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fuel at 75% power and fuel burn for descent.
• Range and endurance shown includes descent to final destination at 160 KIAS and
500 fpm.
• Range is decreased by 5% if nose wheel pant and fairings removed.
• Range is decreased by 15% if nose and main wheel pants and fairings removed.
Conditions: Example:
• Weight ...................................3000 LB Power Setting .............................75%
• Temperature ................. Standard Day Takeoff Press Alt .................. 2000 FT
• Winds ..........................................Zero Cruise Press Alt.................... 6000 FT
• Mixture ............................. See Tables
• Total Fuel........................... 56 Gallons Fuel to Climb 1.3 Gal.
Cruise Fuel Flow 11.6 GPH
Endurance 4.0 Hr
Range 617 NM
True Airspeed 152 Knots
75% POWER Mixture = Best Power
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
0 0.0 46.3 143 11.6 4.0 576 12.3
2000 0.6 45.7 147 11.6 4.0 594 12.6
4000 1.3 45.0 150 11.6 4.0 606 12.7
6000 2.0 44.3 152 11.6 4.0 617 12.7
8000 2.9 43.4 155 11.6 4.0 627 12.8
10000 3.8 42.5
12000 5.0 41.3
14000 6.8 39.5
Figure 5-17
Sheet 1 of 2
March 2010
5-30 Information Manual
Section 5 Cirrus Design
Performance Data SR20
Figure 5-17
Range / Endurance Profile
65% POWER Mixture = Best Power
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
0 0.0 46.3 137 10.5 4.4 608 13.0
2000 0.6 45.7 139 10.5 4.4 620 13.1
4000 1.3 45.0 141 10.5 4.4 628 13.2
6000 2.0 44.3 143 10.5 4.4 635 13.2
8000 2.9 43.4 145 10.5 4.4 645 13.3
10000 3.8 42.5 147 10.5 4.4 654 13.3
12000 5.0 41.3 150 10.5 4.4 666 13.4
14000 6.8 39.5
55% POWER Mixture = Best Economy
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
0 0.0 46.3 127 8.4 5.5 708 15.2
2000 0.6 45.7 130 8.4 5.5 726 15.5
4000 1.3 45.0 131 8.4 5.5 731 15.4
6000 2.0 44.3 134 8.4 5.5 745 15.6
8000 2.9 43.4 136 8.4 5.5 755 15.7
10000 3.8 42.5 139 8.4 5.4 768 15.9
12000 5.0 41.3 141 8.4 5.4 776 15.9
14000 6.8 39.5 144 8.4 5.4 785 16.0
Sheet 2 of 2
March 2010
Information Manual 5-31
Cirrus Design Section 5
SR20 Performance Data
Balked Landing Climb Gradient
• 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: Example:
• Power .............................. Full Throttle Outside Air Temp.......................20° C
• Mixture ................................. Full Rich Weight .................................. 2500 LB
• Flaps ................................ 100% (DN) Pressure Altitude .................. 2000 FT
• Airspeed............... Best Rate of Climb
Climb Airspeed .....................74 Knots
Rate of Climb....................679 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet per Nautical Mile
Temperature ~ °C
-20 0 20 40 ISA
2900
SL 75 779 699 626 558 644
2000 74 664 585 515 449 547
4000 73 548 475 408 346 451
6000 72 440 369 305 - 359
8000 71 335 268 206 - 271
10000 70 235 170 - - 186
2500
SL 75 987 894 807 728 829
2000 74 851 762 679 603 716
4000 73 721 635 557 484 608
6000 72 596 514 439 - 502
8000 71 477 398 327 - 401
10000 70 362 287 - - 305
Figure 5-18
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西锐20飞机信息手册CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA(45)
