FUEL PRESSURE Boost pump pressure limits to injector inlet: Zero Fuel Flow 45 psi maximum Maximum fuel flow 14 psi minimum CYLINDER HEAD TEMPERATURE Maximum (red line) F. C.) 500’ (260’ Normal Operating (green arc) F. to F. 180’ 435’ High Performance Cruise F. below 435’ Economy Cruise below F. 400’ TACHOMETER Maximum RPM (red line) 2700 RPM Normal Operating (green arc) 600 to 2700 RPM EXHAUST GAS TEMPERATURE (EGT) Do not exceed F. 1650’ VACUUM PRESSURE Operating Range 4.3 to 5.9 ins Hg. CENTRE OF GRAVITY LIMTS WARNING These figures are dependent on the airplane being within safe Centre of Gravity limits. Do not fly the airplane if its computed flight CG falls outside of the published limits. Due to variables such as fuel, passenger and baggage weight, these figures may be reduced somewhat. Before each flight, the CG should be computed to determine whether the aircraft is within safe limits. Forward Limit Station 82. 21
FUEL PRESSURE Boost pump pressure limits to injector inlet: Zero Fuel Flow 45 psi maximum Maximum fuel flow 14 psi minimum CYLINDER HEAD TEMPERATURE Maximum (red line) 500’ F. (260’ C.) Normal Operating (green arc) 180’ F. to 435’ F. High Performance Cruise below 435’ F. Economy Cruise below 400’ F. TACHOMETER Maximum RPM (red line) 2700 RPM Normal Operating (green arc) 600 to 2700 RPM EXHAUST GAS TEMPERATURE (EGT) Do not exceed 1650’ F. VACUUM PRESSURE Operating Range 4.3 to 5.9 ins Hg. CENTRE OF GRAVITY LIMTS WARNING These figures are dependent on the airplane being within safe Centre of Gravity limits. Do not fly the airplane if its computed flight CG falls outside of the published limits. Due to variables such as fuel, passenger and baggage weight, these figures may be reduced somewhat. Before each flight, the CG should be computed to determine whether the aircraft is within safe limits. Forward Limit Station 82. 21
example%20POH%20200hp%20-Glasair%20II%20FT.1.1.docx