landing gear throttle stop operation and mechanism immediately and after every 100 hours of operation. Install placard Culver Dwg. 7132 indicating 'Never unlock landing gear with throttle retarded below cruising setting'.

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

Compliance Time

immediately

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

Affected Aircraft

Superior Aircraft Company Models LCA and LFA Aircraft

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

Federal Register Abstract

Landing Gear Throttle Stop

Applicability Source Text

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Details
AD Number:
46-04-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Culver Models LCA and LFA Aircraft
Subject:
Landing Gear Throttle Stop
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Superior Aircraft Company
Model:
LCA | LFA
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Superseded AD: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Superseded By: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: 46-04-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   46-04-01

SUBJECT HEADING:   Airworthiness Directives; Culver Models LCA and LFA Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   46-04-01 CULVER (Was Service Note 7 of AD-730-2.) Applies to LCA and LFA Aircraft.

Inspect immediately and after every 100 hours of operation, the landing gear throttle stop operation and mechanism for proper clearance. Install placard (Culver Dwg. 7132) "Never unlock landing gear with throttle retarded below cruising setting."

(Culver Service Memorandum No. 22 dated October 26, 1945, covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_46-04-01.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
46-04-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Culver Models LCA and LFA Aircraft
Subject:
Landing Gear Throttle Stop
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Superior Aircraft Company
Model:
LCA | LFA
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: 46-04-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   46-04-01

SUBJECT HEADING:   Airworthiness Directives; Culver Models LCA and LFA Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   46-04-01 CULVER (Was Service Note 7 of AD-730-2.) Applies to LCA and LFA Aircraft.

Inspect immediately and after every 100 hours of operation, the landing gear throttle stop operation and mechanism for proper clearance. Install placard (Culver Dwg. 7132) "Never unlock landing gear with throttle retarded below cruising setting."

(Culver Service Memorandum No. 22 dated October 26, 1945, 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.