AD 59-06-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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.
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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).
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Compliance Time
by first block overhaul after receipt of parts but not later than December 1, 1959
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Affected Aircraft
Douglas DC-7, DC-7B, DC-7C aircraft
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Federal Register Abstract
Landing Gear Orifice Check Valve
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_59-06-02.html Copy URL 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The Boeing Company Model: DC-7 | DC-7B | DC-7C Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 59-06-02 CITATION: This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:
Document Text
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AD Final Rules - DRS_59-06-02.html Copy URL 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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