曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

knots headwind.
Tailwind: Add 10% for each 2 knots
tailwind up to 10 knots.
Runway Slope: Reference Notes.
Dry Grass: Add 20% to Ground Roll.
Wet Grass: Add 30% to Ground Roll.
PRESS
ALT
FT
DISTANCE
FT
TEMPERATURE ~°C
0 10 20 30 40 ISA
SL Grnd Roll 917 990 1067 1146 1229 1028
50 ft 1432 1539 1650 1764 1883 1594
1000 Grnd Roll 1011 1092 1176 1264 1355 1117
50 ft 1574 1691 1813 1939 2069 1728
2000 Grnd Roll 1116 1206 1299 1395 1496 1215
50 ft 1732 1861 1995 2133 2276 1874
3000 Grnd Roll 1234 1332 1435 1542 1653 1323
50 ft 1907 2049 2196 2349 2507 2035
4000 Grnd Roll 1365 1474 1588 1706 1829 1441
50 ft 2102 2259 2422 2590 2764 2212
5000 Grnd Roll 1512 1633 1758 1889 2025 1572
50 ft 2320 2493 2673 2858 3051 2407
6000 Grnd Roll 1676 1810 1950 2095 2245 1717
50 ft 2564 2755 2953 3159 3371 2622
7000 Grnd Roll 1861 2009 2164 2325 2492 1877
50 ft 2837 3048 3267 3494 3729 2859
8000 Grnd Roll 2068 2233 2405 2584 2770 2054
50 ft 3142 3376 3619 3871 4131 3122
9000 Grnd Roll 2302 2485 2677 2875 3082 2250
50 ft 3485 3744 4014 4293 4581 3412
10000 Grnd Roll 2564 2769 2982 3204 3434 2468
50 ft 3870 4158 4457 4767 5088 3733
March 2010
5-14 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Takeoff Distance - 2900 LB
Weight: 2900 LB
Speed at Liftoff: 70 KIAS
Speed over 50 Ft. Obstacle: 74 KIAS
Flaps: 50%
Power: Takeoff
Runway: Dry, Paved, Level
Headwind: Subtract 10% for each 12
knots headwind.
Tailwind: Add 10% for each 2 knots
tailwind up to 10 knots.
Runway Slope: Reference Notes.
Dry Grass: Add 20% to Ground Roll.
Wet Grass: Add 30% to Ground Roll.
PRESS
ALT
FT
DISTANCE
FT
TEMPERATURE ~°C
0 10 20 30 40 ISA
SL Grnd Roll 610 659 710 763 818 684
50 ft 971 1043 1118 1195 1275 1080
1000 Grnd Roll 673 727 783 841 902 743
50 ft 1066 1146 1228 1313 1401 1170
2000 Grnd Roll 743 802 864 929 995 809
50 ft 1173 1260 1351 1444 1541 1269
3000 Grnd Roll 821 887 955 1026 1100 880
50 ft 1292 1388 1487 1590 1697 1378
4000 Grnd Roll 908 981 1057 1135 1217 959
50 ft 1424 1530 1639 1753 1871 1498
5000 Grnd Roll 1006 1086 1170 1257 1348 1046
50 ft 1571 1688 1809 1935 2065 1630
6000 Grnd Roll 1116 1205 1298 1394 1494 1143
50 ft 1736 1865 1999 2138 2281 1775
7000 Grnd Roll 1238 1337 1440 1547 1659 1249
50 ft 1920 2063 2211 2365 2523 1936
8000 Grnd Roll 1376 1486 1601 1720 1843 1367
50 ft 2127 2285 2449 2619 2795 2113
9000 Grnd Roll 1532 1654 1781 1914 2051 1498
50 ft 2359 2534 2716 2904 3099 2309
10000 Grnd Roll 1707 1843 1985 2132 2285 1643
50 ft 2619 2814 3016 3225 3441 2527
March 2010
Cirrus Design Section 5
SR22 Performance Data
Information Manual 5-15
Takeoff Climb Gradient
• Note •
Climb Gradients shown are the gain in altitude for the horizontal distance
traversed expressed as Feet per Nautical Mile.
Fuel flow must be set to the placarded limit for all takeoffs and climbs.
Cruise climbs or short duration climbs are permissible at best power as long
as altitudes and temperatures remain within those specified in the table.
For operation in air colder than this table provides, use coldest data shown.
For operation in air warmer than this table provides, use extreme caution.
Conditions:
• Power ....................................................................................................Full Throttle
• Mixture ............................................................................................Set per Placard
• Flaps .................................................................................................................50%
• Airspeed.....................................................................................Best Rate of Climb
Weight
LB
Press
Altitude
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet per Nautical Mile
Temperature ~°C
-20 0 20 40 ISA
3400
SL 91 939 896 853 811 864
2000 90 834 793 752 711 770
4000 89 734 694 654 615 680
6000 88 638 600 561 524 594
8000 88 546 509 472 436 510
10000 87 458 422 387 353 431
2900
SL 91 1172 1122 1070 1019 1083
2000 90 1049 1000 950 902 972
4000 89 931 884 836 790 867
6000 88 818 773 727 683 766
8000 88 711 667 623 581 669
10000 87 608 566 524 484 576
March 2010
5-16 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Takeoff Rate of Climb
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：西銳20飛機(jī)信息手冊 SR22 AIRPLANE INFORMATION MANUAL 2979(42)