Adjusting Fuel Flow - Twin Cessna Flyer

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Pressure Altitude(Set Altimeter at29.92 in. Hg.)TABLE 10. ALTITUDE FUEL SCHEDULEIO-550-B ENGINEFULL OPEN THROTTLE, FULL RICH MIXTURE300 BHP @ 2700 RPMFuel Flow(lbs/hr)Fuel Flow(gals/hr)Metered FuelPressure PSIDSea LevelMin.146Max.156Min.24.9Max.26.6Min.17.2 18.31000 145.5 155.5 24.8 26.5 17.1 18.22,000 145 155 24.7 26.4 17.0 18.13000 144 154 24.5 26.3 16.9 17.94,000 142 152 24.2 25.9 16.5 17.55000 139 149 23.7 25.4 16.1 17.06,000 135.5 145.5 23.1 24.8 15.5 16.58,000 127 137 21.6 23.3 14.2 15.110,000 117 127 19.9 21.6 12.8 13.612,000 110 120 18.7 20.4 11.9 12.614,000 105 115 17.9 19.6 11.3 11.9Gasoline = 5.87 lbs per gallon @ 70° F.Max.160150Altitude Leaning ScheduleIO-550-BFull Rich, 2700 RPMPoint AAneroid adjusted out two turnsFuel Flow (pph)140130120Point A1101000 1 2 3 4 5 6 7 8 9 10 11 12 13 14Pressure Altitude (X 1000 ft)CHART 7ISSUED REVISED PAGE NO REVISIONMO DAY YEAR MO DAY YEARTM30 of 4003 24 97 02 25 2005 Teledyne Continental Motors, Inc. SID97-3A Te le d y n e Te c hn o lo g ie s C o m p a n yCP.O. Box 90 Mobile Alabama • 251-438-3411
Pressure Altitude(Set Altimeter at29.92 in. Hg.)TABLE 11. ALTITUDE FUEL SCHEDULEIO-550-C ENGINEFULL OPEN THROTTLE, FULL RICH MIXTURE300 BHP @ 2700 RPMFuel Flow(lbs/hr)Fuel Flow(gals/hr)Metered FuelPressure PSIDMin. Max. Min. Max. Min. Max.Sea Level 152 160 25.9 27.2 18.2 18.91000 151 159 25.7 27.1 18.0 18.72,000 148 156 25.2 26.6 17.5 18.23000 143 151 24.4 25.7 16.7 17.44,000 138 146 23.5 24.9 15.9 16.55000 134 142 22.8 24.2 15.3 15.96,000 130 138 22.1 23.5 14.7 15.38,000 123 131 21.0 22.3 13.6 14.110,000 118 126 20.1 21.5 12.9 13.412,000 113 121 19.3 20.6 12.3 12.714,000 108 116 18.4 19.8 11.7 12.1Gasoline = 5.87 lbs per gallon @ 70° F.170Altitude Leaning ScheduleIO-550-CFull Rich, 2700 RPM160Fuel Flow (pph)1501401301201101000 1 2 3 4 5 6 7 8 9 10 11 12 13 14Pressure Altitude (X 1000 ft)CHART 8ISSUED REVISED PAGE NO REVISIONMO DAY YEAR MO DAY YEARTM31 of 4003 24 97 02 25 2005 Teledyne Continental Motors, Inc. SID97-3A Te le d y n e Te c hn o lo g ie s C o m p a n yCP.O. Box 90 Mobile Alabama • 251-438-3411
Page 2 and 3: Any fuel system that cannot be adju
Page 4 and 5: torque, to the value specified, a p
Page 6 and 7: 17. If any of the recorded readings
Page 8 and 9: F. FLIGHT TEST:Naturally Aspirated
Page 10 and 11: TABLE 1Torque Specifications for Ho
Page 12 and 13: ENGINETABLE 3. Fuel System Adjustme
Page 20 and 21: CHART 1IO-240-B with Altitude Compe
Page 22 and 23: CHART 1AIO240B Equipped With Altitu
Page 24 and 25: Table 5Flight Test Verification, IO
Page 26 and 27: TABLE 6. ALTITUDE FUEL SCHEDULEIO-3
Page 28 and 29: TABLE 8. ALTITUDE FUEL SCHEDULEIO-3
Page 32 and 33: Pressure Altitude(Set Altimeter at2
Page 34 and 35: VAPORRETURNVAPORRETURNADJUSTABLEORI
Page 36 and 37: THROTTLELEVERINLET SCREENFUEL INLET
Page 38 and 39: 2FUELPRESSURE46810METERED FUELPRESS
Page 40 and 41: FUELINLETVAPORRETURNAMBIENTPRESSURE

Adjusting Fuel Flow - Twin Cessna Flyer

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