AD 47-06-07

final rule

DOUGLAS Model DC3 Series Aircraft

AD Number
47-06-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC3-G102 DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3-G102A DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3-G103A DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3-G202A DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3A-S1C3G DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3A-S1CG DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3A-S4C4G DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3A-SC3G DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3A-SCG DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3C-R-1830-90C DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3C-S1C3G DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3C-S4C4G DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3C-SC3G DOUGLAS Model DC3 Series Aircraft
aircraft The Boeing Company DC3D-R-1830-90C DOUGLAS Model DC3 Series Aircraft

Unsafe Condition

Excessive wear of the aluminum conduit covering the fire extinguisher release cable causes increased trigger pull force exceeding 50 pounds in the CO2 fire extinguishing system.

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

Required Actions

Check the trigger pull force on the CO2 fire extinguishing system. Replace the aluminum conduit if the trigger pull exceeds 50 pounds due to conduit wear. Repeat the check at each specified inspection period until the aluminum conduit is replaced with stainless steel conduit.

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

Compliance Time

not later than the next periodic inspection, or in the case of scheduled air carrier aircraft, at the next major inspection

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

Affected Aircraft

The Boeing Company DC3 Series Aircraft including models DC3-G102, DC3-G102A, DC3-G103A, DC3-G202A, DC3A-S1C3G, DC3A-S1CG, DC3A-S4C4G, DC3A-SC3G, and others as listed.

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

Federal Register Abstract

Fire Extinguishing System

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_47-06-07.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
47-06-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
DOUGLAS Model DC3 Series Aircraft
Subject:
Fire Extinguishing System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company
Model:
DC3-G102 | DC3-G102A | DC3-G103A | DC3-G202A | DC3A-S1C3G | DC3A-S1CG | DC3A-S4C4G | DC3A-SC3G | DC3...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: 47-06-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-06-07

SUBJECT HEADING:   DOUGLAS Model DC3 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
47-06-07 DOUGLAS: (Was Service Note 12 of AD-618-3, Supplement 1; Service Note 15 of AD-669-3, Supplement 1.) Applies to All DC3 Series Aircraft.

To be accomplished not later than the next periodic inspection, or in the case of scheduled air carrier aircraft, at the next major inspection.

Check the pull necessary to trip the trigger on the CO2 fire extinguishing system. If the trigger pull exceeds 50 pounds due to wear of the aluminum conduit covering the fire extinguisher release cable, this conduit must be replaced immediately. This procedure is to be repeated at each specified inspection period until such time as the aluminum cable conduit is replaced by stainless steel conduit.

(Douglas Service Bulletin DC3 No. 246 dated November 22, 1946, covers this same subject.)


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_47-06-07.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
47-06-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
DOUGLAS Model DC3 Series Aircraft
Subject:
Fire Extinguishing System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company
Model:
DC3-G102 | DC3-G102A | DC3-G103A | DC3-G202A | DC3A-S1C3G | DC3A-S1CG | DC3A-S4C4G | DC3A-SC3G | DC3...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: 47-06-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-06-07

SUBJECT HEADING:   DOUGLAS Model DC3 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
47-06-07 DOUGLAS: (Was Service Note 12 of AD-618-3, Supplement 1; Service Note 15 of AD-669-3, Supplement 1.) Applies to All DC3 Series Aircraft.

To be accomplished not later than the next periodic inspection, or in the case of scheduled air carrier aircraft, at the next major inspection.

Check the pull necessary to trip the trigger on the CO2 fire extinguishing system. If the trigger pull exceeds 50 pounds due to wear of the aluminum conduit covering the fire extinguisher release cable, this conduit must be replaced immediately. This procedure is to be repeated at each specified inspection period until such time as the aluminum cable conduit is replaced by stainless steel conduit.

(Douglas Service Bulletin DC3 No. 246 dated November 22, 1946, covers this same subject.)


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.