|
gptkbp:instanceOf
|
light sport aircraft
|
|
gptkbp:aircraft
|
high wing
light sport aircraft
8.8 lbs/sq ft
N-number_in_the_USA
|
|
gptkbp:avionics
|
modern glass cockpit
|
|
gptkbp:climbRate
|
800 ft/min
|
|
gptkbp:constructionMaterial
|
composite
|
|
gptkbp:controls
|
yoke
|
|
gptkbp:covers
|
split flaps
|
|
gptkbp:crew_size
|
2
|
|
gptkbp:customerService
|
global network
|
|
gptkbp:debutYear
|
2006
|
|
gptkbp:enginePower
|
100 hp
|
|
gptkbp:engineType
|
Rotax 912
|
|
gptkbp:firstFlight
|
2006
|
|
gptkbp:fuel_capacity
|
30 gallons
|
|
gptkbp:fuelType
|
MOGAS or AVGAS
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
8.5 feet
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Flight Design CTLS
|
|
gptkbp:inspiration
|
recreational flying
|
|
gptkbp:is_used_in
|
flight training
|
|
gptkbp:isATypeOf
|
S-LSA
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
22.5 feet
|
|
gptkbp:manufacturer
|
Flight_Design_GmbH
|
|
gptkbp:market_segment
|
light sport aviation
|
|
gptkbp:marketedAs
|
CTLS
|
|
gptkbp:maximum_speed
|
120 knots
|
|
gptkbp:maxTakeoffWeight
|
1,320 lbs
|
|
gptkbp:notable_feature
|
glass cockpit
|
|
gptkbp:operational_status
|
in production
|
|
gptkbp:origin
|
gptkb:Germany
|
|
gptkbp:passenger_traffic
|
20 knots
540 lbs
|
|
gptkbp:productionYears
|
2006 onwards
|
|
gptkbp:proportions
|
8.5
|
|
gptkbp:propulsion
|
variable pitch
|
|
gptkbp:range
|
600 nautical miles
|
|
gptkbp:region
|
global
|
|
gptkbp:regulatoryCompliance
|
FAR Part 23
|
|
gptkbp:safety_features
|
crash-resistant fuel system
|
|
gptkbp:service_ceiling
|
15,000 feet
|
|
gptkbp:speed
|
docile
100 knots
45 knots
|
|
gptkbp:surrounding_area
|
150 sq ft
|
|
gptkbp:takeoffDistance
|
60 knots
|
|
gptkbp:team
|
Flight_Design_GmbH_engineers
|
|
gptkbp:warranty
|
2 years
5 years
|
|
gptkbp:weight
|
780 lbs
|
|
gptkbp:wingspan
|
no
31.5 feet
|