Flat Wing Area
19.9742 m²
Cruise Speed
444.4796 km/h
Entry Into service
1968-01-01
Maximum Take-Off Weight
3.3793 t (paragliders: kg)
Total Fuel Capacity
779.7948
Maximum Range
2753.924 km
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Cessna 421 Golden Eagle |
3.3793 |
779.7948 |
2753.924 |
Similar airplanes
All data (25 fields)
- Name
- Cessna 421 Golden Eagle
- Manufacturer
- Advanced Aircraft
- Description
- The Cessna 421 Golden Eagle is an American six or seven seat twin-engined light transport aircraft, developed in the 1960s by Cessna as a pressurized version of the earlier Cessna 411.
- ICAO Code
- C421
- First Flight
- 1965-10-14
- Entry Into service
- 1968-01-01
- Production End
- 1985-01-01
- Designer
- Advanced Aircraft
- Type
- Light transport
- Length (m)
- 10.9728
- Height (m)
- 3.3528
- Max Speed (km/h)
- 474.1116
- Cruise Speed (km/h)
- 444.4796
- Max Ceiling (m)
- 9204.96
- Rate of Climb (m/s)
- 9.8552
- Capacity Description
- Six passengers
- National Origin
- United States of America
- Number Built
- 1916
- Powerplant Description
- 2 × Continental GTSIO-520-L turbocharged, fuel injected and geared flat-six engines, 280 kW (375 hp) each
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Cessna_421_Golden_Eagle
- Flat Wing Span (m)
- 12.4968
- Flat Wing Area (m²)
- 19.9742
- Wake Category
- L
- Aircraft Engine
- Continental IO-520
- Number of Engines
- 2