Tecnam P2010 2015 - 8. Take-off Rate of Climb

AFMS N" D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
~TECNAM ~®'ll® c ~IJ'@ucrum IFO~@OU~ INJ&iOU(!!)&l0 Pag e APvs- 11
8. T AKE-OFF RATE OF CLIMB
To account for likely in service pelformance variations apply a
factored to rate of climb of0 .90
Throttle Lever: Fu ll Forward
Propeller: 2600 RPM
Flaps: Take-Off
Pressure
Olmb
Rate of Olmb [ft/mln]
Weight
(kg)
([lb])
1160
(2557)
1060
(2337)
960
(2116)
Altitude
Speed
Vy
Temperature ("C]
[ft] [KIAS] -25 0 25
S.L
72 974
808 659
2000
71
848
684
538
4000
70 721
560 41 7
6000
69 596 437 296
8000
68
47 0
315 176
10000
67 345 193
56
12000
67 221 71 - 63
14000
66 96
-51 - 182
S.L
70 1 11 8 943 787
2000
69 985 813 660
4000
69 8 53 684 533
6000
68
721
555 406
8000
68 589 4 26 280
10000
67 458 298 155
12000
66 327 170 29
14000
66 197 43
- 95
S.L
69 1288 1103 937
2000
69
1147 964
801
4000
68 1 006
827
666
6000
68 866 689
532
8000
67 726 553 398
10000
66 586 416 264
12000
66 44 7 280 1 31
14000
65 309 145 -2
Section 5 - Performance
TAKE-OFF RATE OF CLIMB
50
5 25
406
287
169
51
·67
- 184
-300
64 7
522
397
273
14 9
26
- 97
-220
787
654
522
390
258
127
-3
-134
ISA
717
617
518
419
320
221
122
23
848
744
640
536
431
327
223
119
1001
890
780
669
558
448
337
226
Ed . 2. Rev.a