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(including takeoff, step climb FL 310, 350, 390, cruise, descent)
(Honeywell FMS)
Table 40. A340-313E CFM .
Time / .
Fuel
Distance : 6000nm
Takeoff weight : 250 000 kg
New cost index (kg/min)
0 50 80 100 150 200
Initial cost index (kg/min) 0 min kg -16 1100 -20 1790 -23 2260 -25 3000 -25 3450
50 16 -1100 -4 690 -7 1170 -9 1910 -9 2360
80 20 -1790 4 -690 -3 480 -5 1220 -5 1670
100 23 -2260 7 -1170 3 -480 -2 740 -2 1190
150 25 -3000 9 -1910 5 -1220 2 -740 0 450
200 25 -3450 9 -2360 5 -1670 2 -1190 0 -450
(including takeoff, step climb FL 310, 350, 390, cruise, descent)
(Honeywell FMS)
Table 41. A340-313E CFM .
Time / .
Fuel
Distance : 7000nm
Takeoff weight : 260 000 kg
New cost index (kg/min)
0 50 80 100 150 200
Initial cost index (kg/min) 0 min kg -15 1320 -23 2100 -25 2590 -29 3430 -28 3960
50 15 -1320 -8 780 -10 1270 -14 2120 -13 2640
80 23 -2100 8 -780 -2 490 -6 1330 -5 1860
100 25 -2590 10 -1270 2 -490 -4 850 -3 1370
150 29 -3430 14 -2120 6 -1330 4 -850 -1 530
200 28 -3960 13 -2640 5 -1860 3 -1370 1 -530
(including takeoff, step climb FL 310, 350, 390, cruise, descent)
(Honeywell FMS)
Table 42. A340-313E CFM .
Time / .
Fuel
Distance : 8000nm
Takeoff weight : 271 000 kg
New cost index (kg/min)
0 50 80 100 150 200
Initial cost index (kg/min) 0 min kg -19 1550 -25 2430 -28 2940 -32 4140 -35 4830
50 19 -1550 -6 880 -9 1390 -13 2590 -16 3280
80 25 -2430 6 -880 -3 510 -7 1710 -10 2400
100 28 -2940 9 -1390 3 -510 -4 1190 -7 1880
150 32 -4140 13 -2590 7 -1710 4 -1190 -3 690
200 35 -4830 16 -3280 10 -2400 7 -1880 3 -690
APPENDIX 2
A300-600/A310 DEFAULT COST INDEX OPTION
If the company cost index is not known or if it is preferred to refrain from the calculated concept, a default cost index value can easily be assessed to fly in PROFILE (A300-600/A310) at any desired Mach Number compatible with an operational objective 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：getting to grips with the cost index(30)
