3 PERFORMANCE, FLIGHT PLANNING

3.1 Performance

Performance calculation concerning speeds, gradients, masses in all conditions for take off, en route, approach
and landing according to the documentation available, e.g. for take-off V1, Vmbe, Vr, Vlof, V2, take-off distance,
maximum take-off mass and the required stop distance with respect to the following factors:

&amp;ndash; accelerate/stop distance
&amp;ndash; take-off run and distance available (TORA, TODA)
&amp;ndash; ground temperature, pressure altitude, slope, wind
&amp;ndash; maximum load and maximum mass (e.g. ZFM)
&amp;ndash; minimum climb gradient after engine failure
&amp;ndash; influence of snow, slush, moisture and standing water on the runway
&amp;ndash; possible single and/or dual engine failure during cruise flight
&amp;ndash; use of anti-icing systems
&amp;ndash; failure of water injection system and/or antiskid system
&amp;ndash; speeds at reduced thrust, V1, V1red, Vmbe, Vmu, Vr, Vlof, V2
&amp;ndash; safe approach speed Vref, with respect to Vmca and turbulent conditions
&amp;ndash; effects of excessive approach speed and abnormal glideslope with respect to the landing distance
&amp;ndash; minimum climb gradient during approach and landing
&amp;ndash; limiting values for a go around with minimum fuel
&amp;ndash; maximum allowable landing mass and the landing distance for the destination and alternate
aerodrome with respect to the following factors:
&amp;ndash; available landing distance
&amp;ndash; ground temperature, pressure altitude, runway slope and wind
&amp;ndash; fuel consumption to destination or alternate aerodrome
&amp;ndash; influence of moisture on the runway, snow, slush and standing water
&amp;ndash; failure of the water injection system and/or the anti skid system
&amp;ndash; influence of thrust reverser and spoilers

3.2 Flight planning

Flight planning for normal and abnormal conditions

&amp;ndash; optimum/maximum flight level
&amp;ndash; minimum required flight altitude
&amp;ndash; drift down procedure after an engine failure during cruise flight
&amp;ndash; power setting of the engines during climb, cruise and holding under various circumstances, as
well as the most economic cruising flight level
&amp;ndash; calculation of a short range/long range flight plan
&amp;ndash; optimum and maximum flight level and power setting of the engines after engine failure


5 EMERGENCY PROCEDURES

5.1 Recognition of the situation as well as immediate memory actions in correct sequence and for those

conditions recognised as emergencies by the manufacturer and certification authority:

&amp;ndash; engine failure during take off before and after V1, as well as inflight
&amp;ndash; malfunctions of the propeller system
&amp;ndash; engine overheat, engine fire on ground and inflight
&amp;ndash; wheel well fire
&amp;ndash; electrical smoke and/or fire
&amp;ndash; rapid decompression and emergency descent
&amp;ndash; air-conditioning overheat, anti ice system overheat
&amp;ndash; fuel pump failure
&amp;ndash; fuel freezing/overheat
&amp;ndash; electric power failure
&amp;ndash; equipment cooling failure
&amp;ndash; flight instrument failure
&amp;ndash; partial or total hydraulic failure
&amp;ndash; failures at the lift devices and flight controls including boosters
&amp;ndash; cargo compartment smoke and/or fire

5.2 Actions according to the approved abnormal and emergency checklist

&amp;ndash; engine restart inflight
&amp;ndash; landing gear emergency extension
&amp;ndash; application of the emergency brake system
&amp;ndash; emergency extension of lift devices
&amp;ndash; fuel dumping
&amp;ndash; emergency descent