Airworthiness Directive
AD 2019-17-02: Airbus Helicopters Deutschland GmbH
Airworthiness Directives; Airbus Helicopters Deutschland GmbH
- Effective
- Sep 25, 2019
- Published
- Sep 10, 2019
- Registered aircraft
- 108
Models this AD may apply to
AI-extracted — verify against originalMatched from the AD's applicability section. Applicability must be confirmed by a mechanic against the aircraft's records.
Aircraft
- Only with: With longitudinal single-axis actuator P/N L673M20A1008 or L673M30A2111, collective single-axis actuator P/N L673M20A1012, L673M30A1211, or E673M30A1201, or lateral single-axis actuator P/N L673M20A1011 or L673M30A2311 installed that have, as of April 23, 2019, accumulated 6 or more years since manufacturing date or last overhaul, whichever occurs later.
- Only with: With longitudinal single-axis actuator P/N L673M20A1008 or L673M30A2111, collective single-axis actuator P/N L673M20A1012, L673M30A1211, or E673M30A1201, or lateral single-axis actuator P/N L673M20A1011 or L673M30A2311 installed that have, as of April 23, 2019, accumulated 6 or more years since manufacturing date or last overhaul, whichever occurs later.
Applicability
From the AD textThis AD applies to Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, and EC135T3 helicopters, certificated in any category, with any of the following installed that have, as of April 23, 2019, accumulated 6 or more years since manufacturing date or last overhaul, whichever occurs later: (1) Longitudinal single-axis actuator part number (P/N) L673M20A1008 or P/N L673M30A2111; (2) Collective single[hyphen]axis actuator P/N L673M20A1012, P/N L673M30A1211, or P/N E673M30A1201; or (3) Lateral single[hyphen]axis actuator P/N L673M20A1011or P/N L673M30A2311.
Related ADs
Superseded or revised by AD 2021-09-07.
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