AD 63-19-05

final rule
Data completeness: 70%

Airworthiness Directives; Sud Aviation Models SE 3130 Alouette II Aircraft

AD Number
63-19-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: September 10, 1963

Applicability

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

Unsafe Condition

Fatigue failure of the main rotor hub P/N 3130.12.20.001.

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

Required Actions

Replace the main rotor hub with a new hub prior to accumulating more than 600 hours' time in service. If extending service life to 1,200 hours' time in service, inspect hubs using ultrasonic method per Sud Service Bulletin No. AL.II 12.11.204/A or FAA-approved equivalent, with inspection intervals not exceeding 50 hours' time in service. Replace cracked hubs before further flight.

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

Compliance Time

Prior to accumulating more than 600 hours' time in service (or as per extended inspection intervals for service life up to 1,200 hours).

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

Affected Aircraft

All SE 3130 Alouette II Aircraft.

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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View Official Source ↗ Find More ADs for Airbus Helicopters SE 3130-Alouette II

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