[fltsim.0] title=PC-7 MKII Astra sim=PC7 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=L-011 ui_manufacturer=Pilatus ui_type=Pilatus PC-7 MKII Astra ui_variation=RNAF Trainer description=The Royal Dutch Air Force uses 13 Pilatus PC-7 Turbo Trainers. These 2-seaters are stationed at Woensdrecht Airbase. The Pilatus PC-7 Turbo Trainer is in use for the Elementary Military Flying Training and the advanced training. atc_heavy=0 atc_airline=KLu atc_flight_number=KT-02 [General] atc_type=PC7 atc_model= performance=Max Level Speed : 300 kts\nInitial Rate of Climb: 2,840 ft\min\nRange : 955 nautical miles with 5% reserve\nWeights : Empty: 3,715lb Max T\/O: 7,055 lb.\nPowerplant: 1x PW&C PT6A-62 Turboprop of 950 SHP (Flat Rated).\n\n \n \n \n \n \n \n [SMOKESYSTEM] smoke.0=-0.52, -10.02, 3.09, fx_smoke_w smoke.1=-0.52, -12.02, 3.09, fx_smoke_w smoke.2=-0.52, -14.02, 3.09, fx_smoke_w [WEIGHT_AND_BALANCE] max_gross_weight=6283.000 empty_weight=3682.000 reference_datum_position=16.200, 0.000, 0.000 empty_weight_CG_position=-16.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=170.000, -16.000, -1.500, 0.000 ;Moments of Inertia empty_weight_pitch_MOI=4524.000 empty_weight_roll_MOI=2477.000 empty_weight_yaw_MOI=6121.000 empty_weight_coupled_MOI=0.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=0.450 induced_drag_scalar=1.200 elevator_effectiveness=1.000 aileron_effectiveness=2.000 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 [GeneralEngineData] engine_type=5 Engine.0=-2.400, 0.000, 0.000 fuel_flow_scalar=1.120 [propeller] thrust_scalar=1.200 propeller_type=0 propeller_diameter=8.500 propeller_blades=4 propeller_moi=19.000 beta_max=40.000 beta_min=15.600 min_gov_rpm=25520.000 prop_tc=0.004 gear_reduction_ratio=17.400 fixed_pitch_beta=0.000 low_speed_theory_limit=80.000 prop_sync_available=0 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=700.000 beta_feather=88.000 power_absorbed_cf=0.900 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=1.000 minimum_reverse_beta=-14.000 [TurbineEngineData] fuel_flow_gain=0.011 inlet_area=1.000 rated_N2_rpm=33000.000 static_thrust=158.000 afterburner_available=0 [turboprop_engine] power_scalar=1.000 maximum_torque=2725.000 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 [pitot_static] vertical_speed_time_constant=1.0 //Increasing this value will cause a more instantaneous reaction in the VSI [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, -16.18, -16.85, -0.21, fx_navred light.1=3, -16.18, 16.85, -0.21, fx_navgre light.2=3, -35.10, 0.00, -0.50, fx_navwhi light.3=2, -16.29, -16.87, -0.21, fx_strobe light.4=2, -16.29, 16.87, -0.21, fx_strobe light.5=1, -22.40, 0.00, 2.53, fx_beacon light.6=4, -22.40, 0.816, -2.59, fx_beacon [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=3,0 //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, -7.10, 0.00, -5.40, 1500, 0, 0.5, 35.0, 0.3, 2.5, 0.7, 3.0, 4.0, 0 point.1=1, -17.50, -4.00, -5.25, 2500, 1, 0.5, 0.0, 0.3, 2.5, 0.7, 4.0, 6.0, 2 point.2=1, -17.50, 4.00, -5.25, 2500, 2, 0.5, 0.0, 0.3, 2.5, 0.7, 5.0, 6.0, 3 point.3=2, -15.90, -26.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5 point.4=2, -15.90 26.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6 point.5=2, -39.23, 0.0, 0.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9 point.6=2, -2.50, 0.0, -2.17, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4 point.7=2, -42.00, 0.0, 10.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7 max_number_of_points=21 static_pitch=0.24 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=5.25 //feet, altitude of CG when at rest on the ground [Views] eyepoint=-15.0, 0.0, 2.25 //(feet) longitudinal, lateral, vertical distance from reference datum [fuel] LeftMain=-18.400, -1.100, 2.500, 79.166, 3.600 RightMain=-18.400, 1.100, 2.500, 79.166, 3.600 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [airplane_geometry] wing_area=175.000 wing_span=33.250 wing_root_chord=6.400 wing_dihedral=3.900 wing_incidence=1.000 wing_twist=-1.000 oswald_efficiency_factor=0.850 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=-16.000 wing_pos_apex_vert=0.000 htail_area=39.000 htail_span=11.700 htail_pos_lon=-30.900 htail_pos_vert=0.000 htail_incidence=2.000 htail_sweep=5.000 vtail_area=38.000 vtail_span=5.800 vtail_sweep=0.000 vtail_pos_lon=-28.800 vtail_pos_vert=1.500 elevator_area=18.360 aileron_area=12.240 rudder_area=21.000 elevator_up_limit=28.000 elevator_down_limit=28.000 aileron_up_limit=25.000 aileron_down_limit=15.000 rudder_limit=24.000 elevator_trim_limit=19.500 spoiler_limit=20.000 spoilerons_available=0 aileron_to_spoileron_gain=1.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 [Reference Speeds] flaps_up_stall_speed=80.000 full_flaps_stall_speed=65.000 cruise_speed=260.000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=2000.0 autothrottle_available=0 pitch_takeoff_ga=8.000 [forcefeedback] 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=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 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 [Flaps.0] type=1 span-outboard=0.500 extending-time=4.700 system_type=0 damaging-speed=155.000 blowout-speed=160.000 lift_scalar=1.000 drag_scalar=2.000 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=20.000, 0.000 flaps-position.2=40.000, 0.000
