Pilot Operating Handbook - Ecoflight.ch

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Rev. 02 – July 16 th , 2009 5 Performance 5.3 Cruise Speed, RPM, Fuel Consumption, Range Rotax 912 UL, 80 hp engine, Tonini Fixed Pitch Prop Engine Speed Fuel Consumption True Airspeed Maximum Endurance Maximum Range rpm gph 3.000 ft, mph / kts hr NM 5.400 4,7 107 / 93 4,4 412 5.200 4,3 103 / 90 4,9 441 5.000 3,9 100 / 87 5,5 473 4.800 3,5 95 / 83 6,1 505 4.600 3,1 91 / 79 6,8 537 4.400 2,8 86 / 75 7,6 569 4.200 2,5 81 / 71 8,4 602 Rotax 912 UL-S, 100 hp engine, Tonini Fixed Pitch Prop Engine Speed Fuel Consumption True Airspeed Maximum Endurance Maximum Range rpm gph 3.000 ft, mph / kts hr NM 5.400 6,7 113 / 98 3,2 311 5.200 6,0 109 / 95 3,5 332 5.000 5,4 104 / 91 3,9 353 4.800 4,9 100 / 87 4,3 375 4.600 4,4 95 / 83 4,8 401 4.400 3,9 91 / 79 5,4 425 4.200 3,5 86 / 75 6,0 446 Rotax 912 UL-S, 100 hp engine, Sensenich Ground Adjustable Prop Engine Speed Fuel Consumption True Airspeed Maximum Endurance Maximum Range rpm gph 3.000 ft, mph / kts hr NM 5.400 6,7 130 / 113 3,2 362 5.200 6,0 123 / 107 3,5 375 5.000 5,4 117 / 102 3,9 398 4.800 4,9 111 / 97 4,3 417 4.600 4,4 105 / 91 4,8 437 4.400 3,9 98 / 85 5,4 459 4.200 3,5 92 / 80 6,0 480 All values related to the 22 gallon fuel tank system (21 gallons usable), within the ICAO standard atmosphere. Performance 5 - 5
Rev. 02 – July 16 th , 2009 5 Performance Rotax 912 UL-S, 100 hp engine, Neuform Ground Adjustable Prop Engine Speed Fuel Consumption True Airspeed Maximum Endurance Maximum Range rpm gph 3.000 ft, mph / kts hr NM 5.400 6,7 130 / 113 3,2 362 5.200 6,0 123 / 107 3,5 375 5.000 5,4 117 / 102 3,9 398 4.800 4,9 111 / 97 4,3 417 4.600 4,4 105 / 91 4,8 437 4.400 3,9 98 / 85 5,4 459 4.200 3,5 92 / 80 6,0 480 The following table contains technical data about fuel consumption and maximum range for the constant speed propeller. Manifold pressure shall serve as advice only. It is acceptable to choose the power setting “Full Throttle” over the total engine speed range (see also Rotax-Manual). However for economic reasons is advised to adhere to the following table. Rotax 912 UL-S, 100 hp engine, Rospeller (*) – Constant Speed Prop Engine Speed Man. Press. Fuel Consumption True Airspeed Maximum Endurance Maximum Range rpm in Hg gph 3.000 ft, mph / kts hr NM 5.500 27 6,3 125 / 109 3,3 363 5.200 27 5,9 122 / 106 3,6 379 5.000 26 5,5 117 / 102 3,8 387 4.800 26 4,6 111 / 97 4,6 442 4.300 24 3,6 102 / 89 5,9 528 4.100 24 2,9 91 / 79 7,3 576 3.800 23 2,4 86 / 75 8,9 660 All values related to the 22 gallon fuel tank system (21 gallons usable), within the ICAO standard atmosphere. (*) Not for ASTM aircrafts certified in USA Comment: Flight performances can vary significantly due to tolerances of propeller and engine, flights without doors, deviations from temperature and air density from standard ISA conditions, etc. Performance 5 - 6
Page 1 and 2: Pilot Operating Handbook including
Page 3 and 4: Rev. 02 - July 16 th , 2009 Introdu
Page 9 and 10: Rev. 02 - July 16 th , 2009 1 Gener
Page 11 and 12: Rev. 02 - July 16 th , 2009 2 Airpl
Page 27 and 28: Rev. 02 - July 16 th , 2009 3 Opera
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Page 31 and 32: Rev. 02 - July 16 th , 2009 4 Weigh
Page 37 and 38: Rev. 02 - July 16 th , 2009 5 Perfo
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Page 43 and 44: Rev. 02 - July 16 th , 2009 6 Emerg
Page 49 and 50: Rev. 02 - July 16 th , 2009 7 Norma
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