DA 62 AFM
Performance
Take-Off Climb - Flaps T/O
Flaps: T/O
Power: 95%
v
Y
: 86 KIAS
Gear: retracted
Weight [kg]/
[lb]
Press.
Alt.
[ft]
Press.
Alt.
[m]
Rate of Climb - [ft/min]
Outside Air Temperature - [°C]
/[°F]
-20
-10
0
10
20
30
40
50
ISA
-4
14
32
50
68
86
104
122
2
/
4
1
6
0
3
0
0
SL
1130
1130
1120
1120
1110
1100
1050
940
1114
2000
610
1120
1110
1100
1090
1080
1080
1000
890
1092
4000
1219
1090
1080
1070
1060
1060
1030
940
830
1067
6000
1829
1060
1050
1050
1040
1030
970
880
1043
8000
2438
1040
1030
1020
1000
980
900
790
1017
10000
3048
1010
990
980
960
910
800
986
12000
3658
970
950
930
900
800
680
952
14000
4267
890
870
830
760
630
510
874
16000
4877
790
760
720
610
490
777
18000
5486
670
640
600
480
370
667
20000
6096
560
530
470
340
569
For the rate of climb in [m/s] divide by 196.8 or multiply by 0.00508.
Doc. No. 11.01.05-E
Rev. 0
11-Jan-2019
Page 5 - 37
Summary of Contents for DA 62
Page 2: ...DA 62 AFM Introduction Intentionally left blank Page 0 0a Rev 0 11 Jan 2019 Doc 11 01 05 E ...
Page 36: ...DA 62 AFM General 1 7 THREE VIEW DRAWING Doc No 11 01 05 E Rev 0 11 Jan 2019 Page 1 19 ...
Page 363: ...Performance DA 62 AFM Intentionally left blank Page 5 92 Rev 0 11 Jan 2019 Doc No 11 01 05 E ...
Page 438: ...Airplane Description DA 62 AFM Page 7 46 Rev 0 11 Jan 2019 Doc No 11 01 05 E ...
Page 496: ...Handling Care Maintenance DA 62 AFM Page 8 10 Rev 0 11 Jan 2019 Doc No 11 01 05 E 1 4 5 2 3 ...