Decrease field limit weight by 4500 kg when using manual speedbrakes.
Copyright . The Boeing Company. See title page for details.
Performance Dispatch
737-700/CFM56-7B20 Landing
FAA Category A Brakes
737 Flight Crew Operations Manual
Landing Field Limit Weight - Wet Runway Flaps 40 Based on anti-skid inoperative and manual speedbrakes Wind Corrected Field Length (M)
FIELD LENGTH AVAILABLE (M) WIND COMPONENT (KTS)
-15 -10 -5 0 10 20 30 40
1800 2000 2200 1910 2000 2200 1950 2160 2360 2120 2330 2550 2300 2510 2730 2470 2700 2920
2400 2600 2800 1940 2020 2200 2110 2300 2490 2400 2600 2800 2570 2770 2980 2760 2970 3180 2950 3160 3380 3140 3370 3590
3000 3200 3400 2120 2290 2470 2390 2580 2760 2690 2880 3070 3000 3200 3400 3190 3390 3600 3390 3600 3810 3590 3810 4030 3810 4030 4260
3600 3800 4000 2650 2830 3010 2950 3130 3320 3260 3460 3650 3600 3800 4000 3810 4010 4220 4030 4240 4450 4250 4460 4680 4480 4700 4930
4200 4400 4600 3180 3360 3540 3510 3690 3880 3840 4030 4230 4200 4400 4600 4420 4630 4840 4660 4870 5080 4900 5110 5330 5150 5370 5590
4800 5000 5200 3720 3900 4070 4060 4250 4440 4420 4610 4810 4800 5000 5200 5040 5250 5460 5290 5510 5720 5550 5760 5980 5820 6040 6260
5400 5600 4250 4430 4620 4810 5000 5190 5400 5600 5660 5870 5930 6140 6200 6410 6490
Field Limit Weight (1000 KG)
WIND CORR'D FIELD LENGTH (M) AIRPORT PRESSURE ALTITUDE (FT)
0 2000 4000 6000 8000 10000
2400 2600 2800 39.9 44.4 48.9 41.7 46.0 38.6 42.7 39.9
3000 3200 3400 53.5 58.0 62.5 50.3 54.6 58.9 46.7 50.8 54.8 43.7 47.5 51.3 40.7 44.3 47.9 41.2 44.6
3600 3800 4000 67.2 72.2 77.2 63.1 67.4 72.0 58.9 62.8 66.8 55.0 58.7 62.4 51.5 54.9 58.3 47.9 51.2 54.4
4200 4400 4600 81.7 76.7 80.9 71.0 75.4 79.5 66.1 70.1 74.1 61.7 65.2 68.8 57.6 60.8 64.0
4800 5000 5200 83.5 78.1 81.8 72.6 76.4 80.0 67.3 70.8 74.3
5400 5600 83.4 77.9 81.1
Copyright . The Boeing Company. See title page for details.
PD.12.4 September 27, 2004
737-700/CFM56-7B20
Performance Dispatch
FAA
Landing
Category A 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
50 48 46 122 118 115 51.4 52.5 53.6 51.1 52.1 53.2 50.6 51.7 52.7 51.3 52.3
44 42 40 111 108 104 54.6 55.8 56.9 54.4 55.5 56.6 53.8 55.0 56.1 53.4 54.5 55.6
38 36 34 100 97 93 58.0 59.2 60.3 57.7 58.9 60.0 57.3 58.4 59.5 56.7 57.9 59.0
32 30 28 90 86 82 61.6 62.8 62.9 61.2 62.4 62.5 60.7 62.0 62.2 60.2 61.3 61.7
26 24 22 79 75 72 63.0 63.0 63.1 62.6 62.6 62.7 62.3 62.3 62.4 61.7 61.8 61.8
20 18 16 68 64 61 63.1 63.2 63.2 62.7 62.8 62.8 62.4 62.5 62.5 61.8 61.9 61.9
14 12 10 -40 57 54 50 -40 63.2 63.3 63.3 63.8 62.8 62.9 62.9 63.4 62.5 62.6 62.6 63.1 62.0 62.0 62.0 62.5
With engine bleed for packs off, increase weight by 1400 kg.
With engine anti-ice on, decrease weight by 150 kg.
With engine and wing anti-ice on, decrease weight by 750 kg.
When operating in icing conditions during any part of the flight with forecast landing temperature below
10°C, decrease weight by 5150 kg.
Copyright . The Boeing Company. See title page for details.
Performance Dispatch
737-700/CFM56-7B20 Landing
FAA Category A 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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