Tecnam P2010 - Page 301

AFMS N°D02 FOR VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page V5-12
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
Section 5 - Performances
EN-ROUTE RATE OF CLIMB
2
nd
Edition, Rev. 0