AIRBUS A310-200/300

The A310 first began life as the A300B10, one of a number of projected developments and derivatives of Airbus' original A300B airliner.
While based on the larger A300, the A310 introduced a number of major changes. The fuselage was shortened by 13 frames compared to the A300B, reducing seating to around 200 to 230 passengers and a new higher aspect ratio wing of smaller span and area was developed. New and smaller horizontal tail surfaces, fly-by-wire outboard spoilers and a two crew EFIS flightdeck were incorporated, while the engine pylons were common to suit both engine options.

The first flight of the A310 occurred on April 3 1982, after the program was launched in July 1978. Service entry was with Lufthansa in April 1983. Early production A310s did not have the small winglets that became a feature of later build A310-200s and the A310-300. The A310-300 is a longer range development of the base A310-200, and has been in production since 1985. This version can carry a further 7000kg (15,430lb) of fuel in the tailplane.

MAIN panel

• EFIS
  ND, PFD, EWD, all the ECAM system pages reproduced in detail.

• Mag/true push button, Baro Reference Display Window Brakes,Radio,

• Analog instruments ,Distance and Radio Magnetic Indicator displays, clock,  Baro Reference Flaps indicator,Analog twoAltimeter(feed,meter)Airspeed Indicator

• Gear lever