Tecnam P2010 2015 - 7. Take-Off Performances

AFMS N"D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
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7. TAKE•OFF PERFORMANCES
To account for likely in service peiformance varialions apply a faclored to dislances of I. JO
Weight= 1160 !$g (2557 lb}
Flaps: T/O
Corrections
Speed at Uft..()ff = 60 KIAS
Headwind: -10 m for each kn
Speed Over SOft Obstacle = 65 KIAS
Tailwind: +20 m for each kn
Throttle and Propeller Lever: Full Forward
Grass Runway: + 10% to Ground Roll
Runway: Paved
Runway slope: +10% to Ground Roll for each +1%
Pressure
Altitude
[ft)
S.L
1000
2000
3000
4000
5000
6000
Distance [m]
(Distance [ft])
Temperature ("CJ
-25
0 25
Ground Roll
234 295 364
(768) (968) (1194)
At SO ft AGL
421 526 644
(1381) (1726) (2113)
Ground Roll
256 322 397
(840) (1056) (1302)
At50ftAGL
458
572 701
(1503) {1877)
(2300)
Ground Roll
279 352 434
(915) (1155) (1424)
At50ftAGL
499 622
762
(1637)
(2041)
(2500)
Ground Roll
305 384 474
(1001) (1260) (1555)
At50ftAGL
543
678 830
(1781) (2224) (2723)
Ground Roll
333 420 518
(1093) (1378) (1699)
At SO ft AGL
591 738 904
(1939) (2421) (2966)
Ground Roll
364 459 566
(1194) (1506) (1857)
At SO ft AGL
645 805 986
(2116) (2641)
(3235)
Ground Roll
399 502 620
(1309) (1647) (2034)
At SO ft AGL
703 878 1075
(2306) (2881) (3527)
Section 5 - Performance
TAKE-OFF PERFORMANCES
so ISA
442 336
(1450) (1102)
776 595
(2546) (1952)
482 360
(1581)
(1181)
844
637
(2769) (2090)
526 387
(1726) (1270)
918
682
(3012)
12238)
575 415
(1886) (1362)
1000 731
(3281) (2398)
628
446
(2060)
(1463)
1089
783
(3573) (2569)
687 480
(2254) (1575)
1188 840
(3898) (2756)
752 516
(2467)
(1693)
1296 901
(4252) (2956)
Ed. 2, Rev.O