Field Limit Weight (1000 KG)
WIND CORR'D FIELD LENGTH (M)  AIRPORT PRESSURE ALTITUDE (FT) 
0  2000  4000  6000  8000  10000 
1400 1600 1800  45.3 54.3 61.6  42.6 51.1 58.7  40.1 48.1 55.9  45.1 52.8  42.3 49.6  39.6 46.4 
2000 2200 2400  71.1 78.6 85.6  66.5 74.8 81.9  62.4 71.1 77.8  59.4 66.9 74.0  56.4 62.3 70.3  53.3 59.1 64.6 
2600 2800 3000  87.7  84.5  80.3 86.0  76.3 82.3 86.3  72.4 78.0 82.8 
3200 3400  85.4 88.1 

Decrease field limit weight 6000 kg when using manual speedbrakes.
Copyright . The Boeing Company. See title page for details.
737-900/CFM56-7B26

Performance Dispatch
FAA
Landing
Category G Brakes
737 Flight Crew Operations Manual
Landing Climb Limit Weight Valid for approach with flaps 15 and landing with flaps 40 Based on engine bleed for packs on and anti-ice off
AIRPORT OAT (°C)  LANDING CLIMB LIMIT WEIGHT (1000 KG) 
AIRPORT PRESSURE ALTITUDE (FT) 
-2000  0  2000  4000  6000  8000  10000 
54 52 50  68.1 69.3 70.5  63.8 65.5 67.4  61.9 
48 46 44  71.8 73.2 74.5  68.7 69.9 71.1  63.5 65.1 66.4  59.9 61.4 
42 40 38  75.8 77.0 78.3  72.4 73.6 74.9  67.7 68.9 70.1  62.9 64.0 65.1  57.6 58.9 60.3  54.9 
36 34 32  79.5 80.7 80.9  76.2 77.5 78.9  71.3 72.6 73.8  66.5 67.8 68.8  61.4 62.5 63.4  55.8 56.8 57.8  52.2 53.2 
30 28 26  80.9 81.0 81.1  80.2 80.3 80.4  74.9 75.9 76.8  69.7 70.5 71.2  64.4 65.3 65.9  58.9 59.8 60.7  54.3 55.1 56.0 
24 22 20  81.2 81.2 81.3  80.5 80.5 80.6  76.8 76.9 76.9  71.8 72.3 72.3  66.5 67.0 67.5  61.5 61.9 62.3  56.6 57.1 57.6 
18 16 14  81.4 81.4 81.5  80.7 80.7 80.8  77.0 77.0 77.1  72.4 72.4 72.5  68.0 68.0 68.1  62.7 63.1 63.5  58.0 58.4 58.7 
12 10 -40  81.6 81.6 82.3  80.8 80.9 81.5  77.1 77.1 77.7  72.5 72.5 73.0  68.1 68.1 68.6  63.5 63.5 64.0  59.1 59.4 59.9 

With engine bleed for packs off, increase weight by 1200 kg.
With engine anti-ice on, decrease weight by 200 kg.
With engine and wing anti-ice on, decrease weight by 1350 kg.
When operating in icing conditions during any part of the flight with forecast landing temperature below
10°C, decrease weight by 5500 kg.
Includes brake energy limits.

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

737-900/CFM56-7B26 Landing
FAA Category G 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  2.66 3.33 3.83  2.27 2.91  1.87 
42 38 34  4.35 4.87 5.38  3.38 3.86 4.37  2.46 2.91 3.38  1.41 1.93 2.37  0.84 1.23  0.31 
30 26 22  5.93 5.97 6.00  4.83 5.19 5.21  3.77 4.06 4.28  2.74 3.02 3.21  1.64 1.99 2.23  0.72 1.06 1.28 
18 14 10  6.02 6.04 6.07  5.23 5.24 5.26  4.29 4.30 4.32  3.38 3.40 3.41  2.39 2.53 2.54  1.45 1.59 1.73 

Gradient Adjustment for Weight (%)
WEIGHT  REFERENCE GO-AROUND GRADIENT (%) 
(1000 KG)  0  1  2  3  4  5  6 
80  -2.40  -2.75  -3.04  -3.32  -3.59  -3.86  -4.12 
75  -1.93  -2.21  -2.44  -2.66  -2.88  -3.09  -3.30 
70  -1.40  -1.58  -1.75  -1.91  -2.06  -2.22  -2.37 
65  -0.76  -0.85  -0.94  -1.03  -1.11  -1.19  -1.28 
60  0.00  0.00  0.00  0.00  0.00  0.00  0.00 
55  0.91  1.02  1.12  1.23  1.33  1.43  1.54 
50  2.00  2.25  2.47  2.70  2.92  3.15  3.39 

Gradient Adjustment for Speed (%)
SPEED  WEIGHT ADJUSTED GO-AROUND GRADIENT (%) 
(KIAS)  0  1  2  3  4  5  6  7 
VREF40 VREF40+5 VREF40+10  -0.24 0.00 0.14  -0.24 0.00 0.14  -0.24 0.00 0.13  -0.25 0.00 0.12  -0.25 0.00 0.11  -0.25 0.00 0.10  -0.25 0.00 0.09  -0.25 0.00 0.08 
　
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