AD 81-14-51 R1

final rule
Data completeness: 70%

Airworthiness Directives; SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS) Model SA 360C, SA 365C, and SA 365N Helicopters

AD Number
81-14-51 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
81-ASW-32
FR Citation
This information is not available.

Applicability

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

Unsafe Condition

Cracks in the tail rotor internal and external rotating fairings and in the flange of the rotor hub body at the attaching points of the external fairing.

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

Required Actions

Inspect visually for cracks in the tail rotor fairings and rotor hub flange. If cracks are found, remove the affected part before further flight and install a serviceable part. Conduct daily pre-flight checks for cracks. Inspect mating surfaces of rotor hub and external fairing using dye penetrant or equivalent method at intervals not to exceed 150 hours time in service.

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

Compliance Time

Within 5 hours time in service after receipt of this AD for certain helicopters, and thereafter at intervals not to exceed 50 hours. For others, before reaching 50 hours total time in service, and thereafter at intervals not to exceed 50 hours. The dye penetrant inspection must be done within 50 hours time in service after the effective date and thereafter at intervals not to exceed 150 hours time in service.

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

Affected Aircraft

Societe Nationale Industrielle Aerospatiale (SNIAS) Model SA 360C, SA 365C, and SA 365N helicopters, excluding those complying with specified service bulletins.

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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