|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
gptkb:Wright_Model_V-6
biplane
|
|
gptkbp:armament
|
none
|
|
gptkbp:built
|
50
|
|
gptkbp:climbRate
|
1,000 ft/min
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:constructionMaterial
|
metal
Clark Y
|
|
gptkbp:crew
|
1
|
|
gptkbp:customerService
|
gptkb:United_States_Army_Air_Corps
|
|
gptkbp:design
|
Clarence Wright
|
|
gptkbp:enginePower
|
400 hp
|
|
gptkbp:engineType
|
gptkb:Wright_R-975
|
|
gptkbp:firstFlight
|
1930
|
|
gptkbp:fuel_capacity
|
50 gallons
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:historical_significance
|
used for pilot training
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Wright Model V-5
|
|
gptkbp:influenced
|
gptkb:Wright_Model_V-3
|
|
gptkbp:landing_gear
|
tailwheel
|
|
gptkbp:length
|
28 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:maximum_speed
|
150 mph
|
|
gptkbp:maxTakeoffWeight
|
2,500 lbs
|
|
gptkbp:nickname
|
gptkb:Wright_Trainer
|
|
gptkbp:notable_feature
|
high wing loading
|
|
gptkbp:passenger_traffic
|
1
|
|
gptkbp:performances
|
120 mph
|
|
gptkbp:productionYears
|
1929-1931
|
|
gptkbp:proportions
|
6:1
|
|
gptkbp:propulsion
|
fixed-pitch propeller
|
|
gptkbp:range
|
500 miles
|
|
gptkbp:retired
|
gptkb:United_States_Army_Air_Corps
|
|
gptkbp:retirementYear
|
1935
|
|
gptkbp:role
|
training aircraft
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:serviceType
|
various flight schools
|
|
gptkbp:speed
|
60 mph
|
|
gptkbp:succeededBy
|
3.5 seconds per 360°
|
|
gptkbp:successor
|
gptkb:Wright_Model_V-7
|
|
gptkbp:surface
|
ailerons
elevator
rudder
|
|
gptkbp:surrounding_area
|
300 sq ft
|
|
gptkbp:takeoffDistance
|
70 mph
1,200 ft
1,000 ft
|
|
gptkbp:type
|
biplane
|
|
gptkbp:weight
|
1,800 lbs
|
|
gptkbp:wingspan
|
40 ft 0 in
|