+Article 2 (1)

Article 2 (1)

‘aircraft’ means fixed-wing aircraft with a maximum certificated take-off mass of 34 000 kg or more, or with a certificated maximum internal accommodation for the aircraft type in question consisting of 19 passenger seats or more, excluding any seats for crew only;

1. Przegląd

,

1.1 Odwołania

1.2 Zidentyfikowane wymagania

1.3 Powiązane normy

2. Zidentyfikowane wymagania

Wymagania

3. Powiązane normy

Normy