flight operation 飞行运行概述(36)

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Date of the module
 Sustained parameters
 Zp and t°C
 Wind
 Runway slope
 Runway condition
 Wet or equivalent
 Contaminated
(see special chapter
later)
 Chosen parameters
A project supported by AIRBUS and the CAAC
Date of the module
Wet
or
equivalent
contaminated
- Water
- Slush
- Wet snow
- Dry snow
- Compacted
snow
< 3mm
< 2mm
< 4mm
< 15mm
3 to 13 mm
2 to 13mm
4 to 25mm
15 to 51mm
all thickness
2 à 13mm
Wet and contaminated runway
A project supported by AIRBUS and the CAAC
Date of the module
 Chosen parameters
 Flaps/Slats
 Sustained parameters
 Zp and t°C
 Wind
 Runway slope
 Runway condition
A project supported by AIRBUS and the CAAC
Date of the module
60
65
70
75
80
85
90
0.84 0.92 1
TORA 1+F
TORA 2
m(t)
V1/VR
Flaps/slats influence on “runway” limitation
A320/200
 Temperature =
+20°C
 Sea level
 Runway: 2300m
 SWY: 100m
 CWY: 0m
 V2/Vs1g = 1,21
 Slope = 0%
 Wind = 0
A project supported by AIRBUS and the CAAC
Date of the module
60
65
70
75
80
85
90
0.84 0.92 1
TORA 1+F
TODA 1+F
TODA 2
TORA 2
m(t)
V1/VR
Flaps/slats influence on “runway” limitation
A320/200
 Temperature =
+20°C
 Sea level
 Runway: 2300m
 SWY: 100m
 CWY: 0m
 V2/Vs1g = 1,21
 Slope = 0%
 Wind = 0
A project supported by AIRBUS and the CAAC
Date of the module
60
65
70
75
80
85
90
0.84 0.92 1
ASDA 1+F
TORA 1+F
TODA 1+F
ASDA 2
TODA 2
TORA 2
m(t)
V1/VR
73t5
0.97
Flaps/slats influence on “runway” limitation
A320/200
 Temperature =
+20°C
 Sea level
 Runway: 2300m
 SWY: 100m
 CWY: 0m
 V2/Vs1g = 1,21
 Slope = 0%
 Wind = 0
1+F
2
A project supported by AIRBUS and the CAAC
Date of the module
60
65
70
75
80
85
90
0.84 0.88 0.92 0.96 1
2 sgt 1+F
2 sgt 2
m(t)
V1/VR
Flaps/slats influence on “climb requirements” limitation
A320/200
 Temperature =
+20°C
 Sea level
 Runway: 2300m
 SWY: 100m
 CWY: 0m
 V2/Vs1g = 1,21
 Slope = 0%
 Wind = 0
A project supported by AIRBUS and the CAAC
Date of the module
A320/200
 Temperature =
+20°C
 Sea level
 Runway: 2300m
 SWY: 100m
 CWY: 0m
 V2/Vs1g = 1,21
 Slope = 0%
 Wind = 0
 Obstacle :
 Height = 260ft
 Distance =
6450m
60
65
70
75
80
85
90
0.84 0.88 0.92 0.96 1
2 sgt 1+F
Obst. 1+F
2 sgt 2
Obst. 2
m(t)
V1/VR
Flaps/slats influence on “climb requirements” limitation
A project supported by AIRBUS and the CAAC
Date of the module
 Chosen parameters
 Flaps/Slats
 V1/Vr ratio
 Sustained parameters
 Zp and t°C
 Wind
 Runway slope
 Runway condition
A project supported by AIRBUS and the CAAC
Date of the module
 Chosen parameters
 Flaps/Slats
 V1/Vr ratio
 V2/VSR ratio
 Sustained parameters
 Zp and t°C
 Wind
 Runway slope
 Runway condition
A project supported by AIRBUS and the CAAC
Date of the module
m(t)
V2/Vs
130
140
150
160
170
1.2 1.25 1.3 1.35
Runway
2 Sgt
Obstacles
tires
A 300-600
 Temperature =
+30°C
 Pressure Altitude =
5000ft
 Runway: 3000m
　
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