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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.10.13
ADVISORY INFORMATION
TO1 - Slush/Standing Water
5%Thrust Reduction
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 -27 -21 -15 -20 -14 -8 -4 0 0
620 -29 -23 -17 -22 -16 -10 -7 -1 0
580 -31 -25 -19 -25 -19 -13 -11 -5 0
540 -34 -28 -22 -28 -22 -16 -15 -9 -3
500 -36 -30 -24 -31 -25 -19 -20 -14 -8
460 -38 -32 -26 -34 -28 -22 -25 -19 -13
420 -39 -33 -27 -37 -31 -25 -30 -24 -18
380 -41 -35 -29 -38 -32 -26 -33 -27 -21
340 -41 -35 -29 -39 -33 -27 -35 -29 -23
300 -42 -36 -30 -40 -34 -28 -37 -31 -25
787 Flight Crew Operations Manual
Performance Inflight
General
FAA
Category A Brakes
PI.10.14 Boeing Proprietary
ADVISORY INFORMATION
TO1 - Slippery Runway
5%Thrust Reduction
Maximum Reverse Thrust
Weight Adjustments (1000 LB)
V1(MCG) Limit Weight (1000 LB)
TO1 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 -2.3 -5.4 -29.6 -32.7 -35.8 -65.8 -68.9 -72.0
660 0.0 -2.4 -5.5 -32.8 -35.9 -39.0 -66.1 -69.2 -72.3
620 0.0 -2.4 -5.5 -35.1 -38.2 -41.3 -65.4 -68.5 -71.6
580 -1.8 -4.9 -8.0 -36.2 -39.3 -42.4 -63.6 -66.7 -69.8
540 -4.5 -7.6 -10.7 -36.1 -39.2 -42.3 -60.7 -63.8 -66.9
500 -6.3 -9.4 -12.5 -34.9 -38.0 -41.1 -56.6 -59.7 -62.8
460 -7.0 -10.2 -13.3 -32.4 -35.5 -38.6 -51.3 -54.5 -57.6
420 -6.9 -10.0 -13.1 -28.7 -31.9 -35.0 -45.0 -48.1 -51.2
380 -5.7 -8.8 -11.9 -23.9 -27.0 -30.1 -37.4 -40.5 -43.6
340 -3.6 -6.7 -9.8 -17.9 -21.0 -24.1 -28.7 -31.8 -34.9
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
4600 268.8
5000 377.7 268.8
5400 484.1 377.7 268.8
5800 587.2 484.1 377.7
6200 687.2 587.2 484.1 290.6
6600 687.2 587.2 365.7 260.6
7000 687.2 441.9 335.7
7400 519.7 411.2 305.7
7800 599.3 488.3 380.8 269.9
8200 680.8 567.2 457.3 317.0
8600 763.6 647.9 535.4 364.2 265.2
9000 730.5 615.4 412.3 312.3
9400 697.3 461.9 359.5 260.5
9800 513.0 407.4 307.6
10200 565.9 456.9 354.8
10600 620.7 507.8 402.6
11000 677.7 560.5 451.8
11400 736.6 615.2 502.7
11800 671.9 555.2
12200 730.7 609.6
12600 666.1
13000 724.8
1. Enter Weight Adjustment table with reported braking action and TO1 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.10.15
ADVISORY INFORMATION
TO1 - Slippery Runway
5%Thrust Reduction
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 -1 0 2 -10 -8 -6 -21 -19 -17
660 -2 -1 1 -11 -10 -8 -23 -21 -20
620 -4 -2 0 -13 -11 -10 -26 -24 -22
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787机组操作手册Flight Crew Operations Manual 1(62)
