McDonnell Douglas MD530F: Difference between revisions
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Skca54admin (talk | contribs) No edit summary |
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| Line 14: | Line 14: | ||
| EngineQ = 1 | | EngineQ = 1 | ||
| TakeoffPower = 650 shp | | TakeoffPower = 650 shp | ||
| FuelCapacity = | | FuelCapacity = 53.3 Imperial Gallons | ||
| Passengers = 0 | | Passengers = 0 | ||
| Crew = 2 | | Crew = 2 | ||
| Line 20: | Line 20: | ||
| CruiseSpeed = 152 knots | | CruiseSpeed = 152 knots | ||
}} | }} | ||
*Weapons Wing adds 51.7 Imperial Gallons | |||
[[Category:Aircraft]] | [[Category:Aircraft]] | ||
Revision as of 20:28, 14 November 2016
| McDonnell Douglas MD530F | ||||
|---|---|---|---|---|
| Type | Helicopter | |||
| Passengers | 0 | |||
| Crew | 2 | |||
| Range | 232 nm | |||
| Cruise Speed | 152 knots | |||
| Fuel Capacity | 53.3 Imperial Gallons | |||
| Takeoff Power | 650 shp | |||
| Altitude Ceiling | 20,000 ft | |||
| Engine Type | Turbine | |||
| Engine Quantity | 1 | |||
| Engine | Rolls-Royce Model M250-C30HU | |||
| (v1.02) | ||||
- Weapons Wing adds 51.7 Imperial Gallons