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NAMC YS-11: Διαφορά μεταξύ των αναθεωρήσεων

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Γραμμή 109:
*[[Winair]]
 
==Specifications (YS-11A-200)==
{{aero-specs}}
{{aircraft specifications
*Engines: Two [[Rolls-Royce Dart]] Mk542-10K [[turboprop]]s, each rated 3,000 horsepower (2,200 kW)
*Wingspan: 105 ft (32 m)
*Fuselage: 86 ft (26.3 m)<!--quoted from Japanese wikipedia-->
*Dry weight: 32,187 lb (14,600 kg)<!--weight in Kg quoted from Japanese wikipedia, and that in lbs re-calculated on Oct.28, 2006-->
*Maximum load: 11,904 lb (5,400 kg)
*Maximum takeoff weight: 51,808 lb (23,500 kg)▼
*Airspeed: 245kt knots (454 km/h)
*Operating range: 1,367 miles (2,200 km) <!--old values "680miles/1,100km" appear to be wrong-->
*Passengers: 64
*Day of first test flight: August 30th, 1962
 
|plane or copter?=<!-- options: plane/copter --> plane
==Comparable Aircraft==
|jet or prop?=<!-- options: jet/prop/both/neither --> prop
 
|ref=<ref name="green">Green, William, ''The Observers Book of Aircraft'', Frederick Warne & Co. Ltd, 1970. ISBN 0-7232-0087-4</ref>
* [[Avro 748]]▼
 
* [[An-24]]▼
|crew=Two
* [[An-26]]▼
|capacity=64 passengers
|payload main=5,400 kg
|payload alt=11,904 lb
|length main= 26.3 m
|length alt= 86 ft 3 in
|span main= 32.0 m
|span alt= 105 ft 0 in
|height main= 8.99 m
|height alt= 29 ft 6 in
|area main= 94.83 m²
|area alt= 1,020.4 ft²
|airfoil=
 
|empty weight main= 14,600 kg
|empty weight alt= 32,187 lb
|loaded weight main= <!--kg-->
|loaded weight alt= <!--lb-->
|useful load main= <!--kg-->
|useful load alt= <!--lb-->
▲*Maximum|max takeoff weight: 51,808 lbmain= (23,500 kg)
|max takeoff weight alt= 51,808 lb
|more general=
 
|engine (prop)=[[Rolls-Royce Dart]] Mk.542-10K
|type of prop=[[turboprop]] engines
|number of props=2
|power main= 2,280 kW
|power alt= 3,060 shp
|power original=
 
|max speed main= <!--km/h-->
|max speed alt= <!--knots,mph-->
|cruise speed main= 454 km/h
|cruise speed alt= 245 knots, 282 mph
|never exceed speed main= <!--km/h-->
|never exceed speed alt= <!--knots,mph-->
|stall speed main= <!--km/h-->
|stall speed alt= <!--knots,mph-->
|range main= 2,200 km
|range alt= 1,188 nm, 1,367 miles
|ceiling main= 6,982 m
|ceiling alt= 22,900 ft
|climb rate main= 6.2 m/s
|climb rate alt= 1,220 ft/min
|loading main= <!--kg/m²-->
|loading alt= <!--lb/ft²-->
|power/mass main= <!--W/kg-->
|power/mass alt= <!--hp/lb-->
|more performance=
|avionics=
}}
 
==External links==
Γραμμή 132 ⟶ 175 :
 
==References==
{{reflist}}
<references/>
 
==Related content==
{{commons|YS-11}}
{{aircontent|
|related=
 
|similar aircraft=
▲* [[Avro 748]]
▲* [[An-24]]
▲* [[An-26]]
|sequence=
 
|lists=
* [[List of airliners]]
|see also=
 
}}
 
{{airlistbox}}
[[Category:Japanese airliners]]
[[Category:Multiple engine aircraft]]
[[Category:Propeller aircraft]]
[[Category:Low wing aircraft]]
 
{{Link FA|ja}}
Ανακτήθηκε από "https://el.wikipedia.org/wiki/NAMC_YS-11"