CEAPR DR400/120D User Manual

Supplement POH DR400/120D, DR400/140B,
DR400/180R, DR400/200R, DR400/RP
Page 5 - 2 Issue 3 – July 2014
TAKEOFF PERFORMANCE
At max. take-off weight 980 kg (2161 lb), without wind, flaps in takeoff
position, engine full power
Conditions
 No wind, flaps in takeoff position (1
st
notch), engine full power on
brakes before release
 Level, dry, asphalt runway
 Rotation speed v
r
......................................................... 96 km/h (52 kt)
 Lift off speed Vlof ...................................................... 105 km/h (57 kt)
 Speed at 15 m (50 ft) height obstacle clearance ...... 113 km/h (61 kt)
Pressure
Altitude
[ft]
Take off distance [m] at 980 kg (2161 lb)
ISA conditions
ISA + 10°C
ISA + 20°C
To lift-off
to 50 ft
height
To lift-off
to 50 ft
height
To lift-off
to 50 ft
height
0
240
440
260
480
280
520
1000
260
470
270
500
290
540
2000
270
490
290
530
310
570
3000
280
510
300
550
320
590
4000
300
540
320
580
340
630
5000
310
580
330
620
360
670
6000
330
620
350
660
380
720
7000
360
690
380
730
400
790
8000
390
760
410
810
430
880
9000
410
810
430
850
450
930
Table 5-2 Takeoff distance (m) at 980 kg (MTOW)
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CEAPR DR400/120D Specifications

General

Brand	CEAPR
Model	DR400/120D
Category	Aircrafts
Language	English