NAMC YS-11

ยท NAMC
Length
26.3 m
Flat Wing Span
32 m
Height
8.98 m
Flat Wing Area
94.83 m²
Flat Wing Aspect Ratio
10.8
Max Seating
64
Cruise Speed
469 km/h
Max Ceiling
6982 m
Number of Engines
2
First Flight
1962-08-30
Entry Into service
1965-03-30
Number Built
182
Maximum Take-Off Weight
24.5 t (paragliders: kg)
Maximum Range
2110 km

Pictures

No pictures yet for this family.

Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
NAMC YS-11 24.5 2110

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Canadair CC-109 Cosmopolitan Napier Eland 24.6888 32.004 64 Compare
Fairchild C-82 Packet Pratt & Whitney R-2800 Double Wasp 23.4696 32.3088 42 Compare
British Aerospace ATP Pratt & Whitney Canada PW100 26 30.63 64 Compare
Ilyushin Il-114 TV7-117 26.88 30 64 Compare
Fairchild AC-119 26.2128 33.2232 Compare
Airspeed Ambassador 24.6888 35.052 60 Compare
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