|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Canadair_CL-44
retired
cargo transport
high-wing
cantilever wing
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:constructed_in
|
50
|
|
gptkbp:crew
|
2
|
|
gptkbp:decommissioned
|
gptkb:1980s
|
|
gptkbp:design
|
gptkb:public_transportation_system
Canadair design team
|
|
gptkbp:engine
|
2
1,500 hp
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:first_flight
|
gptkb:1954
|
|
gptkbp:fuel_capacity
|
5,000 L
|
|
gptkbp:height
|
8.23 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
C-51 A
|
|
gptkbp:is_used_by
|
gptkb:Royal_Canadian_Air_Force
|
|
gptkbp:landing_gear
|
gptkb:horse_race
|
|
gptkbp:length
|
22.86 m
|
|
gptkbp:manufacturer
|
gptkb:Canadair
|
|
gptkbp:material
|
monocoque
|
|
gptkbp:max_speed
|
500 km/h
|
|
gptkbp:max_takeoff_weight
|
20,865 kg
|
|
gptkbp:nickname
|
gptkb:C-51
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:price
|
$1.5 million
|
|
gptkbp:primary_user
|
gptkb:Royal_Canadian_Air_Force
|
|
gptkbp:production_location
|
gptkb:Montreal,_Canada
|
|
gptkbp:production_years
|
1954-1960
|
|
gptkbp:propulsion
|
variable-pitch
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:retired
|
gptkb:1980s
|
|
gptkbp:role
|
gptkb:Company
|
|
gptkbp:seating_capacity
|
gptkb:television_series
3,600 kg
rear ramp
|
|
gptkbp:service_ceiling
|
7,620 m
|
|
gptkbp:services
|
gptkb:1955
gptkb:1980s
|
|
gptkbp:successor
|
gptkb:CC-115_Buffalo
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
C-51 A North Star
|
|
gptkbp:wingspan
|
28.96 m
|
|
gptkbp:bfsParent
|
gptkb:Curtiss_C-51
gptkb:Curtiss_C-51_Condor
|
|
gptkbp:bfsLayer
|
7
|