[fltsim.0] title=Fuerza Aérea Uruguaya C-212M-200 FAU-532 sim=Casa212 model= panel= sound= texture=FAU-532 kb_checklists=Casa_check kb_reference=Casa_212_ref atc_id=FAU-532 atc_airline=FAU atc_flight_number=532 atc_parking_codes=FAU atc_parking_types=GATE,RAMP ui_manufacturer=CASA ui_type=C-212M-200 ui_variation=Fuerza Aerea Uruguaya FAU-532 description=Fuerza Aérea Uruguaya C-212M-200 FAU-532 (CN 189)(CX-BPI).Original by Thinus Pretorius.Repainted, panel and aerodynamics by Daniel Nole.FAUsim http://fau510.webs.com/ [fltsim.1] title=Fuerza Aérea Uruguaya C-212M-200 FAU-533 sim=Casa212 model= panel= sound= texture=FAU-533 kb_checklists=Casa_check kb_reference=Casa_212_ref atc_id=FAU-533 atc_airline=FAU atc_flight_number=533 atc_parking_codes=FAU atc_parking_types=GATE,RAMP ui_manufacturer=CASA ui_type=C-212M-200 ui_variation=Fuerza Aerea Uruguaya FAU-533 description=Fuerza Aérea Uruguaya C-212M-200 FAU-533 (CN 198)(CX-BPJ).Original by Thinus Pretorius.Repainted, panel and aerodynamics by Daniel Nole.FAUsim http://fau510.webs.com/ [General] atc_type=CASA atc_model=C212 editable=1 performance=Weight(MTOW)17.637 lbs,Power(2)Garret TPE331-10R-513C(900 shp),Maximum Speed 200 kt, Cruise speed 162 kt,Range 1446 nm.Service ceiling 26.000 ft,Payload 6217 lbs, Accomodation two (flight deck), maximum of 18-26 passengers [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight= 17637.000 empty_weight= 9688.000 reference_datum_position= 0.000, 0.000, 0.000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position= 0.000, 0.000, 0.000 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=180.000000, 5.000000, -2.000000, 0.000000, Pilot station_load.1=180.000000, 5.000000, 2.000000, 0.000000, Co-Pilot station_load.2=1080.000000, -2.100000, -2.000000, 0.000000, Pax seats 1-6" station_load.3=1080.000000, -2.100000, 2.000000, 0.000000, Pax seats 7-12" station_load.4=1080.000000, -5.300000, -2.000000, 0.000000, Pax seats 13-18" station_load.5=625.000000, -5.300000, 2.000000, 0.000000, Baggage" ;Moments of Inertia empty_weight_pitch_MOI= 30000.000 empty_weight_roll_MOI= 18200.000 empty_weight_yaw_MOI= 36500.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] LeftMain= 0.000, 0.000, 0.000, 278.000, 0.000 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain= 0.000, 0.000, 0.000, 278.000, 0.000 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 [GeneralEngineData] engine_type= 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0= -8.300, -4.800, 0.500 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1= -8.300, 4.800, 0.500 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 0.83 //Fuel flow scalar min_throttle_limit=-0.25; //Minimum percent throttle. Generally negative for turbine reverser [TurbineEngineData] fuel_flow_gain= 0.0250 //Gain on fuel flow inlet_area= 3.700 //Square Feet, engine nacelle inlet area rated_N2_rpm= 29920.000 //RPM, second stage compressor rated value static_thrust= 188.972 //Lbs, max rated static thrust at Sea Level afterburner_available= 0 [turboprop_engine] power_scalar=1.000 //Scalar on Turboprop power maximum_torque= 3270.000 //Maximum torque available (ft-lbs) max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [propeller] thrust_scalar=1.000 //Propeller thrust scalar propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 8.800 //Propeller Diameter, (feet) propeller_blades= 4 //Number of propeller blades propeller_moi= 120.000 //Propeller moment of inertia beta_max= 62.000 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 15.200 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 12250.000 //Miminum governed RPM prop_tc= 0.004 //Prop time-constant gear_reduction_ratio= 17.950 //Propeller gear reduction ratio fixed_pitch_beta= 20.000 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80.000 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available= 1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available= 1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 700.000 //Minimum RPM for prop feathering beta_feather= 79.300 //Feathering pitch angle (degrees) power_absorbed_cf= 0.900 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available= 1.000 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta= 1.000 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= -14.000 //Minimum pitch angle in reverse, (degrees) [Reference Speeds] flaps_up_stall_speed= 96.000 //Knots True (KTAS) full_flaps_stall_speed= 78.000 //Knots True (KTAS) cruise_speed= 191.000 //Knots True (KTAS) max_mach=0.58 max_indicated_speed=220 //Red line (KIAS) [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=100.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_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 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 starter2=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 <0=none,1=wheel, 2=scrape, 3=float> //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0= 1.000, 13.000, 0.000, -4.100, 1181.000, 0.000, 0.596, 39.900, 0.296, 2.500, 0.952, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, -1.670, -8.580, -4.700, 1574.000, 1.000, 0.596, 0.000, 0.642, 2.500, 0.815, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, -1.670, 8.580, -4.700, 1574.000, 2.000, 0.596, 0.000, 0.642, 2.500, 0.815, 0.000, 0.000, 3.000, 0.000, 0.000 point.3= 2.000, -3.330, -23.920, -3.000, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -3.330, 23.920, -3.000, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -22.670, 0.000, 0.000, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 23.080, 0.000, -1.500, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 0.000 //Degrees static_cg_height= 4.300 //Feet gear_system_type=1 //Hydraulic [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=1.0 //Brake scalar [Views] eyepoint=13.300, 0.000, 0.602 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [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=150, 250 aileron=150, 250 rudder=150, 250 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit. 5=landing light.0=3, 1.213, -30.668, 5.116, fx_navred light.1=3, 1.181, 30.611, 5.122, fx_navgre light.2=2, 0.253, -30.611, 5.122, fx_strobe light.3=2, 0.253, 30.611, 5.122, fx_strobe light.4=2, 6.619, 0.014, -2.273, fx_strobe light.5=1, -25.376, 0.00, 16.946, fx_beacon [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [airplane_geometry] wing_area= 430.600 wing_span= 66.583 wing_root_chord= 9.083 wing_dihedral= 2.000 wing_incidence= -0.494 wing_twist= -1.000 oswald_efficiency_factor= 0.864 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 125.000 htail_span= 25.000 htail_pos_lon= -22.500 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 100.000 vtail_span= 11.402 vtail_sweep= 0.000 vtail_pos_lon= -23.583 vtail_pos_vert= 5.833 elevator_area= 31.250 aileron_area= 24.120 rudder_area= 17.000 elevator_up_limit= 17.502 elevator_down_limit= 15.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.481 spoiler_limit= 59.989 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [autopilot] use_no_default_pitch=1 use_no_default_bank=1 autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 700.0 autothrottle_available= 0 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 0.0 default_pitch_mode=0 default_bank_mode=0 [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 [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=3,0 [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 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 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=2 [Flaps.0] system_type=0 span-outboard=0.500000 extending-time=6.000000 damaging-speed= 250.000 // KIAS blowout-speed= 300.000 // KIAS lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0=0.000000,0.000000 flaps-position.1=16.333334,0.000000 flaps-position.2=32.666668,0.000000 flaps-position.3=49.000001,0.000000 type=1 [exits] number_of_exits=2 exit_rate.0=0.4 [hydraulic_system] electric_pumps=1 //no electric pumps engine_map=1,1,0,0 //pumps on Eng1,2 normal_pressure=3000.0 //PSI [gear_warning_system] gear_warning_available=0 //1=Normal 0=None pct_throttle_limit=0.000000 //Percent throttle that activates warning flap_limit_power=0.000000 //Flap angle that activates warning at idle flap_limit_idle=0.000000 //Flap angle that activates warning at above idle
