Tecnam P2010 - Page 300

AFMS N°D02 FOR VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page V5-11
8. TAKE-OFF RATE OF CLIMB
To account for likely in service performance variations apply a
factored to rate of climb of 0.90
Throttle Lever: Full Forward
Propeller: 2600 RPM
Flaps: Take-Off
Weight
Pressure
Altitude
Climb
Speed
V
y
Rate of Climb [ft/min]
Temperature [°C]
ISA
[kg]
([lb])
[ft] [KIAS] -25 0 25 50
1160
(2557)
S.L.
72 974 808 659 525 717
2000
71 848 684 538 406 617
4000
70 721 560 417 287 518
6000
69 596 437 296 169 419
8000
68 470 315 176 51 320
10000
67 345 193 56 -67 221
12000
67 221 71 -63 -184 122
14000
66 96 -51 -182 -300 23
1060
(2337)
S.L.
70 1118 943 787 647 848
2000
69 985 813 660 522 744
4000
69 853 684 533 397 640
6000
68 721 555 406 273 536
8000
68 589 426 280 149 431
10000
67 458 298 155 26 327
12000
66 327 170 29 -97 223
14000
66 197 43 -95 -220 119
960
(2116)
S.L.
69
1288
1103
937
787
1001
2000
69
1147
964
801
654
890
4000
68
1006
827
666
522
780
6000
68
866
689
532
390
669
8000
67
726
553
398
258
558
10000
66
586
416
264
127
448
12000
66
447
280
131
-3
337
14000
65
309
145
-2
-134
226
NOTE
Section 5 - Performances
TAKE-OFF RATE OF CLIMB
2
nd
Edition, Rev. 0