19
2500 km
Innovative technology platform belonging to the family of promising STOL aircraft with a capacity of 19 passenger seats
General view. Main flight performance data.
Comparative analysis of the main geometric dimensions
24,21 m Е-20Х DOCKER (including wingtip)
22,0 m Е-20Х DOCKER (without wingtip)
22,063 m (M-28PZL)
m19,81 м (DHC-6)
m19,48 м (L-410NG)
m16,97 м (DO-228NG)
16,42 m Е-20Х DOCKER
16,56 m (DO-228NG)
15,77 m (DHC-6)
15,07 m (L-410NG)
13,10 m (M-28PZL)
Design and technological features of the E-20 X aircraft family
Advanced materials
The design uses advanced materials, including thermoplastic composite (60%) and aluminum -lithium alloys (40%)
Technical control system
The on-board system for technical control and maintenance of the aircraft covers 100% of the aircraft's systems, which increases reliability, safety and reduces downtime
Wing design
Advanced wing design provides a significant advantage in aerodynamics and weight efficiency, short take-off and landing (STOL)
Manufacturing procedure
For the production of items and aggregate assembling of structural elements using advanced digital technologies
Aircraft systems
Aircraft systems of new generation provide additional functionality, increase reliability and safety, and also reduce the weight of the structure
Less turbulence
Intelligent sensors detect turbulence and regulate control surfaces, dampening movement and reducing motion-induced sickness of passengers
CFRP air propeller
Carbon PCM (CFRP) air propeller with anti-ice system has 14% less weight compared to similar aluminum alloys, and aerodynamic profiling provides 8% more thrust in cruising mode
Landing gear design
Taxiing, takeoff and landing on unpaved, snowy, icy airfields, including on airfields with a ground strength of 4.5 kg/cm2
К=24 Aerodynamic efficiency of aircraft
ATR (active turbulence reduction) Active turbulence reduction system
HUD (Head-Up Display) Head-Up Display and information display system
Al - Li The widespread use of aluminum-lithium alloys in the construction of the airframe
4 PFD/MFD Digital "glass cockpit" manufactured in Russia
EVS/SVS (optional) Enhanced vision system or synthetic vision system
+50С…−60С Temperature range of operation, including in the conditions of the Arctic zone
UHAR (ultra high aspect ratio wing design) Aerodynamic design of ultra high aspect ratio wing
Weather radar (optional) Weather radar with turbulence detection function
ANVS (Active Noise and Vibration Suppression System) active noise and vibration suppression system in the passenger cabin
Ultra light prop Ultra light prop made of carbon polymer composites
Ramp loading (cargo version) Ramp loading, the possibility of landing paratroopers and cargo
STOL Wing high lift devices and aerodynamic configuration of the aircraft provide a short take-off and landing
Anti-Ice Anti-ice system of the wing, vertical and horizontal stabilizers
Features of the E-20X passenger cabin
More cabin luggage
The luggage rack allows to place more standardsized cabin luggage for aircraft of class CS-23
The luggage rack allows to place more standardsized cabin luggage for aircraft of class CS-23
Ergonomic seats
Reduced backrest thickness expands living space, while design and materials provide maximum comfort
Reduced backrest thickness expands living space, while design and materials provide maximum comfort
More personal space
The wide-body fuselage in the CS-23 class aircraft provides free movement during landing and exiting the aircraft
The wide-body fuselage in the CS-23 class aircraft provides free movement during landing and exiting the aircraft
More light
Natural lighting (large portholes) in combination with artificial lighting create an atmosphere of comfort
Natural lighting (large portholes) in combination with artificial lighting create an atmosphere of comfort
Comfort for passengers with reduced mobility
Wide entry space and increased aisle width between the seats provide comfort for passengers with reduced mobility.
Wide entry space and increased aisle width between the seats provide comfort for passengers with reduced mobility.
Lower noise level
The cabin has a reduced noise level compared to the CS-23 class aircraft, which provides psychological comfort during long-range flights
The cabin has a reduced noise level compared to the CS-23 class aircraft, which provides psychological comfort during long-range flights
Healthy environment
The air conditioning system provides multi-zone temperature and humidity control in the cabin
The air conditioning system provides multi-zone temperature and humidity control in the cabin
Comfort technologies for passengers of the E-20X aircraft family
+30% view increase and improved comfort
Lack of discomfort during the flight and the feeling of confined space
Smart ergonomics and design of the seats ensure the comfort of passengers during long-range flights
Comfort / Prestige
860 мм
1070 mm
Total weight of luggage and cabin luggage per passenger
33 kg
Possibilities for the transportation of cargo, airfreight containers and pallets.
Comparative analysis of the aircraft basic specifications
Comparative analysis of takeoff and landing performance data
Total distance over 50 ft obstacle**, ISA, H = 0 ft (SL)
Take-off run ISA**, H = 0 ft (SL)
EV-55
342 m
342 m
DHC-6
349 m
349 m
Е-20Х
407 m
407 m
С-208В
417 m
417 m
Do-228NG
469 m
469 m
М-28PZL
494 m
494 m
L-410NG
500 m
500 m
L-410NG
590 m
590 m
408 Cessna
1006 m
1006 m
Е-20Х
499 m
499 m
STOL – short takeoff and landing
ISA – international standard atmosphere
* – data obtained by analytical method
** – takeoff run distances are not to scale
ISA – international standard atmosphere
* – data obtained by analytical method
** – takeoff run distances are not to scale
FAR Part 91 – General Operating and Flight Rules FAR Part 121 – Certification and Operations: Airplanes Having a Seating Capacity of 20 or More Passengers or a Payload Capacity of 6,000 Pounds or More FAR Part 135 – Operating Requirements: Commuter and On Demand Operations and Rules Governing Persons on Board Such Aircraft Balanced Field Length (BFL) is the distance obtained by determining the decision speed (V1) at which the take-off distance and the accelerate-stop distance are equal (fixed-wing multi-engine aircraft only). BFL is based on a Dry Level Runway, No Wind, NBAA IFR Reserves and 86 degrees F.
Comparison of the flight range depending on load, weight limits, competitive advantage
E-20X RATIONING OF WEIGHT, WEIGHT OF LUGGAGE AND CABIN LUGGAGE
The combined mass of one passenger with luggage and cabin luggage
119 kg
86 kg
23 kg
10 kg
AP-23 WEIGHT RATIONING, CS-23 WEIGHT LIMITS
86-95 kg
77-86 kg
The combined mass of one passenger with luggage and cabin luggage
The weight of luggage and cabin luggage is determined by the airline, but according to statistics it does not exceed 10 kg per passenger for light aircraft of category CS-23
Competitive comparison of flight range and aircraft load
Competitive comparison of weight indicators, fuel efficiency
Contact us at:
SAIF Executive Office P8-06-63
Sharjah - U.A.E
phone: +971 50 849 0302
e-mail: info@docker.ae