AD 47-51-04

final rule

Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Airplanes

AD Number
47-51-04
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 Airlift International, Inc. | Curtiss-Wright Corporation | Flying Tiger Line, Inc. | L. B. Smith Aircraft Corporation | Skyways International Trading and Transport Co. | Tempo Design Corporation C-46A Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Airplanes
aircraft Airlift International, Inc. | Curtiss-Wright Corporation | Flying Tiger Line, Inc. | L. B. Smith Aircraft Corporation | Skyways International Trading and Transport Co. | Tempo Design Corporation C-46D Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Airplanes
aircraft Airlift International, Inc. | Curtiss-Wright Corporation | Flying Tiger Line, Inc. | L. B. Smith Aircraft Corporation | Skyways International Trading and Transport Co. | Tempo Design Corporation C-46F Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Airplanes
aircraft Airlift International, Inc. | Curtiss-Wright Corporation | Flying Tiger Line, Inc. | L. B. Smith Aircraft Corporation | Skyways International Trading and Transport Co. | Tempo Design Corporation C-46R Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Airplanes
aircraft Airlift International, Inc. | Curtiss-Wright Corporation | Flying Tiger Line, Inc. | L. B. Smith Aircraft Corporation | Skyways International Trading and Transport Co. | Tempo Design Corporation C-46E Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Airplanes
aircraft Airlift International, Inc. | Curtiss-Wright Corporation | Flying Tiger Line, Inc. | L. B. Smith Aircraft Corporation | Skyways International Trading and Transport Co. | Tempo Design Corporation C-46/CW20-T Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Airplanes
aircraft Airlift International, Inc. | Curtiss-Wright Corporation | Flying Tiger Line, Inc. | L. B. Smith Aircraft Corporation | Skyways International Trading and Transport Co. | Tempo Design Corporation Super C-46/CW20-T Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Airplanes

Unsafe Condition

Failure of the propeller flexible feathering line due to disintegration and deterioration of the flexible propeller feathering hose and lagging material.

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

Required Actions

Inspect the flexible propeller feathering hose and lagging material for disintegration and deterioration, replace the hose if deteriorated, install an antiheat shield with fabricated clamps as per Figure 1, and check propeller feathering system operation after installation.

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

Compliance Time

March 1, 1948

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

Affected Aircraft

CURTISS-WRIGHT Model C-46 Series Airplanes incorporating Hamilton Standard Propellers, including models C-46A, C-46D, C-46F, C-46R, C-46E, C-46/CW20-T, and Super C-46/CW20-T.

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

Federal Register Abstract

Propeller Antiheat Shield

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_47-51-04.html
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AD Number:
47-51-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Airplanes
Subject:
Propeller Antiheat Shield
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Airlift International, Inc. | Curtiss-Wright Corporation | Flying Tiger Line, Inc. | L. B. Smith Air...Show more
Model:
C-46A | C-46D | C-46F | C-46R | C-46E | C-46/CW20-T | Super C-46/CW20-T
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: 47-51-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-51-04

SUBJECT HEADING:   Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Airplanes


ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
47-51-04 CURTISS-WRIGHT Applies to All C-46 Series Airplanes Incorporating Hamilton Standard Propellers.

Compliance required by March 1, 1948.

To eliminate failure of the propeller flexible feathering line, an antiheat shield shall be installed in accordance with the following instructions:

(a) Remove the engine cowling adjacent to the propeller feathering line and inspect the flexible propeller feathering hose and lagging material (if installed) for disintegration and deterioration. Replace hose if deterioration is evident.

(b) Fabricate the antiheat shield and attaching clamps as shown in Figure 1.

(c) Place antiheat shield over the flexible hose and mount the shield on the engine mount by use of the clamps shown in Figure 1. The shield should be centered over the flexible hose. It may be necessary to rebend the metal feathering line slightly to achieve proper centering.

(d) Upon completion of installation, check operation of propeller feathering system.

(The above information is also contained in Army Air Forces Technical Order 01-25L- 105 dated April 2, 1947. Copies of this Technical Order are not available for distribution by the FAA.)





FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_47-51-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
47-51-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Airplanes
Subject:
Propeller Antiheat Shield
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Airlift International, Inc. | Curtiss-Wright Corporation | Flying Tiger Line, Inc. | L. B. Smith Air...Show more
Model:
C-46A | C-46D | C-46F | C-46R | C-46E | C-46/CW20-T | Super C-46/CW20-T
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: 47-51-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-51-04

SUBJECT HEADING:   Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Airplanes


ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
47-51-04 CURTISS-WRIGHT Applies to All C-46 Series Airplanes Incorporating Hamilton Standard Propellers.

Compliance required by March 1, 1948.

To eliminate failure of the propeller flexible feathering line, an antiheat shield shall be installed in accordance with the following instructions:

(a) Remove the engine cowling adjacent to the propeller feathering line and inspect the flexible propeller feathering hose and lagging material (if installed) for disintegration and deterioration. Replace hose if deterioration is evident.

(b) Fabricate the antiheat shield and attaching clamps as shown in Figure 1.

(c) Place antiheat shield over the flexible hose and mount the shield on the engine mount by use of the clamps shown in Figure 1. The shield should be centered over the flexible hose. It may be necessary to rebend the metal feathering line slightly to achieve proper centering.

(d) Upon completion of installation, check operation of propeller feathering system.

(The above information is also contained in Army Air Forces Technical Order 01-25L- 105 dated April 2, 1947. Copies of this Technical Order are not available for distribution by the FAA.)





FOOTER:

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Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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