AD 48-02-01

final rule

Airworthiness Directives; Bell Model 47B Series Airplanes

AD Number
48-02-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

Applicability

TypeManufacturerModelDetails
aircraft Scotts-Bell 47 Inc 47B Airworthiness Directives; Bell Model 47B Series Airplanes
aircraft Scotts-Bell 47 Inc 47B3 Airworthiness Directives; Bell Model 47B Series Airplanes

Unsafe Condition

Failure of the tail rotor drive shaft bearing hangers could result in loss of tail rotor control.

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

Required Actions

Reinforce the tail rotor drive shaft bearing hangers by riveting reinforcement plates (Bell P/N 47-267-001-152, -153, -154, -155, -156, and -157) with AN 470-AD3-4 rivets.

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

Compliance Time

before next 25 hours of operation

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

Affected Aircraft

Scotts-Bell 47 Inc Model 47B | 47B3, serial numbers through 78.

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

Federal Register Abstract

Tail Rotor Drive Shaft

Applicability Source Text

Show captured applicability text from the source AD
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Details
AD Number:
48-02-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 47B Series Airplanes
Subject:
Tail Rotor Drive Shaft
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Scotts-Bell 47 Inc
Model:
47B | 47B3
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Superseded AD: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Superseded By: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: 48-02-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   48-02-01

SUBJECT HEADING:   Airworthiness Directives; Bell Model 47B Series Airplanes

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
48-02-01 BELL: Applies to All 47B Series, Through Serial Number 78.

Compliance required before next 25 hours of operation.

Reinforce the tail rotor drive shaft bearing hangers by riveting reinforcement plates, Bell P/N 47-267-001-152, -153, -154, -155, -156, and -157, to the appropriate hangers with AN 470- AD3-4 rivets.

(Bell Service Bulletin 47C56 dated September 10, 1947, also covers this subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_48-02-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
48-02-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 47B Series Airplanes
Subject:
Tail Rotor Drive Shaft
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Scotts-Bell 47 Inc
Model:
47B | 47B3
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: 48-02-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   48-02-01

SUBJECT HEADING:   Airworthiness Directives; Bell Model 47B Series Airplanes

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
48-02-01 BELL: Applies to All 47B Series, Through Serial Number 78.

Compliance required before next 25 hours of operation.

Reinforce the tail rotor drive shaft bearing hangers by riveting reinforcement plates, Bell P/N 47-267-001-152, -153, -154, -155, -156, and -157, to the appropriate hangers with AN 470- AD3-4 rivets.

(Bell Service Bulletin 47C56 dated September 10, 1947, also covers this 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.