Tecnam P2010 - Landing Performances

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV5 - 17
Section 5 – Performance-
LANDING PERFORMANCES
Ed. 1, Rev.0
11. LANDING PERFORMANCES
To account for likely in service performance variations apply a
factored to distances of 1.67
Weight = 1160 kg (2557 lb)
Flaps: LAND
Short Final Approach Speed = 66 KIAS
Throttle Lever: Idle
Runway: Paved
Corrections
Headwind: -4 m for each kn
Tailwind: +13 m for each kn
Grass Runway: +10% to Ground Roll
Runway slope: -3% to Ground Roll for each +1%
Pressure
Altitude
Distance [m]
(Distance [ft])
Temperature [°C]
ISA
[ft]
-25
0
25
50
S.L.
Ground Roll
204
(669)
225
(738)
245
(804)
266
(873)
237
(778)
At 50 ft AGL
488
(1601)
509
(1670)
529
(1736)
550
(1804)
521
(1709)
1000
Ground Roll
212
(696)
233
(764)
254
(833)
276
(906)
244
(801)
At 50 ft AGL
496
(1627)
517
(1696)
538
(1765)
560
(1837)
528
(1732)
2000
Ground Roll
220
(722)
242
(794)
264
(866)
286
(938)
251
(823)
At 50 ft AGL
504
(1654)
526
(1726)
548
(1798)
570
(1870)
535
(1755)
3000
Ground Roll
228
(748)
251
(823)
274
(899)
297
(974)
259
(850)
At 50 ft AGL
512
(1680)
535
(1755)
558
(1831)
581
(1906)
543
(1781)
4000
Ground Roll
236
(774)
260
(853)
284
(932)
308
(1010)
267
(876)
At 50 ft AGL
520
(1706)
544
(1785)
568
(1864)
592
(1942)
551
(1808)
5000
Ground Roll
245
(804)
270
(886)
295
(968)
320
(1050)
275
(902)
At 50 ft AGL
529
(1736)
554
(1818)
579
(1900)
604
(1982)
559
(1834)
6000
Ground Roll
255
(837)
280
(919)
306
(1004)
332
(1089)
284
(932)
At 50 ft AGL
539
(1768)
564
(1850)
590
(1936)
616
(2021)
568
(1864)
NOTE