Robin DR400/140B - Glide Performance

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.