[fltsim.0] title=PC-7 Klu sim=PC-7 model= panel= sound= texture=klu kb_checklists= kb_reference= atc_id_color=0x00ff0000 atc_id=302 ui_manufacturer=Pilatus ui_type=PC-7 ui_variation=Royal Netherlands Air Force description=Repaint by P. van Hulst atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 ui_createdby="Piglet's Peculiar Planes" Typerole=Militair visual_damage=1 prop_anim_ratio = 1.72 [General] atc_type=Pilatus atc_model=PC-7 editable=1 performance=Powered by a Pratt and Whitney PT-6 turboprop engine, developing 550 SHP max. category=airplane [weight_and_balance] // ACM V2.5 max_gross_weight =4188.0 empty_weight =2932.00000 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0.000, 0.000, 0.000 empty_weight_pitch_MOI =3706.63000 empty_weight_roll_MOI =1862.97000 empty_weight_yaw_MOI =4205.95000 empty_weight_coupled_MOI =0.00000 max_number_of_stations =2 station_load.0= 200, 0.000, 0.000, 0.000, Student station_load.1= 200, 0.000, 0.000, 0.000, Instructor [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -0.34, -17.15, 0, fx_navred light.1 = 3, -0.34, 17.15, 0, fx_navgre light.2 = 4, 0.57, -0.99, 0.66, fx_vclight_deepred light.3 = 4, -2.51, 0.99, 0.61, fx_vclight_deepred light.4 = 2, -0.51, 17.14, 0, fx_strobe light.5 = 2, -0.51, -17.14, 0, fx_strobe [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type =5 fuel_flow_scalar =1.00000 min_throttle_limit =0.00000 engine.0 =8.250, 0.000, 0.000 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 startup = , 1 windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type =2 number_of_tank_selectors =1 electric_pump =1 LeftMain = 0.000, -8.000, -1.450, 52.000, 0.000 RightMain = 0.000, 8.000, -1.450, 52.000, 0.000 fuel_dump_rate=0.02000 anemometer_pump=0 engine_driven_pump=1 manual_pump=0 [contact_points] static_pitch = 1.880 static_cg_height = 5.150 tailwheel_lock =0 gear_system_type =0 max_number_of_points =7 point.0= 1, 6.484, 0.000, -5.350, 2378, 0, 0.780, 45.000, 0.178, 2.596, 0.800, 3.000, 3.000, 0, 200.0, 250.0 point.1= 1, -1.160, -4.290, -4.970, 2969, 1, 0.900, 0.000, 0.170, 2.059, 0.800, 3.000, 4.000, 2, 200.0, 250.0 point.2= 1, -1.160, 4.290, -4.970, 2969, 2, 0.900, 0.000, 0.170, 2.059, 0.800, 3.000, 4.000, 3, 200.0, 250.0 point.3= 2, -0.690, -17.010, -0.300, 787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5 point.4= 2, -0.690, 17.010, -0.300, 787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6 point.5= 2, -16.000, 0.000, -1.321, 787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9 point.6= 2, -0.078, 0.000, -2.499, 787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4 [keyboard_response] elevator = 140, 240 aileron = 200, 1000 rudder = 200, 1000 [forcefeedback] gear_bump_nose_magnitude =6000 gear_bump_nose_direction =18000 gear_bump_nose_duration =250000 gear_bump_left_magnitude =6000 gear_bump_left_direction =35500 gear_bump_left_duration =250000 gear_bump_right_magnitude =6000 gear_bump_right_direction =500 gear_bump_right_duration =250000 ground_bumps_magnitude1 =3250 ground_bumps_angle1 =8900 ground_bumps_intercept1 =5 ground_bumps_slope1 =0.48 ground_bumps_magnitude2 =750 ground_bumps_angle2 =9100 ground_bumps_intercept2 =0.075 ground_bumps_slope2 =1 crash_magnitude1 =10000 crash_direction1 =1000 crash_magnitude2 =10000 crash_direction2 =9000 crash_period2 =75000 crash_duration2 =2500000 stick_shaker_magnitude =5000 stick_shaker_direction =0 stick_shaker_period =111111 [airplane_geometry] wing_area =178.00000 wing_span =34.47000 wing_root_chord =6.00000 wing_dihedral =7.00000 wing_incidence =0.00000 wing_twist =0.00000 oswald_efficiency_factor =0.60000 wing_winglets_flag =0 wing_sweep =0.00000 wing_pos_apex_lon =1.30226 wing_pos_apex_vert =-1.41000 htail_area =28.00000 htail_span =11.41000 htail_pos_lon =-18.02000 htail_pos_vert =0.00000 htail_incidence =0.00000 htail_sweep =0.00000 vtail_area =13.75000 vtail_span =5.55000 vtail_sweep =0.00000 vtail_pos_lon =-15.42000 vtail_pos_vert =0.83000 elevator_area =15.19000 aileron_area =18.40000 rudder_area =10.43000 elevator_up_limit =26.00000 elevator_down_limit =16.00000 aileron_up_limit =20.00000 aileron_down_limit =15.00000 rudder_limit =30.00000 elevator_trim_limit =20.00000 spoiler_limit =0.00000 aileron_to_spoileron_gain =0.00000 spoiler_handle_available =0 min_ailerons_for_spoilerons =0.00000 min_flaps_for_spoilerons =0.00000 spoilerons_available =0 auto_spoiler_available=0 positive_g_limit_flaps_up=8.00000 negative_g_limit_flaps_up=-6.40000 positive_g_limit_flaps_down=5.60000 negative_g_limit_flaps_down=-4.80000 load_safety_factor=1.00000 [electrical] max_battery_voltage = 28 generator_alternator_voltage = 28 max_generator_alternator_amps = 120 engine_generator_map = 1 electric_always_available = 0 flap_motor = 0, 5, 17 avionics_bus = 0, 5, 9.5 avionics = 1, 5, 9.5 pitot_heat = 0, 15, 17 additional_system = 0, 2, 9.5 marker_beacon = 1, 2, 9 fuel_pump = 0, 5, 9 starter1 = 0, 20, 17 light_nav = 0, 5, 17 light_landing = 0, 5, 17 light_panel = 0, 5, 17 standby_vacuum = 0, 15, 17 [flight_tuning] cruise_lift_scalar=1.00000 parasite_drag_scalar=1.00000 induced_drag_scalar=1.00000 elevator_effectiveness=1.00000 aileron_effectiveness=1.00000 rudder_effectiveness=1.00000 pitch_stability=1.00000 roll_stability=1.00000 yaw_stability=1.00000 elevator_trim_effectiveness=1.00000 aileron_trim_effectiveness=1.00000 rudder_trim_effectiveness=1.00000 p_factor_on_yaw =0.50000 torque_on_roll =0.50000 hi_alpha_on_roll=1.00000 hi_alpha_on_yaw=1.00000 gyro_precession_on_roll=1.00000 gyro_precession_on_yaw=1.00000 [flaps.0] //Trailing Edge Flaps type= 1 system_type=0 span-outboard= 0.500 extending-time= 5.0 damaging-speed=200.0 blowout-speed=250.0 flaps-position.0=0.00, 200.0 flaps-position.1=22.00, 180.0 flaps-position.2=45.00, 150.0 lift_scalar=1.00 drag_scalar=1.00 pitch_scalar=1.00 [propeller] thrust_scalar=1.00000 propeller_type=0 propeller_diameter=8.00000 propeller_blades=3 propeller_moi=20.27925 beta_max=45.00000 beta_min=15.00000 min_gov_rpm=700.00000 prop_tc=0.01000 gear_reduction_ratio=13.88000 fixed_pitch_beta=2.00000 low_speed_theory_limit=80.00000 prop_sync_available=0 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=0.00000 beta_feather=0.00000 power_absorbed_cf=0.00000 defeathering_accumulators_available=1 prop_reverse_available=0 minimum_on_ground_beta=0.00000 minimum_reverse_beta=0.00000 [brakes] parking_brake =1 toe_brakes_scale =0.85000 differential_braking_scale =1.00000 auto_brakes=0 hydraulic_system_scalar=0.00000 [hydraulic_system] normal_pressure =0.00000 [Views] eyepoint= .08, 0.00, 2.17 [exits] number_of_exits = 1 exit_rate.0 = 0.8 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Nav.1=1, 0, 1 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=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=1,0 [Reference Speeds] flaps_up_stall_speed=70.99997 full_flaps_stall_speed=63.99997 cruise_speed=222.00000 max_indicated_speed =300.00000 max_mach=1.00000 [autopilot] autopilot_available=0 flight_director_available=0 autothrottle_available=0 autothrottle_arming_required=0 default_pitch_mode=0 default_bank_mode=0 use_no_default_bank=1 use_no_default_pitch=1 default_vertical_speed=1000.00000 autothrottle_takeoff_ga=1.00000 autothrottle_max_rpm=90.00000 pitch_takeoff_ga=8.00000 max_pitch=10.00000 max_pitch_acceleration=1.00000 max_pitch_velocity_lo_alt=2.00000 max_pitch_velocity_hi_alt=1.50000 max_pitch_velocity_lo_alt_breakpoint=20000.00000 max_pitch_velocity_hi_alt_breakpoint=28000.00000 max_bank=25.00000 max_bank_acceleration=1.80000 max_bank_velocity=3.00000 max_throttle_rate=0.10000 nav_proportional_control=9.00000 nav_integrator_control=0.25000 nav_derivative_control=0.00000 nav_integrator_boundary=2.50000 nav_derivative_boundary=0.00000 gs_proportional_control=9.52000 gs_integrator_control=0.26000 gs_derivative_control=0.00000 gs_integrator_boundary=0.70000 gs_derivative_boundary=0.00000 yaw_damper_gain=0.00000 [stall_warning] type=2 stick_shaker=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=25.00000 flap_limit_idle=33.75000 flap_limit_power=16.87500 [AirWrench] Aircraft_Length=32.00000 Vmax_sl=310.71033 Vmax_ca=330.04342 V_rc=179.52152 Climb_Rate=2000.00000 Climb_Weight=2932.00000 Max_gforce=8.00000 Emergency_hp=550.00000 nose_position_lon=8.50000 ActualIncidence=1.00000 ActualTwist=0.00000 ActualTailIncidence=0.00000 Aircraft_Type=1 FlowCorrection=1.00000 JetAltitude=0.00000 turboprop_critical_altitude=20000.00000 target_roll_Vopt=310.82541 target_roll_rate=226.60000 pitch_damping=1.00000 yaw_damping=1.00000 elevator_scalar=1.00000 rudder_scalar=1.00000 dihedral_scalar=1.00000 Elevator_FF=60.00000 Aileron_FF=-60.00000 Roll_Response=30.00000 Adverse_Yaw=100.00000 Control_Response=100.00000 V_Max_Control=350.00000 V_Zero_Control=506.30000 Spin_Stability=32.00000 Stall_Stability=100.00000 Elevator_Propwash=1.00000 Rudder_Propwash=1.00000 spoiler_time=0.00000 afterburner_thrust=0.00000 mach_scale=1.00000 spoiler_type=0 spoiler_cd=0.00000 spoiler_cl=0.00000 spoiler_cm=0.00000 flaps_type=2 flaps_cd_scalar=0.90700 flaps_cm_scalar=0.25000 vfe_enabled=1 gear_cd_scalar=0.14000 gear_cm_scalar=-0.12000 cylinder_head_temperature=501.00000 exhaust_gas_temperature=1201.00000 fuel_pressure=24.00000 oil_pressure=60.00000 oil_temperature=241.00000 radiator_temperature=211.00000 exhaust_pressure_ratio=1.50000 interstage_turbine_temperature=1859.00000 knots_flag=1 cfs1_flag=0 cfs2_ai_flag=0 fs8_flag=1 laminar_flow=0 direct_edit_mach=0 fixed_wing_pos=0 AirWrenchVersion=1.01.45 VSI_Weight=4188.00000 ReheatCutoff=1.20000 OptimumMach=0.90000 Power_Calibration=1.00000 IdleRPM=850.00000 weathervane=1.00000 aileron_scalar=1.00000 prop_yaw_damping_scalar=1.00000 V_Max_RdrControl=350.00000 V_Zero_RdrControl=506.30000 Roll_Off=0.45000 ClAoA_k0=1.00000 ClAoA_k1=1.00000 ClAoA_k2=0.85000 ClAoA_k3=0.80000 prop_design_altitude=5000.00000 prop_material_type=1 protect_airfile=0 critical_mach_number=0.80000 max_mach_cd0=60 mach_slope=1.00000 direct_edit_drag=0 lo_rpm_friction=1.00000 hi_rpm_friction=1.00000 cfs2_flag=0 AI_flag=0 edit_tp_torque=0 direct_edit_2dtab=0 range_est_alt=0.00000 range_est_rpm=3400.00000 range_est_mp=48.00000 range_est_fuel=100.00000 [SMOKESYSTEM] smoke.0=-10.00, -0.70, 0.0, fx_smoke_w [TurbineEngineData] static_thrust=158.00000 inlet_area=1.50000 rated_N2_rpm=33000.00000 fuel_flow_gain=0.01100 reverser_available=0 afterburner_available=0 [turboprop_engine] maximum_torque=1514.96267 power_scalar=1.00000 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=0.150000 [deice_system] structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots