曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

8600 6710 7280 7900 8600 9010 9370 9860 10340
9000 7050 7640 8280 9000 9430 9790 10310 10800
9400 7390 8000 8660 9400 9860 10210 10750 11260
9800 7730 8370 9050 9800 10280 10630 11200 11720
10200 8070 8680 9400 10200 10700 11050 11640 12180
10600 8400 8990 9750 10600 11120 11470 12090 12640
WIND CORRECTED
FIELD LENGTH
(FT)
AIRPORT PRESSURE ALTITUDE (FT)
0 2000 4000 6000 8000
4600 325.0 305.8
5000 363.6 342.2 321.4 301.7
5400 402.3 378.8 356.1 334.4 313.8
5800 441.5 415.8 391.0 367.2 344.9
6200 478.3 453.2 426.2 400.4 376.1
6600 506.6 486.3 461.9 434.0 407.7
7000 529.5 511.0 491.6 467.8 439.5
7400 551.8 532.6 513.7 494.7 471.6
7800 573.6 553.7 534.1 515.0 496.1
8200 594.6 574.3 554.1 534.3 515.0
8600 615.1 594.2 573.5 553.1 533.2
9000 635.1 613.6 592.4 571.5 551.0
9400 654.2 632.6 610.8 589.5 568.5
9800 672.8 650.8 628.9 606.9 585.5
10200 691.1 668.5 646.2 624.1 602.1
10600 709.4 685.6 662.9 640.5 618.2
11000 700.2 677.1 654.7 632.7
11400 714.8 689.6 666.7 644.4
11800 701.8 678.4 655.7
12200 714.0 689.8 666.7
12600 701.0 677.3
13000 712.1 687.7
With 1 brake deactivated, decrease weight by 35700 lb.
With 2 brakes deactivated, decrease weight by 72500 lb.
With manual speedbrakes, decrease weight by 38500 lb.
787 Flight Crew Operations Manual
Performance Dispatch
Landing
FAA
Category A Brakes
Boeing Proprietary PD.12.3
Landing Climb Limit Weight
Valid for approach with flaps 20 and landing with flaps 25 or 30
AIRPORT OAT LANDING CLIMB LIMIT WEIGHT (1000 LB)
AIRPORT PRESSURE ALTITUDE (FT)
°C °F 0 1000 2000 3000
54 129 537.5
52 126 550.3 529.0
50 122 563.0 542.1 520.9
48 118 575.5 554.8 533.6 512.0
46 115 588.0 567.1 545.8 522.9
44 111 601.6 579.3 557.7 533.7
42 108 615.8 591.7 569.4 544.3
40 104 629.3 604.3 580.9 554.8
38 100 640.8 616.5 592.5 564.8
36 97 651.7 627.3 603.5 574.7
34 93 662.3 637.9 613.8 584.6
32 90 672.0 647.3 623.1 593.8
30 86 678.8 656.4 632.0 602.9
28 82 681.6 663.2 640.3 611.4
26 79 681.7 665.6 646.8 619.1
24 75 681.8 665.7 649.5 625.7
22 72 681.9 665.8 649.6 628.2
20 68 682.0 665.9 649.7 628.3
18 64 682.1 666.0 649.8 628.4
16 61 682.3 666.1 649.9 628.5
14 57 682.4 666.3 650.0 628.6
12 54 682.5 666.4 650.1 628.7
10 50 682.7 666.5 650.2 628.8
-40 -40 685.7 669.4 652.9 631.7
With engine bleed for packs off, increase weight by 2000 lb.
With engine and wing anti-ice on, decrease weight by 3400 lb.
When operating in icing conditions during any part of the flight with forecast landing temperature below
10°C, decrease weight by 45400 lb.
787 Flight Crew Operations Manual
Performance Dispatch
Landing
FAA
Category A Brakes
PD.12.4 Boeing Proprietary
ENGINE INOP
ADVISORY INFORMATION
Go-Around Climb Gradient
Flaps 20, Gear Up
Based on engine bleed for packs on or off, engine anti-ice on or off and wing
anti-ice off.
Weight Adjustment
Speed Adjustment
OAT
(°C)
REFERENCE GO-AROUND GRADIENT (%)
PRESSURE ALTITUDE (FT)
0 2000 4000 6000 8000 10000
54 5.52
50 6.26 5.09
46 6.98 5.83 4.60
42 7.77 6.50 5.12 4.07
38 8.42 7.09 5.60 4.49 3.44
34 8.95 7.59 6.08 4.90 3.84 2.85
39 9.47 8.05 6.54 5.33 4.21 3.17
26 9.50 8.43 6.92 5.70 4.57 3.49
22 9.50 8.46 7.23 6.00 4.83 3.76
18 9.51 8.47 7.30 6.13 5.01 3.88
14 9.51 8.48 7.30 6.19 5.23 4.04
10 9.52 8.49 7.31 6.19 5.23 4.27
WEIGHT
(1000 LB)
REFERENCE GO-AROUND GRADIENT (%)
3 4 5 6 7 8 9 10
600 -4.09 -4.46 -4.80 -5.15 -5.51 -5.87 -6.23 -6.58
550 -3.40 -3.68 -3.97 -4.26 -4.55 -4.85 -5.15 -5.43
500 -2.51 -2.71 -2.93 -3.15 -3.37 -3.59 -3.81 -4.02
450 -1.41 -1.51 -1.64 -1.77 -1.89 -2.01 -2.14 -2.25
400 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00
350 1.81 1.97 2.13 2.28 2.45 2.63 2.82 3.04
300 4.21 4.60 4.97 5.36 5.77 6.21 6.66 7.12
SPEED
(KIAS)
WEIGHT ADJUSTED GO-AROUND GRADIENT (%)
0 1 2 3 4 5 6 7 8 9
VREF -0.27 -0.28 -0.29 -0.30 -0.31 -0.32 -0.32 -0.33 -0.33 -0.32
VREF+5 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00
VREF+10 0.16 0.16 0.15 0.16 0.16 0.16 0.16 0.16 0.16 0.15
VREF+15 0.27 0.26 0.26 0.26 0.27 0.28 0.28 0.26 0.24 0.22
VREF+20 0.33 0.32 0.32 0.33 0.34 0.35 0.34 0.32 0.28 0.23
VREF+25 0.35 0.34 0.33 0.34 0.35 0.36 0.35 0.31 0.26 0.20
VREF+30 0.32 0.30 0.29 0.28 0.29 0.28 0.26 0.22 0.17 0.11
With engine and wing anti-ice on, decrease gradient by 0.1%.
When operating in icing conditions during any part of the flight with forecast landing temperatures below
　
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