Copyright . The Boeing Company. See title page for details.
737-800/CFM56-7B24 FAA Category C Brakes 737 Flight Crew Operations Manual

Landing Field Limit Weight Flaps 40 Wind Corrected Field Length (M)
FIELD LENGTH AVAILABLE (M)  WIND COMPONENT (KTS) 
-15  -10  -5  0  10  20  30  40 
1000  810  900  1000  1060  1130  1200  1270 
1200  900  1000  1100  1200  1270  1340  1420  1500 
1400  1080  1180  1290  1400  1470  1560  1640  1720 
1600  1250  1360  1480  1600  1680  1770  1850  1940 
1800  1430  1550  1670  1800  1890  1980  2070  2170 
2000  1610  1730  1860  2000  2090  2190  2290  2390 
2200  1790  1920  2050  2200  2300  2400  2510  2620 
2400  1970  2100  2250  2400  2510  2610  2720 
2600  2140  2290  2440  2600  2720 
2800  2320  2470  2630  2800 
3000  2500  2650 
3200  2680 

Field Limit Weight (1000 KG)
WIND CORR’D FIELD LENGTH (M)  AIRPORT PRESSURE ALTITUDE (FT) 
0  2000  4000  6000  8000  10000 
DRY  WET  DRY  WET  DRY  WET  DRY  WET  DRY  WET  DRY  WET 
1000 1200 1400  36.0 46.0 55.7  38.2 46.9  43.4 52.9  36.0 44.2  40.9 49.9  41.7  38.5 47.1  39.2  36.2 44.3  36.9  41.6 
1600 1800 2000  63.7 72.3 81.3  55.4 62.3 69.6  60.8 68.7 77.1  52.5 59.5 66.1  58.1 65.2 73.2  49.5 56.8 63.0  55.4 62.2 69.4  46.7 54.1 60.2  52.4 59.3 65.8  43.9 51.0 57.4  49.3 56.5 62.6  41.3 48.0 54.7 
2200 2400 2600  88.5  77.4 85.0 90.4  85.3  73.4 80.8 87.1  81.2 87.8  69.7 76.7 83.7  77.0 84.5 89.8  66.1 72.7 79.3  72.9 80.1 85.6  62.9 68.8 75.1  69.0 75.7 81.7  60.0 65.2 71.0 
2800 3000 3200  88.8  85.5 90.1  88.4  81.3 85.7 88.2  84.8 87.1 89.4  76.8 81.8 84.6 
3400 3600 3800  90.6  86.6 88.6 90.6 

Decrease field limit weight 4300 kg when using manual speedbrakes.
Copyright . The Boeing Company. See title page for details.
Performance Dispatch

737-800/CFM56-7B24 Landing
FAA Category C 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  LANDING CLIMB LIMIT WEIGHT (1000 KG) 
AIRPORT PRESSURE ALTITUDE (FT) 
°C  °F  0  1000  2000  3000 
54 52 50  129 126 122  57.6 58.7 59.9  56.6 57.7  55.5 
48 46 44  118 115 111  61.0 62.3 63.4  58.8 60.0 61.1  56.6 57.7 58.9  54.5 55.6 56.6 
42 40 38  108 104 100  64.6 65.9 67.1  62.3 63.5 64.7  60.0 61.1 62.3  57.7 58.8 60.0 
36 34 32  97 93 90  68.4 69.6 70.9  65.9 67.1 68.3  63.4 64.6 65.8  61.1 62.2 63.3 
30 28 26  86 82 79  72.3 72.3 72.4  69.6 70.9 71.0  67.1 68.3 69.6  64.5 65.7 67.0 
24 22 20  75 72 68  72.5 72.5 72.6  71.1 71.1 71.2  69.7 69.7 69.8  68.2 68.3 68.3 
18 16 14  64 61 57  72.6 72.7 72.7  71.2 71.3 71.3  69.8 69.9 69.9  68.4 68.4 68.5 
12 10 -40  54 50 -40  72.8 72.9 73.4  71.4 71.4 72.0  70.0 70.0 70.6  68.5 68.6 69.2 

With engine bleed for packs off, increase weight by 1200 kg.
With engine anti-ice on, decrease weight by 250 kg.
With engine and wing anti-ice on, decrease weight by 1200 kg.
When operating in icing conditions during any part of the flight with forecast landing temperature below
10°C, decrease weight by 5800 kg.

Copyright . The Boeing Company. See title page for details.
737-800/CFM56-7B24

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 
　
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