1in may, 994, Boeing bought a second-hand A320 aircraft and displayed it in Seattle to inspire Boeing employees, which may be Airbus's greatest honor. A320
Airbus Industrial Company Europe 1979 announced the A320 passenger plane scheme, 1983 officially launched the A320 plan in February, 1987 conducted the first flight test on February 22, and 1988 obtained the airworthiness certificate and delivered it in February. The main models are:
A320- 100 basic model, produced by * * * 2 1. 1988 delivered to air France for the first time in March;
The A320-200 remote model is the product after the 22nd one on the production line. The difference between A320-200 and 100 is that the central wing fuel tank is adopted, which increases the payload and range. The first one was delivered to Anse Airlines on July 1988.
A320-200 Basic data:
Span (m) 34.09
Captain (male) 37.57
Machine height (m) 1 1.76
Standard two-class cabin layout passenger (person) 150
Cargo hold volume (m3) 37.42
Commercial load (ton) 16.3
Empty weight (ton) 4 1
Maximum tank capacity (liter) 23860
Maximum gross takeoff weight (ton) 73.5
The maximum cruising speed is Mach 0.82.
Range (km) 5000
Power plant two turbofan engines
Engine model CFM company CFM56-5 series; IAE company V2500 series; Puhui PW6000
A32 1
The first project of European Airbus Industry Company was completely completed through commercial financing. Compared with A320, the extended model directly derived from A320 has 24% more seats and 40% more space. Two emergency exits are added at the front and rear of the wing, and the wing is partially extended. The project started in May 1989 and made its maiden voyage in March of the same year 1 1. The main models are: A32 1- 100 basic model; A32 1-200-200 extended flight type,1995 was established in April.
Main parameters of A32 1-200
The fuselage length is 44.51m.
The fuselage width is 3.96 meters.
Wingspan 34.09 meters
The height of the machine is11.76m.
The cabin length is 34.44 meters.
The maximum cabin width is 3.70 meters.
The number of seats in the second class is186; Number of seats in single-deck cabin 220
Cargo hold volume (m3) 5 1.76
Commercial load (ton) 2 1.6
The empty machine weighs 48200kg.
Maximum tank capacity (liter) 29680
The maximum takeoff weight is 93,500 kg.
The maximum cruising speed is Mach 0.82.
Maximum service limit (m): 12000
Whole journey (km) 5600
Power plant two turbofan engines
Engine model CFM company CFM56-5 series, IAE company V2500 series.
A3 19
Compared with A320, the shortened model directly derived from A320 has a shorter fuselage, which is 3.73 meters. There is an emergency exit on the wing, and the bulk cargo compartment at the rear of the fuselage is cancelled. /kloc-0 was established in June, 1993./kloc-0 made its first flight in August, 1995, was awarded to type certificate in April and put into use in May. The main models are: A3 19 basic model, A3 19CJ model and commercial model.
A3 19- 100 Main parameters
The fuselage length is 33.84m m.
The fuselage width is 3.96 meters.
Wingspan 34.09 meters
The height of the machine is11.76m.
The cabin is 23.77 meters long.
The maximum cabin width is 3.70 meters.
The number of seats in second class is 124, and the number of seats in first class is 142.
Cargo hold volume (m3) 27.64
Commercial load (ton) 12.9
The empty machine weighs 40600kg.
Maximum tank capacity (liter) 29840
The maximum takeoff gross weight is 75,500 kg.
The maximum cruising speed is Mach 0.82.
Full-load voyage 6800 kilometers (3700 nautical miles)
Power plant two turbofan engines
Engine model CFM company CFM56-5 series, IAE company V2500 series.
A3 18
1On April 26th, 1994, the A3 19 shortened 100 passenger plane A3 18 was officially launched. A3 18 continues to be common with A320 series, providing customers with a new choice of 100 class passenger aircraft. June 5438+1October 65438+May, 2002, and will be delivered soon.
A3 18 Main parameters
The fuselage length is 31.45m..
The fuselage width is 3.96 meters.
Span (m) 34.09
Machine height (m) 12.56
Engine room length is 21.38m.
The maximum cabin width is 3.70 meters.
The number of seats in the two-class cabin layout is 107.
Cargo hold volume (m3) 2 1.2438+0
Commercial load (ton) 1 1. 1
The empty machine weighs 39300kg.
Maximum tank capacity (liter) 23860
The maximum takeoff weight is 68,000 kg.
The maximum cruising speed is Mach 0.82.
The voyage is 6000 kilometers (3250 nautical miles)
Power plant two turbofan engines
Engine model CFM company CFM56-5 series, Pratt & Whitney PW6 122.