Saturday, February 16, 2013

Average Jet Charter Rates


Average Jet Charter Rates (Per Hour)


Gulfstream 550
$8,640
GlobalExpress/XRS
$8,045
Falcon 7X
$7,865
Falcon 900
$6,075
Gulfstream IV
$5,884
Challenger 604
$5,053
Citation X
$4,533
Hawker 800
$3,582
Citation Excel/XLS
$3,388
Learjet 60
$3,347
Citation Mustang
$1,674

Monday, February 11, 2013

New aircraft in the Ijet Aviation fleet: Airbus A318- Elite

Airbus A318- Elite 






CHARACTERISTICS

 Seating 4+18/120 
Wing loading 110.4 
Power loading 0.32 
Noise (EPNdB): To/Sideline/Apr 82.2/92.0/93.9 

DIMENSIONS 

  External -    
                                 
  Length  103.2 
Height 42.1 
Span 111.8 

Internal -      
                
Length (O/A Net)  70.2/70.2 
Height 7.4 
Width: Max /floor 12.2/11.6 

BAGAGGE  

Internal -  Cu. ft / lb  330/NA

External -  Cu. ft / lb  680/NA 

POWER 

 Engines 
2 CFMI 
CFM56-5B9-P 
Output(lb. ea)/Flat rating 23,300/ISA +15°C 
Inspection interval OC 

WEIGHTS (lb) 

Max  Ramp 146,390 
Max Takeoff 145,505 
Max Landing 126,765 
Zero fuel 120,150 

BOW/OWE 

93,720 
Max payload 26,430 
Useful load 51,785 
Executive payload 3,600 
Max Fuel 45,761 
Available payload with Max fuel 6,909 
Available fuel with Max payload 26,240 
Available fuel with exec payload 49,070 

LIMITS 

 Mmo 0.820 
Trans Alt FL/Vmo 26,400ft/0.82M/350Kts 
PSI 8.3 

Monday, February 04, 2013

Ijet Aviation: Agusta 109 Power


AGUSTA 109 POWER


The Agusta A109 respectively AW109 is a light eight-seat twin-engine multi-purpose helicopter produced by the Italian manufacturer Agusta (today AgustaWestland) since 1971. The A109 is in use of both civil and military operators, and now its part of our extensive fleet of aircrafts.









Crew:                    1-2

Passengers:           6-7

Propulsion:           2 Turboshaft Engines

Engine Model:     Allison / Rolls-Royce 250-C20B

Engine Power (each):  313 kW 420 shp

Max. Cruise Speed:  278 km/h, 150 kts, 173 mph

Max. Speed (vne):    311 km/h, 168 kts, 193 mph

Service Ceiling:        4.572 m, 15.000 ft

Rate of climb:           503 m/min, 1650 ft/min

Range:                       948 km, 512 NM, 589 mi.

Empty Weight:         1.418 kg, 3.126 lbs

MTOW:                    2.600 kg, 5.732 lbs

Rotor Blades (main/tail):  4/2, 4/2

Main Rotor Diameter:      11,00 m, 36,1 ft

Tail Rotor Diameter:        2,03 m, 6,7 ft

Rotor Disc Area:              95,0 m², 1023 ft²

Length (Fuselage):           11,45 m, 37,6 ft

Length:                             13,04 m, 42,8 ft

Height:                              3,40 m, 11,2 ft