Tecnam P2010 2015 - 11. Landing Performances

AFMS N"D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
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11. LANDING PERFORMANCES
To account for likely in service performance variations apply a
factored to distances of 1.67
Weight= 1160 kg (2557 lb)
Corrections
Flaps: LAND
Headwind: -4 m for each kn
Short Final Approach Speed = 66 KIAS
Tailwind: +13 m for each kn
Throttle Lever: Idle
Grass Runway: +10% to Ground Roll
Runway: Paved
Runway slope: -3% to Ground Roll fur each + 1%
Pressure
Altitude
[ft]
S.L
1000
2000
3000
4000
5000
6000
Distance [m]
(Distance [ft])
Temperature ('C)
-25
0 25
Ground Roll
204 225 245
(669) (738) (804)
At SO ft AGL
488 509
529
(1601) (1670)
(1736)
Ground Roll
212 233 254
(696) (764) (833)
At SO ft AGL
496 517
538
(1627) (1696) (1765)
Ground Roll
220 242
264
(722)
(794) (866)
At SO ft AGL
504 526
548
(1654)
(1726) (1798)
Ground Roll
228 251 274
(748}
(823) (899)
At SO ft AGL
512 535 558
(1680) (1755) (1831)
Ground Roll
236 260 284
(774)
(853)
(932)
At SO ft AGL
520 544 568
(1706) (1785) (1864)
Ground Roll
245 270
295
(804) (886) (968)
579
At SO ft AGL
529 554
(1736) (1818)
(1900)
Ground Roll
255 280 306
(837)
(919)
(1004)
590
At SO ft AGL
539
564
(1768) (1850) (1936)
Section 5 - Performance
LANDING PERFORMANCES
so
ISA
266 237
(873) (778)
550
521
(1804) (17091
276 244
(906) (801)
560 528
(1837) (17321
286 251
(938) (823)
570 535
(1870) (1755)
297 259
(974) (850)
581 543
(1906) (1781)
308
267
(1010) (876]
592
551
(1942) (1808)
320 275
(1050} (902)
604
559
(1982) (18341
332 284
(1089) (932)
616 568
(2021) (1864)
Ed. 2, Rev.O