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.53.5
Performance Dispatch
737-800/CFM56-7B27 Text
FAA Category C Brakes
737 Flight Crew Operations Manual
Intentionally
Blank
Copyright . The Boeing Company. See title page for details.
737-900/CFM56-7B26 FAA Category G 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 1220 1430 1650 1210 1420 1630 1210 1420 1620 1200 1410 1610 1200 1400 1600 1190 1380 1560 1180 1350 1530 1170 1330 1490 1160 1310 1460
1800 2000 2200 1860 2080 2300 1840 2060 2280 1830 2040 2250 1810 2020 2230 1800 2000 2200 1750 1940 2130 1700 1880 2050 1660 1820 1980 1610 1760 1910
2400 2600 2800 2530 2750 2970 2490 2710 2930 2460 2670 2890 2430 2640 2840 2400 2600 2800 2310 2500 2690 2230 2400 2580 2140 2310 2470 2060 2210 2360
3000 3200 3400 3190 3430 3660 3140 3370 3600 3100 3310 3530 3050 3260 3470 3000 3200 3400 2880 3070 3250 2760 2930 3110 2630 2800 2960 2510 2660 2810
3600 3800 4000 3900 4150 4410 3820 4060 4310 3750 3970 4200 3670 3890 4100 3600 3800 4000 3440 3630 3820 3280 3460 3630 3120 3280 3450 2960 3110 3260
4200 4400 4600 4670 4900 5130 4550 4780 5000 4430 4650 4870 4320 4530 4730 4200 4400 4600 4000 4190 4380 3810 3980 4160 3610 3770 3930 3410 3560 3710
4800 5000 5360 5590 5220 5440 5080 5300 4940 5150 4800 5000 4570 4750 4330 4510 4100 4260 3860 4010
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 890 1050 1220 990 1170 1350 1100 1280 1470 1200 1400 1600 1270 1470 1680 1340 1550 1760 1410 1620 1840 1480 1700 1920
1800 2000 2200 1390 1560 1720 1530 1700 1880 1660 1850 2040 1800 2000 2200 1890 2090 2300 1970 2180 2390 2060 2280 2490 2150 2370 2590
2400 2600 2800 1890 2060 2220 2060 2240 2420 2230 2420 2610 2400 2600 2800 2500 2710 2910 2610 2820 3030 2710 2930 3150 2820 3040 3270
3000 3200 3400 2390 2560 2720 2590 2770 2950 2800 2990 3170 3000 3200 3400 3120 3320 3530 3240 3450 3660 3360 3580 3800 3490 3710 3940
3600 3800 4000 2890 3060 3230 3130 3310 3480 3360 3550 3740 3600 3800 4000 3740 3940 4150 3870 4090 4300 4020 4230 4450 4160 4380 4610
4200 4400 4600 3390 3560 3730 3660 3840 4020 3930 4120 4310 4200 4400 4600 4350 4560 4760 4510 4720 4930 4670 4890 5100 4830 5050 5280
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737NG机组操作手册Flight Crew Operations Manual FCOM 2(18)
