AD 48-07-03

final rule

Airworthiness Directives; DOUGLAS DC-6

AD Number
48-07-03
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

Failure of door latch bolts, operating mechanisms, or locking mechanisms could result in unintended door opening or malfunction during pressurized flight, compromising structural integrity and safety.

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

Required Actions

Install new latch bolts with a notch for slow depressurization on specified doors; rework door operating and locking mechanisms to increase strength; install visual inspection plugs for lock bolt inspection; and install assist handles above main cabin door handles.

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

Compliance Time

September 15, 1948

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

Affected Aircraft

Douglas DC-6, DC-6A, DC-6B models with serial numbers 42854 Through 42896; 43000 Through 43024; 43035 through 43053; 43055 Through 43064; 43103 Through 43119; 43129 and 43132.

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

Federal Register Abstract

Door Rework

Applicability Source Text

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AD Final Rules - DRS_48-07-03.html
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AD Number:
48-07-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DOUGLAS DC-6
Subject:
Door Rework
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Superseded AD: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Superseded By: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: 48-07-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   48-07-03

SUBJECT HEADING:   Airworthiness Directives; DOUGLAS DC-6

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
48-07-03 DOUGLAS: Applies to DC-6 Serial Numbers 42854 Through 42896; 43000 Through 43024; 43035 through 43053; 43055 Through 43064; 43103 Through 43119; 43129 and 43132 (Note: Some of the Above Airplanes May Have Had Part of the Changes Installed Before Delivery From the Factory.)

Compliance required by September 15, 1948.

To provide safer and more satisfactory operation of all the doors, the following reworks must be accomplished:

(1) Install new latch bolts on all emergency exit doors, main passenger door, crew door, heater compartment door, and belly cargo compartment doors, to incorporate a notch which allows slow depressurization before the door can be fully opened in the event the handles are inadvertently turned toward the "OPEN" position while the cabin is pressurized.

(2) Rework the operating and locking mechanisms of the passenger, crew, and emergency exit doors, to increase their strength and prevent malfunctioning.

(3) Install visual inspection plugs in the passenger, crew, and emergency exit doors to allow individual inspection of each lock bolt to determine if it is properly locked.

(4) Install an assist handle above the main cabin door handle to prevent accidental grabbing of the inside door handle. (NOTE: Even in cases where the door handles have been changed so that the handle points downward when the door is closed and locked, it will still be necessary to install the assist handles.)


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_48-07-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
48-07-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; DOUGLAS DC-6
Subject:
Door Rework
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: 48-07-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   48-07-03

SUBJECT HEADING:   Airworthiness Directives; DOUGLAS DC-6

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
48-07-03 DOUGLAS: Applies to DC-6 Serial Numbers 42854 Through 42896; 43000 Through 43024; 43035 through 43053; 43055 Through 43064; 43103 Through 43119; 43129 and 43132 (Note: Some of the Above Airplanes May Have Had Part of the Changes Installed Before Delivery From the Factory.)

Compliance required by September 15, 1948.

To provide safer and more satisfactory operation of all the doors, the following reworks must be accomplished:

(1) Install new latch bolts on all emergency exit doors, main passenger door, crew door, heater compartment door, and belly cargo compartment doors, to incorporate a notch which allows slow depressurization before the door can be fully opened in the event the handles are inadvertently turned toward the "OPEN" position while the cabin is pressurized.

(2) Rework the operating and locking mechanisms of the passenger, crew, and emergency exit doors, to increase their strength and prevent malfunctioning.

(3) Install visual inspection plugs in the passenger, crew, and emergency exit doors to allow individual inspection of each lock bolt to determine if it is properly locked.

(4) Install an assist handle above the main cabin door handle to prevent accidental grabbing of the inside door handle. (NOTE: Even in cases where the door handles have been changed so that the handle points downward when the door is closed and locked, it will still be necessary to install the assist handles.)


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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