AD 75-26-02

final rule
Data completeness: 70%

Airworthiness Directives; Societe Nationale Industrielle Aerospatiale, (S.N.I.A.S., formerly Sud Aviation) Models SA-315B, SE-3160, SA-316B, SA-316C, and SA-319B Helicopter

AD Number
75-26-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters SA.315B Alouette III Airworthiness Directives; Societe Nationale Industrielle Aerospatiale, (S.N.I.A.S., formerly Sud Aviation) Models SA-315B, SE-3160, SA-316B, SA-316C, and SA-319B Helicopter
aircraft Airbus Helicopters SA.316B Alouette III Airworthiness Directives; Societe Nationale Industrielle Aerospatiale, (S.N.I.A.S., formerly Sud Aviation) Models SA-315B, SE-3160, SA-316B, SA-316C, and SA-319B Helicopter
aircraft Airbus Helicopters SA.316C Alouette III Airworthiness Directives; Societe Nationale Industrielle Aerospatiale, (S.N.I.A.S., formerly Sud Aviation) Models SA-315B, SE-3160, SA-316B, SA-316C, and SA-319B Helicopter
aircraft Airbus Helicopters SA.319B Alouette III Airworthiness Directives; Societe Nationale Industrielle Aerospatiale, (S.N.I.A.S., formerly Sud Aviation) Models SA-315B, SE-3160, SA-316B, SA-316C, and SA-319B Helicopter
aircraft Airbus Helicopters SE.3160 Alouette III Airworthiness Directives; Societe Nationale Industrielle Aerospatiale, (S.N.I.A.S., formerly Sud Aviation) Models SA-315B, SE-3160, SA-316B, SA-316C, and SA-319B Helicopter

Unsafe Condition

Failure of the fixed levers of the main rotor head hydraulic drag dampers due to cracks in the area of the eccentric attachment hole.

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

Required Actions

Daily visual inspections for cracks in the fixed levers until paragraph (c) is completed. Replace any cracked levers before flight. Within 100 hours after the effective date, remove, inspect, rectify, and reinstall the dampers per specified service bulletins.

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

Compliance Time

Within the next 100 hours' time in service 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 models SA-315B, SE-3160, SA-316B, SA-316C, and SA-319B helicopters with main rotor heads P/N's 3160S.12.10.000.11 through .14, P/N's 3160S.12.20.000.4 through .7, modified per Modification No. S296-AM 1108 or Service Bulletin No. 65-52, or P/N's 3160S.12.20.000.1 through .3 modified per Modification No. S296-AM 1108 or Service Bulletin No. 65-52.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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