Page 227 - Aeronautical Engineer Data Book

Airport design and compatibility 183
Notes:
• Consult using airline for specific operating procedure prior to facility design
• Zero runway gradient
• Zero wind 8 8,000 (2,439)
Pressure altitude
FAR landing runway length (1,000 meters) 2.25 7 2,000 (609)
Feet
Meters
10,000 (3,049
2.50
6,000 (1,829)
4,000 (1,219)
Sea level
2.00
5 1,000 Feet
6
1.75
1.50
1.25
4
Wet runway
1.00
3
300 320 340 360 380 400 420 440 460
1,000 pounds Dry runway
140 150 160 170 180 190 200 210
(1,000 kilograms) operational landing weight
Fig. 11.11 Aircraft:airport compatibility – landing
runway length requirements. Figure shows Boeing 777­
200. Courtesy Boeing Commercial Airplane Group

Notes:
• Consult using airline for specific operating procedure prior to facility design
• Air conditioning off
• Zero runway gradient
• Zero wind 14 Standard ay
F.A.R. Takeoff runway length (1,000 meters) 4.0 13 Pressure 8,000 (2,438) 9) Flap 20 Flap 15 545,000 LB (247,300 kg )
4.5 15
d
12
3.5
11
Flap 5
3.0 10
9
2.5
8
altitude
ers)
7
(met
2.0
9,000 (2,743)
Feet
6
6,000 (1,829)
5
1.5
(1,21
w
Maximum takeoff eight
2,000 (610)
4,000
4
Sea level
1.0
3
340 360 380 400 420 440 460 480 500 520 540 560 580
1,000 pounds
160 170 180 190 200 210 220 230 240 250 260
(1,000 kilograms) Brake-release gross weight
Fig. 11.12 Aircraft:airport compatibility – take-off
runway length requirements. Figure shows Boeing 777­
200. Courtesy Boeing Commercial Airplane Group