Robin DR400 Series Pilot Operating Handbook page 92

Rate of climb, Flaps retracted, 880 kg
Pressure
Altitude
[ft]
conditions
0
500
1000
1500
2000
2500
3000
3500
4000
4500
5000
5500
6000
6500
7000
7500
8000
8500
9000
9500
10 000
10 500
11 000
11 500
12 000
12 500
13 000
13 500
14 000
14 500
15 000
15 500
16 000
16 500
Page 5 - 6
Supplement
DR400/180R, DR400/200R, DR400/RP
Rate of climb [ft/min] at 880 kg (1940 lb)
ISA
ISA+10°C
910
910
910
910
910
910
910
900
890
870
860
840
820
810
790
780
760
730
720
720
600
580
570
550
540
520
500
460
450
420
400
380
350
310
Table 5-6 Rate of climb at 880 kg
POH DR400/120D,
900
900
900
900
900
900
900
890
880
860
850
830
810
800
780
770
750
720
720
720
600
580
570
550
540
520
500
460
450
420
400
380
350
310
DR400/140B,
ISA+20°C
860
860
860
860
860
860
860
850
840
820
820
800
780
770
750
740
720
690
690
690
580
570
570
550
540
520
500
460
450
420
400
380
350
310
Issue 3 – July 2014