AD 54-24-01

final rule

Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters

AD Number
54-24-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Scotts-Bell 47 Inc 47B Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters
aircraft Scotts-Bell 47 Inc 47B3 Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters
aircraft Scotts-Bell 47 Inc 47D Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters
aircraft Scotts-Bell 47 Inc 47D1 Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters
aircraft Scotts-Bell 47 Inc 47E Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters
aircraft Scotts-Bell 47 Inc 47G Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters

Unsafe Condition

Improper installation of the antitorque pedal assembly for dual controls could lead to loss of antitorque control.

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

Required Actions

Install two stop assemblies, part number 47-722-165-1, to preclude improper installation of the antitorque pedal assembly.

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

Compliance Time

next 25-hour inspection

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

Affected Aircraft

Bell Model 47B, 47B3, 47D, 47D1, 47E, and 47G helicopters except serial numbers 1286, 1287, 1294, 1295, and 1299 and subsequent.

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

Federal Register Abstract

Antitorque Pedal Stops

Applicability Source Text

Show captured applicability text from the source AD
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AD Number:
54-24-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters
Subject:
Antitorque Pedal Stops
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Scotts-Bell 47 Inc
Model:
47B | 47B3 | 47D | 47D1 | 47E | 47G
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Superseded AD: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Superseded By: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: 54-24-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   54-24-01

SUBJECT HEADING:   Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
54-24-01 BELL: Applies to All Models 47B, 47B3, 47D, 47D1, 47E, 47G Except 47G Serial Numbers 1286, 1287, 1294, 1295, and 1299 and Subsequent.

Compliance required no later than next 25-hour inspection.

In order to preclude improper installation of antitorque pedal assembly for dual controls, install two stop assemblies, P/N 47-722-165-1.

(Bell Mandatory Service Bulletin No. 98 dated October 29, 1954, covers this same subject and outlines the details for the installation.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_54-24-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
54-24-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters
Subject:
Antitorque Pedal Stops
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Scotts-Bell 47 Inc
Model:
47B | 47B3 | 47D | 47D1 | 47E | 47G
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: 54-24-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   54-24-01

SUBJECT HEADING:   Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
54-24-01 BELL: Applies to All Models 47B, 47B3, 47D, 47D1, 47E, 47G Except 47G Serial Numbers 1286, 1287, 1294, 1295, and 1299 and Subsequent.

Compliance required no later than next 25-hour inspection.

In order to preclude improper installation of antitorque pedal assembly for dual controls, install two stop assemblies, P/N 47-722-165-1.

(Bell Mandatory Service Bulletin No. 98 dated October 29, 1954, covers this same subject and outlines the details for the installation.)

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.