DA 62 AFM
Performance
One Engine Inoperative Climb
Flaps: UP
Power: 95%
v
YSE
: 87 KIAS
Gear: retracted
W
/
[lb
e
]
ight [kg]
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
1
/
3
8
9
0
6
0
8
SL
425
415
410
400
390
380
350
300
393
2000
610
410
400
390
380
370
360
320
270
377
4000
1219
390
380
365
355
345
330
290
235
360
6000
1829
365
355
345
335
325
295
250
342
8000
2438
345
335
320
310
295
250
200
323
10000
3048
320
305
295
280
245
195
300
12000
3658
290
275
260
235
180
125
276
14000
4267
240
220
195
150
85
20
226
16000
4877
170
150
115
60
0
164
18000
5486
90
70
40
-20
-75
93
20000
6096
20
0
-40
-100
29
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 - 53
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 ...