Balked Landing Climb Gradient - Cirrus DESIGN SR20 Information Manual

Cirrus Design
SR20

Balked Landing Climb Gradient

Conditions:
• Power .............................. Full Throttle
• Mixture ................................. Full Rich
• Flaps ................................ 100% (DN)
• Airspeed ............... Best Rate of Climb
• 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.
Weight Press
Alt
LB FT
SL
2000
4000
2900
6000
8000
10000
SL
2000
4000
2500
6000
8000
10000
P/N 13999-002 Info Manual
September 2011
• Note •
CLIMB GRADIENT ~ Feet per Nautical Mile
Climb
Speed
KIAS -20
75 779
74 664
73 548
72 440
71 335
70 235
75 987
74 851
73 721
72 596
71 477
70 362
Figure 5-18
Example:
Outside Air Temp .......................20° C
Weight .................................. 2500 LB
Pressure Altitude .................. 2000 FT
Climb Airspeed .....................74 Knots
Rate of Climb....................679 FT/NM
Temperature ~ °C
0 20
699 626
585 515
475 408
369 305
268 206
170 -
894 807
762 679
635 557
514 439
398 327
287 -
Section 5
Performance Data
40 ISA
558 644
449 547
346 451
- 359
- 271
- 186
728 829
603 716
484 608
- 502
- 401
- 305
5-31