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gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
light aircraft
biplane configuration
|
|
gptkbp:climbRate
|
500 ft/min
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|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:constructionMaterial
|
wood
fabric
|
|
gptkbp:controls
|
ailerons
elevator
rudder
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
gptkb:William_Boeing
|
|
gptkbp:engine
|
gptkb:Wright_J-5
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1927
June 15, 1927
|
|
gptkbp:fuelCapacity
|
30 gallons
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:height
|
8 ft 0 in
|
|
gptkbp:historicalSignificance
|
first aircraft produced by Boeing
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing Model 100
|
|
gptkbp:influenced
|
gptkb:Boeing_Model_40
|
|
gptkbp:introduced
|
1927
|
|
gptkbp:landingGear
|
tailwheel
conventional landing gear
|
|
gptkbp:length
|
25 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:maxSpeed
|
120 mph
|
|
gptkbp:maxTakeoffWeight
|
2,200 lb
|
|
gptkbp:notableUsers
|
Boeing_School_of_Aeronautics
|
|
gptkbp:numberBuilt
|
15
|
|
gptkbp:operationalHistory
|
used in early commercial aviation.
|
|
gptkbp:passengerCapacity
|
2
|
|
gptkbp:productionYears
|
1927-1930
|
|
gptkbp:propulsion
|
fixed-pitch propeller
|
|
gptkbp:range
|
400 miles
|
|
gptkbp:retirementYear
|
1930s
|
|
gptkbp:role
|
civil aviation
trainer aircraft
|
|
gptkbp:services
|
10,000 ft
|
|
gptkbp:speed
|
50 mph
|
|
gptkbp:succeededBy
|
3.5 sec per 360°
|
|
gptkbp:successor
|
gptkb:Boeing_Model_40
|
|
gptkbp:takeoffDistance
|
600 ft
500 ft
|
|
gptkbp:type
|
biplane
|
|
gptkbp:variant
|
Boeing_Model_100A
|
|
gptkbp:weight
|
1,500 lb
|
|
gptkbp:wingArea
|
250 sq ft
|
|
gptkbp:wingspan
|
36 ft 0 in
|