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

3. Find V1(MCG) limit weight for adjusted field length and pressure altitude.
4. Max allowable slush/standing water limited weight is lesser of weights from 1 and 3.
787 Flight Crew Operations Manual
Performance Inflight
General
FAA
Category A Brakes
Boeing Proprietary PI.10.5
ADVISORY INFORMATION
Slush/Standing Water Takeoff
No Reverse Thrust
V1 Adjustment (KIAS)
1. Obtain V1, VR and V2 for the actual weight.
2. If V1(MCG) limited, set V1 = V1(MCG). If not V1(MCG) limited, enter V1 Adjustment table with the
actual weight to obtain V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG).
V1 not to exceed VR.
WEIGHT
(1000 LB)
SLUSH/STANDING WATER DEPTH
0.12 INCHES (3 mm) 0.25 INCHES (6 mm) 0.50 INCHES (13 mm)
PRESS ALT (FT) PRESS ALT (FT) PRESS ALT (FT)
S.L. 4000 8000 S.L. 4000 8000 S.L. 4000 8000
660 -30 -24 -18 -23 -17 -11 -8 -2 0
620 -32 -26 -20 -25 -19 -13 -11 -5 0
580 -34 -28 -22 -28 -22 -16 -15 -9 -3
540 -36 -30 -24 -31 -25 -19 -19 -13 -7
500 -38 -32 -26 -34 -28 -22 -24 -18 -12
460 -40 -34 -28 -37 -31 -25 -28 -22 -16
420 -42 -36 -30 -39 -33 -27 -32 -26 -20
380 -43 -37 -31 -41 -35 -29 -35 -29 -23
340 -43 -37 -31 -41 -35 -29 -37 -31 -25
787 Flight Crew Operations Manual
Performance Inflight
General
FAA
Category A Brakes
PI.10.6 Boeing Proprietary
ADVISORY INFORMATION
Slippery Runway Takeoff
Maximum Reverse Thrust
Weight Adjustments (1000 LB)
V1(MCG) Limit Weight (1000 LB)
DRY
FIELD/OBSTACLE
LIMIT WEIGHT
(1000 LB)
REPORTED BRAKING ACTION
GOOD MEDIUM POOR
PRESS ALT (FT) PRESS ALT (FT) PRESS ALT (FT)
S.L. 4000 8000 S.L. 4000 8000 S.L. 4000 8000
700 0.0 -3.2 -6.4 -33.2 -36.5 -39.7 -69.1 -72.3 -75.5
660 0.0 -3.2 -6.4 -36.0 -39.2 -42.4 -68.8 -72.0 -75.2
620 -0.7 -3.9 -7.1 -37.6 -40.8 -44.0 -67.5 -70.7 -73.9
580 -3.8 -7.0 -10.2 -38.1 -41.3 -44.5 -65.1 -68.3 -71.5
540 -6.1 -9.3 -12.5 -37.4 -40.6 -43.8 -61.5 -64.8 -67.9
500 -7.4 -10.6 -13.8 -35.6 -38.8 -42.0 -56.9 -60.1 -63.3
460 -7.7 -10.9 -14.1 -32.6 -35.8 -39.0 -51.2 -54.4 -57.6
420 -7.2 -10.4 -13.6 -28.5 -31.7 -34.9 -44.3 -47.5 -50.7
380 -5.7 -8.9 -12.1 -23.3 -26.5 -29.7 -36.4 -39.6 -42.8
340 -3.3 -6.5 -9.7 -16.9 -20.1 -23.3 -27.4 -30.6 -33.8
ADJUSTED
FIELD
LENGTH
(FT)
REPORTED BRAKING ACTION
GOOD MEDIUM POOR
PRESS ALT (FT) PRESS ALT (FT) PRESS ALT (FT)
S.L. 4000 8000 S.L. 4000 8000 S.L. 4000 8000
5000 337.6
5400 442.3 337.6
5800 543.8 442.3 337.6
6200 642.3 543.8 442.3
6600 738.3 642.3 543.8 329.6
7000 738.3 642.3 402.9 300.4
7400 738.3 477.5 373.4 271.3
7800 553.8 447.5 344.2
8200 631.8 523.1 417.7 288.9
8600 711.6 600.4 492.7 334.6
9000 679.5 569.3 380.5 284.3
9400 759.8 647.6 427.6 330.0
9800 727.6 476.0 375.9 279.7
10200 526.0 422.8 325.4
10600 577.6 471.1 371.2
11000 631.1 520.9 418.1
11400 686.7 572.4 466.2
11800 743.7 625.7 515.9
12200 681.0 567.2
12600 738.0 620.3
13000 675.4
1. Enter Weight Adjustment table with reported braking action and dry field/obstacle limit weight to
obtain slippery runway weight adjustment.
2. Adjust “Good” field length available by -90 ft/+90 ft for every 5°C above/below 4°C.
Adjust “Medium” field length available by -130 ft/+130 ft for every 5°C above/below 4°C.
Adjust “Poor” field length available by -190 ft/+190 ft for every 5°C above/below 4°C.
3. Find V1(MCG) limit weight for adjusted field length and pressure altitude.
4. Max allowable slippery runway limited weight is lesser of weights from 1 and 3.
787 Flight Crew Operations Manual
Performance Inflight
General
FAA
Category A Brakes
Boeing Proprietary PI.10.7
ADVISORY INFORMATION
Slippery Runway Takeoff
Maximum Reverse Thrust
V1 Adjustments (KIAS)
1. Obtain V1, VR and V2 for the actual weight.
2. If V1(MCG) limited, set V1 = V1(MCG). If not V1(MCG) limited, enter V1 Adjustment table with the
actual weight to obtain V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG).
V1 not to exceed VR.
WEIGHT
(1000 LB)
REPORTED BRAKING ACTION
GOOD MEDIUM POOR
PRESS ALT (FT) PRESS ALT (FT) PRESS ALT (FT)
S.L. 4000 8000 S.L. 4000 8000 S.L. 4000 8000
700 -3 -1 1 -13 -11 -9 -25 -23 -21
660 -4 -2 0 -14 -12 -10 -27 -25 -23
620 -6 -4 -2 -16 -14 -12 -30 -28 -26
580 -7 -5 -3 -18 -16 -14 -33 -31 -29
540 -8 -6 -4 -20 -18 -16 -35 -33 -31
500 -10 -8 -6 -22 -20 -18 -38 -36 -34
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：787機組操作手冊Flight Crew Operations Manual 1(59)