AD 75-24-14

final rule

Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters

AD Number
75-24-14
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 Airbus Helicopters SA 3180-Alouette Astazou Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters
aircraft Airbus Helicopters SA 318B-Alouette Astazou Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters
aircraft Airbus Helicopters SA 318C-Alouette Astazou Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters
aircraft Airbus Helicopters SA.315B Alouette III Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters
aircraft Airbus Helicopters SA.316B Alouette III Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters
aircraft Airbus Helicopters SA.316C Alouette III Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters
aircraft Airbus Helicopters SA.319B Alouette III Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters
aircraft Airbus Helicopters SE 3130-Alouette II Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters
aircraft Airbus Helicopters SE 313B-Alouette II Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters
aircraft Airbus Helicopters SE.3160 Alouette III Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters

Unsafe Condition

Excessive vibration or ground resonance due to main rotor hydraulic dampers P/N 3130S.13.60.000.

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

Required Actions

Modify and reidentify main rotor hydraulic dampers P/N 3130S.13.60.000 in accordance with specified service bulletins. Remove existing placards for certain models and install a temporary placard indicating maximum density altitude of 8200 feet.

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

Compliance Time

Prior to October 30, 1975, and prior to further flight.

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

Affected Aircraft

Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA-316C, SA-3180, SA-318B, SA-318C, and SA-319B equipped with main rotor hydraulic dampers P/N 3130S.13.60.000.

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

Federal Register Abstract

Excessive Vibration

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_75-24-14.html
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AD Number:
75-24-14
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-31...Show more
Subject:
Excessive Vibration
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/30/1975
Make:
Airbus Helicopters
Model:
SA 3180-Alouette Astazou | SA 318B-Alouette Astazou | SA 318C-Alouette Astazou | SA.315B Alouette II...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: 75-24-14
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2440

AD NUMBER:   75-24-14

SUBJECT HEADING:   Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective October 30, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-24-14 SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE: Amendment 39- 2440. Applies to Alouette Helicopters SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B equipped with main rotor hydraulic dampers P/N 3130S.13.60.000.

Compliance is required as indicated, unless already accomplished.

To prevent excessive vibration or ground resonance, accomplish the following:

(a) Prior to October 30, 1975, modify and reidentify main rotor hydraulic dampers P/N 3130S.13.60.000 in accordance with subparagraphs 2B(1), 2B(2), and 2(c) of Lama Service Bulletin No. 65.20 dated July 4, 1975, for Model SA-315B and Alouette Service Bulletin No. 65.107 dated July 4, 1975, for the other designated models, or equivalents approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region, c/o American Embassy, APO New York, New York, N.Y. 09667.

(b) Prior to further flight, for Models SA-3160, SA-316B, SA-316C, and SA-319B, remove the placard required by AD 75-17-30, if installed, and install a temporary placard on the instrument panel, in full view of the pilot, reading as follows: "Maximum density altitude: 8200 feet". Temporary placard may be removed upon accomplishment of paragraph (a) of this AD.

(Alouette Service Bulletin No. 01.39 also refers to paragraph (b) of this AD).

This AD supersedes Amendment 39-2335 (40 FR 33010), AD 75-17-30.

This amendment is effective upon publication in the FEDERAL REGISTER as to all persons except those persons to whom it was made immediately effective by telegram dated September 30, 1975, which contained this amendment.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-24-14.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-24-14
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-31...Show more
Subject:
Excessive Vibration
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/30/1975
Make:
Airbus Helicopters
Model:
SA 3180-Alouette Astazou | SA 318B-Alouette Astazou | SA 318C-Alouette Astazou | SA.315B Alouette II...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: 75-24-14
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2440

AD NUMBER:   75-24-14

SUBJECT HEADING:   Airworthiness Directives; Societe Nationale Industrielle Aerospatiale Models SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective October 30, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-24-14 SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE: Amendment 39- 2440. Applies to Alouette Helicopters SE-3130, SE-313B, SA-315B, SE-3160, SA-316B, SA- 316C, SA-3180, SA-318B, SA-318C, and SA-319B equipped with main rotor hydraulic dampers P/N 3130S.13.60.000.

Compliance is required as indicated, unless already accomplished.

To prevent excessive vibration or ground resonance, accomplish the following:

(a) Prior to October 30, 1975, modify and reidentify main rotor hydraulic dampers P/N 3130S.13.60.000 in accordance with subparagraphs 2B(1), 2B(2), and 2(c) of Lama Service Bulletin No. 65.20 dated July 4, 1975, for Model SA-315B and Alouette Service Bulletin No. 65.107 dated July 4, 1975, for the other designated models, or equivalents approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region, c/o American Embassy, APO New York, New York, N.Y. 09667.

(b) Prior to further flight, for Models SA-3160, SA-316B, SA-316C, and SA-319B, remove the placard required by AD 75-17-30, if installed, and install a temporary placard on the instrument panel, in full view of the pilot, reading as follows: "Maximum density altitude: 8200 feet". Temporary placard may be removed upon accomplishment of paragraph (a) of this AD.

(Alouette Service Bulletin No. 01.39 also refers to paragraph (b) of this AD).

This AD supersedes Amendment 39-2335 (40 FR 33010), AD 75-17-30.

This amendment is effective upon publication in the FEDERAL REGISTER as to all persons except those persons to whom it was made immediately effective by telegram dated September 30, 1975, which contained this amendment.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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