|
gptkbp:instanceOf
|
gptkb:light_jet
|
|
gptkbp:avionics
|
gptkb:Rockwell_Collins_Pro_Line_21
|
|
gptkbp:category
|
gptkb:business_jet
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:crew
|
1
|
|
gptkbp:cruiseSpeed
|
451 mph
|
|
gptkbp:FAATypeCertificate
|
A00010WI
|
|
gptkbp:firstFlight
|
2001
|
|
gptkbp:fuselageMaterial
|
carbon fiber composite
|
|
gptkbp:height
|
15 ft 4 in
|
|
gptkbp:ICAOTypeDesignator
|
BE40
|
|
gptkbp:introduced
|
2005
|
|
gptkbp:landingGear
|
tricycle retractable
|
|
gptkbp:length
|
46 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Beechcraft
|
|
gptkbp:maximumSpeed
|
526 mph
|
|
gptkbp:maxTakeoffWeight
|
12,500 lb
|
|
gptkbp:numberOfEngines
|
2
|
|
gptkbp:powerplant
|
gptkb:Williams_FJ44-2A_turbofan
|
|
gptkbp:primaryUser
|
private owners
corporate operators
|
|
gptkbp:productionEndYear
|
2012
|
|
gptkbp:range
|
1,380 nmi
|
|
gptkbp:seatingCapacity
|
6
|
|
gptkbp:serviceCeiling
|
41,000 ft
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
Beechcraft Premier II
|
|
gptkbp:wingspan
|
44 ft 6 in
|
|
gptkbp:bfsParent
|
gptkb:Beechcraft_Premier_I
|
|
gptkbp:bfsLayer
|
7
|
|
http://www.w3.org/2000/01/rdf-schema#label
|
Beechcraft Premier IA
|