FAA 2020-13-02

Effective 2021-04-01 · Applies to: Leonardo 119

Cross-jurisdiction flags

Timing differs from EASA by 287 days
FAA effective 2021-04-01; EASA 2020-0128 effective 2020-06-18

Subject

The FAA is superseding Airworthiness Directive (AD) 2020-13-02 for Leonardo S.p.A. (Leonardo) Model A119 and AW119 MKII helicopters. AD 2020-13-02 required inspecting for movement and the tightening torque of the tail rotor (T/R) plug, the installation of the outboard and inboard faces of the T/R duplex bearing, and the condition of the T/R duplex bearing, T/R plug threads, and nut threads. Depending on the inspection results, AD 2020-13-02 required corrective actions and reporting information. This new AD retains the requirements of AD 2020- 13-02 except the reporting requirement, updates the service information, and requires repeating the inspection. This AD was prompted by Leonardo's update to the service information. The actions of this AD are intended to address an unsafe condition on these products.

Compliance time

Within 10 hours time-in-service (TIS), remove the lockwire that secures the T/R plug P/N 129-0160-45-103 (T/R plug) to the bearing liner assembly P/N 109-0135-16-101 (bearing liner assembly).

Referenced Service Bulletins

  • Leonardo EASB No. 119-105
Source: FAA · scraped 2026-06-21 04:02 UTC