AD 82-05-04

final rule

Airworthiness Directives; SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS) Model SA360C and SA365C Series Helicopters

AD Number
82-05-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
82-ASW-4
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters SA-360C Dauphin Airworthiness Directives; SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS) Model SA360C and SA365C Series Helicopters
aircraft Airbus Helicopters SA-365C Airworthiness Directives; SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS) Model SA360C and SA365C Series Helicopters
aircraft Airbus Helicopters SA-365C1 Airworthiness Directives; SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS) Model SA360C and SA365C Series Helicopters
aircraft Airbus Helicopters SA-365C2 Airworthiness Directives; SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS) Model SA360C and SA365C Series Helicopters

Unsafe Condition

Excessive deformation of the pilot's and copilot's seat long slides and resulting tilt of the seats.

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

Required Actions

Add doublers to the 4 long slides as prescribed in Aerospatiale Dauphin Service Bulletin No. 25.08, or an equivalent modification approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Office. Aircraft may be flown under FAR 21.197 and 21.199 to a base where the slide doublers may be installed.

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

Compliance Time

within 30 days after the effective date of this AD

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

Affected Aircraft

Societe Nationale Industrielle Aerospatiale (SNIAS) Model SA360C and SA365C series helicopters certificated in all categories

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

Federal Register Abstract

Pilot/Co-Pilot Seat Slides

Applicability Source Text

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AD Number:
82-05-04
Document Type:
AD Final Rules
Docket Number:
82-ASW-4
Subject Heading:
Airworthiness Directives; SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS) Model SA360C and SA365...Show more
Subject:
Pilot/Co-Pilot Seat Slides
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/12/1982
Make:
Airbus Helicopters
Model:
SA-360C Dauphin | SA-365C | SA-365C1 | SA-365C2
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: 82-05-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   82-ASW-4

AMENDMENT:   39-4331

AD NUMBER:   82-05-04

SUBJECT HEADING:   Airworthiness Directives; SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS) Model SA360C and SA365C Series Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective March 12, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-05-04 SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS): Amendment 39-4331. Applies to Model SA360C and SA365C series helicopters certificated in all categories (Airworthiness Docket No. 82-ASW-4).

Compliance is required within 30 days after the effective date of this AD.

To prevent possible excessive deformation of the pilot's and copilot's seat long slides and resulting tilt of the seats, accomplish the following modification unless already accomplished.

(a) Add doublers to the 4 long slides as prescribed in Aerospatiale Dauphin Service Bulletin No. 25.08, dated March 23, 1981, or as prescribed in an equivalent modification approved by Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Office.

(b) Aircraft may be flown in accordance with FAR 21.197 and 21.199 to a base where the slide doublers may be installed.

This amendment becomes effective March 12, 1982.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_82-05-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
82-05-04
Document Type:
AD Final Rules
Docket Number:
82-ASW-4
Subject Heading:
Airworthiness Directives; SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS) Model SA360C and SA365...Show more
Subject:
Pilot/Co-Pilot Seat Slides
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/12/1982
Make:
Airbus Helicopters
Model:
SA-360C Dauphin | SA-365C | SA-365C1 | SA-365C2
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: 82-05-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   82-ASW-4

AMENDMENT:   39-4331

AD NUMBER:   82-05-04

SUBJECT HEADING:   Airworthiness Directives; SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS) Model SA360C and SA365C Series Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective March 12, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-05-04 SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS): Amendment 39-4331. Applies to Model SA360C and SA365C series helicopters certificated in all categories (Airworthiness Docket No. 82-ASW-4).

Compliance is required within 30 days after the effective date of this AD.

To prevent possible excessive deformation of the pilot's and copilot's seat long slides and resulting tilt of the seats, accomplish the following modification unless already accomplished.

(a) Add doublers to the 4 long slides as prescribed in Aerospatiale Dauphin Service Bulletin No. 25.08, dated March 23, 1981, or as prescribed in an equivalent modification approved by Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Office.

(b) Aircraft may be flown in accordance with FAR 21.197 and 21.199 to a base where the slide doublers may be installed.

This amendment becomes effective March 12, 1982.

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.