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DATA
• Takeoff from Paris-Orly, Runway 08
• Slat/Flap configuration: 1+F
• Actual TOW = 66 tons
• OAT = 24ºC
• Wind = +20 Kt headwind
• QNH = 1013 hPa
• Air conditioning: Off
• Runway state: D
A project supported by AIRBUS and the CAAC
Date of the module
Example: Flexible Temperature and Speeds Determination
RESULT
• Flex Temp = 68ºC
• V1 = 145 Kt, VR = 145 Kt, V2 = 150 Kt
Note: In case of deviation from the chart
reference conditions (QNH, air conditioning…),
corrections have to be applied to the flexible
temperature.
A project supported by AIRBUS and the CAAC
Date of the module
A project supported by AIRBUS and the CAAC
Date of the module
• Table of contents
• Flight operations duties
• European Applicable Regulation
• General
• General aircraft limitations
• Payload Range
• Operating limitations
• In flight performance
• One engine inoperative performance
• Flight planning
• weight and balance
A project supported by AIRBUS and the CAAC
Date of the module
• Flight operations duties
• JAA and JAR OPS 1
• General aircraft limitations
• Payload Range
• Operating limitations
• In flight performance
• One engine inoperative performance
• Flight planning
A project supported by AIRBUS and the CAAC
Date of the module
Maximum weights
Maximum structural take-off weight: MTOW
Maximum structural landing weight: MLW
Maximum zero fuel weight: MZFW
Capacities
Cabin capacity
A project supported by AIRBUS and the CAAC
Date of the module
Maximum weights
Maximum structural take off weight: MTOW
Maximum structural landing weight: MLW
Maximum zero fuel weight: MZFW
Capacities
Cabin capacity
Cargo capacity
A project supported by AIRBUS and the CAAC
Date of the module
Maximum weights
Maximum structural take-off weight: MTOW
Maximum structural landing weight: MLW
Maximum zero fuel weight: MZFW
Capacities
Cabin capacity
Cargo capacity
Tanks capacity
A project supported by AIRBUS and the CAAC
Date of the module
tow = dow + payload + fuel <= MTOW
lw = dow+ payload + fuel - trip fuel <= MLW
zfw = dow + payload <= MZFW
trip fuel + reserves + taxi fuel <= Tanks capacity
A project supported by AIRBUS and the CAAC
Date of the module
Payload <= (MTOW - dow - AF - HF) - (TF + RR)
Payload
Range
A project supported by AIRBUS and the CAAC
Date of the module
Payload <= (MTOW - dow - AF - HF) - (TF + RR)
Payload <= (MLW - dow - AF - HF) - RR
Payload
Range
A project supported by AIRBUS and the CAAC
Date of the module
Payload <= (MTOW - dow - AF - HF) - (TF + RR)
Payload <= (MLW - dow - AF - HF) - RR
Payload <= (MZFW - dow)
Payload
Range
A project supported by AIRBUS and the CAAC
Date of the module
Payload <= (MTOW - dow - AF - HF) - (TF + RR)
Payload <= (MLW - dow - AF - HF) - RR
Payload <= (MZFW - dow)
Trip fuel + reserves <= tanks capacity - taxi fuel
Payload
Range
A project supported by AIRBUS and the CAAC
Date of the module
Payload <= (MTOW - dow - AF - HF) - (TF + RR)
Payload <= (MLW - dow - AF - HF) - RR
Payload <= (MZFW - dow)
Trip fuel + reserves <= tanks capacity - taxi fuel
Allowed payload
Payload Payload
Range Range
A project supported by AIRBUS and the CAAC
Date of the module
A project supported by AIRBUS and the CAAC
Date of the module
A project supported by AIRBUS and the CAAC
Date of the module
A project supported by AIRBUS and the CAAC
Date of the module
• Table of contents
• Flight operations duties
• European Applicable Regulation
• General
• General aircraft limitations
• Payload Range
• Operating limitations
• In flight performance
• One engine inoperative performance
• Flight planning
• weight and balance
A project supported by AIRBUS and the CAAC
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flight operation 飛行運行概述(43)
