Supplement
POH
DR400/120D,
DR400/140B,
DR400/180R, DR400/200R, DR400/RP
Issue 3
– July 2014
Page 5 - 9
Pressure
Altitude
[ft]
Time to climb [min] at 880 kg (1940 lb) (MTOW)
ISA conditions
ISA+10°C
ISA+20°C
9500
11.3
11.4
11.9
10 000
11.9
12.1
12.6
10 500
12.8
12.9
13.5
11 000
13.6
13.8
14.3
11 500
14.5
14.6
15.2
12 000
15.4
15.6
16.1
12 500
16.4
16.5
17.1
13 000
17.3
17.4
18.0
13 500
18.3
18.4
19.0
14 000
19.4
19.5
20.1
14 500
20.5
20.6
21.2
15 000
21.7
21.8
22.4
15 500
23.0
23.1
23.7
16 000
24.3
24.4
25.0
16 500
25.7
25.8
26.4
Table 5-10 Time to climb (mn) at 880 kg (MTOW), 9500
– 16500 ft
Rate of climb, flaps in takeoff position
Best rate of climb:
Subtract 10% from the flaps retracted rates of climb in the above tables.
Maximum angle of climb:
8.3% at sea level, standard atmosphere, MTOW, and 120 km/h (65 kt).
Glide performance
Engine off, the aircraft glides8 times its altitude above ground (without
wind) at 145 km/h (78 kt).
Altitude and temperature do not have perceptible influence.
Summary of Contents for DR400/120D
Page 1: ...PILOT S OPERATING HANDBOOK SUPPLEMENT DR400 135CDI Document n 1001639GB ...
Page 2: ......
Page 4: ...Supplement POH DR400 120D DR400 140B DR400 180R DR400 200R DR400 RP Page ii Issue 3 July 2014 ...
Page 12: ...Supplement POH DR400 120D DR400 140B DR400 180R DR400 200R DR400 RP Page x Issue 3 July 2014 ...
Page 50: ......
