sonaca aircraft S201 - Page 155

S201 AFM
5 - PERFORMANCE
5.3 - PERFORMANCE TABLES
AND DIAGRAMS
27/06/2019
SONAIR-S2-D-MAN-006
Page : 5-13
Rev. : A
5.3.8 CLIMB PERFORMANCE – CRUISE CLIMB
Conditions: Full Power - MAP = 39
Weight - 750 kg
Flaps - UP setting
V
x, 0°
- 65 KIAS for best climb angle of 11%
V
Y, 0°
- 68 KIAS for best climb rate of 760 ft/min
Climb rate at
V
Y, 0
[ft/min]
Delta with ISA [°C]
AP [ft]
-30
-20
-10
0
10
20
30
0
915
865
810
760
710
655
620
2000
875
825
770
720
670
620
585
4000
830
780
730
680
635
585
550
6000
785
735
690
625
595
550
515
8000
735
690
630
585
555
510
480
Climb Angle
at V
x, 0°
[%]
Delta with ISA [°C]
AP [ft]
-30
-20
-10
0
10
20
30
0
13
12
11
11
10
9
9
2000
12
12
11
10
9
9
8
4000
12
11
10
9
9
8
8
6000
11
10
10
9
8
8
7
8000
10
10
9
8
8
7
7
CAUTION
Maximum take-off power should only be maintained for a maximum of 5
minutes, after which the throttle setting should be set back to maximum
continuous power.