|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
high performance
low-wing
single-engine piston
|
|
gptkbp:aircraft_type
|
fixed-wing aircraft
|
|
gptkbp:avionics
|
modern glass cockpit
|
|
gptkbp:climb_rate
|
1,000 ft/min
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:competitors
|
gptkb:Boeing_707
|
|
gptkbp:cruise_speed
|
140 knots
145 knots
|
|
gptkbp:design
|
gptkb:Mooney_Aircraft_Company
|
|
gptkbp:engine_power
|
300 hp
|
|
gptkbp:engine_type
|
gptkb:IO-550-G
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
50 US gallons
|
|
gptkbp:fuel_economy
|
12 gph
|
|
gptkbp:height
|
8 ft 6 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mooney M20 R
|
|
gptkbp:is_often_used_in
|
personal and business travel
|
|
gptkbp:landing_distance
|
1,200 ft
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
24 ft 9 in
|
|
gptkbp:manufacturer
|
gptkb:Mooney_International_Corporation
|
|
gptkbp:market_segment
|
general aviation
|
|
gptkbp:max_speed
|
160 knots
|
|
gptkbp:max_takeoff_weight
|
2,800 lbs
|
|
gptkbp:notable_features
|
low drag design
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:offers_certificate
|
TC A00001 SE
|
|
gptkbp:orbital_altitude
|
10,000 ft
|
|
gptkbp:payload_capacity
|
1,000 lbs
|
|
gptkbp:power_consumption
|
9.3 lbs/hp
|
|
gptkbp:production_status
|
out of production
|
|
gptkbp:production_years
|
1995-2002
|
|
gptkbp:propeller
|
gptkb:3
constant speed propeller
|
|
gptkbp:range
|
1,200 nautical miles
1,200 nm
|
|
gptkbp:safety_features
|
advanced avionics
|
|
gptkbp:seating_capacity
|
gptkb:4
|
|
gptkbp:service_ceiling
|
18,000 ft
|
|
gptkbp:stall_speed
|
60 knots
|
|
gptkbp:successor
|
gptkb:Mooney_M20_V
|
|
gptkbp:takeoff_distance
|
1,500 ft
|
|
gptkbp:weight
|
1,800 lbs
|
|
gptkbp:wing_area
|
174 sq ft
|
|
gptkbp:wing_configuration
|
16.1 lbs/sq ft
|
|
gptkbp:wingspan
|
36 ft 0 in
|
|
gptkbp:bfsParent
|
gptkb:Mooney_International_Corporation
|
|
gptkbp:bfsLayer
|
6
|