AD 46-13-01

final rule

Airworthiness Directives; Lockheed Model 18 Series Aircraft

AD Number
46-13-01
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 Lockheed Aircraft Corporation 18 Airworthiness Directives; Lockheed Model 18 Series Aircraft

Unsafe Condition

Longer ferrules on landing gear actuating cylinder flexible hose P/N 55252-3 may cause hose damage by the landing gear scissors.

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

Required Actions

Compare ferrule lengths when replacing hose P/N 55252-3. Insert an elbow between the hose and cylinder aft port if longer ferrules are found to prevent hose damage.

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

Affected Aircraft

Lockheed Model 18 Series Aircraft, all serial numbers.

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

Federal Register Abstract

Landing Gear Hose Ferrules

Applicability Source Text

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AD Final Rules - DRS_46-13-01.html
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Details
AD Number:
46-13-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Lockheed Model 18 Series Aircraft
Subject:
Landing Gear Hose Ferrules
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Lockheed Aircraft Corporation
Model:
18
Product Type:
Aircraft
Product Subtype:
Large 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Superseded AD: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Superseded By: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: 46-13-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   46-13-01

SUBJECT HEADING:   Airworthiness Directives; Lockheed Model 18 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
46-13-01 LOCKHEED: (Was Service Note 2 of AD-723-2.) Applies to All Model 18 Aircraft.
When replacing the landing gear actuating cylinder flexible hose, P/N 55252-3, the length of ferrules should be compared. If longer ferrules are found on the new hoses, an elbow should be inserted between the hose and the cylinder aft port, to prevent possible damage to the hose by the landing gear scissors. (Lockheed Service Letter No. 18-28, dated June 15, 1945, revised December 10, 1945, covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_46-13-01.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
46-13-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Lockheed Model 18 Series Aircraft
Subject:
Landing Gear Hose Ferrules
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Lockheed Aircraft Corporation
Model:
18
Product Type:
Aircraft
Product Subtype:
Large 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: 46-13-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   46-13-01

SUBJECT HEADING:   Airworthiness Directives; Lockheed Model 18 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
46-13-01 LOCKHEED: (Was Service Note 2 of AD-723-2.) Applies to All Model 18 Aircraft.
When replacing the landing gear actuating cylinder flexible hose, P/N 55252-3, the length of ferrules should be compared. If longer ferrules are found on the new hoses, an elbow should be inserted between the hose and the cylinder aft port, to prevent possible damage to the hose by the landing gear scissors. (Lockheed Service Letter No. 18-28, dated June 15, 1945, revised December 10, 1945, covers this same subject.)

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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