Tecnam P2010 2015 - Page 147

AFMS N"D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
~ TECNAM [?~@1)@
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Welmt = 9§Q ~ (2112 lbl
Corrections
Flaps:T/O
Headwind: -10 m for each kn
Speed at Llft.()ff = 60 KIAS Tailwind: +20 m for each kn
Speed Over 50ft Obstacle = 65 KIAS Grass Runway: + 10% to Ground Roll
Throttle and Propeller Lever: Full Forward
Runway slope: +10% to Ground Roll for each +1%
Runway: Paved
Pressure
Altitude
(ft]
S.L
1000
2000
3000
4000
5000
6000
Distance (m]
(Distance [ft])
Temperature ['C]
-25
0
25
Ground Roll
149
187 231
(489) (614)
(758)
At SO ft AGL
272
340 416
(892) (1115) (1365)
Ground Roll
162 204
252
(531)
(669)
(827)
At50ftAGL
296 369 452
(971) (1211) (1483)
Ground Roll
177 223 275
(581) 732)
(902)
At SO ft AGL
322 402
492
(1056) (1319)
(1614)
Ground Roll
194
244 301
(636) (801)
(988)
At SO ft AGL
350 438 536
(1148) (1437) (1759)
Ground Roll
212
266 329
(696) (873) (1079)
At SO ft AGL
382 477
584
(1253) (1565) (1916)
Ground Roll
231
291 360
(758) (955) (1181)
At SO ft AGL
416 520 636
(1365) (1706) {2087)
Ground Roll
253 319
393
(830) (1047) (1289)
At SO ft AGL
454 567 694
(1489)
{1860)
(2277)
Section 5 - Performance
TAKE-OFF PERFORMANCES
so
ISA
281 213
(922) (699)
501 384
(1644)
(1260)
306 229
(1004)
(751)
545 411
{1788) (1348)
334 245
(1096) (804)
593 440
(1946)
(1444)
365 264
(1198)
(866)
645 472
(2116) (1549)
399 283
(1309) (928)
703
506
(2306) (1660)
436 305
(1430) (1001)
766 542
(2513) (1778)
477 328
(1565) (1076)
836 582
(2743)
(1909)
Ed. 2. Rev.O