737-800/CFM56-7B26 Text
FAA Category C Brakes
737 Flight Crew Operations Manual
To determine the maximum weight for terrain clearance, enter the table with required net level off pressure altitude and expected ISA deviation to obtain weight.  Adjust weight for anti-ice operation as noted below the table.
Extended Range Operations
Regulations require that flights conducted over a route that contains a point further than one hour’s time at “normal one engine inoperative speed” from an adequate diversion airport comply with rules set up specifically for “Extended Range Operation with Two Engine airplanes.” This section provides reserve fuel planning information for the "Critical Fuel Scenario" based on two engine operation at Long Range Cruise as well as single engine operation at Long Range Cruise.
Long Range Cruise Critical Fuel Reserves
Enter the Ground to Air Miles Conversion table with forecast wind and ground distance to diversion airport from critical point to obtain air distance. Now enter the Critical Fuel table with air distance and expected weight at the critical point and read required fuel. Apply the noted fuel adjustments as necessary.  Regulations require a 5% allowance for performance deterioration unless a value has been established by the operator for inservice deterioration.
As noted below each table, the fuel required is the greater of the two engine fuel and the single engine fuel.  This fuel is compared to the amount of fuel normally onboard the airplane at that point in the route.  If the fuel required by the critical fuel reserves exceeds the amount of fuel normally expected, the fuel load must be adjusted accordingly.
Landing
Tables are provided for determining the maximum landing weight as
limited by field length or climb requirements for a single landing flap. Maximum landing weight is the lowest of the field length limit weight, climb limit weight, or maximum certified landing weight.
Landing Field Limit Weight
Obtain wind corrected field length by entering the Wind Corrected Field Length table with field length available and wind component along the runway. Now enter the Field Limit Weight table with wind corrected field length and pressure altitude to read field limit weight for the expected runway condition.
Copyright . The Boeing Company. See title page for details.
737-800/CFM56-7B26

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.43.5
Performance Dispatch

737-800/CFM56-7B26 Text
FAA Category C Brakes
737 Flight Crew Operations Manual
Intentionally
Blank

Copyright . The Boeing Company. See title page for details.
737-800/CFM56-7B27 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  1200 1430 1650  1200 1420 1640  1200 1410 1630  1200 1410 1610  1200 1400 1600  1190 1380 1570  1170 1350 1530  1160 1330 1500  1140 1300 1460 
1800 2000 2200  1870 2100 2320  1860 2070 2290  1840 2050 2260  1820 2020 2230  1800 2000 2200  1760 1950 2140  1710 1890 2070  1670 1840 2010  1620 1780 1940 
2400 2600 2800  2550 2770 3000  2510 2730 2950  2470 2690 2900  2440 2640 2850  2400 2600 2800  2330 2510 2700  2250 2430 2600  2180 2340 2500  2100 2250 2400 
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737NG機組操作手冊Flight Crew Operations Manual FCOM 2(2)