AD 55-15-05

final rule

Airworthiness Directives; DOUGLAS All DC-7 Aircraft

AD Number
55-15-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft propeller assembly
Problem area Propeller

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-7 Airworthiness Directives; DOUGLAS All DC-7 Aircraft
aircraft The Boeing Company DC-7B Airworthiness Directives; DOUGLAS All DC-7 Aircraft
aircraft The Boeing Company DC-7C Airworthiness Directives; DOUGLAS All DC-7 Aircraft

Unsafe Condition

Propeller feathering lines forward of the firewall in zone 2 may fail due to fire exposure, compromising the integrity of the propeller feathering system during a powerplant fire.

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

Required Actions

Replace existing propeller feathering lines forward of the firewall in zone 2 with fireproof/fire resistant lines and hose assemblies per Aeroquip Drawings 304005-10S-46 and Douglas P/N 3500614-2. Install Aeroquip 304 protective sleeves or acceptable alternatives as specified.

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

Compliance Time

By first scheduled engine change after November 1, 1955, but not later than November 1, 1956.

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 with serial numbers below 486 equipped with Hamilton Standard propellers.

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

Federal Register Abstract

Propeller Feathering Lines

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_55-15-05.html
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AD Number:
55-15-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DOUGLAS All DC-7 Aircraft
Subject:
Propeller Feathering Lines
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Superseded AD: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Superseded By: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: 55-15-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   55-15-05

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

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
55-15-05 DOUGLAS: Applies to All DC-7 Aircraft Below Fuselage No. 486 Equipped With Hamilton Standard Propellers.

Compliance required by first scheduled engine change after November 1, 1955, but not later than November 1, 1956.

To increase the integrity of the propeller feathering system in the event of a powerplant fire, all existing propeller feathering lines located forward of the firewall in zone 2 must be replaced with lines and flexible hose assemblies which will meet current fireproof and fire resistant requirements.

(a) Install Aeroquip 304 protective sleeves on the propeller feathering line forward of the feathering pump, in accordance with Aeroquip Drawing 304005-10S-46. Resistoflex SSFR-3800-10 hose assembly and Aeroquip 309009-10S hose assembly are also considered acceptable for this application.

(b) Remove the existing short 304 sleeves from the feathering pump supply line between the oil tank and feathering pump and install a fireproof cover, Douglas P/N 3500614-2. Aeroquip 601000 hose assembly equipped with Aeroquip 304 full-length protective sleeve, or Aeroquip 680-16S hose assembly equipped with Aeroquip 304 short sleeves covering the end fittings are also considered acceptable for this application.

(Douglas Service Bulletin DC-7 No. 74 dated July 19, 1955, covers this same subject.)


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_55-15-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
55-15-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DOUGLAS All DC-7 Aircraft
Subject:
Propeller Feathering Lines
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: 55-15-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   55-15-05

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

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
55-15-05 DOUGLAS: Applies to All DC-7 Aircraft Below Fuselage No. 486 Equipped With Hamilton Standard Propellers.

Compliance required by first scheduled engine change after November 1, 1955, but not later than November 1, 1956.

To increase the integrity of the propeller feathering system in the event of a powerplant fire, all existing propeller feathering lines located forward of the firewall in zone 2 must be replaced with lines and flexible hose assemblies which will meet current fireproof and fire resistant requirements.

(a) Install Aeroquip 304 protective sleeves on the propeller feathering line forward of the feathering pump, in accordance with Aeroquip Drawing 304005-10S-46. Resistoflex SSFR-3800-10 hose assembly and Aeroquip 309009-10S hose assembly are also considered acceptable for this application.

(b) Remove the existing short 304 sleeves from the feathering pump supply line between the oil tank and feathering pump and install a fireproof cover, Douglas P/N 3500614-2. Aeroquip 601000 hose assembly equipped with Aeroquip 304 full-length protective sleeve, or Aeroquip 680-16S hose assembly equipped with Aeroquip 304 short sleeves covering the end fittings are also considered acceptable for this application.

(Douglas Service Bulletin DC-7 No. 74 dated July 19, 1955, covers this same subject.)


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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