IV FUEL(2) RANGE IN AIR MILES U.S. IMP STATUTE NAUTICAL GALS AT S.L. AT 1200 AT S.L. AT 1200 233 194 ______ 960 ______ 835 200 167 910 790 190 158 865 750 180 150 815 710 170 142 770 665 160 133 720 625 150 125 670 585 140 117 625 540 130 108 575 500 120 100 530 460 110 92 480 415 100 83 430 375 90 75 385 335 80 67 335 290 70 58 290 250 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 20000 2250 181 157 F.T 55 46 15000 2000 189 164 F.T 52 43 12000 1900 189 164 29 50 42 9000 1850 189 164 29 47 39 6000 1850 189 164 29 45 37 3000 1850 187 162 29 43 36 S.L. 1800 185 161 29 41 34 (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_ * 33 GAL. FOR WARM-UP, TAKE-OFF AND CLIMB, NOT AVAILABLE IN FLIGHT