Cirrus DESIGN SR20 User Manual

Cirrus Design Section 5
SR20 Performance Data
P/N 11934-004 5-25
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:
• 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/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
Original Issue

Cirrus DESIGN SR20 Specifications

General

Brand	Cirrus
Model	DESIGN SR20
Category	Aircrafts
Language	English