Flat Wing Aspect Ratio
10.8
Entry Into service
1965-03-30
Maximum Take-Off Weight
24.5 t (paragliders: kg)
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
NAMC YS-11 |
24.5 |
2110 |
Similar airplanes
All data (28 fields)
- Name
- NAMC YS-11
- Manufacturer
- NAMC
- Description
- The NAMC YS-11 is a turboprop airliner designed and built by the Nihon Aircraft Manufacturing Corporation (NAMC), a Japanese consortium.
- ICAO Code
- YS11
- First Flight
- 1962-08-30
- Entry Into service
- 1965-03-30
- Production End
- 1974-01-01
- Designer
- NAMC
- Type
- Turboprop airliner
- Length (m)
- 26.3
- Height (m)
- 8.98
- Cockpit Crew
- 2
- Max Seating
- 64
- Cruise Speed (km/h)
- 469
- Min Speed (km/h)
- 140
- Max Ceiling (m)
- 6982
- Rate of Climb (m/s)
- 6.2
- Capacity Description
- 64 passengers / 6604 kg
- National Origin
- Japan
- Number Built
- 182
- Powerplant Description
- 2 × Rolls-Royce Dart Mk.542-10K turboprop engines, 2250 kW (3017 hp) each
- Status
- Three in service with the Japan Air Self-Defense Force (as of 30 June 2024)
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/NAMC_YS-11
- Flat Wing Span (m)
- 32
- Flat Wing Area (m²)
- 94.83
- Flat Wing Aspect Ratio
- 10.8
- Wake Category
- M
- Number of Engines
- 2