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AIRPORT OAT  LANDING CLIMB LIMIT WEIGHT (1000 KG) 
AIRPORT PRESSURE ALTITUDE (FT) 
°C  °F  0  2000  4000  6000  8000  10000 
50 48 46  122 118 115  66.4 67.8 69.0  61.4 62.9 64.4  59.4 
44 42 40  111 108 104  70.2 71.5 72.7  65.6 66.8 68.0  60.8 62.2 63.4  57.1 58.4 
38 36 34  100 97 93  74.0 75.3 76.7  69.1 70.4 71.7  64.5 65.7 66.9  59.7 60.8 61.9  54.4 55.3 56.3  51.5 
32 30 28  90 86 82  78.1 79.4 79.5  72.9 74.0 75.0  68.0 68.8 69.6  62.9 63.8 64.6  57.3 58.3 59.2  52.7 53.7 54.5 
26 24 22  79 75 72  79.5 79.6 79.7  75.9 75.9 76.0  70.3 70.9 71.4  65.2 65.7 66.1  60.1 60.9 61.3  55.5 56.0 56.6 
20 18 16  68 64 61  79.7 79.8 79.9  76.0 76.1 76.1  71.4 71.5 71.5  66.7 67.1 67.1  61.7 62.1 62.5  57.1 57.3 57.8 
14 12 10 -40  57 54 50 -40  79.9 80.0 80.0 80.6  76.2 76.2 76.3 76.8  71.6 71.6 71.6 72.1  67.2 67.2 67.2 67.7  62.9 62.9 62.9 63.3  58.1 58.4 58.8 59.3 

With engine bleeds for packs off, increase weight by 1200 kg.
With engine anti-ice on, decrease weight by 300 kg.
With engine and wing anti-ice on, decrease weight by 1400 kg.
When operating in icing conditions during any part of the flight with forecast landing temperature below
10°C, decrease weight by 5500 kg.

Copyright . The Boeing Company. See title page for details.
737-800/CFM56-7B26

Performance Dispatch
FAA
Landing
Category C Brakes
737 Flight Crew Operations Manual

ADVISORY INFORMATION
Go-Around Climb Gradient Flaps 15 Based on engine bleed for packs on and anti-ice off
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%.
　
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本文鏈接地址：737NG機組操作手冊Flight Crew Operations Manual FCOM 1(172)