|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
experimental aircraft
light jet
N2100L
|
|
gptkbp:built
|
funding issues
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:competitors
|
gptkb:Cessna_Citation
business aviation sector
|
|
gptkbp:construction_cost
|
$1.5 million
|
|
gptkbp:constructionMaterial
|
composite materials
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:design
|
gptkb:Gordon_L._Lear
|
|
gptkbp:design_feature
|
Lear Fan 2100 to 2000
|
|
gptkbp:engineType
|
turbofan
|
|
gptkbp:firstFlight
|
1981
limited
|
|
gptkbp:fuel_capacity
|
1,200 lbs
|
|
gptkbp:height
|
14 ft 0 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lear Fan
|
|
gptkbp:influenced
|
Learjet series
|
|
gptkbp:inspiration
|
fuel efficiency
low drag design
NASA_studies
|
|
gptkbp:inventor
|
Lear Fan 2100
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
influenced future designs.
|
|
gptkbp:length
|
40 ft 0 in
|
|
gptkbp:location
|
gptkb:United_States
|
|
gptkbp:manufacturer
|
gptkb:Lear_Fan_Corporation
|
|
gptkbp:market_segment
|
general aviation
|
|
gptkbp:maximum_speed
|
400 knots
|
|
gptkbp:notable_event
|
prototype crash
|
|
gptkbp:notable_feature
|
canard_configuration
|
|
gptkbp:notableContestants
|
gptkb:Bob_Hoover
|
|
gptkbp:operational_status
|
cancelled
|
|
gptkbp:operationalHistory
|
limited production
|
|
gptkbp:passenger_traffic
|
6 to 8 passengers
|
|
gptkbp:patentNumber
|
N2100L
|
|
gptkbp:performance
|
high speed cruise
|
|
gptkbp:productionCompany
|
Lear Fan 2000
|
|
gptkbp:productionYears
|
1970s to 1980s
|
|
gptkbp:range
|
1,500 nautical miles
|
|
gptkbp:role
|
business jet
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:service_ceiling
|
35,000 ft
|
|
gptkbp:speed
|
350 knots
|
|
gptkbp:surrounding_area
|
400 sq ft
|
|
gptkbp:targetMarket
|
1980s
corporate operators
|
|
gptkbp:team
|
Lear_Fan_Corporation_engineers
|
|
gptkbp:type
|
twin-engine aircraft
|
|
gptkbp:wingspan
|
50 ft 0 in
|