Cirrus DESIGN SR20 User Manual

Cirrus Design Section 5
SR20 Performance Data
P/N 11934-004 5-17
Enroute Climb Gradient
• Note •
Climb Gradients shown are the gain in altitude for the horizontal distance
traversed expressed as Feet per Nautical Mile.
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 .......................................................................................................Full Rich
• Flaps .......................................................................................................... 0% (UP)
• 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 96 650 589 533 481
549
2000 96 560 502 448 398
474
4000 95 474 418 367 319
402
6000 94 392 338 289 244
332
8000 93 313 216 214 171
265
10000 92 237 188
200
12000 91 164 118
139
14000 90 95 51
80
2500
SL 93 846 777 712 652
728
2000 93 741 674 612 554
640
4000 92 640 576 516 461
555
6000 91 543 482 425
473
8000 91 451 392 337
395
10000 90 363 306
320
12000 89 279 224
248
14000 88 198 147
180
Original Issue

Cirrus DESIGN SR20 Specifications

General

Brand	Cirrus
Model	DESIGN SR20
Category	Aircrafts
Language	English