OMA SUD presents:

the latest state of the art, innovative, piston twin: SKYCAR.

SKYCAR has been designed to be the actual sole multiutility/multipurpose aircraft in the General Aviation High Performance Piston marketplace with a opening bonnet on fly.

The internal layout is flexible and can be changed in various configurations and for different uses such as aero taxi, light cargo, and for special military and civil missions.

Its latest generation 3D Synthetic Vision Digital Glass Cockpit makes flying easier and safer.

The synergetic architecture makes possible:
an unequalled cabin volume that provides a top class passenger comfort and the largest baggage compartment in the same class aircraft.

Two tail boom and two engines mounted on the wing in pushed configuration less fuel and less D.O.C.


THE MISSION;
OMA SUD Engineering Team designed SKYCAR with the following key points in minds:

– High Aerodynamic efficiency;
– Top Class Passenger Comfort: more space, low internal noise;
– Flexibility to meet various mission profiles
– Last generation Avionic concepts of Glass Cockpit based on a safer and easier flying.


THE RESULT

Experience the exhilaration of flight: fly the difference, fly the innovation, FLY SKYCAR!

skycar-basico-TESTA

Aircraft dimensions

Fuselage height 2,55 m – 8,37 ft
Fuselage length 8,92 m – 29,27 ft
Wingspan 12 m – 39,37 ft
Cabin volume 4,98 m3 – 176 ft3
Max seating capacity 4/5
Fuel tank capacity 2×250 lt – 2×66 US Gal

Powerplant

Engine Manufacturer Lycoming IO-360 C1E6
Engine power 200 HP
Propeller Two-bladed Variable Pitch
Fuel consumption 31,9 lt/h – 8,43 US Gal /h
Fuel type Avgas

Measures

trittico-standard

Design Weigth & Loading

MTOW 1995 kg – 4400 lb
Useful Load 389 kg – 860 lb
Baggage Allowance 334 kg – 736 lb

Performance

Vmax 283 km/h – 153 kts
Cruise speed 75% 260 km/h – 140 kts
Stall speed 113 km/h – 61 kts
Pratical ceiling 5500 m – 18000 ft
Take off run 300 m – 984 ft
Take off distance 386 m – 1266 ft
Landing run 343 m – 1125 ft
Landing distance 528 m – 1732 ft
Rate of climb 5,9 m/s – 1160 ft/min
Range 55% ‘Best Economy’ 720 NM
Range 65% ‘Best Economy’ 700 NM
Range 75% ‘Best Power’ 570 NM

Interiors

The interiors design is based on an Automotive concept, with the interiors production like a expensive limousine , to offer comfort to the passangers.
– Two crew & passenger doors
– Rear windshield
– Front & Rear bonnets
– Front bonnet: to house electronics equipment, battery, electrical generation and distribution, avionics ..
– Rear bonnet: luggage ..

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Skycar Certification

08th Jenuary 2010
Type Certificate issued by EASA

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14th March 2011
Type Certificate issued by FAA

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04th July 2016
Type Certificate Acceptance by DGCA-India

INDIA-DGCA

SKYCAR COMPETITOR COMPARISON CABIN ACCESSIBILITY

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SKYCAR COMPETITOR COMPARISON EXTERNAL VISIBILITY ACCESSIBILITY

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COMPETITOR COMPARISON CROSS SECTION

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COMPETITOR COMPARISON CABIN COMFORT

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SKYCAR is designed to be easily disassembled…

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Avionics

SKYCAR is designed for a single pilot IFR operations.

The cockpit design philosophy is to keep it simple, but use state-of-the-art technology. It’s completely “glass cockpit” drives for:Enhancing situational awareness;

Improving system monitoring and control;The design is based on an integrated digital avionics suite, which concentrates most of avionic functions, and uses of a large-scale colour displays. In addition, dual sensor configuration increases A/C reliability.

The suite completely integrates flight instruments, autopilot, communication, navigation, optional weather radar and lightning warning systems, interfaces to engine indication and crew alerting, and to other aircraft systems, providing a highly reliable system designed for ease of operation and reduced cockpit workload.
The design implements comprehensive integrated architecture both for baseline and optional functions and equipment.

Basic Avionics Package
#1 Primary Flight Display (PFD)
#1 Multi Function Display (MFD)
#1 Analogy Interface Unit
#2 Air Data Attitude Heading Reference System (ADAHRS)
#1 GPS/WAAS Receiver
#2 VHF Communication Radio/ VHF Nav function and GPS Receiver
#1 Two – axis fail-safe Auto Flight Control System (AFCS),
#1 Audio Panel with Marker Beacon
#1 Mode-S ATC Transponder
#1 Emergency Locator Transmitter Tx
#2 Engine Monitoring System
Electrical Stand-by Instrument System provides triple architecture redundancy with the following equipments:
1# Electrical Attitude Indicator – 2 inch
1# Airspeed indicator – 2 inch
1# Altitude Indicator – 2 inch
1# Magnetic Compass
Optional Avionics Package
#1 2nd Co-pilot Primary Flight Display (PFD)
#1 2nd Co-pilot Multi Function Display (MFD)
#1 ADF Receiver
#1 DME Receiver
#1 Radar Altimeter
#1 Weather Radar Sensor
#1 Stormscope ®
#1 TAS
Powerplant
Skycar aircraft is powered by two Lycoming engines IO-360 C1E6.
It is a reliable aircraft engine that powers almost the 80% of the General Aviation Aircraft around the world.
– Engines
SKYCAR is powered by two Lycoming engines IO-360-C1E6 installed in pusher configuration. Engines are fuel injected and supply 200 Hp ea @ 2700 RPM. Lycoming is a reliable aircraft engine that powers almost the 80% of the General Aviation Aircraft around the world.
engines
– Propeller
2-Blade Constant Speed Hydraulically Controller with Feathering Propeller, Hartzell.
engines
– Cowling
Engine cowling has been designed through the aid of CFD methods to reduce cooling drag and to improve engine cooling both on ground and in flight.
engines
Landing Gear
The retractable landing gear employ three electrical actuators with a backup mechanical emergency extension system to provide both normal and emergency operations. Emergency operation consists in pulling the red lever for 14 times. engines
Features
  • Less components, low costs;
  • Electrical actuation increase reliability compared with the hydraulic one;
  • Emergency mechanical actuation is more reliable than the pneumatic or gravity one;
  • Each actuator is independent on the others;
engines
Other Systems
Flight control systemsThe Skycar Aircraft is designed with superb pilot handling in mind. Emphasis is placed on ease of control, flight safety and system redundancy.
The primary flight controls are of conventional type operated by dual control wheels and dual rudder pedals; they are constituted by push-pull rod:
– Ailerons
– Stabilator all movable
– Twin rudder
– Steering, with automatic in-flight disengagement;
Features
• Increased safety and reliability
• Low backlash
• Improved control feeling
• Easy maintenance operations
• Low maintenance costs
• Dual redundant, dual rudder control
Secondary flight controls are electrically actuated:- Flap;
– Rudder Trim;
– Pitch trim/tab;
Features• State of the art technology;
• Reduced pilot workload;
• Easy operations;
• Electrical indicators for secondary surfaces position;
• Redundant control system for the pitch trim/tab; .

Anti Ice system
The A/C is not certified for flying in known icing conditions.
A propeller electrical de-ice is provided as standard equipment, while a wing de-ice system is provided as optional equipment.

Fuel
Two tanks are provided in each wing (250 litres each).
The fuel system is designed taking into account:
– Safety – Reliability
– Easy Operations
– Reduced pilot workload
– Maintenability

Features:
• Tank design prevents the interruption of fuel supply also in long non steady manoeuvres;
• Low shut-off time;
• Fast fuel supply when shifting to X-Fed;
• Reliable resistive fuel indicator;
• Lighted overhead fuel control panel.

The available fuel type is AvGas 100 or 100LL grade.