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
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