AD 61-16-07

final rule

Airworthiness Directives; Sud Aviation Models All Alouette II SE 3130 Helicopters

AD Number
61-16-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: August 5, 1961
Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters SE 3130-Alouette II Airworthiness Directives; Sud Aviation Models All Alouette II SE 3130 Helicopters

Unsafe Condition

Cracks in the main rotor hubs P/N 3130. S12.20.001

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

Required Actions

Retire main rotor hubs P/N 3130. S12.20.001 from service upon accumulation of 660 hours' time in service. Hubs with 650 or more hours' time in service by August 5, 1961 must be retired within the next 10 hours' time in service.

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

Compliance Time

Effective August 5, 1961

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

Affected Aircraft

Sud Aviation Models All Alouette II SE 3130 Helicopters with main rotor hubs P/N 3130. S12.20.001

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

Federal Register Abstract

Main Rotor Hubs

Applicability Source Text

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AD Number:
61-16-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Sud Aviation Models All Alouette II SE 3130 Helicopters
Subject:
Main Rotor Hubs
Status:
Current
Citation:
Federal Register: August 5, 1961
Citation Publish Date:
08/05/1961
Effective Date:
08/05/1961
Make:
Airbus Helicopters
Model:
SE 3130-Alouette II
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Superseded AD: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Superseded By: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: 61-16-07
CITATION:   [Federal Register: August 5, 1961]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   61-16-07

SUBJECT HEADING:   Airworthiness Directives; Sud Aviation Models All Alouette II SE 3130 Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective August 5, 1961.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
61-16-07 SUD AVIATION: Amdt. 321 Part 507 Federal Register August 5, 1961. Applies to All Alouette II SE 3130 Helicopters.

Compliance required as indicated.

As a result of two cases of cracks in the main rotor hubs, all main rotor hubs P/N 3130. S12.20.001 must be retired from service upon accumulation of 660 hours' time in service, except that main rotor hubs which have already accumulated 650 or more hours' time in service on the effective date of this directive must be retired from service within the next 10 hours' time in service.

(Sud Aviation Helicopters Service Alouette II SE 3130 No. AL 12.11.204 covers this subject.)

This directive effective August 5, 1961.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_61-16-07.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
61-16-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Sud Aviation Models All Alouette II SE 3130 Helicopters
Subject:
Main Rotor Hubs
Status:
Current
Citation:
Federal Register: August 5, 1961
Citation Publish Date:
08/05/1961
Effective Date:
08/05/1961
Make:
Airbus Helicopters
Model:
SE 3130-Alouette II
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: 61-16-07
CITATION:   [Federal Register: August 5, 1961]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   61-16-07

SUBJECT HEADING:   Airworthiness Directives; Sud Aviation Models All Alouette II SE 3130 Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective August 5, 1961.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
61-16-07 SUD AVIATION: Amdt. 321 Part 507 Federal Register August 5, 1961. Applies to All Alouette II SE 3130 Helicopters.

Compliance required as indicated.

As a result of two cases of cracks in the main rotor hubs, all main rotor hubs P/N 3130. S12.20.001 must be retired from service upon accumulation of 660 hours' time in service, except that main rotor hubs which have already accumulated 650 or more hours' time in service on the effective date of this directive must be retired from service within the next 10 hours' time in service.

(Sud Aviation Helicopters Service Alouette II SE 3130 No. AL 12.11.204 covers this subject.)

This directive effective August 5, 1961.

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.