AD 56-15-03

final rule

Airworthiness Directives; Bell Model 47H1 Helicopters

AD Number
56-15-03
Status
final_rule
Effective Date
Product Category
aircraft
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 Scotts-Bell 47 Inc 47H-1 Airworthiness Directives; Bell Model 47H1 Helicopters

Unsafe Condition

Failure of a control cable of the synchronized elevator control system can result in loss of control of the helicopter.

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

Required Actions

Installation of the fail safe synchronized elevator centering spring, Bell Kit No. 47-2573-1, is mandatory to provide a self-centering device for the synchronized elevator.

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

Compliance Time

as soon as possible but not later than August 15, 1956

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

Affected Aircraft

Bell Model 47H1 Helicopters, Serial Numbers 1347 Through 1349 and 1351 Through 1371

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

Federal Register Abstract

Elevator Control System

Applicability Source Text

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Details
AD Number:
56-15-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 47H1 Helicopters
Subject:
Elevator Control System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Scotts-Bell 47 Inc
Model:
47H-1
Product Type:
Aircraft
Product Subtype:
Rotorcraft
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 56-15-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   56-15-03

SUBJECT HEADING:   Airworthiness Directives; Bell Model 47H1 Helicopters

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
56-15-03 BELL: Applies to Model 47H1 Helicopters, Serial Numbers 1347 Through 1349 and 1351 Through 1371.
Compliance required as soon as possible but not later than August 15, 1956.

Failure of a control cable of the synchronized elevator control system can result in loss of control of the helicopter. Installation of the fail safe synchronized elevator centering spring, Bell Kit No. 47-2573-1, is mandatory and provides a self-centering device for the synchronized elevator so that control of the helicopter can be maintained in event of elevator control cable failure.

(Bell Mandatory Service Bulletin No. 109 dated June 15, 1956, covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_56-15-03.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
56-15-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 47H1 Helicopters
Subject:
Elevator Control System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Scotts-Bell 47 Inc
Model:
47H-1
Product Type:
Aircraft
Product Subtype:
Rotorcraft
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 56-15-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   56-15-03

SUBJECT HEADING:   Airworthiness Directives; Bell Model 47H1 Helicopters

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
56-15-03 BELL: Applies to Model 47H1 Helicopters, Serial Numbers 1347 Through 1349 and 1351 Through 1371.
Compliance required as soon as possible but not later than August 15, 1956.

Failure of a control cable of the synchronized elevator control system can result in loss of control of the helicopter. Installation of the fail safe synchronized elevator centering spring, Bell Kit No. 47-2573-1, is mandatory and provides a self-centering device for the synchronized elevator so that control of the helicopter can be maintained in event of elevator control cable failure.

(Bell Mandatory Service Bulletin No. 109 dated June 15, 1956, 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.