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Lockheed JetStar
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==Specifications (JetStar II)== [[File:Lockheed Jetstar 3-view.jpg|340|right]] {{Aircraft specs |prime units?=imp |ref=Lockheed Aircraft since 1913<ref name="Frnc Lock p396">Francillon 1982, p. 396.</ref> |crew=two [[aviator|pilots]] and typically one [[flight attendant]] |capacity=8β10 passengers |length ft= 60 |length in= 5 |length m= 18.41 |span ft= 54 |span in= 5 |span m= 16.59 |height ft= 20 |height in= 5 |height m= 6.22 |wing area sqft= 542.5 |wing area sqm= 50.4 |empty weight lb= 24,750 |empty weight kg= 11,226 |gross weight lb=41,535 |gross weight kg=18,840 |max takeoff weight lb= 44,500 |max takeoff weight kg= 20,185 |eng1 name= [[Garrett TFE731|Garrett TFE731-3]]<ref name="Frnc Lock p394">Francillon 1982, p. 394.</ref> |eng1 type= [[turbofan]] |eng1 number=4 |eng1 lbf=3,700 |eng1 kn=16.5 |max speed mph=547 |max speed kts=476 |max speed kmh=883 |max speed note=at 30,000 ft (9,145 m) |cruise speed mph=504 |cruise speed kts=438 |cruise speed kmh=811 |range miles= 2,995 |range nmi=2,604 |range km=4,820 |ceiling ft= 43,000 |ceiling m= 13,105 |climb rate ftmin=4,150 |climb rate ms=21.1 |power/mass= }}
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