Tecnam P2010 - Take -Off Performances

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV5 - 8
Section 5 – Performance-
TAKE-OFF PERFORMANCES
Ed. 1, Rev.0
7. TAKE-OFF PERFORMANCES
To account for likely in service performance variations apply a factored to distances of 1.10
Weight = 1160 kg (2557 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
234
(768)
295
(968)
364
(1194)
442
(1450)
336
(1102)
At 50 ft AGL
421
(1381)
526
(1726)
644
(2113)
776
(2546)
595
(1952)
1000
Ground Roll
256
(840)
322
(1056)
397
(1302)
482
(1581)
360
(1181)
At 50 ft AGL
458
(1503)
572
(1877)
701
(2300)
844
(2769)
637
(2090)
2000
Ground Roll
279
(915)
352
(1155)
434
(1424)
526
(1726)
387
(1270)
At 50 ft AGL
499
(1637)
622
(2041)
762
(2500)
918
(3012)
682
(2238)
3000
Ground Roll
305
(1001)
384
(1260)
474
(1555)
575
(1886)
415
(1362)
At 50 ft AGL
543
(1781)
678
(2224)
830
(2723)
1000
(3281)
731
(2398)
4000
Ground Roll
333
(1093)
420
(1378)
518
(1699)
628
(2060)
446
(1463)
At 50 ft AGL
591
(1939)
738
(2421)
904
(2966)
1089
(3573)
783
(2569)
5000
Ground Roll
364
(1194)
459
(1506)
566
(1857)
687
(2254)
480
(1575)
At 50 ft AGL
645
(2116)
805
(2641)
986
(3235)
1188
(3898)
840
(2756)
6000
Ground Roll
399
(1309)
502
(1647)
620
(2034)
752
(2467)
516
(1693)
At 50 ft AGL
703
(2306)
878
(2881)
1075
(3527)
1296
(4252)
901
(2956)
NOTE