The ambient outside pressure exceeds the cabin pressure

Anti ice is selected on prior to entering an area of ice, de ice after entering it

The expansion valve allows low pressure fluid to be released into the evaporator at higher pressure, which in turn causes the fluid to revert to vapour

You will now have to manually fly the approach and/or missed approach

All aircraft with a takeoff weight in excess of 5700kg

Resistance to flow

The base of the reservoir

To contain enough fluid for for all system user units to be operated simultaneously

the speed will not change significantly

1.33 times the maximum differential pressure

ensures fluid reversal does not occur

Able to supply a greater degree of cooling to the same volume of air space

That enough wheel brake energy is available for high speed rejected takeoff

10,000ft

More than 300ft from the selected cruise altitude

A constant altitude

After approx 6mm of ice has accreted onto the surface

the heat exchanger

Three entirely separate means

Provides a measure of feedback to the pilot as to the loads being imparted on the controls, and senses dynamic pressures

Pilot inputs to the rudder are modified using signals from the CADC to prevent over stress

CADC and Intertial Reference system

they are normally turned on during all phases of flight and the pilots pedals will not move in response to yaw damper movements

The flaps retract to a lesser setting, the cockpit flap lever does not move and the flap returns to the original setting as speed reduces to less than limit speed

It changes to a gas

28V

The autopilot takes its commands from the flight director unit

the EADI

the EADI

That one or both outboard ailerons will continue move at high speeds, with control yoke inputs

one or both outboard ailerons will not operate during the approach

Revers thrust selected

A ratio changer is incorporated to reduce rudder deflection at low airspeeds

Failure of the leading edge devices to deploy will cause a higher approach speed and higher nose angle on approach, with increased cockpit cut off angle

Positive longitudinal static stability and negative dynamic stability

Decreased controllability

a decrease in angle of attack and positive longitudinal static stability

increase the vertical fin area and position the CoG further forward

Improves lateral stability and counters spiral divergence

Increasing wing sweep or dihedral, but at the risk of increasing dutch roll tendency

FDR's must record at least 25hrs of operational data, and CVR's at least the previous 30minutes of cockpit audio data

Whenever powered is provided to the cockpit

It was designed to be used in conjunction with wipers, when the wipers alone cannot cope

Most modern aircraft use electric de ice/anti ice and are better able to survive bird impacts if heat is selected on

Shut off the left wing anti-ice selector valve to prevent damage to the aircraft structure

The airspeed indicator could over read

The crew should approach at higher speed, as stall speed may be higher and stick shaker operation may be compromised

The provision of ice inhibiting chemicals in the fuel, and the heating of fuel in the fuel lines

RAs will not be aurally or visually. The highest level of symbology is a yellow circle TA