CEAPR DR400/120D, Руководство по эксплуатации для пилотов

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Supplement POH DR400/120D, DR400/140B,
DR400/180R, DR400/200R, DR400/RP
Page 5 - 12 Issue 3
– July 2014
LANDING PERFORMANCE
At max. takeoff weight 980 kg (2161 lb)
Without wind, flaps in landing position, engine at idle.
Concrete, flat and dry runway
Altitude Temperature Weight 980 kg (2161 lb)
Ft (m) °C °F
Landing Distance
(ground touch)
Landing Distance
from 15 m (50 ft)
(m) (ft) (m) (ft)
0
-5 23 266 873 479 1570
Std=15 59 282 925 507 1663
35 95 298 976 535 1755
2 000
(610)
-9 16 277 909 498 1635
11 52 294 964 528 1733
31 88 310 1018 558 1830
3 000
(914)
-11 12 284 931 510 1674
9 48 301 987 541 1775
29 84 318 1043 572 1875
4 000
(1219)
-13 9 291 953 527 1728
7 45 308 1011 559 1833
27 81 326 1069 591 1937
Table 5-13 Landing performance
Headwind influence:
 For 10 kt, multiply by 0.85
 For 20 kt, multiply by 0.65
 For 30 kt, multiply by 0.55
Tailwind influence:

Add 10 % to distance for each additional 2 kt
Dry grass runway:
 Add 15 %