Use of advanced technology and construction such as composite materials
Results in unmatched fuel efficiency, reduced maintenance costs, and increasedreliability
Airbus A320
Controlled by a computer managed fly-by-wire system
Offers protection against exceeding normal flight envelope
Airbus Industries
A consortium of 4 European aerospace companies
Components manufactured by Airbus Industries consortium
Tail section, flaps, and spoilers by Daimler Benz's Airbus in Germany
Wing section by aerospace from England
Horizontal stabilizers and elevators, nose landing gear doors, and forward cabin entry doors by CASA in Spain
Forward fuselage and engine pylon by Aerospatiale in France
Engines come from CFM International and all components are shipped to Toulouse, France for final assembly
Beluga A300-600 ST (Super Transporter)
Based on an A300-600
Large enough to carry fuselage sections or two complete A320 wings
CFM56-5 engines
High bypass turbofan engines producing 25,000 lbs of thrust at sea level
Produced by CFM International, a joint venture between Snecma in France and GE Aircraft in the USA
Airbus A320 cockpit
Designed for two-man crew operation
Can accommodate up to two observers
Airbus A320
Two large cargo compartments and one baggage compartment under the main cabin floor
Cargo floor fitted with automatic ULD loading system, can be delivered without the system and cargo must then be manually loaded
Airbus A320
Pressurized for passenger and crew comfort, except for the nose cone section where the radar antennae are housed, the air conditioning compartment, and the APU section
Airbus A320
123 feet 3 inches long, 38 feet 7 inches high to the top of the tail, and 111 feet 10 inches wide (wing tip to wing tip)
Airbus A320 nose wheel
Controlled by two algebraically interconnected steering handwheels located on the captain and first officer side consoles
Can steer the nose wheel up to 75° in either direction
Fly-by-wire system with no direct mechanical linkage between the handwheels and the nose wheel
Minimum radius dimensions are displayed, and the green arc at the wing describes the forward limit of the aircraft nose
The antenna for the navigation and communication equipment is installed, and there are various ground service connection and access panels
Airbus A320 cockpit
Designed for two flight crew members
System controls arranged for ease of use and monitoring by both crew members
Pilots' instrument panels have six identical and interchangeable display units
Airbus A320 cockpit controls and displays
Multipurpose control and display units
Thrust levers
Manual trim wheels
Speedbrake and flap levers
Radio communication panels
Airbus A320 overhead panel
Extensive use of pushbutton switches
Contains status and failure indications following a color code (green for normal, blue for temporary normal, amber for caution, red for warning)
Airbus A320 pilot seats
Can be adjusted horizontally or vertically using electrical or mechanical adjustment
Can be reclined manually
Lumbar cushion can be adjusted vertically and horizontally
Have a 5-point quick release seat belt and a lock-on lever for the shoulder harness
The side arm rest can be adjusted in the vertical direction by pushing in the locking lever on the end of the armrest
Airbus SOP calls for the table to be stowed for takeoff, but airline policy may differ
Airbus A320 cockpit windows
Two for-export shields, two sliding side windows, and two fixed side windows
All windows are heated
Maximum speed limitation with the cockpit window open is 200 knots
The cockpit windows can be used as emergency exits, and the unlocking button must be pressed, then the control handle pulled inward and rearward to open the window
Sunglasses are installed in front of each pilot, and semi-transparent reflective roller-type sun blinds are installed on all side windows
Airbus A320 emergency equipment
Located in the left rear corner of the flight deck
Includes the fourth occupancy seat, which folds out from the wall into a horizontal position
The captain and first officer's life jackets are stowed in compartments on their respective seat backs, and the fourth occupant's life jackets are stowed in a compartment below their seats
A portable flashlight is stowed at each pilot station in a holder near the floor