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Using the Payload/Range and Takeoff Field Length Charts in the Airplan

CHARACTERISTICS UNITS BASELINE AIRPLANE HIGH GROSS WEIGHT OPTION MAX DESIGN P O U N D S 5 0 8 , 0 0 0 5 1 7 , 0 0 0 5 3 7 , 0 0 0 5 8 2 , 0 0 0 5 9 2 , 0 0 0 6 3 4 , 5 0 0 TAXI WEIGHT K I L O G R A

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Using the Payload/Range and Takeoff Field Length Charts in the Airplan






Presentation on theme: "Using the Payload/Range and Takeoff Field Length Charts in the Airplan"— Presentation transcript:

Using the Payload/Range and Takeoff Field Length Charts in the Airplane Characteristics for Airport Planning DocumentsA question that is common is how to use the data provided in Section 3 - Airplane CHARACTERISTICS UNITS BASELINE AIRPLANE HIGH GROSS WEIGHT OPTION MAX DESIGN P O U N D S 5 0 8 , 0 0 0 5 1 7 , 0 0 0 5 3 7 , 0 0 0 5 8 2 , 0 0 0 5 9 2 , 0 0 0 6 3 4 , 5 0 0 TAXI WEIGHT K I L O G R A M S 2 3 0 , 4 5 0 2 3 4 , 5 0 0 2 4 3 , 5 0 0 2 6 3 , 6 4 0 2 6 8 , 4 8 0 2 8 7 , 8 0 0 MAX DESIGN P O U N D S 5 0 6 , 0 0 0 5 1 5 , 0 0 0 5 3 5 , 0 0 0 5 8 0 , 0 0 0 5 9 0 , 0 0 0 6 3 2 , 5 0 0 TAKEOFF WEIGHT K I L O G R A M S 2 2 9 , 5 0 0 2 3 3 , 6 0 0 2 4 2 , 6 3 0 2 6 3 , 0 3 0 2 6 7 , 5 0 0 2 8 6 , 9 0 0 MAX DESIGN P O U N D S 4 4 1 , 0 0 0 4 4 5 , 0 0 0 4 4 5 , 0 0 0 4 6 0 , 0 0 0 4 6 0 , 0 0 0 4 6 0 , 0 0 0 LANDING WEIGHT K I L O G R A M S 2 0 0 , 0 5 0 2 0 1 , 8 0 0 2 0 1 , 8 0 0 2 0 8 , 7 0 0 2 0 8 , 7 0 0 2 0 8 , 7 0 0 MAX DESIGN ZERO P O U N D S 4 2 0 , 0 0 0 4 2 0 , 0 0 0 4 2 0 , 0 0 0 4 3 0 , 0 0 0 4 3 0 , 0 0 0 4 3 0 , 0 0 0 FUEL WEIGHT K I L O G R A M S 1 9 0 , 4 7 0 1 9 0 , 4 7 0 1 9 0 , 4 7 0 1 9 5 , 0 0 0 1 9 5 , 0 0 0 1 9 5 , 0 0 0 SPEC OPERATING P O U N D S 2 9 8 , 9 0 0 2 9 8 , 9 0 0 2 9 9 , 5 5 0 3 0 4 , 5 0 0 3 0 4 , 5 0 0 3 0 4 , 5 0 0 EMPTY WEIGHT (1) K I L O G R A M S 1 3 5 , 5 5 0 1 3 5 , 5 5 0 1 3 5 , 8 5 0 1 3 8 , 1 0 0 1 3 8 , 1 0 0 1 3 8 , 1 0 0 MAX STRUCTURAL P O U N D S 1 2 1 , 1 0 0 1 2 1 , 1 0 0 1 2 0 , 4 5 0 1 2 5 , 5 5 0 1 2 5 , 5 5 0 1 2 5 , 5 5 0 PAYLOAD K I L O G R A M S 5 4 , 9 2 0 5 4 , 9 2 0 5 4 , 6 2 0 5 6 , 9 4 0 5 6 , 9 4 0 5 6 , 9 4 0 SEATING TWO-CLASS 375 - 30 FIRST + 345 ECONOMY CAPACITY (1) THREE-CLASS 305 - 24 FIRST + 54 BUSINESS + 227 ECONOMY MAX CARGO CUBIC FEET 5,656(2 ) 5,656(2 ) 5 , 6 5 6 ( 2 ) 5 , 6 5 6 ( 2 ) 5 , 6 5 6 ( ) 5 , 6 5 6 ( 2 ) - LOWER DECK CUBIC METERS 160.3 (2) 160.3 (2) 160.3 (2) 160.3 (2) 160.3 (2) 160.3 (2) USABL E F U E L U S G A L L O N S 3 1 , 0 0 0 3 1 , 0 0 0 3 1 , 0 0 0 4 5 , 2 2 0 4 5 , 2 2 0 4 5 , 2 2 0 L I T E R S 1 1 7 , 3 0 0 1 1 7 , 3 0 0 1 1 7 , 3 0 0 1 7 1 , 1 0 0 1 7 1 , 1 0 0 1 7 1 , 1 0 0 P O U N D S 2 0 7 , 7 0 0 2 0 7 , 7 0 0 2 0 7 , 7 0 0 3 0 2 , 2 7 0 3 0 2 , 2 7 0 3 0 2 , 2 7 0 K I L O G R A M S 9 4 , 2 4 0 9 4 , 2 4 0 9 4 , 2 4 0 1 3 7 , 4 6 0 1 3 7 , 4 6 0 1 3 7 , 4 6 0 NOTES: (1) SPEC WEIGHT FOR BASELINE CONFIGURATION OF 375 PASSENGERS. CONSULT WITH AIRLINE FOR SPECIFIC WEIGHTS AND CONFIGURATIONS. (2) FWD CARGO = 18 LD3' S AT 158 CU FT EACH. AFT CARGO = 14 LD3' S AT 158 CU FT EACH. BULK CARGO = 600 CU FT 2.1.1 GENERAL CHARACTERISTICS MODEL 777-200 (GENERAL ELECTRIC ENGINES) D6-5832 9 JULY 1998 9 3.2.1 PAYLOAD/RANGE FOR 0.84 MACH CRUISE MODEL 777-200 (BASELINE AIRPLANE) D6-5832 9 42 JULY 1998 3300 3.3.1 F.A.R. TAKEOFF RUNWAY LE NGTH REQUIREMENTS - STANDARD DAY MODEL 777-200 (BASELINE AIRPLANE) D6-5832 9 46 JULY 1998