Flat Wing Area
39.9483 m²
Cruise Speed
449.007 km/h
Entry Into service
1941-01-01
Maximum Take-Off Weight
7.59 t (paragliders: kg)
Maximum Range
1659.234 km
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Piaggio P.111 |
7.59 |
1659.234 |
Similar airplanes
All data (20 fields)
- Name
- Piaggio P.111
- Manufacturer
- Piaggio Aero
- Description
- The Piaggio P.111 was an Italian high-altitude research aircraft designed and built by Piaggio for the Regia Aeronautica (Italian Royal Air Force).
- First Flight
- 1941-04-09
- Entry Into service
- 1941-01-01
- Service End
- 1943-01-01
- Designer
- Piaggio Aero
- Length (m)
- 12.4
- Height (m)
- 3.6576
- Max Speed (km/h)
- 574.5358
- Cruise Speed (km/h)
- 449.007
- Max Ceiling (m)
- 12009.12
- National Origin
- Italy
- Number Built
- 1
- Powerplant Description
- 2 × Piaggio P.XII R.C.100/2v 18-cylinder air-cooled radial piston engines, 746 kW (1000 hp) each
- Primary Users
- Regia Aeronautica (Italian Royal Air Force)
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Piaggio_P.111
- Flat Wing Span (m)
- 17.0688
- Flat Wing Area (m²)
- 39.9483
- Number of Engines
- 2