Performance Dispatch
FAA
Text
Category C Brakes
737 Flight Crew Operations Manual
Landing Climb Limit Weight
Enter the table with airport OAT and pressure altitude to read landing climb limit weight.  Apply the noted adjustments as required.
Go-Around Climb Gradient
Enter the Reference Go-Around Gradient table with airport OAT and pressure altitude to determine the reference go-around gradient. Then adjust the reference gradient for airplane weight and speed using the tables provided to determine the weight and speed adjusted go-around gradient. Apply the necessary corrections for engine bleed configuration and icing conditions as noted.
Quick Turnaround Limit Weight
Enter the table with airport pressure altitude and OAT to read maximum quick turnaround weight.  Apply the noted adjustments as required. 
If the landing weight exceeds the maximum quick turnaround weight, wait the specified time and then check that the wheel thermal plugs have not melted before executing a subsequent takeoff, or ensure the brake temperature is within limits using the alternate procedure described on the page.
Copyright . The Boeing Company. See title page for details.
September 27, 2004  PD.33.5
Performance Dispatch

737-800/CFM56-7B24 Text
FAA Category C Brakes
737 Flight Crew Operations Manual
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Copyright . The Boeing Company. See title page for details.
737-800/CFM56-7B26 FAA Category C Brakes 737 Flight Crew Operations Manual

Takeoff Field Corrections - Dry Runway Slope Corrections
FIELD LENGTH AVAILABLE (M)  SLOPE CORRECTED FIELD LENGTH (M) 
RUNWAY SLOPE (%) 
-2.0  -1.5  -1.0  -0.5  0.0  0.5  1.0  1.5  2.0 
1200 1400 1600  1230 1450 1670  1220 1440 1650  1210 1430 1640  1210 1410 1620  1200 1400 1600  1190 1370 1560  1170 1350 1530  1160 1320 1490  1140 1300 1450 
1800 2000 2200  1900 2120 2340  1870 2090 2310  1850 2060 2270  1820 2030 2240  1800 2000 2200  1750 1940 2130  1700 1880 2060  1650 1820 1980  1600 1760 1910 
2400 2600 2800  2560 2790 3010  2520 2740 2960  2480 2690 2900  2440 2650 2850  2400 2600 2800  2320 2500 2690  2230 2410 2590  2150 2310 2480  2060 2220 2370 
3000 3200 3400  3230 3450 3680  3170 3390 3610  3120 3330 3540  3060 3260 3470  3000 3200 3400  2880 3070 3260  2760 2940 3120  2640 2810 2970  2520 2680 2830 
3600 3800 4000  3900 4130 4370  3820 4050 4280  3750 3970 4190  3670 3880 4090  3600 3800 4000  3450 3630 3820  3290 3470 3650  3140 3300 3470  2980 3140 3290 
4200 4400 4600  4610 4850 5090  4510 4740 4970  4410 4630 4850  4300 4510 4720  4200 4400 4600  4010 4200 4390  3820 4000 4180  3630 3800 3960  3440 3600 3750 
4800 5000  5330 5570  5200 5430  5070 5290  4930 5140  4800 5000  4580 4760  4350 4530  4130 4290  3900 4060 

Wind Corrections
SLOPE CORR'D FIELD LENGTH (M)  SLOPE & WIND CORRECTED FIELD LENGTH (M) 
WIND COMPONENT (KTS) 
-15  -10  -5  0  10  20  30  40 
1200 1400 1600  880 1050 1220  990 1170 1350  1090 1280 1470  1200 1400 1600  1260 1460 1670  1320 1530 1740  1390 1610 1820  1470 1690 1910 
1800 2000 2200  1390 1560 1720  1530 1700 1880  1660 1850 2040  1800 2000 2200  1870 2080 2280  1950 2160 2370  2040 2250 2470  2130 2350 2570 
2400 2600 2800  1890 2060 2230  2060 2240 2420  2230 2420 2610  2400 2600 2800  2490 2690 2900  2580 2790 3000  2680 2900 3110  2790 3010 3230 
3000 3200 3400  2400 2570 2730  2600 2780 2960  2800 2990 3180  3000 3200 3400  3100 3310 3510  3210 3420 3630  3330 3540 3760  3460 3680 3900 
3600 3800 4000  2900 3070 3240  3130 3310 3490  3370 3560 3750  3600 3800 4000  3720 3920 4130  3840 4050 4260  3970 4190 4410  4120 4340 4560 
4200 4400 4600  3410 3570 3740  3670 3850 4030  3940 4120 4310  4200 4400 4600  4330 4540 4740  4470 4680 4890  4620 4840 5050  4780 5000 5220 
4800 5000  3910 4080  4210 4390  4500 4690  4800 5000  4950 5150  5100 5310  5270 5480  5440 5660 

Copyright . The Boeing Company. See title page for details.
September 27, 2004  PD.40.1
Performance Dispatch
　
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