737-700/CFM56-7B22 Landing
FAA Category A Brakes
737 Flight Crew Operations Manual
Landing Field Limit Weight - Wet Runway - High Altitudes 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
2600 2800 3000 2800 3000 2790 2990 3200 2980 3190 3400 3180 3390 3610 3390 3610 3830
3200 3400 3600 2950 2880 3080 3270 3200 3400 3600 3400 3600 3810 3610 3820 4030 3830 4040 4260 4050 4270 4490
3800 4000 4200 2810 2990 3170 3130 3320 3510 3460 3660 3850 3800 4000 4200 4010 4220 4420 4230 4440 4650 4470 4690 4910 4710 4930 5150
4400 4600 4800 3350 3530 3710 3690 3880 4070 4040 4240 4430 4400 4600 4800 4630 4830 5030 4860 5070 5280 5120 5340 5550 5370 5590 5810
5000 5200 5400 3890 4070 4250 4250 4440 4630 4620 4820 5010 5000 5200 5400 5240 5440 5650 5490 5700 5910 5770 5990 6200 6030 6250 6470
5600 5800 6000 4430 4620 4800 4810 5000 5190 5200 5400 5590 5600 5800 6000 5850 6060 6260 6120 6320 6530 6420 6630 6850 6690 6910 7130
6200 6400 4980 5160 5370 5560 5780 5980 6200 6400 6460 6670 6740 6950 7070 7280 7350 7570
Field Limit Weight (1000 KG)
WIND CORR'D FIELD LENGTH (M) AIRPORT PRESSURE ALTITUDE (FT)
10000 11000 12000 13000 13500
3200 3400 3600 41.2 44.6 47.9 39.9 43.1 46.3 38.6 41.7 44.8 40.3 43.3 39.7 42.6
3800 4000 4200 51.2 54.4 57.6 49.5 52.6 55.7 47.9 50.9 53.9 46.2 49.2 52.1 45.5 48.3 51.2
4400 4600 4800 60.8 64.0 67.3 58.8 61.9 65.0 56.9 59.9 62.8 55.0 57.9 60.7 54.1 56.9 59.7
5000 5200 5400 70.8 74.3 77.9 68.3 71.6 75.1 65.8 69.1 72.3 63.6 66.6 69.7 62.6 65.4 68.5
5600 5800 6000 81.1 84.2 87.4 78.5 81.5 84.6 75.7 78.9 81.8 72.9 76.1 79.2 71.5 74.7 77.8
6200 6400 6600 87.6 84.8 87.7 82.0 84.9 87.7 80.7 83.5 86.3
Copyright . The Boeing Company. See title page for details.
PD.22.8 September 27, 2004
737-700/CFM56-7B22
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 2000 4000 6000 8000 10000
54 52 50 129 126 122 54.6 55.7 56.8 53.1
48 46 44 118 115 111 57.9 59.1 60.2 54.2 55.3 56.3 51.6 52.6
42 40 38 108 104 100 61.4 62.6 63.8 57.4 58.6 59.7 53.6 54.7 55.8 49.5 50.5 51.5 46.7
36 34 32 97 93 90 65.1 66.4 67.7 60.9 62.1 63.3 56.9 58.0 59.1 52.5 53.6 54.6 47.6 48.6 49.5 44.6 45.6
30 28 26 86 82 79 69.0 69.0 69.1 64.4 65.6 66.7 60.1 61.2 62.3 55.5 56.5 57.5 50.5 51.4 52.3 46.5 47.4 48.3
24 22 20 75 72 68 69.1 69.2 69.3 66.7 66.8 66.8 63.4 64.5 64.6 58.7 59.7 60.8 53.2 54.2 55.3 49.2 50.0 50.9
18 16 14 64 61 57 69.3 69.3 69.4 66.9 66.9 67.0 64.6 64.7 64.7 61.7 61.8 61.8 56.5 57.8 58.9 51.8 52.7 53.9
12 10 -40 54 50 -40 69.4 69.5 70.0 67.0 67.1 67.6 64.8 64.8 65.3 61.8 61.9 62.4 59.0 59.0 59.4 55.1 56.1 56.4
With engine bleed for packs off, increase weight by 1000 kg.
With engine anti-ice on, decrease weight by 200 kg.
With engine and wing anti-ice on, decrease weight by 600 kg.
When operating in icing conditions during any part of the flight with forecast landing temperature below
10°C, decrease weight by 4700 kg.
Copyright . The Boeing Company. See title page for details.
Performance Dispatch
737-700/CFM56-7B22 Landing
FAA Category A Brakes
737 Flight Crew Operations Manual
Landing Climb Limit Weight - High Altitudes Valid for approach with Flaps 15 and landing with Flaps 40 Based on engine bleed for packs on and anti-ice off
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