Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов, Страница: 656 / 923

Page 4-59
Sub-section 4
CRUISE - ENROUTE
Hawker 800XP Pro Line 21
Section IV - FLIGHT PLANNING DATA
Pilot’s Operating Manual
Revision A1: Nov, 2002
EN ROUTE FUEL CHECK
ALTITUDE ft PRESENT WEIGHT thousands of lb
41,000
19 21 22 23 24
39,000
19 21 22 23 24 25 26
37,000
19 21 22 24 25 26
35,000
19 21 22 23 24 25 26 27
33,000
19 20 21 23 24 25 26 27
31,000
19 20 21 23 24 25 27
HEADWIND <----(KT)----> TAILWIND
GR
OUND
DIST
AN
CE
T
O
GO
nm
100 80 60 40 20 0 -20 -40 -60 -80 -100
149 160 170 180 189 200 210 220 230 240 250 440 440 450 460 470 490 490 500 510 520 530 530 540 560
225 240 255 270 285 300 315 330 345 360 375 710 710 730 750 760 780 800 810 820 840 860 860 880 910
FU
EL
(l
b)
T
O
150
0
feet
300 320 340 360 380 400 420 440 460 480 500 870 970 1010 1030 1060 1090 1110 1130 1140 1160 1180 1200 1220 1260
375 400 425 450 475 500 525 550 575 600 625 1140 1240 1290 1320 1350 1390 1420 1440 1460 1480 1520 1530 1560 1610
450 480 510 540 570 600 630 660 690 720 750 1410 1520 1570 1610 1640 1690 1730 1760 1780 1810 1850 1870 1910 1970
525 560 595 630 665 700 735 770 805 840 875 1680 1780 1850 1900 1940 2010 2040 2080 2110 2140 2190 2220 2260 2320
600 640 680 720 760 800 840 880 920 960 1000 1960 2060 2140 2190 2240 2320 2360 2400 2430 2470 2530 2560 2610 2690
675 720 765 810 855 900 945 990 1035 1080 1125 2240 2340 2430 2490 2550 2630 2680 2730 2760 2810 2870 2910 2960 3040
750 800 850 900 950 1000 1050 1100 1150 1200 1250 2630 2720 2790 2850 2940 3010 3060 3090 3140 3210 3260 3310 3410
825 880 935 990 1045 1100 1155 1210 1265 1320 1375 2910 3020 3100 3160 3270 3330 3380 3430 3480 3560 3610 3670 3780
900 960 1020 1080 1140 1200 1260 1320 1380 1440 1500 3210 3320 3410 3480 3590 3660 3720 3770 3830 3910 3960 4030 4150
975 1040 1105 1170 1235 1300 1365 1430 1495 1560 1625 3500 3620 3720 3790 3910 3990 4060 4110 4170 4260 4320 4390 4520
1050 1120 1190 1260 1330 1400 1470 1540 1610 1680 1750 3790 3920 4030 4110 4240 4320 4390 4450 4520 4620 4670 4760 4890
1125 1200 1275 1350 1425 1500 1575 1650 1725 1800 1875 4110 4240 4350 4440 4570 4660 4730 4790 4870 4970 5030 5110 5260
1200 1280 1360 1440 1520 1600 1680 1760 1840 1920 2000 4560 4670 4760 4910 5000 5080 5140 5220 5320 5390 5480 5630
1275 1360 1445 1530 1615 1700 1785 1870 1955 2040 2125 4870 5000 5090 5240 5340 5420 5490 5570 5680 5750 5840 6010
1350 1440 1530 1620 1710 1800 1890 1980 2070 2160 2250 5200 5330 5430 5580 5680 5770 5840 5920 6040 6110 6210 6380
1425 1520 1615 1710 1805 1900 1995 2090 2185 2280 2375 5660 5760 5920 6020 6110 6180 6270 6380 6460 6560 6730
1500 1600 1700 1800 1900 2000 2100 2200 2300 2400 2500 5990 6100 6270 6370 6460 6540 6630 6750 6820 6930 7110
1575 1680 1785 1890 1995 2100 2205 2310 2415 2520 2625 6340 6440 6610 6720 6810 6890 6980 7100 7180 7280 7470
1650 1760 1870 1980 2090 2200 2310 2420 2530 2640 2750 6940 7040 7140 7220 7310 7430 7510 7620 7810
1725 1840 1955 2070 2185 2300 2415 2530 2645 2760 2875 7290 7410 7500 7580 7680 7810 7880 8000 8190
1800 1920 2040 2160 2280 2400 2520 2640 2760 2880 3000 7760 7850 7930 8020 8150 8230 8340 8530
1875 2000 2125 2250 2375 2500 2625 2750 2875 3000 3125 8080 8180 8260 8360 8490 8570 8680 8880
1950 2080 2210 2340 2470 2600 2730 2860 2990 3120 3250 8630 8730 8860 8940 9060 9260
2025 160 295 430 565 2700 2835 2970 3105 3240 3375 8960 9060 9190 9270 9380 9580
2100 2240 2380 2520 2660 2800 2940 3080 3220 3360 3500 9320 9420 9560 9640 9750 9950
8XC170
INSTRUCTIONS FOR USE OF TABLE
The numbers in the instructions below refer to the stage numbers shown on the table.
1. Enter the left part of the table with headwind or tailwind as appropriate, then
move down to the ground distance to go . Move across to the right to identify
the entry row in part
.
2. Enter the top part with cruise altitude and move along that row to the present
weight . Move down to identify the entry column in part .
3. The intersection of the row and column thus identified in part of the table will
show the fuel required to cover the remaining distance to the destination.
NOTES:
1. If the ground distance to go falls between two values in the table
then interpolate the fuel required from the corresponding rows in
part
.
2. The effect of temperature on the en route fuel check is negligible.
1
2
3
1
3
2
4
5
4
5
5
5
5