Airbus A319 ACJ for sale

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  • Airbus A319 ACJ for sale and lease – Price on request

Airbus ACJ319
2013 (YEAR)
1180 (TTAF)
POR

Airbus ACJ319
2009 (YEAR)
6400 (TTAF)
POR

Airbus A340
1997 (YEAR)
46000 (TTAF)
POR

Airbus ACJ320
2002 (YEAR)
29300 (TTAF)
POR

Airbus A340
2005 (YEAR)
43000 (TTAF)
POR

Airbus A330-200F
2010 (YEAR)
24000 (TTAF)
POR

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Information about Airbus A319 ACJ

A319CJ Corporate Jetliner is a long-haul passenger aircraft of enhanced comfort, developed by the Western European consortium Airbus based on the medium-haul passenger aircraft Airbus A319. The aircraft was built as a European alternative to the Boeing Business Jet, Bombardier Global Express and Gulfstream V.

For the first time the aircraft was presented in 1997 at the Paris Aviation Exhibition. The first built Samoyel was removed from the hangar plant in Hamburg in October 1998. Aircraft certification was planned to be completed by the end of 1999. At the same time it was planned to begin mass production of aircraft.

By the end of 1998, several aircraft were ordered, including for a private person from Kuwait, 2 aircraft for the Italian Air Force and for Taiwan’s Eva Air. Unlike the Boeing Business Jet, the Airbus A319CJ was created with minimal design changes in the aircraft design, which allows Airbus to be more flexible in its customer orders. The cost of the aircraft with standard equipment is 35 million dollars.

Cockpit crew Two
Exit limit 160 / 150
1-class max. seating 156 at 28–30 in (71–76 cm) pitch
1-class, typical 134 at 32 in (81 cm) pitch
2-class, typical 124 (8F @ 38 in, 116Y @ 32 in)
Cargo capacity 27.7 m3 (980 cu ft)
Unit load devices 4× LD3-45
Length 33.84 m (111 ft 0 in)
Wheelbase 11.04 m (36 ft 3 in)
Track 7.59 m (24 ft 11 in)
Wingspan 35.8 m (117 ft 5 in) 
Wing area 122.4 m2 (1,318 sq ft)
Wing sweepback 25 degrees
Tail height 11.76 m (38 ft 7 in)
Cabin width 3.70 m (12 ft 2 in)
Fuselage width 3.95 m (13 ft 0 in)
Fuselage height 4.14 m (13 ft 7 in)
Operating empty weight (OEW) 40.8 t (90,000 lb)
Maximum zero-fuel weight (MZFW) 58.5 t (129,000 lb)
Maximum landing weight (MLW) 62.5 t (138,000 lb)
Maximum takeoff weight (MTOW) 75.5 t (166,000 lb)
Cruising speed Mach 0.78 (829 km/h; 515 mph)
Maximum speed Mach 0.82 (871 km/h; 541 mph)
Range, typical payload[d] 3,750 nmi, 6,950 km
ACJ range 6,000 nmi, 11,100 km
Takeoff (MTOW, SL, ISA) 1,850 m (6,070 ft)
Landing (MLW, SL, ISA) 1,360 m (4,460 ft)
Fuel capacity 24,210–30,190 L (6,400–7,980 US gal)
Service ceiling 39,100–41,000 ft (11,900–12,500 m)
Engines (×2) CFM56-5B, 68.3 in (1.73 m) fan
IAE V2500A5, 63.5 in (1.61 m) fan
Thrust (×2) 98–120 kN (22,000–27,000 lbf)

Source: https://en.wikipedia.org/wiki/Airbus_A319

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