|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
twin-engine
civil aircraft
multi-engine aircraft
|
|
gptkbp:avionics
|
modern avionics
|
|
gptkbp:capacity
|
6
|
|
gptkbp:category
|
light aircraft
|
|
gptkbp:cockpit
|
pressurized
|
|
gptkbp:controls
|
yoke
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
low-wing monoplane
high wing loading
Aero_Commander_design_team
|
|
gptkbp:electrification
|
2 × Lycoming IO-540-U4A5
|
|
gptkbp:engine
|
2
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:features
|
spacious cabin
|
|
gptkbp:firstFlight
|
1965
|
|
gptkbp:fuelCapacity
|
1,200 lb
|
|
gptkbp:height
|
3.05 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Aero Commander 680D
|
|
gptkbp:influences
|
gptkb:Aero_Commander_680E
|
|
gptkbp:introduced
|
1965
|
|
gptkbp:landingGear
|
tricycle gear
short field landing
|
|
gptkbp:length
|
8.84 m
|
|
gptkbp:manufacturer
|
gptkb:Aero_Commander
|
|
gptkbp:market
|
general aviation
|
|
gptkbp:marketSegment
|
business aviation
|
|
gptkbp:maximumDepth
|
1,600 kg
|
|
gptkbp:maxSpeed
|
200 knots
|
|
gptkbp:maxTakeoffWeight
|
3,402 kg
short takeoff distance
|
|
gptkbp:navigationEquipment
|
VOR,_ADF
|
|
gptkbp:notableUsers
|
gptkb:U.S._military
|
|
gptkbp:numberBuilt
|
over 1,000
|
|
gptkbp:operationalStatus
|
moderate
|
|
gptkbp:performance
|
good climb rate
|
|
gptkbp:produces
|
1965-1980
|
|
gptkbp:productionLocation
|
gptkb:USA
|
|
gptkbp:propulsion
|
2-bladed
|
|
gptkbp:range
|
1,200 nautical miles
|
|
gptkbp:relatedAircraft
|
gptkb:Aero_Commander_680
|
|
gptkbp:retired
|
1980s
|
|
gptkbp:role
|
utility aircraft
|
|
gptkbp:safety
|
good safety record
|
|
gptkbp:services
|
25,000 ft
|
|
gptkbp:successor
|
gptkb:Aero_Commander_680E
|
|
gptkbp:type
|
business aircraft
|
|
gptkbp:variant
|
gptkb:Aero_Commander_680
|
|
gptkbp:weight
|
1,800 kg
|
|
gptkbp:wingArea
|
22.86 m²
|
|
gptkbp:wingspan
|
11.58 m
|