AD 48-02-04

final rule

Airworthiness Directives; DOUGLAS DC-6

AD Number
48-02-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-6 Airworthiness Directives; DOUGLAS DC-6
aircraft The Boeing Company DC-6A Airworthiness Directives; DOUGLAS DC-6
aircraft The Boeing Company DC-6B Airworthiness Directives; DOUGLAS DC-6

Unsafe Condition

Brake lining becoming wedged between brake disc and housing due to the present adjustment pin Goodyear P/N 511940-1 and spring plate Goodyear P/N 512139.

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

Required Actions

Replace the adjustment pin Goodyear P/N 511940-1 and spring plate Goodyear P/N 512139 with the single piece adjusting pin Goodyear P/N 9510744.

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

Compliance Time

next No. 3 inspection

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

Affected Aircraft

Douglas DC-6 Serial Numbers 42854 Through 42880; 42882 Through 42896; 43000 Through 43017; 43035 Through 43038; 43055; 43056; 43062, and 43063.

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

Federal Register Abstract

Brake Adjusting Pin Replacement

Applicability Source Text

Show captured applicability text from the source AD
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Details
AD Number:
48-02-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DOUGLAS DC-6
Subject:
Brake Adjusting Pin Replacement
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company
Model:
DC-6 | DC-6A | DC-6B
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Superseded AD: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Superseded By: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: 48-02-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   48-02-04

SUBJECT HEADING:   Airworthiness Directives; DOUGLAS DC-6


ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
48-02-04 DOUGLAS: Applies to DC-6 Serial Numbers 42854 Through 42880; 42882 Through 42896; 43000 Through 43017; 43035 Through 43038; 43055; 43056; 43062, and 43063.

Compliance required by the next No. 3 inspection.

To prevent the brake lining from becoming wedged between brake disc and housing, replace the present adjustment pin Goodyear P/N 511940-1 and spring plate Goodyear P/N 512139 by the single piece adjusting pin Goodyear P/N 9510744.

(Douglas Service Bulletin DC-6 No. 90 covers this same subject.)


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_48-02-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
48-02-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DOUGLAS DC-6
Subject:
Brake Adjusting Pin Replacement
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company
Model:
DC-6 | DC-6A | DC-6B
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: 48-02-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   48-02-04

SUBJECT HEADING:   Airworthiness Directives; DOUGLAS DC-6


ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
48-02-04 DOUGLAS: Applies to DC-6 Serial Numbers 42854 Through 42880; 42882 Through 42896; 43000 Through 43017; 43035 Through 43038; 43055; 43056; 43062, and 43063.

Compliance required by the next No. 3 inspection.

To prevent the brake lining from becoming wedged between brake disc and housing, replace the present adjustment pin Goodyear P/N 511940-1 and spring plate Goodyear P/N 512139 by the single piece adjusting pin Goodyear P/N 9510744.

(Douglas Service Bulletin DC-6 No. 90 covers this same subject.)


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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