Tecnam P2010 2015 - 9. En-Route Rate of Climb

AFMS N"D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
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9. EN·ROUTE RATE OF CLIMB
To account for likely in serwce performance variations apply a
factored to rate ofc/1mb of0 .90
Throttle Lever: Fu ll Forward
Propeller: 2600 RPM
Flaps: UP
Pressure
Climb
Rate of Climb [ft/mini
Weight
[kg]
([lb])
1160
(2557)
1060
(2337)
960
(2116)
Altitude
Speed
Temperature ["C]
Vv
[ft] [KIAS] -25
0
25
S.L 82 11 31 9 44 77 6
2000
81
989
804 639
4000 80 84 6 665
503
6000
79
705
526 367
8000
78 563 388
232
10000
77 423 251 97
12000
76 282 11 3 -37
14000 76
142
- 23
- 171
S.L
82
12 84
1085 907
2000
81 1133 937 762
4000 80 98 2 789 61 8
6000
79 831
642
474
8000
78 6 82 4 96
330
10000 77
532
350
187
12000 76 383 204 45
14000
75 235 59
- 97
S.L.
81 14 65 1251 1060
2000
80
1302 1092
905
4000
79
114 0
934 749
6000
78
979 776
595
8000
77
818
619 441
10000
76 658 462 287
12000
75
498
306 134
14000
74 339 150 -18
Section 5 - Performance
EN·ROUTE RATE OF CLIMB
50
62 5
491
357
224
91
-41
-173
-305
747
605
463
322
181
40
-99
- 239
88 8
735
583
432
281
130
-20
-170
ISA
841
729
618
506
394
282
171
59
976
857
739
621
502
384
265
147
1134
1007
880
753
625
498
371
244
Ed. 2, Rev.0