[fltsim.0] title=Curtiss Condor T32 sim=Curtiss Condor model= panel= sound= texture= kb_checklists=condor_check kb_reference=Condor_ref ui_manufacturer=Curtiss-Wright ui_type=T-32 Condor ui_variation=American Airways atc_heavy=0 atc_id=NC12354 atc_airline=AMERICAN atc_flight_number=22 description=Curtiss-Wright T-32 Condor. The Condor appeared at the same time as the Boeing 247 and the Douglas DC-2, but was a much more oldfashioned design.\n\nNC12354 (c/n 22) was the first production T-32, delivered to American Airways in april 1933. \n\nFS2004 model by Jens B. Kristensen [General] performance=Wright GR1820-F11 9cyl radials rated at 710 HP\sCruising speed 148 kts (167 mph, 269 km/h) at 8000 ft. atc_type=CURTISS atc_model=Condor [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0, 0.000, 0.000 max_number_of_stations=50 station_load.0 = "170.0, 9, -2.0, 0.0, Pilot" //Weight, Lat, Lon, Vert Position station_load.1 = "170.0, 9, 2.0, 0.0, Co-Pilot" //Weight, Lat, Lon, Vert Position station_load.2 = "860.0, 4, 0.0, 0.0, 4 Pax fwd" //Weight, Lat, Lon, Vert Position station_load.3 = "860.0, -2.50, 0.0, 0.0, 4 Pax mid" //Weight, Lat, Lon, Vert Position station_load.4 = "860.0, -9, 0.0, 0.0, 4 Pax aft" //Weight, Lat, Lon, Vert Position empty_weight=11235.000 max_gross_weight=16500.000 ;Moments of Inertia empty_weight_pitch_MOI = 69699.03 empty_weight_roll_MOI = 61179.10 empty_weight_yaw_MOI = 131797.97 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 = 2.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 p_factor_on_yaw = 0.5 torque_on_roll = 1.0 gyro_precession_on_yaw = 1.0 gyro_precession_on_pitch = 1.0 [flaps.0] //Trailing Edge Flaps type = 1 // 1 - tail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 7 // seconds flaps-position.0 = 0 // degrees damaging-speed = 140 // KIAS blowout-speed = 175 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 4 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [GeneralEngineData] engine_type=0 Engine.0=7.300, -9.000, 0.000 Engine.1=7.300, 9.000, 0.000 fuel_flow_scalar= 1.0 //Fuel flow scalar min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser master_ignition_switch = 1 //Master Ignition Switch [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 130.71 //Cubic inches per cylinder compression_ratio= 6.7 //Compression ratio number_of_cylinders=14 //Number of cylinders max_rated_rpm= 2350 //Max rated RPM max_rated_hp= 875 //Max rated HP fuel_metering_type= 2 //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= 37.5 //Max design manifold pressure, (inHg) min_design_mp= 10 //Min design manifold pressure, (inHg) critical_altitude= 13500 //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= 1 //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= 11.53 //Propeller Diameter, (feet) propeller_blades= 3 //Number of propeller blades propeller_moi= 40.2 //Propeller moment of inertia beta_max= 35.0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 18.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 1400 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 1.778 //Propeller gear reduction ratio fixed_pitch_beta= 24.0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80.0 //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= 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= 700.0 //Minimum RPM for prop feathering beta_feather= 89.5 //Feathering pitch angle (degrees) power_absorbed_cf= 0.9 //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= 0.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees) feathering_switches = 1 //Switches which invoke feathering //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=1.000, -28.868, 0.000, -0.656, 1573.938, 0.000, 0.630, 90.000, 0.279, 2.500, 0.895, 15.000, 25.000, 0.000, 0.000, 0.000 point.1=1.000, 2.730, -10.125, -7.3, 1967.423, 1.000, 0.630, 0.000, 0.313, 2.500, 0.845, 7.000, 7.000, 2.000, 0.000, 0.000 point.2=1.000, 2.73, 10.125, -7.3, 1967.423, 2.000, 0.630, 0.000, 0.313, 2.500, 0.845, 8.000, 8.000, 3.000, 0.000, 0.000 point.3=2.000, -1.000, -37.000, 0.000, 1573.938, 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, -1.000, 37.000, 0.000, 1573.938, 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, -1.000, -41.000, 10.000, 1573.938, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.6=2.000, -1.000, 41.000, 10.000, 1573.938, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.7=2.000, -34.333, 0.000, 1.50, 1573.938, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.8=2.000, 14.333, 0.000, -1.500, 1573.938, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=11.597 static_cg_height=6.6081 gear_system_type=1 //Hydraulic tailwheel_lock = 1 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 0.0 //Flap angle that activates warning at idle flap_limit_power = 16.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.3 //Brake scalar differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected [hydraulic_system] normal_pressure = 732.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=9.600,-1.400,2.44 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -1.2, -40.80, 10.0, fx_navred light.1=3, -1.2, 40.80, 10.0, fx_navgre light.2=3, -30.8, 0.00, 13.65, fx_navwhi light.3 = 4, 10.0, 0, 3.5, fx_vclighth, light.4 = 4, -2.2, 0, 3.5, fx_vclight, light.5 = 4, -8.7, 0, 3.5, fx_vclight, light.6 = 4, 3.8, 0, 3.5, fx_vclight, [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 0 Com.2 = 1, 0 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 0 Adf.1 = 1 Adf.2 = 1 Transponder.1 = 0 Marker.1 = 1 [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 =200, 1000 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 direction_indicator.1=2,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 attitude_indicator.1 = 2 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=2,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks startup=fx_engstrt_jenny touchdown=fx_tchdwn_s, 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 25 max_generator_alternator_amps = 100 [fuel] Center1=0.000, 0.000, 8.500, 150.000, 0.000 LeftMain=0.000, -7.000, 8.500, 75.000, 0.000 RightMain=0.000, 7.000, 8.500, 75.000, 0.000 fuel_type=1 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area = 1331.0 //Square feet wing_span = 82.0 //Feet wing_root_chord = 16.2 //Feet (both wings together) wing_dihedral = 2.25 //Degrees wing_incidence = 2.0 //Degrees wing_twist = -1.0 //Degrees oswald_efficiency_factor= 0.7 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 0.0 //Degrees, wing leading edge wing_pos_apex_lon = 4.06 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 3 //Feet, vertical distance from reference point, positive going up htail_area = 115.0 //Square feet htail_span = 25.9 //Feet htail_pos_lon = -23 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 4.0 //Feet, vertical distance from reference point, positive going up htail_incidence = 0.0 //Degrees htail_sweep = 19.0 //Degrees, horizontal tail leading edge vtail_area = 35.0 //Square feet vtail_span = 10.00 //Feet, tip to body vtail_sweep = 12.71 //Degrees, vertical tail leading edge vtail_pos_lon = -25.5 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 4.4 //Feet, vertical distance from reference point, positive going up elevator_area = 60.0 //Square feet aileron_area = 102.8 //Square feet rudder_area = 46.7 //Square feet elevator_up_limit = 30.0 //Degrees elevator_down_limit = 20.0 //Degrees aileron_up_limit = 27.0 //Degrees aileron_down_limit = 18.0 //Degrees rudder_limit = 30.0 //Degrees elevator_trim_limit = 12.0 //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 [Reference Speeds] flaps_up_stall_speed = 67.5 //Knots True (KTAS) full_flaps_stall_speed = 61.5 //Knots True (KTAS) cruise_speed = 150.0 //Knots True (KTAS) max_indicated_speed = 224 //Red line (KIAS) [autopilot] autopilot_available= 1 flight_director_available= 0 pitch_takeoff_ga=0.0 default_vertical_speed=700.000000 autothrottle_available=1 direction_indicator=1 attitude_indicator =1 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain = 0.0 default_bank_mode=2 //Default to Heading Hold autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 [forcefeedback] ground_bumps_magnitude1=2600 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.6 ground_bumps_magnitude2=1200 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.085 ground_bumps_slope2=0.65 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=3500000 ; in microseconds [stall_warning] type=1 [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second