CEAPR DR400/120D, Pilot Operating Handbook

Page: 88 / 104

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)