AD 57-03-02

final rule

Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series

AD Number
57-03-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company | Lockheed Aircraft Corporation DC-7 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation DC-7B Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation DC-7C Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 1049-54 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 1049B-55 (Navy R7V-1) Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 1049C-55 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 1049D-55 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 1049E-55 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 1049F-55 (USAF C-121C) Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 1049G-82 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 1049H-82 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 149-46 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 1649A-98 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 49-46 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 649-79 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 649A-79 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 749-79 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
aircraft The Boeing Company | Lockheed Aircraft Corporation 749A-79 Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series

Unsafe Condition

The fuel inlet strainer and other parts in the engine master control can become clogged with ice due to entrained water in the fuel freezing on the screen, causing a loss of power on all engines simultaneously.

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

Required Actions

Install a screen with a bypass valve (Bendix P/N 366204) in replacement of the screen without a bypass valve, as per Bendix Service Bulletin No. 797.

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

Compliance Time

not later than December 1, 1957

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

Affected Aircraft

Lockheed Constellation Series Airplanes and Douglas DC-7 Series Airplanes with Wright Engines.

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

Federal Register Abstract

Fuel Strainer Screen

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_57-03-02.html
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Details
AD Number:
57-03-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
Subject:
Fuel Strainer Screen
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company | Lockheed Aircraft Corporation
Model:
DC-7 | DC-7B | DC-7C | 1049-54 | 1049B-55 (Navy R7V-1) | 1049C-55 | 1049D-55 | 1049E-55 | 1049F-55 (...Show more
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: 57-03-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   57-03-02

SUBJECT HEADING:   Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
57-03-02 DOUGLAS AND LOCKHEED: Applies to Lockheed Constellation Series Airplanes and Douglas DC-7 Series Airplanes With Wright Engines.

Compliance required not later than December 1, 1957.

Under certain cold weather operating conditions it is possible for the fuel inlet strainer and other parts in the engine master control to become clogged with ice as a result of entrained water in the fuel freezing on the screen. This has caused a loss of power on all engines simultaneously.

To relieve strainer icing, a screen having a bypass valve Bendix P/N 366204 should be installed in replacement of the screen not having a bypass valve. Bendix Service Bulletin No. 797 covers this subject. It should be noted that the incorporation of the screen with bypass will not positively prevent power loss from fuel ice; therefore, work is continuing to develop a means to protect other portions of the master control downstream of the inlet strainer. If necessary, a supplement to this note will be published when additional information becomes available.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_57-03-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
57-03-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series
Subject:
Fuel Strainer Screen
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company | Lockheed Aircraft Corporation
Model:
DC-7 | DC-7B | DC-7C | 1049-54 | 1049B-55 (Navy R7V-1) | 1049C-55 | 1049D-55 | 1049E-55 | 1049F-55 (...Show more
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: 57-03-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   57-03-02

SUBJECT HEADING:   Airworthiness Directives; DOUGLAS DC-7 Series and LOCKHEED Constellation Series

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
57-03-02 DOUGLAS AND LOCKHEED: Applies to Lockheed Constellation Series Airplanes and Douglas DC-7 Series Airplanes With Wright Engines.

Compliance required not later than December 1, 1957.

Under certain cold weather operating conditions it is possible for the fuel inlet strainer and other parts in the engine master control to become clogged with ice as a result of entrained water in the fuel freezing on the screen. This has caused a loss of power on all engines simultaneously.

To relieve strainer icing, a screen having a bypass valve Bendix P/N 366204 should be installed in replacement of the screen not having a bypass valve. Bendix Service Bulletin No. 797 covers this subject. It should be noted that the incorporation of the screen with bypass will not positively prevent power loss from fuel ice; therefore, work is continuing to develop a means to protect other portions of the master control downstream of the inlet strainer. If necessary, a supplement to this note will be published when additional information becomes available.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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