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S.L. 4000 8000 S.L. 4000 8000 S.L. 4000 8000
6000 30.8 39.2
6500 32.6 38.7 47.2 35.9
7000 40.9 47.1 33.8 55.2 42.3 36.2
7500 49.8 33.8 56.1 40.3 33.8 63.2 48.8 41.8
8000 59.2 40.6 33.0 65.3 47.3 39.6 55.2 47.4
8500 68.8 47.7 39.0 54.6 45.6 61.7 53.0
9000 55.3 45.2 62.1 51.9 58.6
9500 63.1 51.6 58.3 64.2
10000 58.4 64.8
10500 65.3
1. Enter Weight Adjustment table with slush/standing water depth and 20K Derate dry field/obstacle limit
weight to obtain slush/standing water weight adjustment.
2. Find V1(MCG) limit weight for temperature adjusted field length and pressure altitude.
3. Max allowable slush/standing water limited weight is lesser of weights from 1 and 2.
WEIGHT
(1000 KG)
SLUSH/STANDING WATER DEPTH
3mm (0.12 INCHES) 6mm (0.25 INCHES) 13mm (0.50 INCHES)
PRESS ALT (FT) PRESS ALT (FT) PRESS ALT (FT)
S.L. 4000 8000 S.L. 4000 8000 S.L. 4000 8000
60 -20 -20 -16 -11 -11 -10 4 -7 0
56 -22 -22 -18 -14 -12 -9 2 1 1
52 -26 -24 -20 -19 -16 -11 -2 2 1
48 -27 -27 -22 -22 -20 -13 -7 -1 1
44 -29 -28 -24 -25 -23 -16 -12 -6 1
40 -30 -29 -26 -27 -25 -19 -17 -12 -1
36 -31 -30 -28 -28 -27 -23 -22 -18 -7
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).
June 3, 2005
737 Flight Crew Operations Manual
Performance Inflight -
General
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
PI.20.18
ADVISORY INFORMATION
Slippery Runway Takeoff (20K Derate)
Maximum Reverse Thrust
Weight Adjustment (1000 KG)
V1 (MCG) Limit Weight (1000 KG)
20K DERATE
DRY
FIELD/OBSTACLE
LIMIT WEIGHT
(1000 KG)
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
68 0.0 0.0 0.0 -3.6 -3.6 -3.6 -7.5 -7.5 -7.5
64 -0.2 -0.2 -0.2 -3.9 -3.9 -3.9 -7.3 -7.3 -7.3
60 -0.6 -0.6 -0.6 -4.0 -4.0 -4.0 -6.9 -6.9 -6.9
56 -0.8 -0.8 -0.8 -3.9 -3.9 -3.9 -6.6 -6.6 -6.6
52 -1.1 -1.1 -1.1 -3.8 -3.8 -3.8 -6.3 -6.3 -6.3
48 -1.1 -1.1 -1.1 -3.7 -3.7 -3.7 -5.9 -5.9 -5.9
44 -0.8 -0.8 -0.8 -3.1 -3.1 -3.1 -5.3 -5.3 -5.3
40 -0.3 -0.3 -0.3 -2.6 -2.6 -2.6 -4.5 -4.5 -4.5
36 0.0 0.0 0.0 -2.0 -2.0 -2.0 -3.6 -3.6 -3.6
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
3800 36.3
4200 46.4 29.2
4600 56.6 39.3 28.5
5000 66.1 49.6 32.3 36.7
5400 75.7 59.4 42.3 44.8 30.9
5800 69.0 52.7 52.8 39.2 30.5
6200 62.3 59.1 47.1 33.4 35.6
6600 71.9 65.0 55.0 41.6 40.8
7000 70.8 60.9 49.5 46.2 32.0
7400 66.7 56.8 51.9 37.2
7800 72.6 62.6 57.8 42.4 28.4
8200 68.5 63.6 47.9 33.6
8600 74.3 69.5 53.7 38.8
9000 75.4 59.6 44.0
9400 65.4 49.6
9800 71.3 55.5
10200 61.3
10600 67.2
11000 73.0
1. Enter Weight Adjustment table with reported braking action and 20K derate dry field/obstacle limit
weight to obtain slippery runway weight adjustment.
2. Adjust "Good" field length available by -90ft/+90ft for every 5°C above/below 4°C
Adjust "Medium" field length available by -90ft/+90ft for every 5°C above/below 4°C
Adjust "Poor" field length available by -120ft/+110ft for every 5°C above/below 4°C
3. Find V1(MCG) limit weight for temperature adjusted field length and pressure altitude.
4. Max allowable slippery runway limited weight is lesser of weights from 1 and 3.
June 3, 2005
737 Flight Crew Operations Manual
Performance Inflight -
General
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
 PI.20.19
ADVISORY INFORMATION
Slippery Runway Takeoff (20K Derate)
Maximum Reverse Thrust
V1 Adjustment (KIAS)
WEIGHT
(1000 KG)
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
68 -2 0 0 -9 -7 -5 -23 -20 -17
64 -4 -2 0 -12 -10 -8 -25 -22 -19
60 -6 -4 -2 -15 -13 -11 -28 -25 -22
56 -8 -6 -4 -17 -15 -13 -31 -28 -25
52 -9 -7 -5 -19 -17 -15 -33 -30 -27
48 -11 -9 -7 -21 -19 -17 -35 -32 -29
44 -12 -10 -8 -23 -21 -19 -36 -33 -30
40 -12 -10 -8 -24 -22 -20 -37 -34 -31
36 -13 -11 -9 -25 -23 -21 -38 -35 -32
1. Obtain V1, VR and V2 for the actual weight.
　
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