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The Flight Deck

The flight deck has seats for two pilots (and in some older designs a flight engineer seated behind them). It is usual for the captain to take the left seat and the copilot the right seat. Arrayed around the pilots' seats are controls for the aircraft and its systems and display panels and indicators to tell the pilots how the aircraft and its sys­tems are behaving.

In front of each pilot is a control wheel, which looks like the lower part of a car's steering wheel mounted on a column. The wheel can be turned left and right and also pulled back and pushed forward on its column. The left and right inputs are connected to hydraulic actuators in the air­craft's ailerons and spoilers. The pulling and pushing inputs are connected to actuators in the elevators. The two control wheels are interlinked so that they both move together regardless of which pilot is making the input.

On the later designs of airliner built by Airbus a sidestick replaces the control wheel, one mounted to the left of the left-hand seat pilot, the other to the right of the right-hand seat pilot. Moving the stick sideways has the same effect as turning the control wheel described above. Forward and backward movement of the side stick likewise has the same effect as pushing or pulling the control wheel.

At the feet of each pilot are two rudder pedals one for each foot. When the left pedal is pushed forward the right pedal moves back, and vice versa. The pedal inputs are connected to actuators in the rudder. As with the control wheels, the two sets of pedals are interlinked.

The main engine thrust is controlled by levers located at the forward end of the console. Each engine has its own throttle. Unlike the accelerator pedal in a car, the thrust levers are not spring-loaded to the idle thrust position. Instead they retain the position in which they are set. The reverser controls are attached to the thrust levers.

Just behind the thrust levers are to be found the fuel control switches, which control the valves admitting fuel to the engines. The fuel supply is opened during the engine start sequence and closed to shut down the engines when they are no longer required.

9 Exercise 3.

Reducing fuel burn on the md-11

Aircraft designers have been trying for many years to reduce the amount of fuel which aircraft burn in regular use. Fuel management has become one of the most important functions of pilots on commercial flights. As fuel is the biggest single cost on most flights.

McDonnell Douglas and General Electric are examining ways of reducing fuel burn on the MD-11. Early flight-test data for the MD- 11 indicate that it is burning more fuel than predicted. The aircraft is not meeting performance targets.

Performance figures show that fuel burn on the GE-powered aircraft is consistently 3%-4% above the companies' original estimates, and that the aircraft will therefore not meet its payload/range guarantees.

General Electric is examining various options for improving the specific fuel consumption of the engines, and Douglas is looking at the aircraft's weight and aerodynamics. The aerodynamic performance of the aircraft in flight test has been very good and that remains the case. In the weight area, they are a little over the predicted weight, but they have a weight reduction programme in place which will improve performance by about 0.75%.

Among the options Douglas is examining for weight reduction is the replacement of the MD 11's aluminium floor beams with aluminium-lithium.

10 Exercise 4.

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