الطائرة Legend 600

Introduction

LSA Legend 600 is intended for elementary pilot training of PPL holders, and for traveling. Thanks to low operating costs, it is possible to obtain PPL for the cheapest price possible. Great performance and extra utilizable load allow comfortable and fast traveling. LSA Legend 600 is a full-composite upper wing monoplane made of sandwich materials. Thanks to modern composites, the aircraft exhibits low empty weight and thus also high utilizable load.

Specification

Specification:

Wing Span:	9.06 m
Wing Area:	10.54 m²
Length:	7 m
Height:	2.6 m
Empty Weight:	335 kg
Maximum Take-Off Weight:	600 kg
Maximum crew weight:	200 kg (ROTAX 912 ULS)
Maximum luggage weight:	30 kg
Fuel Tank Capacity:	110 l (130 l)
Performance:	Rotax 912 ULS 100 HP
Speed with flaps:	62 kph
Minimum Landing Speed:	65 kph
Max. Speed, Flaps 40^º:	120 kph
Max. Speed, Flaps 15^º, 30^º:	145 kph
Rough Air Speed	170 kph
Cruise Speed (75 %):	210 kph
Max. horizontal flight speed:	225 kph
Never exceed speed:	225 kph
Range:	1300 km (7 hours)
Climb rate (at ground level):	7 mps

AIRCRAFT ADVANTAGES
- The high standard of the very spacious crew cabin.
- More comfortable boarding and baggage handling.
- Length and height-adjustable seats for pilots of all heights.
- Perfect view from the cabin.
Ergonomics
- Rigid controls.
- Upper pedals.
- Electrical trim on the control yoke.
- Radio controls on the control yoke.
- Flap controls on the throttle lever.
- Parking brake.
Comfort
- More efficient two-zone heating.
- Luxurious leather interior
- Door pockets
- Tilting central armrest
- Sun visors.
Functionality
- Oil preheating
- Spring shock absorber on the front wheel
- Highly effective 3-position flaps
- Possible quick conversion to cargo
- Blocking of flap activation at speeds exceeding 140kph
Design
- Impressive metallic designs.
- Complete ceiling cushioning.
- Leather interior or Alcantara
Flight characteristics
- Excellent flying characteristics and performances
- Easy flight control and stable flying
- Smooth take-off and landing
- Take-off run: 90 m
- Take-off distance to 50 ft: 200 m
- Landing distance from 50 ft: 135 m
- Climb rate at maximum take-off weight: 5.9 MPs
- Horizontal speed 4300 RPM, manifold pressure 27: 195 kph
- Minimum speed – behavior when nearing stall speeds, flap positions:
  - 0^° 77 kph
  - 15^° 68 kph
  - 30^° 60 kph
  - 40^° 57 kph