Figure 35: Airplane Power Setting Table

Cruise power settings 65% Maximum continuous power (or full throttle 2,800 pounds) Press ALT. ISA −20 °C (−36 °F) IOAT °F Feet °C RPM IN HG PSI GPH KTS MPH 27 19 12 5 −2 −8 −15 −22 −29 SL 2,000 4,000 6,000 8,000 10,000 12,000 14,000 16,000 −3 −7 −11 −15 −19 −22 −26 −30 −34 2,450 2,450 2,450 2,450 2,450 2,450 2,450 2,450 2,450 20.7 20.4 20.1 19.8 19.5 19.2 18.8 17.4 16.1 6.6 6.6 6.6 6.6 6.6 6.6 6.4 5.8 5.3 11.5 11.5 11.5 11.5 11.5 11.5 11.5 10.5 9.7 147 149 152 155 157 160 162 159 156 169 171 175 178 181 184 186 183 180 Engine speed MAN. press Fuel flow per engine TAS Standard day (ISA) IOAT °F °C RPM IN HG PSI GPH KTS MPH 63 55 48 41 36 28 21 14 7 17 13 9 5 2 −2 −6 −10 −14 2,450 2,450 2,450 2,450 2,450 2,450 2,450 2,450 2,450 21.2 21.0 20.7 20.4 20.2 19.9 18.8 17.4 16.1 6.6 6.6 6.6 6.6 6.6 6.6 6.1 5.6 5.1 11.5 11.5 11.5 11.5 11.5 11.5 10.9 10.1 9.4 150 153 156 158 161 163 163 160 156 173 176 180 182 185 188 188 184 180 Engine speed MAN. press Fuel flow per engine TAS ISA +20 °C (+36 °F) IOAT °F °C RPM IN HG PSI GPH KTS MPH 99 91 84 79 72 64 57 50 43 37 33 29 26 22 18 14 10 6 2,450 2,450 2,450 2,450 2,450 2,450 2,450 2,450 2,450 21.8 21.5 21.3 21.0 20.8 20.3 18.8 17.4 16.1 6.6 6.6 6.6 6.6 6.6 6.5 5.9 5.4 4.9 11.5 11.5 11.5 11.5 11.5 11.4 10.6 9.8 9.1 153 156 159 161 164 166 163 160 155 176 180 183 185 189 191 188 184 178 Engine speed MAN. press Fuel flow per engine TAS Note: 1. Full throttle manifold pressure settings are approximate. 2. Shaded area represents operation with…