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gptkbp:instanceOf
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fighter aircraft
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gptkbp:aircraft
|
single-engine aircraft
cantilever wing
20 lb/sq ft
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gptkbp:armament
|
machine guns
|
|
gptkbp:climbRate
|
1,200 ft/min
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|
gptkbp:cockpit
|
open cockpit
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gptkbp:constructionMaterial
|
Clark Y
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gptkbp:crew
|
1
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gptkbp:design
|
monoplane
open cockpit and fixed landing gear
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gptkbp:engine
|
gptkb:Pratt_&_Whitney_R-1340_Wasp
|
|
gptkbp:firstFlight
|
1932
1941
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|
gptkbp:floors
|
balanced
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gptkbp:fuelCapacity
|
100 US gallons
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gptkbp:height
|
3.05 m
|
|
gptkbp:historicalSignificance
|
first all-metal monoplane fighter in US service
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing P-26C
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gptkbp:influenced
|
later_US_fighter_designs
|
|
gptkbp:influencedBy
|
gptkb:Boeing_P-12
|
|
gptkbp:introduced
|
1934
|
|
gptkbp:landingGear
|
fixed tailwheel
|
|
gptkbp:length
|
8.23 m
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:maxSpeed
|
360 km/h
|
|
gptkbp:maxTakeoffWeight
|
2,500 lb
|
|
gptkbp:nationalTeam
|
gptkb:United_States
|
|
gptkbp:nickname
|
Peashooter
|
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gptkbp:numberBuilt
|
approximately 100
|
|
gptkbp:operationalStatus
|
frise ailerons
|
|
gptkbp:powerOutput
|
7.5 lb/hp
|
|
gptkbp:primaryUser
|
gptkb:United_States_Army_Air_Forces
|
|
gptkbp:productionCompany
|
1934-1936
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|
gptkbp:propulsion
|
two-bladed
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retired
|
1941
|
|
gptkbp:role
|
air superiority fighter
|
|
gptkbp:serviceHistory
|
used_in_World_War_II
|
|
gptkbp:services
|
1934
10,000 m
|
|
gptkbp:speed
|
60 knots
|
|
gptkbp:steering
|
balanced rudder
|
|
gptkbp:succeededBy
|
30 degrees/second
|
|
gptkbp:successor
|
gptkb:Boeing_P-26
|
|
gptkbp:takeoffDistance
|
1,200 ft
1,000 ft
70 knots
|
|
gptkbp:usedBy
|
gptkb:United_States_Army_Air_Corps
|
|
gptkbp:variant
|
gptkb:Boeing_P-26B
gptkb:Boeing_P-26A
|
|
gptkbp:weight
|
1,600 lb
|
|
gptkbp:wingspan
|
10.67 m
|