AD 56-08-01

final rule

CURTISS Models C632S, C634D and C634S Propellers

AD Number
56-08-01
Status
final_rule
Effective Date
Product Category
propeller
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft Curtiss-Wright Corporation C632S CURTISS Models C632S, C634D and C634S Propellers
aircraft Curtiss-Wright Corporation C634D CURTISS Models C632S, C634D and C634S Propellers
aircraft Curtiss-Wright Corporation C634S CURTISS Models C632S, C634D and C634S Propellers
propeller Curtiss-Wright Corporation C632S CURTISS Models C632S, C634D and C634S Propellers
propeller Curtiss-Wright Corporation C634D CURTISS Models C632S, C634D and C634S Propellers
propeller Curtiss-Wright Corporation C634S CURTISS Models C632S, C634D and C634S Propellers

Unsafe Condition

Failure or malfunction of low pitch limit switches P/N 110425 and P/N 154592 beyond normal service wear could result in improper pitch control or loss of pitch limitation function.

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

Required Actions

Replace low pitch limit switches P/N 110425 at intervals not exceeding specified flight hours per aircraft type. Disassemble and visually inspect low pitch limit switches P/N 154592 at the same intervals, checking for proper operation and mechanical/electrical condition; replace parts or assembly if adverse conditions are found.

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

Compliance Time

Compliance required as indicated.

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

Affected Aircraft

Curtiss-Wright Corporation Models C632S, C634D, and C634S Propellers installed on Douglas DC-6, Lockheed 749, Lockheed 1049, and Convair 240 Series Aircraft.

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

Federal Register Abstract

Pitch Limit Switches

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_56-08-01.html
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AD Number:
56-08-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
CURTISS Models C632S, C634D and C634S Propellers
Subject:
Pitch Limit Switches
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Curtiss-Wright Corporation
Model:
C632S | C634D | C634S
Product Type:
Propeller
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 56-08-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   56-08-01

SUBJECT HEADING:   CURTISS Models C632S, C634D and C634S Propellers

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
56-08-01 CURTISS: Applies to All Models C632S, C634D and C634S Propellers.

Compliance required as indicated.

I. Replace low pitch limit switches P/N 110425 at not more than the following intervals:

Douglas DC-6 Series Aircraft 3,500 Hours

Lockheed 749 Series Aircraft 3,500 Hours

Lockheed 1049 Series Aircraft 3,500 Hours

Convair 240 Series Aircraft 1,000 Hours

(Curtiss Service Bulletin No. 52 dated December 29, 1949, and appropriate service manuals also cover these recommendations.)

II. Disassemble and visually inspect low pitch limit switches P/N 154592 at not more than the same intervals. Inspect for proper switch operation and for mechanical and electrical condition. Failure or malfunction other than normal service wear shall be cause for replacement of switch parts or of the assembly. Switches not revealing adverse conditions may be returned to service.

This supersedes Section III of AD 53-05-01.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_56-08-01.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
56-08-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
CURTISS Models C632S, C634D and C634S Propellers
Subject:
Pitch Limit Switches
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Curtiss-Wright Corporation
Model:
C632S | C634D | C634S
Product Type:
Propeller
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 56-08-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   56-08-01

SUBJECT HEADING:   CURTISS Models C632S, C634D and C634S Propellers

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
56-08-01 CURTISS: Applies to All Models C632S, C634D and C634S Propellers.

Compliance required as indicated.

I. Replace low pitch limit switches P/N 110425 at not more than the following intervals:

Douglas DC-6 Series Aircraft 3,500 Hours

Lockheed 749 Series Aircraft 3,500 Hours

Lockheed 1049 Series Aircraft 3,500 Hours

Convair 240 Series Aircraft 1,000 Hours

(Curtiss Service Bulletin No. 52 dated December 29, 1949, and appropriate service manuals also cover these recommendations.)

II. Disassemble and visually inspect low pitch limit switches P/N 154592 at not more than the same intervals. Inspect for proper switch operation and for mechanical and electrical condition. Failure or malfunction other than normal service wear shall be cause for replacement of switch parts or of the assembly. Switches not revealing adverse conditions may be returned to service.

This supersedes Section III of AD 53-05-01.

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.