Planning & Performance Flashcards
What are the factors affecting Performances ?
Aicraft Mass Air Density Wind strenght and direction Flap settings Runway conditions Other sources of degraded performances
What are the components of Air Density?
Altitude Temperature Humidity
What is ICAO
International Civil Aviation Organization
What is ISA?
ICAO Standard Atmosphere (Density Altitue = 10.000 feet)
What is QFE?
Quick Fix Engineering (Reglage de l’altimetre en prenant en referance la pression au sol sur l’aerodrome)
How to calculate density altitude?
Altitude Density = Pression Altitude +/- (Isa Deviation x 120)
Altitue Pressure = 1013 - QFE = Chiffre HpA. Sachant que 1hpa/30feet. on multiplie et ça donne la pression altitude de l’aerodrome.
ISA deviation = Actual temperature - ISA temperature at AD altitude pressure.
ISA temp at sea level: 15degré
2°temp decrease every 1000 feet increase.
What is the take off safety speed?
> =1,2 Vs
What is the the take off distance?
Take off run + Initial Climb (50 ft screen height)
What is VRef?
VRef = 1,30 VSo (Salling spead in landing configuration)
What is VAC?
Visual Approach Care
What is LDA?
Landing Distance Available
What is TORA?
Take-Off Run Available (excluding any stopway)
What is Stopway?
An extansion to the runway used to bring an aicraft to a stop (emergency for a rejected take-off)
What is ASDA?
Acceleration Stop Distance Available = TORA + Stopway
What is clearway?
Area Beyond the end of the runway. The clearway can include the stopway.
What is TODA?
Totale Take Off Distance Available = TORA + Clearway
Conditions required for Landing and Take-Off?
TORR (Take off run Required) : Minimal Runway Distance required
TODR (Take off Distance Required): TORR + 50 ft
LDF (Landing Distance Required)
What are the available conditions in a AD?
We can find the available conditions on VAC. (TORA, TODA, LDA)
What are the safety factors when calculating TODR and LDR?
For take off performance: 1.33 factor
For landing performance: 1.43 factor
What is POH?
Pilot Operating Handbook
What are the different speed values of an aircraft?
Vx = Best angle of climb airspeed
Vy= Best rate of clim
Speed values for a particular aircaft can be found in a POH
What are the factors affecting angle and rate of climb?
Speed Aircraft mass Aircraft configuration Air density Wind
What is SFC ?
Specific Fuel Consumption? Fuel Flow per unit of power per unit of time.
What is the range?
The maximum distance an aircraft can fly for a given quantity of fuel consumed?