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MSFS engines.cfg issue

Yuxtapuestoelmono

Yuxtapuestoelmono

Messages
80
Country
argentina
Hello, i am trying to make this plane to work, so far everything is there, but i can not make the engine to start.
I am including the engines.cfg so you can help me.
Thanks.
 
There is no engines.cfg included... no one can help you without that.
 
I SWEAR i attached the file, i will just post the contents here.

*****FILE CONTENTS*****


[VERSION]
major = 1 ;
minor = 0 ;

[GENERALENGINEDATA]
engine_type = 0 ; 0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine.0 = 5.8, 0.0, 0.0 ; (feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 ; Fuel flow scalar
min_throttle_limit = 0.0 ; Minimum percent throttle. Generally negative for turbine reverser
master_ignition_switch = 0 ;
starter_type = 0 ; 0=Electric, 1=Manual, 2=Bleed Air
max_contrail_temperature = -1 ;
thrustanglespitchheading.0 = 0,0 ;

[PISTON_ENGINE]
power_scalar = 1.0 ; Piston power scalar
cylinder_displacement = 42.75 ; Cubic inches per cylinder
compression_ratio = 6.3 ; Compression ratio
number_of_cylinders = 4 ; Number of cylinders
max_rated_rpm = 2300 ; Max rated RPM
max_rated_hp = 65 ; Max rated HP
fuel_metering_type = 1 ; 0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type = 0 ; 0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque = 0.3 ; Starter torque factor
turbocharged = 0 ; Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp = 0 ; Max design manifold pressure, (inHg)
min_design_mp = 0 ; Min design manifold pressure, (inHg)
critical_altitude = 0 ; Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type = 0 ; 0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset = 0 ; Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset = 0 ; Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture = 1 ; Automixture available? 0=FALSE, 1=TRUE
auto_ignition = 0 ; Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar = 1.0 ; Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar = 1.0 ; Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar = 1.0 ; Scalar on maximum RPM friction
idle_rpm_friction_scalar = 1.0 ; Scalar on idle RPM friction
magneto_order_left_right_both = 1 ; sets the order of the magneto switch direction
min_cruise_rpm = 545.5 ;
max_cruise_rpm = 2300 ;
max_indicated_rpm = 2800 ;
starter_time = 1.5 ; Time the Starter stays active when pressed
bestpowerspecificfuelconsumption = 0.6 ; SFC at Best Power mixture ratio
egt_tuning_constant = 1.000000 ;
egt_peak_temperature = 1660.000000 ; typical peak EGT: 1200 degF + 460
egt_tc = 2.000000 ;
cht_tuning_constant = 1.000000 ;
cht_cooling_constant = 0.650000 ;
cht_heating_constant = 960.000000 ; max temp degrees Rankine
cht_tc = 0.015000 ;
oil_press_tuning_constant = 1.000000 ;
oil_press_max = 8640.000000 ; max oil pressure (psf)
oil_press_tc = 0.800000 ;
oil_temp_tuning_constant = 1.000000 ;
oil_temp_cooling_constant = 0.210000 ;
oil_temp_heating_constant = 700.000000 ; max oil temperature degrees Rankine
oil_temp_tc = 0.030000 ;
radiator_temp_tuning_constant = 1.000000 ;
radiator_temp_cooling_constant = 0.015000 ;
radiator_temp_max = 670.000000 ; max radiator temperature degrees Rankine
radiator_temp_tc = 0.020000 ;
fuel_press_tuning_constant = 1.000000 ;
fuel_press_max = 2376.000000 ; max fuel pressure (psf)
fuel_press_tc = 2.000000 ;
number_of_magnetos = 2 ;
two_stroke_cycle = 0 ;
supercharged = 0 ;
engine_mechanical_efficiency_table = 0.000000:0.917039,517.500000:0.917039,632.500000:0.417039,1880.000000:0.417039,2350.000000:0.417039 ;
engine_friction_table = -230.000000:-38.391816,230.000000:38.391816,460.000000:7.263404,2350.000000:7.263404 ;
diesel = 0 ; Is it diesel engine?
single_magneto_efficiency = 0.97 ; Efficiency ratio of the engine if it is designed for 2 magnetos but only 1 is currently active.

[PROPELLER]
thrust_scalar = 1.0 ; Propeller thrust scalar
propeller_type = 1 ; 0=Constant Speed, 1=Fixed Pitch
propeller_diameter = 6 ; Propeller Diameter, (feet)
propeller_blades = 2 ; Number of propeller blades
propeller_moi = 3.78 ; Propeller moment of inertia
beta_max = 0 ; Maximum blade pitch angle for constant speed prop, (degrees)
beta_min = 0 ; Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm = 0 ; Miminum governed RPM
prop_tc = 0.1 ; Prop time-constant
gear_reduction_ratio = 1.0 ; Propeller gear reduction ratio
fixed_pitch_beta = 13.75 ; Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit = 80 ; Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available = 0 ; Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available = 0 ; Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available = 0 ; Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available = 0 ; Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather = 0 ; Minimum RPM for prop feathering
beta_feather = 0 ; Feathering pitch angle (degrees)
power_absorbed_cf = 0 ; Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available = 0 ; Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available = 0 ; Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta = 0 ; Miminum pitch angle on ground, (degrees)
minimum_reverse_beta = 0 ; Minimum pitch angle in reverse, (degrees)
use_propeller_rpm = 0 ;
prop_efficiency_table = 0.000000:0.000000:0.100550:0.201101:0.301651:0.423748:0.545845:0.667942:0.790038:0.829540:0.869042:0.908544:0.948046:0.987548,12.750000:0.250000:0.327939:0.405881:0.483821:0.575321:0.666821:0.758321:0.849821:0.849881:0.849940:0.850000:0.850060:0.000000,12.950000:0.250000:0.327939:0.405881:0.483821:0.575321:0.666821:0.758321:0.849821:0.849881:0.849940:0.850000:0.850060:0.000000,13.150000:0.250000:0.327939:0.405881:0.483821:0.575321:0.666821:0.758321:0.849821:0.849881:0.849940:0.850000:0.850060:0.000000,13.350000:0.250000:0.327939:0.405881:0.483821:0.575321:0.666821:0.758321:0.849821:0.849881:0.849940:0.850000:0.850060:0.000000,13.550000:0.250000:0.327939:0.405881:0.483821:0.575321:0.666821:0.758321:0.849821:0.849881:0.849940:0.850000:0.850060:0.000000,13.750000:0.250000:0.327939:0.405881:0.483821:0.575321:0.666821:0.758321:0.849821:0.849881:0.849940:0.850000:0.850060:0.000000,13.950000:0.250000:0.327939:0.405881:0.483821:0.575321:0.666821:0.758321:0.849821:0.849881:0.849940:0.850000:0.850060:0.000000,14.150000:0.250000:0.327939:0.405881:0.483821:0.575321:0.666821:0.758321:0.849821:0.849881:0.849940:0.850000:0.850060:0.000000,14.350000:0.250000:0.327939:0.405881:0.483821:0.575321:0.666821:0.758321:0.849821:0.849881:0.849940:0.850000:0.850060:0.000000,14.550000:0.250000:0.327939:0.405881:0.483821:0.575321:0.666821:0.758321:0.849821:0.849881:0.849940:0.850000:0.850060:0.000000,14.750000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000 ;
prop_power_cf = 0.000000:0.000000:0.100550:0.201101:0.301651:0.423748:0.545845:0.667942:0.790038:0.829540:0.869042:0.908544:0.948046:0.987548,12.750000:0.039212:0.038737:0.038261:0.037786:0.037209:0.036632:0.036055:0.035477:0.035291:0.035104:0.034917:0.034730:0.034544,12.950000:0.039585:0.039110:0.038635:0.038159:0.037582:0.037005:0.036428:0.035851:0.035664:0.035477:0.035291:0.035104:0.034917,13.150000:0.039959:0.039483:0.039008:0.038533:0.037956:0.037379:0.036801:0.036224:0.036038:0.035851:0.035664:0.035477:0.035291,13.350000:0.040332:0.039857:0.039382:0.038906:0.038329:0.037752:0.037175:0.036598:0.036411:0.036224:0.036038:0.035851:0.035664,13.550000:0.040706:0.040230:0.039755:0.039280:0.038703:0.038125:0.037548:0.036971:0.036784:0.036598:0.036411:0.036224:0.036038,13.750000:0.041079:0.040604:0.040128:0.039653:0.039076:0.038499:0.037922:0.037345:0.037158:0.036971:0.036784:0.036598:0.036411,13.950000:0.041453:0.040977:0.040502:0.040027:0.039449:0.038872:0.038295:0.037718:0.037531:0.037345:0.037158:0.036971:0.036784,14.150000:0.041826:0.041351:0.040875:0.040400:0.039823:0.039246:0.038669:0.038092:0.037905:0.037718:0.037531:0.037345:0.037158,14.350000:0.042199:0.041724:0.041249:0.040774:0.040196:0.039619:0.039042:0.038465:0.038278:0.038092:0.037905:0.037718:0.037531,14.550000:0.042573:0.042098:0.041622:0.041147:0.040570:0.039993:0.039416:0.038838:0.038652:0.038465:0.038278:0.038092:0.037905,14.750000:0.042946:0.042471:0.041996:0.041520:0.040943:0.040366:0.039789:0.039212:0.039025:0.038838:0.038652:0.038465:0.038278 ;
 
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