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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