|  |  | 
						
							| I (MAX. CONT. POWER) | FUEL(2) |  
							| RANGE IN AIR MILES | U.S. | IMP |  
							| STATUTE | NAUTICAL | GALS |  
							| AT S.L. | AT 1200 | AT S.L. | AT 1200 | 233 | 194 |  
							| ______ | 490 | ______ | 425 | 200 | 167 |  
							|  | 465 |  | 405 | 190 | 158 |  
							|  | 440 |  | 385 | 180 | 150 |  
							|  | 415 |  | 360 | 170 | 142 |  
							|  | 390 |  | 340 | 160 | 133 |  
							|  | 370 |  | 320 | 150 | 125 |  
							|  | 345 |  | 300 | 140 | 117 |  
							|  | 320 |  | 275 | 130 | 108 |  
							|  | 295 |  | 255 | 120 | 100 |  
							|  | 270 |  | 235 | 110 | 92 |  
							|  | 245 |  | 210 | 100 | 83 |  
							|  | 220 |  | 190 | 90 | 75 |  
							|  | 195 |  | 170 | 80 | 67 |  
							|  | 170 |  | 150 | 70 | 58 |  
							|  | 145 |  | 130 | 60 | 50 |  | 
						
							| DENSITY ALT. | R.P.M. | I.A.S | T.A.S | M.P. | U.S | IMP. |  
							| IN FEET (1) | MP.H. | MP.H. | IN. Hg | G.P.H. | G.P.H. |  
							| 25000 | 2600 | 175 | 152 | F.T. | 69 | 57 |  
							| 20000 | 2600 | 204 | 177 | F.T. | 91 | 76 |  
							| 15000 | 2600 | 230 | 200 | F.T. | 115 | 96 |  
							| 12000 | 2600 | 236 | 205 | 38.3 | 119 | 99 |  
							| 9000 | 2600 | 239 | 208 | 38.3 | 116 | 97 |  
							| 6000 | 2600 | 241 | 209 | 38.3 | 113 | 94 |  
							| 3000 | 2600 | 243 | 211 | 38.3 | 109 | 91 |  
							| S.L. | 2600 | 245 | 213 | 38.3 | 106 | 88 |  
							| (1) INDICATED ALTITUDE CORRECTED FOR FREE AIR TEMPERATURE |  
							| (2) ALLOW___33___U.S. GALS.,___27__IMP. GALS. FOR WARM UP, TAKE-OOF AND CLIMB TO ___9000___FEET ALTITUTUDE. RETURN FUEL FLOWS TO TANKK ___FUSELAGE__ USE FUEL FROM TANKS IN THE FOLLOWING ORDER: _FUS.__FOR 15 MIN., BELLY, FUS. TO 35 GAL., REAR WING, FRONT WING, 35
							GAL. FUS RESERVE_ |  |