AD 59-06-02

final rule

Airworthiness Directives; DOUGLAS All Model DC-7 Series Aircraft

AD Number
59-06-02
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 The Boeing Company DC-7 Airworthiness Directives; DOUGLAS All Model DC-7 Series Aircraft
aircraft The Boeing Company DC-7B Airworthiness Directives; DOUGLAS All Model DC-7 Series Aircraft
aircraft The Boeing Company DC-7C Airworthiness Directives; DOUGLAS All Model DC-7 Series Aircraft

Unsafe Condition

The orifice check valve could malfunction due to contaminants in the hydraulic fluid (approximately 0.003-inch diameter), preventing full extension of the main landing gear.

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

Required Actions

Remove existing orifice check valve assemblies (P/N 4498423-503 or 4498423-5503) from each main landing gear actuating cylinder and replace with new assemblies (P/N 2230565-5-093 or P/N 4481262-5-093).

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

Compliance Time

by first block overhaul after receipt of parts but not later than December 1, 1959

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

Affected Aircraft

Douglas DC-7, DC-7B, DC-7C aircraft

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

Federal Register Abstract

Landing Gear Orifice Check Valve

Applicability Source Text

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AD Final Rules - DRS_59-06-02.html
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Details
AD Number:
59-06-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DOUGLAS All Model DC-7 Series Aircraft
Subject:
Landing Gear Orifice Check Valve
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company
Model:
DC-7 | DC-7B | DC-7C
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Superseded AD: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Superseded By: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: 59-06-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   59-06-02

SUBJECT HEADING:   Airworthiness Directives; DOUGLAS All Model DC-7 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
59-06-02 DOUGLAS: Applies to All Model DC-7 Series Aircraft.

Compliance required by first block overhaul after receipt of parts but not later than December 1, 1959.

Several instances have occurred wherein the green indicator light for one of the main landing gear failed to go on when the landing gears were extended. In one case, after landing, it was noted that the left gear downlatch was not fully engaged and the ground lock safety pin could not be installed. Subsequent investigation and laboratory tests revealed that the orifice check valve could malfunction due to contaminants in the hydraulic fluid of sufficient quantity and size (approximately 0.003-inch diameter) and thereby prevent full extension of the gear.

To overcome this difficulty, remove existing orifice check valve assembly, P/N 4498423-503 (Mineral Oil Aircraft), or P/N 4498423-5503 (Skydrol Aircraft), from each main landing gear actuating cylinder and replace with new orifice check valve assembly, P/N 2230565-5-093 (Mineral Oil Aircraft), or P/N 4481262-5-093 (Skydrol Aircraft). (Douglas Service Bulletin DC-7 No. 353 dated January 30, 1959, covers this same subject.)


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_59-06-02.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
59-06-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DOUGLAS All Model DC-7 Series Aircraft
Subject:
Landing Gear Orifice Check Valve
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company
Model:
DC-7 | DC-7B | DC-7C
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: 59-06-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   59-06-02

SUBJECT HEADING:   Airworthiness Directives; DOUGLAS All Model DC-7 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
59-06-02 DOUGLAS: Applies to All Model DC-7 Series Aircraft.

Compliance required by first block overhaul after receipt of parts but not later than December 1, 1959.

Several instances have occurred wherein the green indicator light for one of the main landing gear failed to go on when the landing gears were extended. In one case, after landing, it was noted that the left gear downlatch was not fully engaged and the ground lock safety pin could not be installed. Subsequent investigation and laboratory tests revealed that the orifice check valve could malfunction due to contaminants in the hydraulic fluid of sufficient quantity and size (approximately 0.003-inch diameter) and thereby prevent full extension of the gear.

To overcome this difficulty, remove existing orifice check valve assembly, P/N 4498423-503 (Mineral Oil Aircraft), or P/N 4498423-5503 (Skydrol Aircraft), from each main landing gear actuating cylinder and replace with new orifice check valve assembly, P/N 2230565-5-093 (Mineral Oil Aircraft), or P/N 4481262-5-093 (Skydrol Aircraft). (Douglas Service Bulletin DC-7 No. 353 dated January 30, 1959, covers this same subject.)


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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