Flat Wing Area
23.5602 m²
Flat Wing Aspect Ratio
9.6
Cruise Speed
479.5845 km/h
Maximum Range
4063.594 km
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All data (26 fields)
- Name
- Cessna 441 Conquest II
- Manufacturer
- Cessna Aircraft Company
- Description
- The Cessna 441 Conquest II was the first turboprop-powered aircraft designed by Cessna and was intended to fill the gap between its piston-engined aircraft and business jets.
- First Flight
- 1975-08-26
- Production End
- 1986-01-01
- Designer
- Cessna Aircraft Company
- Type
- Utility aircraft
- Length (m)
- 11.8872
- Height (m)
- 3.9624
- Cockpit Crew
- 1
- Max Seating
- 10
- Max Speed (km/h)
- 547.177
- Cruise Speed (km/h)
- 479.5845
- Min Speed (km/h)
- 139
- Max Ceiling (m)
- 10668
- Rate of Climb (m/s)
- 12.3698
- Capacity Description
- Up to 10 passengers with one pilot; up to 9 passengers with two pilots
- National Origin
- United States of America
- Number Built
- 362
- Powerplant Description
- 2 × Garrett TPE331-8-403S turboprops, 474 kW (636 hp) each
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Cessna_441_Conquest_II
- Flat Wing Span (m)
- 14.9352
- Flat Wing Area (m²)
- 23.5602
- Flat Wing Aspect Ratio
- 9.6
- Aircraft Engine
- Honeywell TPE331
- Number of Engines
- 2