Logo
Search
  Search
Airplanes by
Manufacturer -
Helicopters by
Manufacturer -
 
  Home - Future aircrafts - Twin Turboprops - OMA SUD - OMA SUD Skycar

OMA SUD Skycar

   
- Current Price 960,000 U.S. $ * ( 2014)

Mixing Practicality With Innovation The OMA SUD Skycar...........

 
Go to -  
 
 
Manufactured
from -

2010 - Onwords
Seating Chart
/ Seats -

5
Travel Range -
2,253.00 Kilometer
1,217 Nautical Miles
County of
Manufacture -

Italy
Editor Rating
( Out of 10 )
7.50
Avg. Pilot Rating
( Out of 10 )
0.00
Avg. Passenger /
Fan Rating
0.00
Total points collected
in last 30 days
1
Blank
 
Photo Copyright Policy!              Company :OMA SUD
Ranking Class: Private Turboprops Rank - 50
Blank
Aircraft
OMA SUD Skycar the future is gorgeous
 
 
Give Points to
This Aircraft
1 2 3 4 5 6 7 8 9 10
 

Photo Gallery - OMA SUD Skycar
blank blank
* Picture of aircraft interiors including charter aircraft, private jets, passenger airplanes, helicopters and military aircraft. Please feel free to report to us about the images in the photo gallery.
BACK TO TOP
  Aircraft Description-

The OMA SUD Skycar feature innovations in both aerodynamic configuration and avionic installation. It has a twin-boom configuration with a twin vertical tail and the two engine mounted in pusher position on the high wing. The horizontal tail is completely mobile. This configuration make the SKYCAR a unique design with a clean and sharp line. Although its dimension are contained, its internal volume is notably superior to that of its competitor, permitting exceptional comfort for the passengers and elevated cargo capacity, characteristics which not other aircraft of its class can boast.

It is the twin boom configuration that has, moreover, permitted the SKYCAR to offer a rear door that can open in flight; this special opening system (unique on this class of aircraft), together with the internal volume in cargo configuration (about 200 ft3 ) and the wide cargo platform, ensures that during ground operations, loading of baggage, or stretchers or pallets etc, is simplified, while during flying operations it is possible  to perform air delivery of medicines, clothing, foods, and also general rescue equipment, such us dinghies and other kit.

The compact dimensions (12 mt. Wing span and 8,92 mt lenght) do not actually penalise the internal volume (6,80 m3  / 240 ft3 ), obtained with the un-pressurised fuselage, which is more than 165 cm. wide.


 

Special configurations with ad hoc instrumentation are available for more wider usage in the military, paramilitary, civil defence and environmental fields thanks to a basic platform which is highly functional and easily adaptable to a variety of uses.

The SKYCAR is fitted with a  retractable undercarriage predisposed for operations from unprepared grass or dirt strips and features latest generation digital instrumentation (full glass cockpit). The prototype  made its first flight from Capua on 21 december 2007, piloted by Test Pilot Maurizio Cheli. Currently the aircraft has flown for some 150 hours, and the trials program was scheduled for completion for the beginning of the summer 2009, with the granting of the relative Type Certificate by EASA/ENAC. From a commercial point of view, several contacts are in course with some potential government clients on an international level, and the first deliveries could take place in the first half of 2010.

  Related News : The Innovative OMA SUD SKYCAR  Date: 7th May, 2009

 
Good Points about the Aircraft -
Innovation - Variety in usage
Bad Points about the Aircraft -
Price may seem a little high
 
 
Specs -
 
 
  Engine -
  2 X Lycoming IO-360-C1E6 pistons
  Power -
  200.00 Horsepower
  Avionics -
  3D Synthetic Vision Digital Glass Cockpit
  Maximum Cruising Speed -
 
348.00 km per hr     216.25 mph
  Service Ceiling -
 
5,486.40 metres     18,000.00 feets
  Rate of Climb -
 
533.40 mpm     1,750.00 fpm
  Numbers Ordered/Sold -
0
Cabin Height -
 
N/A      N/A
  Cabin Width -
 
N/A      N/A
  Cabin Length -
 
N/A      N/A
  Exterior Length -
 
8.92 metres     29.26 feets
  Wingspan / Rotor Diameter -
 
12.00 metres     39.37 feets
  Fuselage Diameter -
 
N/A      N/A
  Baggage Volume -
 
1.81 cubic metre     64.00 cubic feet
  Maximum Take Off Weight -
 
1,990.00 kgs      4,387.15 lbs
  Maximum Payload -
 
610.00 kgs     1,344.81 lbs
  Fuel Tank Capacity -
 
132.00 gallon     499.67 litres
  Fuel Economy -
 
4.50 km per litre10.58 NM per gallon
  Minimum Take Off Distance -
 
299.92 metres984.00 feets
  Minimum Landing Distance -
342.90 metres1,125.00 feets
 
 
 
BACK TO TOP
 
 
     
blank
User Reviews ( Review as Pilot / Passenger / Fan )
blank
1 Review Per Member For 1 Aircraft - Review and Ratings Once Posted Cannot Be Removed By The Memners Irrelevant Reviews Will be removed by the Admin
 
 
View by Category