曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

• Note •
• Balked Landing Climb Gradients shown are the gain in altitude for the horizontal
distance traversed expressed as Feet per Nautical Mile.
• Dashed cells in the table represent performance below the minimum balked landing
climb requirements.
• 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.
• This chart is required data for certification. However, significantly better
performance can be achieved by climbing at Best Rate of Climb speeds shown with
flaps down or following the Go-Around / Balked Landing procedure in Section 4.
Conditions:
• Power ....................................................................................................Full Throttle
• Mixture .......................................................................................................Full Rich
• Flaps ......................................................................................................100% (DN)
• Airspeed.....................................................................................Best Rate of Climb
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet per Nautical Mile
Temperature ~ °C
-20 0 20 40 ISA
3050
SL 84 654 588 527 470 542
2000 81 569 504 444 388 470
4000 78 484 420 361 306 399
6000 75 399 335 277 326
8000 72 313 250 193 253
10000 69 225 164 179
2500
SL 84 878 796 720 650 739
2000 81 779 698 624 556 657
4000 78 680 601 528 461 575
6000 75 582 504 433 493
8000 72 485 408 338 412
10000 69 387 311 329
Revision 01: 08-26-09
36 of 56 11934-S37
Section 9 Cirrus Design
Supplements SR20
Balked Landing Rate of Climb
• Note •
• Balked Landing Rate of Climb values shown are the full flaps change in altitude for
unit time expended expressed in Feet per Minute.
• Dashed cells in the table represent performance below the minimum balked landing
climb requirements.
• 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.
• This chart is required data for certification. However, significantly better
performance can be achieved by climbing at Best Rate of Climb speeds shown with
flaps down or following the Go-Around / Balked Landing procedure in Section 4.
Conditions:
• Power.................................................................................................... Full Throttle
• Mixture....................................................................................................... Full Rich
• Flaps...................................................................................................... 100% (DN)
• Climb Airspeed ...............................................................................................Noted
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB ~ Feet per Minute
Temperature ~ °C
-20 0 20 40 ISA
3050
SL 84 854 798 741 684 756
2000 81 744 685 625 565 652
4000 78 633 571 508 446 549
6000 75 521 455 390 445
8000 72 407 339 271 342
10000 69 293 221 239
2500
SL 84 1140 1076 1010 944 1027
2000 81 1014 946 877 808 908
4000 78 886 815 743 671 790
6000 75 759 683 608 672
8000 72 630 552 474 556
10000 69 502 420 440
Revision 01: 08-26-09
11934-S37 37 of 56
Cirrus Design Section 9
SR20 Supplements
Landing Distance
Factors:
The following factors are to be applied to the computed landing
distance for the noted condition:
• Headwind - Subtract 10% from table distances for each 13
knots headwind
• Tailwind - Add 10% to table distances for each 2 knots tailwind
up to 10 knots.
• Grass Runway, Dry - Add 20% to ground roll distance.
• Grass Runway, Wet - Add 60% to ground roll distance.
• Sloped Runway - Increase table distances by 27% of the
ground roll distance for each 1% of downslope. Decrease table
distances by 9% of the ground roll distance for each 1% of
upslope.
• Caution •
The above corrections for runway slope are required to be
included herein. These corrections should be used with
caution since published runway slope data is usually the net
slope from one end of the runway to the other. Many runways
will have portions of their length at greater or lesser slopes
than the published slope, lengthening (or shortening) landing
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：西銳20飛機信息手冊CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA(135)