Tecnam P2010 - Page 477

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV5 - 10
Section 5 – Performance-
TAKE-OFF PERFORMANCES
Ed. 1, Rev.0
Weight = 960 kg (2116 lb)
Flaps: T/O
Speed at Lift-Off = 60 KIAS
Speed Over 50ft Obstacle = 65 KIAS
Throttle and Propeller Lever: Full Forward
Runway: Paved
Corrections
Headwind: -10 m for each kn
Tailwind: +20 m for each kn
Grass Runway: +10% to Ground Roll
Runway slope: +10% to Ground Roll for each +1%
Pressure
Altitude
Distance [m]
(Distance [ft])
Temperature [°C]
ISA
[ft]
-25
0
25
50
S.L.
Ground Roll
149
(489)
187
(614)
231
(758)
281
(922)
213
(699)
At 50 ft AGL
272
(892)
340
(1115)
416
(1365)
501
(1644)
384
(1260)
1000
Ground Roll
162
(531)
204
(669)
252
(827)
306
(1004)
229
(751)
At 50 ft AGL
296
(971)
369
(1211)
452
(1483)
545
(1788)
411
(1348)
2000
Ground Roll
177
(581)
223
732)
275
(902)
334
(1096)
245
(804)
At 50 ft AGL
322
(1056)
402
(1319)
492
(1614)
593
(1946)
440
(1444)
3000
Ground Roll
194
(636)
244
(801)
301
(988)
365
(1198)
264
(866)
At 50 ft AGL
350
(1148)
438
(1437)
536
(1759)
645
(2116)
472
(1549)
4000
Ground Roll
212
(696)
266
(873)
329
(1079)
399
(1309)
283
(928)
At 50 ft AGL
382
(1253)
477
(1565)
584
(1916)
703
(2306)
506
(1660)
5000
Ground Roll
231
(758)
291
(955)
360
(1181)
436
(1430)
305
(1001)
At 50 ft AGL
416
(1365)
520
(1706)
636
(2087)
766
(2513)
542
(1778)
6000
Ground Roll
253
(830)
319
(1047)
393
(1289)
477
(1565)
328
(1076)
At 50 ft AGL
454
(1489)
567
(1860)
694
(2277)
836
(2743)
582
(1909)