Tecnam P2010 - En-Route Rate of Climb

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV5 - 12
Section 5 – Performance-
EN-ROUTE RATE OF CLIMB
Ed. 1, Rev.0
9. EN-ROUTE 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: UP
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.
82
1131
944
776
625
841
2000
81
989
804
639
491
729
4000
80
846
665
503
357
618
6000
79
705
526
367
224
506
8000
78
563
388
232
91
394
10000
77
423
251
97
-41
282
12000
76
282
113
-37
-173
171
14000
76
142
-23
-171
-305
59
1060
(2337)
S.L.
82
1284
1085
907
747
976
2000
81
1133
937
762
605
857
4000
80
982
789
618
463
739
6000
79
831
642
474
322
621
8000
78
682
496
330
181
502
10000
77
532
350
187
40
384
12000
76
383
204
45
-99
265
14000
75
235
59
-97
-239
147
960
(2116)
S.L.
81
1465
1251
1060
888
1134
2000
80
1302
1092
905
735
1007
4000
79
1140
934
749
583
880
6000
78
979
776
595
432
753
8000
77
818
619
441
281
625
10000
76
658
462
287
130
498
12000
75
498
306
134
-20
371
14000
74
339
150
-18
-170
244
NOTE