CEAPR DR400/120D User Manual

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 %
All manuals and user guides at all-guides.com

CEAPR DR400/120D Specifications

General

Brand	CEAPR
Model	DR400/120D
Category	Aircrafts
Language	English