AD 2020-19-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Various | Airworthiness Directives; Airbus Helicopters |
Unsafe Condition
fatigue cracking of a T/R blade, failure of a T/R blade, and subsequent loss of control of the helicopter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
repetitively inspecting affected T/R blades with the new inspection procedures, and depending on the inspection results, repairing or replacing the T/R blade.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 30 hours time-in-service (TIS) after the effective date of this AD or within 30 hours TIS after last inspecting the T/R blades as required by paragraph (a) of AD 2000-22-19, whichever occurs first, and thereafter at intervals not to exceed 15 hours TIS for blades with de-icing systems installed or 30 hours TIS for blades without de-icing systems installed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Helicopters Model SA330F, G, and J helicopters with a T/R blade part number (P/N) 330A12-0000-(all dash numbers), 330A12-0005-(all dash numbers), or 330A12-0006-(all dash numbers), installed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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