Statements (51)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:aircraft
|
gptkbp:avionics |
modern avionics systems available
|
gptkbp:category |
business aircraft
|
gptkbp:certification |
FAA Type Certificate A23 CE
|
gptkbp:climb_rate |
1,500 ft/min
|
gptkbp:competitors |
competes with other light turboprops
|
gptkbp:crew |
1 to 2 pilots
|
gptkbp:elevation |
25,000 ft
|
gptkbp:engine |
2
|
gptkbp:engine_type |
turboprop
P T6 A-42 |
gptkbp:environmental_impact |
meets modern noise standards
|
gptkbp:features |
high wing design
|
gptkbp:first_flight |
gptkb:1966
|
gptkbp:fuel_capacity |
340 gallons
good fuel efficiency for its class |
gptkbp:height |
14 ft 9 in
|
gptkbp:historical_significance |
popular choice for business aviation
|
https://www.w3.org/2000/01/rdf-schema#label |
King Air 200
|
gptkbp:interior_features |
varied configurations available
|
gptkbp:landing_gear |
tricycle gear
|
gptkbp:length |
40 ft 4 in
|
gptkbp:maintenance |
requires regular maintenance checks
|
gptkbp:manufacturer |
gptkb:Beechcraft
|
gptkbp:market_segment |
light twin turboprop
|
gptkbp:max_speed |
300 knots
|
gptkbp:max_takeoff_weight |
12,500 lbs
2,500 ft required for landing 3,000 ft required for takeoff |
gptkbp:modifications |
winglets available
|
gptkbp:notable_users |
gptkb:aircraft
gptkb:Royal_Canadian_Air_Force various private operators |
gptkbp:operational_area |
suitable for various environments
relatively low operational cost |
gptkbp:performance |
good short field performance
|
gptkbp:production_years |
1966 to present
|
gptkbp:propulsion |
variable pitch
|
gptkbp:range |
1,500 to 1,800 nautical miles
1,800 nautical miles |
gptkbp:safety_record |
generally good safety record
|
gptkbp:seating_capacity |
3,000 lbs
up to 1,500 lbs 6 to 8 passengers |
gptkbp:service_ceiling |
35,000 ft
|
gptkbp:speed |
75 knots
|
gptkbp:training |
requires type rating for pilots
|
gptkbp:wing_area |
300 sq ft
|
gptkbp:wingspan |
54 ft 10 in
|
gptkbp:bfsParent |
gptkb:Beechcraft_King_Air
|
gptkbp:bfsLayer |
4
|