Hello, i am trying to make the FSX default Piper J3C-65 to work in MSFS 2020 (premium deluxe), so far everything is there, but i can not make the engine to start.

I am including the engines.cfg data so you can help me.

Thanks.

ENGINES.CFG FILE DATA

[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 ; 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=2350.00000

max_rated_hp=65.00000

min_cruise_rpm = 1800

max_cruise_rpm = 2350

max_indicated_rpm = 3000

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 = 0.30000 ; Starter torque factor

starter_time = 1.5 ; Time the Starter stays active when pressed

turbocharged = 0 ; Is it turbocharged? 0=FALSE, 1=TRUE

max_design_mp=29.92000

min_design_mp=2.99200

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 ; Scalar on maximum RPM mechanical efficiency

idle_rpm_mechanical_efficiency_scalar = 1

max_rpm_friction_scalar = 1 ; Scalar on maximum RPM friction

idle_rpm_friction_scalar = 1 ; Scalar on idle RPM friction

BestPowerSpecificFuelConsumption = 0.61 ; SFC at Best Power mixture ratio

egt_tuning_constant = 0

egt_peak_temperature = 1661.00000 ; typical peak EGT: 1200 degF + 460

egt_tc = 0.05

cht_tuning_constant = 1

cht_cooling_constant = 0.65

cht_heating_constant = 960 ; max temp degrees Rankine

rpm_on_cht_table = 0.29:0.73, 1:1

cht_tc = 0.015

oil_press_tuning_constant = 1

oil_press_max = 60.00000 ; max oil pressure (psf)

oil_press_tc = 0.8

oil_temp_tuning_constant = 0.8

oil_temp_cooling_constant = 0.21

oil_temp_heating_constant = 700 ; max oil temperature degrees Rankine

oil_temp_tc = 0.03

radiator_temp_tuning_constant = 1

radiator_temp_cooling_constant = 0.015

radiator_temp_max = 670 ; max radiator temperature degrees Rankine

radiator_temp_tc = 0.02

fuel_press_tuning_constant = 1

fuel_press_max = 16.50000 ; max fuel pressure (psf)

fuel_press_tc = 2

number_of_magnetos = 2

two_stroke_cycle = 0

supercharged = 0

radiator_cooling_constant = 0.015

radiator_heating_constant = 670

radiator_tc = 0.02

radiator_tuning_constant = 1

magneto_order_left_right_both = 0

engine_mechanical_efficiency_table = 0:0.77, 700:0.77, 2300:0.77, 2550:0.67, 2700:0.6

engine_friction_table = -300:-25, 300:25, 500:25, 2750:29

manifold_efficiency_table = 0:0.2, 1:0.97

rpm_to_oil_pressure_table = 0:0, 0.1:0.5, 0.7:1

rpm_to_fuel_pressure_table = 0:0, 500:0.3, 1400:1, 2000:1

oil_temp_factor_from_rpm = 0:0.5, 500:0.8, 2000:1 ; Gives the Oil temperature factor (to oil_temp_heating_constant) from rpm.

prop_lever_pos_to_oil_pressure_delta_table = 0:2160, 1:0 ; Delta in oil pressure when governor is taking over

diesel = 0 ; Is it diesel engine?

induction_air_temp_tc = 4 ; Induction Air Temp time constant

carb_heat_delta_temp = 55 ; Delta of temperature when the Carburator Heater is activated (In Rankine)

single_magneto_efficiency = 0.97 ; Efficiency ratio of the engine if it is designed for 2 magnetos but only 1 is currently active.

oil_temp_to_oil_pressure_table = 0:0, 500:-1, 700:-600 ; Pressure differential (in psf) of the oil depending on its temperature (in K).

shaft_torque_tc = 2.5 ; Gives the speed at which the shaft torque reaches its target value.

recip_stop_arc_degrees = 90 ; Gives the amplitude of the motion made by a reciprocating engine while it is having a spring compression behaviour after it stops producing work.

recip_stop_arc_restitution = 0.8 ; Gives the amount of torque in % restituted when reaching its max arc by a reciprocating engine while it is having a spring compression behaviour after it stops producing work.

recip_stop_arc_max_pct_rpm = 0.04 ; Gives the % max rpm at which a reciprocating engine that stopped producing work will start having a spring compression behaviour.

recip_stop_arc_friction_factor = 2 ; Factor on how much friction affects the reciprocating engine while having a spring compression behaviour.

egt_factor_from_pct_power = 0:0.5, 0.5:0.894, 0.64:0.956, 0.75:0.98, 1:1 ; Gives the EGT temperature factor (to egt_peak_temperature) from the pct of power (HP/maxHP)

egt_delta_from_mixture_ratio = 0.043:-100, 0.05:-89.7, 0.067:-50, 0.07:0, 0.075:-4.9, 0.083:-80, 0.108:-120.5 ; Gives the EGT temperature delta (to current egt value after factor is applied) from the mixture ratio

carb_icing_sensiblity = 0.25 ; from 0 for no icing to 1 for full sebsibility

[PROPELLER]

thrust_scalar = 1.0 ; Propeller thrust scalar

propeller_type = 1 ; 0=Constant Speed, 1=Fixed Pitch

propeller_diameter = 6.0 ; Propeller Diameter, (feet)

propeller_blades = 2 ; Number of propeller blades

propeller_moi = 3.86478 ; Propeller moment of inertia

beta_max = 14.75000 ; Maximum blade pitch angle for constant speed prop, (degrees)

beta_min = 12.75000 ; 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 ; Propeller gear reduction ratio

fixed_pitch_beta = 13.75000 ; 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

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)

prop_reverse_max_vel = 2 ; Max uvel when reversing

prop_governor_p = 0 ; Propeller governor controller P

prop_governor_i = 0 ; Propeller governor controller I

prop_governor_d = 0 ; Propeller governor controller D

prop_governor_iboundary = 0 ; Propeller governor controller I Boundary

prop_governor_dboundary = 0 ; Propeller governor controller D Boundary

prop_efficiency_table = 0.0:0.00:0.20:0.40:0.60:0.80:1.00:1.20:1.40:1.60:1.80:2.00:2.20, 15.0:0.15:0.40:0.71:0.86:0.72:0.50:0.34:0.23:0.15:0.11:0.08:0.06, 20.0:0.10:0.30:0.67:0.81:0.80:0.74:0.55:0.42:0.30:0.19:0.12:0.09, 25.0:0.08:0.23:0.49:0.72:0.82:0.87:0.82:0.60:0.41:0.28:0.18:0.13

prop_power_cf = 0.0:0.000:0.200:0.400:0.600:0.800:1.000:1.200:1.400:1.600:1.800:2.000:2.200:2.400, 15.0:0.032:0.029:0.025:0.022:0.009:-0.057:-0.188:-0.338:-0.522:-0.705:-0.915:-1.092:-1.220, 20.0:0.084:0.075:0.066:0.058:0.045:0.010:-0.074:-0.188:-0.338:-0.525:-0.726:-0.942:-1.120, 25.0:0.098:0.094:0.088:0.080:0.070:0.050:0.020:-0.040:-0.134:-0.272:-0.468:-0.717:-0.933, 30.0:0.138:0.132:0.128:0.120:0.110:0.099:0.078:0.040:-0.017:-0.110:-0.248:-0.468:-0.741, 35.0:0.206:0.198:0.188:0.178:0.163:0.150:0.130:0.105:0.070:0.023:-0.074:-0.254:-0.510, 40.0:0.250:0.242:0.233:0.223:0.214:0.204:0.190:0.175:0.150:0.118:0.072:0.019:-0.059

use_propeller_rpm = 0