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者

• For operation in air warmer than this table provides, use extreme caution.
Conditions: Example:
• Power...............................Full Throttle Outside Air Temp ...................... 10° C
• Mixture.......................Set per Placard Weight...................................3400 LB
• Flaps........................................... 50% Pressure Altitude...................6000 FT
• Airspeed ...............Best Rate of Climb
Climb Airspeed..................... 88 Knots
Rate of Climb .......................948 FPM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB ~ Feet per Minute
Temperature ~ °C
-20 0 20 40 ISA
3400
SL 91 1326 1317 1300 1277 1304
2000 90 1214 1200 1179 1153 1189
4000 89 1100 1082 1057 1028 1074
6000 88 985 962 934 901 958
8000 87 869 842 809 774 843
10000 86 851 719 683 644 727
2900
SL 91 1646 1638 1621 1598 1626
2000 90 1518 1505 1484 1457 1494
4000 89 1389 1371 1346 1316 1363
6000 88 1259 1236 1207 1172 1232
8000 87 1128 1100 1066 1028 1101
10000 86 995 962 924 883 971
June 2007
Information Manual 5-23
Cirrus Design Section 5
SR22 Performance Data
Enroute 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: Example:
• Power .............................. Full Throttle Outside Air Temp.......................20° C
• Mixture ................................. Full Rich Weight .................................. 3400 LB
• Flaps .....................................0% (UP) Pressure Altitude .................. 4000 FT
• Airspeed............... Best Rate of Climb
Climb Airspeed .....................98 Knots
Gradient............................639 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT - Feet per Nautical Mile
Temperature ~ °C
-20 0 20 40 ISA
3400
SL 101 911 867 823 781 834
2000 100 813 771 729 689 748
4000 98 720 679 639 600 665
6000 97 630 590 552 515 584
8000 96 544 505 468 433 507
10000 95 461 424 388 354 433
12000 94 381 346 312 279 361
14000 93 304 271 238 207 292
16000 92 231 199 168 139 226
2900
SL 101 1130 1078 1026 975 1039
2000 100 1015 965 915 867 937
4000 98 905 857 809 763 840
6000 97 800 753 708 664 746
8000 96 699 654 611 569 656
10000 95 603 560 518 478 570
12000 94 610 469 429 391 487
14000 93 422 382 344 308 407
16000 92 337 299 263 229 331
Figure 5-12
June 2007
5-24 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Figure 5-13
Enroute Rate of Climb
• Note •
• Rate-of-Climb values shown are change in altitude in feet per unit time expressed in
Feet per Minute.
• 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: Example:
• Power...............................Full Throttle Outside Air Temp ...................... 10° C
• Mixture............................As Required Weight...................................3400 LB
• Flaps.....................................0% (UP) Pressure Altitude...................6000 FT
• Airspeed ...............Best Rate of Climb
Climb Airspeed..................... 97 Knots
Rate of Climb .....................1030 FPM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB ~ Feet per Minute
Temperature ~ °C
-20 0 20 40 ISA
3400
SL 101 1428 1414 1392 1366 1398
2000 100 1311 1292 1267 1238 1279
4000 98 1193 1170 1141 1108 1160
6000 97 1074 1046 1013 977 1041
8000 96 953 921 884 845 922
10000 95 830 794 754 712 803
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(42)