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OAT (°C)  REFERENCE GO-AROUND GRADIENT (%) 
PRESSURE ALTITUDE (FT) 
0  2000  4000  6000  8000  10000 
54 50 46  2.54 3.21 3.72  2.15 2.80  1.75 
42 38 34  4.23 4.75 5.27  3.27 3.74 4.25  2.35 2.79 3.26  1.29 1.82 2.25  0.73 1.11  0.19 
30 26 22  5.82 5.85 5.88  4.71 5.07 5.09  3.65 3.94 4.16  2.62 2.90 3.09  1.52 1.87 2.11  0.60 0.94 1.16 
18 14 10  5.90 5.92 5.95  5.11 5.12 5.14  4.17 4.18 4.20  3.27 3.28 3.29  2.27 2.41 2.42  1.33 1.47 1.61 
6 2  5.97 5.99  5.16 5.17  4.21 4.22  3.30 3.31  2.44 2.45  1.62 1.63 

Gradient Adjustment for Weight (%)
WEIGHT  REFERENCE GO-AROUND GRADIENT (%) 
(1000 KG)  0  1  2  3  4  5  6 
80  -2.44  -2.78  -3.08  -3.35  -3.62  -3.88  -4.15 
75  -1.98  -2.23  -2.47  -2.68  -2.90  -3.11  -3.32 
70  -1.42  -1.60  -1.76  -1.92  -2.07  -2.23  -2.38 
65  -0.76  -0.86  -0.95  -1.03  -1.12  -1.20  -1.28 
60  0  0  0  0  0  0  0 
55  0.90  1.00  1.10  1.21  1.31  1.41  1.52 
50  2.01  2.23  2.45  2.67  2.90  3.13  3.37 

Gradient Adjustment for Speed (%)
SPEED  WEIGHT ADJUSTED GO-AROUND GRADIENT (%) 
(KIAS)  0  1  2  3  4  5  6  7  8  9  10  11  12 
VREF40  -0.25  -0.27  -0.29  -0.30  -0.31  -0.31  -0.30  -0.30  -0.30  -0.30  -0.29  -0.29  -0.27 
VREF40+5  0  0  0  0  0  0  0  0  0  0  0  0  0 
VREF40+10  0.15  0.14  0.14  0.14  0.13  0.12  0.12  0.12  0.12  0.13  0.13  0.13  0.11 
VREF40+15  0.22  0.21  0.20  0.20  0.18  0.16  0.14  0.13  0.14  0.15  0.16  0.16  0.14 
VREF40+20  0.24  0.22  0.21  0.19  0.17  0.13  0.10  0.09  0.09  0.10  0.11  0.09  0.05 
VREF40+25  0.20  0.17  0.14  0.12  0.08  0.04  -0.01  -0.04  -0.04  -0.03  -0.03  -0.05  -0.11 
VREF40+30  0.12  0.07  0.03  -0.02  -0.08  -0.14  -0.19  -0.22  -0.23  -0.23  -0.23  -0.25  -0.31 

With engine bleed for packs off, increase gradient by 0.2%.
With engine anti-ice on, decrease gradient by 0.1%.
With engine and wing anti-ice on, decrease gradient by 0.3%.
When operating in icing conditions during any part of the flight with forecast landing temperatures below
10°C decrease gradient by 0.9%.

Copyright . The Boeing Company. See title page for details.
Performance Dispatch

737-800/CFM56-7B27 Landing
FAA Category C Brakes
737 Flight Crew Operations Manual
Quick Turnaround Limit Weight Flaps 40
AIRPORT OAT (°C)  LIMIT WEIGHT (1000 KG) 
AIRPORT PRESSURE ALTITUDE (FT) 
0  2000  4000  6000  8000  10000 
54 50 45  79.6 80.2 80.9  77.2 77.8  74.8 
40 35 30  81.6 82.3 83.0  78.5 79.2 79.9  75.4 76.1 76.7  72.4 73.1 73.7  70.1 70.8  67.9 
25 20 15  83.8 84.6 85.4  80.6 81.3 82.1  77.4 78.1 78.9  74.4 75.1 75.8  71.4 72.1 72.7  68.5 69.1 69.8 
10 5 0  86.1 86.1 86.1  82.9 83.7 84.5  79.6 80.4 81.2  76.5 77.2 78.0  73.4 74.1 74.9  70.4 71.1 71.8 
-5 -10 -15  86.1 86.1 86.1  85.4 86.1 86.1  82.0 82.8 83.7  78.8 79.6 80.4  75.6 76.4 77.2  72.5 73.3 74.0 
-20 -30 -40  86.1 86.1 86.1  86.1 86.1 86.1  84.6 86.1 86.1  81.2 83.0 84.9  78.0 79.7 81.5  74.8 76.4 78.1 
-50 -54  86.1 86.1  86.1 86.1  86.1 86.1  86.1 86.1  83.4 84.1  79.9 80.7 

Increase weight by 700 kg per 1% uphill slope.  Decrease weight by 1200 kg per 1% downhill slope. Increase weight by 1850 kg per 10 knots headwind.  Decrease weight by 7750 kg per 10 knots tailwind.
After landing at weights exceeding those shown above, adjusted for slope and wind, wait at least 67 minutes and check that wheel thermal plugs have not melted before executing a subsequent takeoff.
　
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