[fltsim.0] title=Griffon 100M sim=Griffon model= panel= sound= texture= kb_checklists= kb_reference= atc_id= ui_manufacturer="Russian ULM" ui_type="Griffon 100M" ui_variation="Club AviaciĆ³n de Cuba RED" description="" [General] atc_type=ULM atc_model=Griffon editable=0 performance="" [WEIGHT_AND_BALANCE] max_gross_weight = 1650 // (pounds) empty_weight = 935 // (pounds) reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "170, -0.5, -1.0, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "170, -0.5, 1.0, 0.0, Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "0.0, -3.0, 0.0, 0.0, Baggage" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "0.0, 0.0, 0.0, 0.0, no usar" station_load.4 = "0.0, 0.0, 0.0, 0.0, no usar" station_load.5 = "0.0, 0.0, 0.0, 0.0, no usar" station_load.6 = "0.0, 0.0, 0.0, 0.0, no usar" ;Moments of Inertia empty_weight_pitch_MOI = 637.0 empty_weight_roll_MOI = 556.0 empty_weight_yaw_MOI = 993.0 empty_weight_coupled_MOI= 0.0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 p_factor_on_yaw=-0.2 torque_on_roll=-0.2 gyro_precession_on_yaw=-0.2 gyro_precession_on_pitch=-0.2 [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 5.6, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 1.00 //Fuel flow scalar min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 38.0 //Cubic inches per cylinder compression_ratio= 8.5 //Compression ratio number_of_cylinders=4 //Number of cylinders number_of_magnetos = 0 //Number of magnetos max_rated_rpm= 5600 //Max rated RPM max_rated_hp= 150 //Max rated HP fuel_metering_type= 0 //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= 0 //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 [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= 5 //Number of propeller blades propeller_moi= 6.0 //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 //Prop time-constant gear_reduction_ratio= 2.47 //Propeller gear reduction ratio fixed_pitch_beta= 12 //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= 0.9 //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) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor = 0, 5 , 17.0 gear_motor = 0, 5 , 17.0 autopilot = 0, 5 , 17.0 avionics_bus = 0, 5 , 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 2 , 17.0 marker_beacon = 1, 2 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 17.0 starter1 = 0, 20, 17.0 light_nav = 0, 5 , 17.0 light_beacon = 0, 5 , 17.0 light_landing = 0, 5 , 17.0 light_taxi = 0, 5 , 17.0 light_strobe = 0, 5 , 17.0 light_panel = 0, 5 , 17.0 //0 Class //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type [contact_points] point.0 = 1, 3.30, 0.00, -4.00, 1200, 0, 0.8, 22.0, 0.20, 3.5, 0.9, 0.0, 0.0, 0 //nose g point.1 = 1, -1.03, -3.02, -4.00, 1500, 1, 0.8, 0.0, 0.35, 2.5, 0.6, 0.0, 0.0, 2 //left g point.2 = 1, -1.03, 3.02, -4.00, 1500, 2, 0.8, 0.0, 0.35, 2.5, 0.6, 0.0, 0.0, 3 //right g //crash point.3 = 2, 0.0, -16.0, 2.00, 9999, 0, 0.0, 0.0, 0.0, 1.0, 1.0, 0.0, 0.0, 5 //left w point.4 = 2, 0.0, 16.0, 2.00, 9999, 0, 0.0, 0.0, 0.0, 1.0, 1.0, 0.0, 0.0, 6 //right w point.5= 2, 4.0, -1.0, -1.00, 9999, 0, 0.0, 0.0, 0.0, 1.0, 1.0, 0.0, 0.0, 4 //l_nose f point.6= 2, 4.0, 1.0, -1.00, 9999, 0, 0.0, 0.0, 0.0, 1.0, 1.0, 0.0, 0.0, 4 //r_nose f point.7= 2, -3.0, -2.0, -1.00, 9999, 0, 0.0, 0.0, 0.0, 1.0, 1.0, 0.0, 0.0, 7 //left f point.8= 2, -3.0, 2.0, -1.00, 9999, 0, 0.0, 0.0, 0.0, 1.0, 1.0, 0.0, 0.0, 8 //right f point.9= 2, -10.0, -3.0, 2.00, 9999, 0, 0.0, 0.0, 0.0, 1.0, 1.0, 0.0, 0.0, 9 //l_tail point.10= 2, -10.0, 3.0, 2.00, 9999, 0, 0.0, 0.0, 0.0, 1.0, 1.0, 0.0, 0.0, 9 //r_tail max_number_of_points = 21 static_pitch=0.0 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=4.0 //feet, altitude of CG when at rest on the ground [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.6 //Brake scalar [hydraulic_system] normal_pressure = 0.0 //PSI [Views] eyepoint= -1.32, -1.0, 1.32 //(feet) longitudinal, lateral, vertical distance from reference datum [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit //light.0 = 3, -2.88, -18.11, 2.95, fx_navred //light.1 = 3, -2.88, 18.11, 2.95, fx_navgre //light.2 = 1, -20.60, 0.00, 6.33, fx_beacon //light.3 = 4, -2.27, 0.00, 1.45, fx_vclight [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 100, 180 aileron = 200, 1000 rudder = 200, 1000 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=1,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,1 //Turn AND Bank [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain = 0.0, -2.1, 2.3, 22.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = 0.0, 2.1, 2.3, 22.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 159.2 //159.2 sin slats //Square feet wing_span = 33.75 //Feet wing_root_chord = 3.56 //3.56 sin slats //Feet wing_dihedral = 2.0 //Degrees wing_incidence = 3.0 //Degrees wing_twist = 0.0 //Degrees oswald_efficiency_factor= 0.8 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 0 //Degrees, wing leading edge wing_pos_apex_lon = 1.0 //1.0 sin slats //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 2.3 //Feet, vertical distance from reference point, positive going up htail_area = 31.0 //Square feet htail_span = 11.8 //Feet htail_pos_lon = -12.5 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 2.3 //Feet, vertical distance from reference point, positive going up htail_incidence = 3.0 //Degrees htail_sweep = 0.0 //Degrees, horizontal tail leading edge vtail_area = 14.0 //Square feet vtail_span = 4.1 //Feet, tip to body vtail_sweep = 30.0 //Degrees, vertical tail leading edge vtail_pos_lon = -13.2 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 2.0 //Feet, vertical distance from reference point, positive going up elevator_area = 16.6 //Square feet aileron_area = 18.3 //Square feet rudder_area = 10.5 //Square feet elevator_up_limit = 28.0 //Degrees elevator_down_limit = 21.0 //Degrees aileron_up_limit = 20.0 //Degrees aileron_down_limit = 15.0 //Degrees rudder_limit = 24.0 //Degrees elevator_trim_limit = 20.0 //Degrees spoiler_limit = 0.0 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 0 //Aileron to spoileron gain min_ailerons_for_spoilerons = 0 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate [flaps.0] //Trailing Edge Flaps type = 1 // 1 - tail, 2 - lead span-outboard = 1.0 // 0.0 .. 1.0 extending-time = 1 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 15.0 // degrees damaging-speed = 120 // KIAS blowout-speed = 120 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 3 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [flaps.1] //Leading Edge Slats type = 2 // 1 - tail, 2 - lead span-outboard = 1.0 // 0.0 .. 1.0 extending-time = 0 // seconds flaps-position.0 = 5 // degrees damaging-speed = 120 // KIAS blowout-speed = 120 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 3 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [Reference Speeds] flaps_up_stall_speed = 38.0 //Knots True (KTAS) full_flaps_stall_speed = 33.0 //Knots True (KTAS) cruise_speed = 70.0 //Knots True (KTAS) max_indicated_speed = 97 //Red line (KIAS) //max_horzontal = 80 kts [autopilot] autopilot_available= 0 [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [stall_warning] type=1