AD 70-08-02

final rule

Airworthiness Directives; Bell Model 47 Series Helicopters

AD Number
70-08-02
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 47 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47B Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47B3 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47D Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47D1 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47E Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-2 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-2A Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-2A-1 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-3 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-3B Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-3B-1 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-3B-2 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-3B-2A Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-4 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-4A Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-5 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-5A Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47H-1 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47J Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47J-2 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47J-2A Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47K Airworthiness Directives; Bell Model 47 Series Helicopters

Unsafe Condition

Failure from internal corrosion of tail rotor drive shaft assemblies with part numbers 47-644-172-3, 47-644-180-1, 47-644-180-5, 47-644-214-1, 47-644-186-1, 47-644-187-5, or 47-644-187-11.

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

Required Actions

Remove and replace the specified tail rotor drive shaft assemblies with the corresponding replacements listed in Bell Service Bulletin No. 47-145, Rev. B. Compliance must be completed no later than March 1, 1971, with replacement recommended at the next 1200-hour overhaul.

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

Compliance Time

no later than March 1, 1971

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

Affected Aircraft

Scotts-Bell 47 Inc Model 47, 47B, 47B3, 47D, 47D1, 47E, 47G, 47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1, and other models incorporating tail rotor drive shaft assemblies with part numbers 47-644-172-3, 47-644-180-1, 47-644-180-5, 47-644-214-1, 47-644-186-1, 47-644-187-5, or 47-644-187-11.

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
AD Final Rules - DRS_70-08-02.html
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AD Number:
70-08-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 47 Series Helicopters
Subject:
Tail Rotor Drive Shaft
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/01/1971
Make:
Scotts-Bell 47 Inc
Model:
47 | 47B | 47B3 | 47D | 47D1 | 47E | 47G | 47G-2 | 47G-2A | 47G-2A-1 | 47G-3 | 47G-3B | 47G-3B-1 | 4...Show more
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: 70-08-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1137

AD NUMBER:   70-08-02

SUBJECT HEADING:   Airworthiness Directives; Bell Model 47 Series Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective January 1, 1971.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
70-08-02 BELL: Amendment 39-968 as amended by Amendment 39-1137 Applies to all Bell Model 47 Series Helicopters and all other helicopters incorporating any of the following tail rotor drive shaft assemblies:



47-644-172-3	
47-644-180-1	47-644-186-1
47-644-180-5	47-644-187-5
47-644-214-1	47-644-187-11

Compliance required no later than March 1, 1971; however, replacement is recommended at the next 1200-hour overhaul.

To prevent failure from internal corrosion, remove and replace all tail rotor drive shaft assemblies installed on applicable helicopters as indicated below in accordance with the applicable maintenance and overhaul manual:



Remove
	Replace With

47-644-172-3
	47-644-172-9

47-644-180-1
	47-644-180-9

47-644-180-5
	47-644-180-11

47-644-214-1
	47-644-214-9

47-644-186-1
	47-644-186-5

47-644-187-5
	47-644-187-17

47-644-187-11
	47-644-187-19

(Bell Service Bulletin No. 47-145, Rev. B, dated March 26, 1970, pertains to this matter) Amendment 39-968 effective May 9, 1970.

This amendment, 39-1137, becomes effective January 1, 1971.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_70-08-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
70-08-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 47 Series Helicopters
Subject:
Tail Rotor Drive Shaft
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/01/1971
Make:
Scotts-Bell 47 Inc
Model:
47 | 47B | 47B3 | 47D | 47D1 | 47E | 47G | 47G-2 | 47G-2A | 47G-2A-1 | 47G-3 | 47G-3B | 47G-3B-1 | 4...Show more
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: 70-08-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1137

AD NUMBER:   70-08-02

SUBJECT HEADING:   Airworthiness Directives; Bell Model 47 Series Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective January 1, 1971.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
70-08-02 BELL: Amendment 39-968 as amended by Amendment 39-1137 Applies to all Bell Model 47 Series Helicopters and all other helicopters incorporating any of the following tail rotor drive shaft assemblies:



47-644-172-3	
47-644-180-1	47-644-186-1
47-644-180-5	47-644-187-5
47-644-214-1	47-644-187-11

Compliance required no later than March 1, 1971; however, replacement is recommended at the next 1200-hour overhaul.

To prevent failure from internal corrosion, remove and replace all tail rotor drive shaft assemblies installed on applicable helicopters as indicated below in accordance with the applicable maintenance and overhaul manual:



Remove
	Replace With

47-644-172-3
	47-644-172-9

47-644-180-1
	47-644-180-9

47-644-180-5
	47-644-180-11

47-644-214-1
	47-644-214-9

47-644-186-1
	47-644-186-5

47-644-187-5
	47-644-187-17

47-644-187-11
	47-644-187-19

(Bell Service Bulletin No. 47-145, Rev. B, dated March 26, 1970, pertains to this matter) Amendment 39-968 effective May 9, 1970.

This amendment, 39-1137, becomes effective January 1, 1971.

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.