+Article 2 (1)
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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. Übersicht
| Bezeichnung |
Regulierung |
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1.1 Referenzen
1.2 Identifizierte Anforderungen
1.3 Zugehörige Standards
2. Identifizierte Anforderungen
Anforderungen
| Quelle |
Anforderung |
3. Zugehörige Standards
Standards
| Quelle |
Anforderung |
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