Performance And Planning Flashcards
Ds
What are the factors affecting performances?!
Aircraft mass Air density Wind/stenght direction Flap settings Runway conditions Others sources of degraded performances
What are the components of air density
ATH : Altitude, temperature and humidity
What is ICAO
International Civil aviation organisation
What is ISA
ICAO standars atmosphere (10000ft)
QFE
Quick fix engineering ( reglage altimetre pression au sol sur l’aerodrome)
How to calculate altitude density?
DENSITY ALTITUDE = PRESSURE ALTITUDE +/- (ISA deviation X 120 ft)
pressure alt = 1013,25-QFE sachant que 30ft=1hpa
ISA deviation = Actual temp - ISA temp at aerodrome altitude pressure
ISA temp at sea lvl = 15 °C
2° temp decrease every 1000 feet increase
What is the take off safety speed?
The take-off safety speed is = (≥1,2 Vs)
What is the take off distance?
Take off run + initial climb (50ft climb)
What is Vref?
Vref is equal to 1,3 Vso ( stalling speed in landing config)
What is VAC?
Visual approach card
What is LDA
Landing distance available
What is TORA
Take off run available (excluding any stop way)
What is stop way?
An extension to the runway used to bring an aircraft to a stop (emergency for a rejected take off)
What is ASDA
TORA + Stop way = acceleration stop distance available
What is clearway
Area beyond the end of the runway. It can includes the stopway
What is TODA?
TORA + clearway
Conditions required for landing and take off?
TORR (take off runway required=minimal runway required)
TODR (take off distance required=TORR + 50ft)
LDR (Landing distance required)
What are the available conditions in aerodrome?
We can found the available conditions on the VAC ( TORA, TODA and LDA)
What are the safety factors when calculating TODR and LDR?
For take off performances : 1.33 factor
For landing performances : 1,43 factor
What is POH?
Pilot operating handbook
What are the different speed values of an aircraft?
Vx and Vy
Vx = best angle of climb (airspeed)
Vy = best rate of climb
Normal climb speed is the compromise beetwen both
Speed values depend of the aircraft and can be found in the POH
What are the factors affecting the rate of climb and the angle?
Speed Aircraft mass Aircraft configuration air density wind