Tecnam P2010 - Page 476

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV5 - 9
Section 5 – Performance-
TAKE-OFF PERFORMANCES
Ed. 1, Rev.0
Weight = 1060 kg (2337 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
189
(620)
238
(781)
293
(961)
356
(1168)
270
(886)
At 50 ft AGL
342
(1122)
427
(1401)
523
(1716)
630
(2067)
483
(1585)
1000
Ground Roll
206
(676)
259
(850)
320
(1050)
388
(1273)
290
(951)
At 50 ft AGL
372
(1220)
464
(1522)
569
(1867)
685
(2247)
517
(1696)
2000
Ground Roll
225
(738)
283
(928)
349
(1145)
424
(1391)
311
(1020)
At 50 ft AGL
405
(1329)
505
(1657)
619
(2031)
745
(2444)
554
(1818)
3000
Ground Roll
246
(807)
309
(1014)
382
(1253)
463
(1519)
334
(1096)
At 50 ft AGL
441
(1447)
550
(1804)
674
(2211)
812
(2664)
593
(1946)
4000
Ground Roll
268
(879)
338
(1109)
417
(1368)
506
(1660)
359
(1178)
At 50 ft AGL
480
(1575)
599
(1965)
734
(2408)
884
(2900)
636
(2087)
5000
Ground Roll
294
(965)
370
(1214)
456
(1496)
553
(1814)
386
(1266)
At 50 ft AGL
523
(1716)
653
(2142)
800
(2625)
964
(3163)
682
(2238)
6000
Ground Roll
321
(1053)
404
(1325)
499
(1637)
605
(1985)
416
(1365)
At 50 ft AGL
571
(1873)
713
(2339)
873
(2864)
1052
(3451)
732
(2402)