Airbus A310 for sale

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  • Airbus A310 VIP for sale and lease – Year 2013 – TTAF 9114 – Price on request

Airbus A310-300
1993 (YEAR)
65400 (TTAF)
POR

Airbus ACJ320
2002 (YEAR)
29300 (TTAF)
POR

Airbus A340
2005 (YEAR)
43000 (TTAF)
POR

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

Airbus ACJ319
2013 (YEAR)
1180 (TTAF)
POR

Airbus ACJ319
2009 (YEAR)
6400 (TTAF)
POR

Airbus A340
1997 (YEAR)
46000 (TTAF)
POR

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Information about Airbus A310 

At the beginning of 1982, the Airbus Industry consortium announced the development of a version of the A310-300 aircraft for operation on routes longer than the A310-200 aircraft. Officially, the development of the aircraft began in March 1983 after the start of deliveries of aircraft A310-200. The main difference of the A310-300 aircraft from the original one is the presence of an additional fuel tank with a capacity of 6100 liters in the horizontal tail unit and the application of an automated fuel transfer system to maintain optimal balancing of the aircraft in flight. At the ends of the wing, small arrow-shaped aerodynamic surfaces (“washers”) were installed, which later became installed on A310-200 aircraft.

The first flight of the prototype A310-300 with Pratt & Whitney JT9D-7R4 engines took place on July 8, 1985, and the first flight of the aircraft with General Electric CF6-80C2 engines in September 1985. The certification of the aircraft was completed in December 1985, and the same month, the Swiss airline Swisser received the first aircraft. In October 1991, the A310-300 aircraft was certified by the Aviaregistr of the Russian Federation, as a result of which it received the right to operate in Russian airlines. Currently, Aeroflot-Russian International Airlines has 10 A310-300 aircraft, two of which are leased from the Yakut airline Diamond Saha. Several А310-200 and -300 airplanes are used in the air forces of a number of countries (Canada, Germany, France and Thailand) for the transportation of high-ranking officials, as well as military transport vehicles. In 1995, one A310-300 aircraft was converted into a transport aircraft MRTT. The MRTT aircraft can carry a variety of military cargoes, as well as additional fuel weighing 28 tons, designed for refueling one or two aircraft in flight.

The aircraft is equipped with the EFIS digital avionics complex, which consists of four multi-color display to display the necessary information about the flight, and a digital system for monitoring the operation of on-board systems and warning of failures ESAM. Radio navigation equipment complies with the ARINC 700 standard. Serially produced since 1985. By the beginning of 1997, 176 aircraft of this modification were sold, 167 were delivered. The total number of A310 aircraft sold to mid-1997 is 261, of which 249 aircraft were in operation.

Airbus A310 modifications:

  • Airbus A310
  • Airbus A310-200
  • Airbus A310-300
Model A310-200 A310-300
Crew Two
Length 46.66 metres (153 ft 1 in)
Height 15.8 metres (51 ft 10 in)
Wingspan 43.9 metres (144 ft)
Wing area 219 m2 (2,360 sq ft)
Wing sweep 28 °
Cross section 5.64 metres (18 ft 6 in)
2-class 220 passengers (20F + 200Y)
1-class 237Y 8-abreast 243Y 8-abreast / 265Y 9-abreast
Maximum Payload 32,834 kg (72,386 lb) 37,293 kg (82,216 lb)
Exit limit 275 passengers
Lower deck cargo 14 LD3 containers
MTOW 144,000 kg (317,465 lb) 164,000 kg (361 557 lb)
MLW 122,000 kg (268,963 lb) 124,000 kg (273,372 lb)
MZFW 112,000 kg (246,917 lb) 116,500 kg (256,838 lb)
OEW CF6—80: 79,207 kg (174,619 lb), JT9D: 77,397 kg (170,631 lb), PW4000: 79,166 kg (174,528 lb)
Max fuel 61,070 L 16,132 US gal
Cruise speed (M) Mach 0.8 (459 kn)
MMO Mach 0.84 (482 kn)
Ceiling 41 100 ft. (12 530 m)
Thrust (×2) 20,380–25,740 decanewtons (45,800–57,900 lbf)
Engines JT9D-7R4 / GE CF6-80 JT9D-7R4E1 / PW4000 / CF6-80C2
Range 3,500 nmi (6,500 km)  5,150 nmi (9,540 km) 

Source: https://en.wikipedia.org/wiki/Airbus_A310

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