Tecnam P2010 - Take-Off Rate of Climb

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV5 - 11
Section 5 – Performance-
TAKE-OFF RATE OF CLIMB
Ed. 1, Rev.0
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