|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
retired
light aircraft
single-engine
civil aircraft
cantilever wing
|
|
gptkbp:aspectRatio
|
7.5
|
|
gptkbp:climbRate
|
5 m/s
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:constructionMaterial
|
metal
|
|
gptkbp:controls
|
elevator, ailerons, rudder
|
|
gptkbp:covers
|
split flaps
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
low-wing monoplane
|
|
gptkbp:engine
|
Hirth HM 504
|
|
gptkbp:firstFlight
|
1948
|
|
gptkbp:fuelCapacity
|
120 L
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:height
|
2.30 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bücker Bü 182B
|
|
gptkbp:introduced
|
1948
|
|
gptkbp:landingGear
|
no
tailwheel
|
|
gptkbp:length
|
7.60 m
|
|
gptkbp:manufacturer
|
gptkb:Bücker_Flugzeugbau
|
|
gptkbp:maximumDepth
|
400 kg
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:missions
|
dual controls
|
|
gptkbp:notableUsers
|
gptkb:Luftwaffe
|
|
gptkbp:numberBuilt
|
approximately 200
|
|
gptkbp:powers
|
140 hp
|
|
gptkbp:productionCompany
|
Germany,_Switzerland
|
|
gptkbp:productionYears
|
1948-1958
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
trainer aircraft
aerobatic training
|
|
gptkbp:service_ceiling
|
4,000 m
|
|
gptkbp:speed
|
60 km/h
|
|
gptkbp:succeededBy
|
3.5°/s
|
|
gptkbp:successor
|
gptkb:Bücker_Bü_181
|
|
gptkbp:usedBy
|
gptkb:Germany
|
|
gptkbp:variant
|
gptkb:Bücker_Bü_182B-2
gptkb:Bücker_Bü_182B-1
|
|
gptkbp:weight
|
800 kg
|
|
gptkbp:wingArea
|
12.00 m²
|
|
gptkbp:wingspan
|
9.00 m
|