DA 62 AFM
Performance
One Engine Inoperative Climb
Flaps: UP
Power: 95%
v
YSE
: 89 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
280
275
260
250
245
235
210
170
247
2000
610
265
250
240
230
220
210
185
145
231
4000
1219
245
230
220
210
200
185
155
110
213
6000
1829
220
210
200
185
175
150
120
196
8000
2438
200
185
175
160
145
115
75
174
10000
3048
175
160
145
130
105
60
151
12000
3658
145
130
115
90
45
-5
128
14000
4267
95
75
50
10
-45
-95
81
16000
4877
30
5
-20
-70
-120
22
18000
5486
-45
-65
-95
-140
-185
-44
20000
6096
-115
-130
-165
-220
-103
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 - 51
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 ...