Bell UH-1B Iroquois
Aircraft of the Royal Australian Navy
Development
Entwicklung
Variants
Versionen
Einsatzgeschichte
1947
1947
Zeichnungen
| Specifications | UH-1B | |
|
Rotor diameter |
Rotordurchmesser |
14.63 m |
|
Length |
Länge |
12.69 m |
|
Height |
Höhe |
4.50 m |
|
Engine |
Motor |
1× Lycoming T53-L-11A turboshaft, 1,100 shp |
|
Maximum speed |
Höchstgeschwindigkeit |
220 km/h |
|
Empty weight |
Leergewicht |
2,085 kg |
|
Loaded weight |
Startgewicht |
4,310 kg |
|
Climb Rate |
Steigrate |
8.9 m/s |
|
Service ceiling |
Gipfelhöhe |
5,910 m |
|
Range |
Reichweite |
533 km |
|
Armament |
Bewaffnung |
various |
| Serial Bell 204 Iroquois | ||||||
| Typ | RAN Serial | Buzz | s/n | Delivered | Withdrawn | Remarks |
| UH-1B | N9-881 | 856, 896 | 63-12953 | May 1964 | 5. Jun. 1968 | Crashed |
| UH-1B | N9-882 | 857, 897 | 63-12954 | May 1964 | 31. May 1989 | - |
| UH-1B | N9-883 | 858 | 63-12955 | May 1964 | 11. Nov. 1964 | Crashed |
| UH-1B | N9-3101 | 853, 893 | 64-17621 | 1965 | 31. May 1989 | - |
| UH-1B | N9-3102 | 854, 894 | 64-17622 | 1965 | 31. Oct. 1988 | - |
| UH-1B | N9-3103 | 855, 895 | 64-17623 | 1965 | 26. Mar. 1981 | Crashed |
| UH-1B | N9-3104 | 898 | 65-12846 | 1965 | 29. Mar. 1971 | Crashed |
|
Last update 23. January 2023 |
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