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Aviation
safety
+7 (3462) 555-751
General questions
+7 (3462) 555-446
Aerial works
+7 (3462) 555-751 (202)
Charter flights

 

 

 

 

 

 

AGUSTA AW109 GRAND NEW

   It’s a light multipurpose Italian helicopter.  Equipped with gas turbine engines Pratt & Whitney with electronic control system FADEC, which ensures low fuel consumption. Robust airframe (cocoon) in addition to the impact-resistant fuel system and shock-proof seats for the pilots and passengers provides a high level of security.

 

   Helicopter has a retractable tricycle landing gear with nose self-castoring wheel. The main and tail rotor have the optimized geometric parameters, which allows to achieve the high aerodynamic stability and to reduce the noise to a level lower than required by the ICAO standards. Also, this aircraft is the first in a class of light helicopters equipped with synthetic vision system SVS and Helicopter Terrain Awareness and Warning System (HTAWS), which is capable to display a relief of the underlying surface and artificial obstacles.

 

   Type of helicopters like Agusta AW109 Grand New is an example of a successful combination of high performance and low operating costs. Excellent flight performance characteristics, unmatched security and reliability levels.  These helicopters are successfully used for the comfortable transportation of passengers, search and rescue, marine and medical operations, using border authorities, law enforcement agencies, as well as perform the function of patrolling and monitoring.

 

   SKOL Airline helicopter is additionally equipped with a special removable medical unit allowing the transportation of bedridden patients in need of emergency medical care, which allows to use a helicopter for evacuation operations.

 

Aircraft configuration options:

– 1 bedridden patient + 3 accompanying

–  6/7 of passengers

 

Our Park - 1 unit

 

 

TECHNICAL CHARACTERISTICS

 

Engine...........................................2 х Pratt & Whitney Canada PW206C

Take-off power (horsepower)..........................................…..……..2х640
Aircrew…..........……...............................................................……….1-2
Passengers…..…........................................……………......................6-7
Full take-off weight, kg…......................................……………....2850
Fuel margin, l.....................….…...........................................…….....605
Base weight without load, kg…......................................……………1570
Load on the external sling, kg ...........……………......................…..1000
Max. speed, km/h.................................................................………..311
Cruising speed, km/h..................................................……………….285
Service ceiling, m.............................................…...................….…5974
Range, km......………...............................................................……..948

 

Diameter of rotor blades, m.......................……………........................11
 
 
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