Airplane Description
DA 62 AFM
Auxiliary Tank (if installed) Configuration
Fuel Quantity Indicator II: Pitch Angle Reading
Usable Fuel Quantity
2°
3°
4°
5°
5°
US gal
Liter
87
92/85
92/86
92/86
92/85
1
3.8
110
110
112/105
110/100
110/100
2
7.6
120
123
125
127
130
3
11.4
135
135
140
142
145
4
15.1
150
150
155
158
163
5
18.9
160
167
170
175
185
6
22.7
170
175
180
185
190
7
26.5
185
190
195
205
210
8
30.3
200
210
215
220
230
9
34.1
217
220
225
235
245
10
37.9
230
235
245
250
260
11
41.6
235
245
255
265
275
12
45.4
250
260
270
280
290
13
49.2
260
270
285
300
310
14
53.0
270
285
300
315
325
15
56.8
Page 7 - 56
Rev. 0
11-Jan-2019
Doc. No. 11.01.05-E
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 ...