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
Intentionally
Blank
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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