gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:air_support
|
certified for flight
|
gptkbp:aircraft_operated
|
civil aircraft
|
gptkbp:avionics
|
optional avionics package
|
gptkbp:climb_rate
|
700 ft/min
|
gptkbp:cockpit
|
two-seat cockpit
|
gptkbp:community
|
active owner community
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
gptkbp:control_system
|
conventional control system
|
gptkbp:crew
|
gptkb:1
|
gptkbp:cruise_speed
|
130 knots
|
gptkbp:design
|
low-wing monoplane
|
gptkbp:design_features
|
all-metal construction
|
gptkbp:engine_power
|
150 hp
|
gptkbp:engine_type
|
piston engine
|
gptkbp:first_flight
|
gptkb:1970
|
gptkbp:flaps
|
split flaps
|
gptkbp:fuel_capacity
|
30 US gallons
|
gptkbp:fuel_type
|
avgas
|
gptkbp:fuselage_material
|
NACA 2412 airfoil
|
gptkbp:height
|
8 ft 6 in
|
gptkbp:historical_significance
|
popular among private pilots
|
https://www.w3.org/2000/01/rdf-schema#label
|
Grumman AA-5 C
|
gptkbp:instrumentation
|
basic flight instruments
|
gptkbp:landing_distance
|
1,000 ft
60 knots
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
23 ft 8 in
|
gptkbp:manufacturer
|
gptkb:Grumman_Aircraft_Engineering_Corporation
|
gptkbp:market_segment
|
general aviation
|
gptkbp:max_speed
|
150 knots
|
gptkbp:max_takeoff_weight
|
2,400 lb
|
gptkbp:nickname
|
gptkb:Tiger
|
gptkbp:number_built
|
1,200
|
gptkbp:passenger_capacity
|
gptkb:3
|
gptkbp:production_location
|
gptkb:United_States
|
gptkbp:production_years
|
1970-1978
|
gptkbp:propeller
|
variable-pitch propeller
|
gptkbp:range
|
600 nautical miles
|
gptkbp:service_ceiling
|
15,000 ft
|
gptkbp:stall_speed
|
50 knots
docile stall characteristics
|
gptkbp:support
|
parts and service support available
|
gptkbp:takeoff_distance
|
1,200 ft
|
gptkbp:trailing_edge
|
trailing-edge flaps
|
gptkbp:type
|
gptkb:light_aircraft
|
gptkbp:variant
|
gptkb:Grumman_AA-5
|
gptkbp:weight
|
1,500 lb
900 lb
|
gptkbp:wing_area
|
160 sq ft
|
gptkbp:wingspan
|
34 ft 0 in
|
gptkbp:bfsParent
|
gptkb:Grumman_AA-5
|
gptkbp:bfsLayer
|
6
|