[fltsim.0] title=PC7 Trainer sim=PC7 Trainer model= panel= sound= texture= kb_checklists=PC7_checklist kb_reference=specs description=Notes Aircraft Pilatus P.C.7 Mk II Astra is a single engine turboprop, all metal, low-wing, two-seat training aircraft from the South African Airforce. \nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008 ui_manufacturer=Pilatus ui_type=PC7 Astra Mk. 2 ui_variation=Trainer atc_heavy=0 atc_id= atc_airline= atc_flight_number= visual_damage=1 atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 atc_parking_types=MIL_COMBAT [fltsim.1] title=PC7 Silver Falcons sim=PC7 Silver Falcons model=1 panel= sound= texture=1 kb_checklists=PC7_checklist kb_reference=specs description=Notes The Aircraft is depicted as Silver Falcon 1 of the South African Airforce. Pilatus P.C.7 Mk II Astra is a single engine turboprop, all metal, low-wing, two-seat training aircraft. \nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008 ui_manufacturer=Pilatus ui_type=PC7 Astra Mk. 2 ui_variation=Silver Falcon 1 atc_heavy=0 atc_id= atc_airline= atc_flight_number= visual_damage=1 atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 atc_parking_types=MIL_COMBAT [fltsim.2] title=PC7 Silver Falcon2 sim=PC7 Silver Falcons model=1 panel= sound= texture=2 kb_checklists=PC7_checklist kb_reference=specs description=Notes 9A:The Aircraft is depicted as Silver Falcon 2 of the South African Airforce. Pilatus P.C.7 Mk II Astra is a single engine turboprop, all metal, low-wing, two-seat training aircraft. \nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008 ui_manufacturer=Pilatus ui_type=PC7 Astra Mk. 2 ui_variation=Silver Falcon2 atc_heavy=0 atc_id= atc_airline= atc_flight_number= visual_damage=1 atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 atc_parking_types=MIL_COMBAT [fltsim.3] title=PC7 Silver Falcon3 sim=PC7 Silver Falcons model=1 panel= sound= texture=3 kb_checklists=PC7_checklist kb_reference=specs description=Notes 7A The Aircraft is depicted as Silver Falcon 3 of the South African Airforce. Pilatus P.C.7 Mk II Astra is a single engine turboprop, all metal, low-wing, two-seat training aircraft. \nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008 ui_manufacturer=Pilatus ui_type=PC7 Astra Mk. 2 ui_variation=Silver Falcon3 atc_heavy=0 atc_id= atc_airline= atc_flight_number= visual_damage=1 atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 atc_parking_types=MIL_COMBAT [fltsim.4] title=PC7 Silver Falcons4 sim=PC7 Silver Falcons model=1 panel= sound= texture=4 kb_checklists=PC7_checklist kb_reference=specs description=Notes The Aircraft is depicted as Basic Trainer of the South African Airforce. Pilatus P.C.7 Mk II Astra is a single engine turboprop, all metal, low-wing, two-seat training aircraft. \nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008 ui_manufacturer=Pilatus ui_type=PC7 Astra Mk. 2 ui_variation=Silver Falcon4 atc_heavy=0 atc_id= atc_airline= atc_flight_number= visual_damage=1 atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 atc_parking_types=MIL_COMBAT [fltsim.5] title=PC7 Solo sim=PC7 Trainer model=solo panel= sound= texture= kb_checklists=PC7_checklist kb_reference=specs description=Notes Aircraft Pilatus P.C.7 Mk II Astra is a single engine turboprop, all metal, low-wing, two-seat training aircraft from the South African Airforce. \nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008 ui_manufacturer=Pilatus ui_type=PC7 Astra Mk. 2 ui_variation=Solo atc_heavy=0 atc_id= atc_airline= atc_flight_number= visual_damage=1 atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 atc_parking_types=MIL_COMBAT [General] performance=AIRCRAFT SPECIFICATION\nTwo seater trainer\nPowerplant:1 x 700 shp P& W Canada PT6A-25C\nMax speed: 350 kts (Mach 0.53)\nVno: 280 kts\nRange:1500 km\nLength:10.13 m \nWing span:10.12 m\nWeight empty:1330 kg \nMax weight: 2700 kg\nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008 atc_type=PILATUS atc_model=PC7 editable=0 category=airplane [weight_and_balance] // ACM V2.5 max_gross_weight = 5164 empty_weight = 3196 reference_datum_position = -0.1, 0, -0.1 empty_weight_CG_position = 0.02, 0, 0 empty_weight_pitch_MOI = 7500 empty_weight_roll_MOI = 2581 empty_weight_yaw_MOI = 5108 empty_weight_coupled_MOI = 0.000 CG_forward_limit = 0.300 CG_aft_limit = 0.500 max_number_of_stations = 2 station_load.0 = 160, 1.600, 0.000, 0.000 station_load.1 = 160, -3.750, 0.000, 0.000 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cabin light.0 = 3, 1.55, -16.706, -0.4, fx_navred light.1 = 3, 1.55, 16.455, -0.4, fx_navgre light.2 = 2, -0.65, 0, -2.758, fx_PC7_nav_red_flash light.3 = 3, -18.2, 0, 0, fx_navwhi light.4 = 6, 10.0, 1.15, 0, fx_PC7_SmokeL light.5 = 6, 10.0, -1.15, 0, fx_PC7_SmokeR [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 5 fuel_flow_scalar = 1.0200 //FFcurve/thr! min_throttle_limit = -0.10000 engine.0 = 7.150, 0.000, -0.20 [smokesystem] smoke.0 = 10.5, 0,0, fx_PC7engine [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_m, 1 startup = fx_engstrt 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 = -0.12, 6, -1.8, 64.5, 1 RightMain = -0.12, -6, -1.8, 64.5, 1 [contact_points] static_pitch = 0.260 static_cg_height = 5.350 tailwheel_lock = 0 gear_system_type = 0 max_number_of_points =10 point.0= 1, 7.000, 0.000, -5.380, 1858, 0, 0.750, 36.500, 0.120, 2.157, 0.595, 5.000, 6.000, 0 point.1= 1, -1.651, -4.450, -5.440, 1926, 1, 0.825, 0.000, 0.288, 2.486, 0.808, 5.200, 5.000, 2 point.2= 1, -1.650, 4.450, -5.440, 1926, 2, 0.825, 0.000, 0.288, 2.486, 0.808, 5.000, 5.200, 3 point.3= 2, -15.500, 0.000, 6.000, 500, 0, 0.000, 0.000, 0.000, -1.000, 0.000, 0.000, 0.000, 9 point.4= 2, 0.000, -16.583, -0.500, 1275, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5 point.5= 2, 9.500, 0.000, -2.300, 500, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4 point.6= 2, 0.000, 16.583, -0.550, 1275, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6 point.7= 2, -17.000, 0.000, -1.900, 1075, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9 point.8= 2, -0.500, 0.000, -2.850, 500, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4 point.9= 2, 1.083, 0.000, 0.500, 275, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4 [keyboard_response] elevator = 120, 240 aileron = 120, 240 rudder = 10, 110 [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] //ACM_AREAW1// 0,0,0,2.4993,0.5842,0.5842,0.0204,2.3947,1.1684,1.1684 //ACM_AREAW2// 0.0408,2.2901,1.7525,1.7525,0.0612,2.1856,2.3368,2.3368,0.0816,2.0810 //ACM_AREAW3// 2.9210,2.9210,0.1018,1.9765,3.5051,3.5051,0.1224,1.8717,4.0893,4.0893 //ACM_AREAW4// 0.1428,1.7673,4.6736,4.6736,0.1632,1.6627,5.2578,5.2578,0.1835,1.5582 //ACM_AREAH1// 0,0,0,1.1683,0.1947,0.1947,0.0170,1.1267,0.3894,0.3894 //ACM_AREAH2// 0.0340,1.0856,0.5841,0.5841,0.0511,1.0441,0.7789,0.7789,0.0680,1.0025 //ACM_AREAH3// 0.9735,0.9735,0.0851,0.9613,1.1683,1.1683,0.1022,0.9200,1.3631,1.3631 //ACM_AREAH4// 0.1190,0.8787,1.5578,1.5578,0.1360,0.8373,1.7525,1.7525,0.1533,0.7957 //ACM_AREAV1// -0.1895,-0.1895,-0.1703,1.7416,0.1703,0.1703,-0.5248,1.6818,0.3406,0.3406 //ACM_AREAV2// 0.0118,1.6409,0.5109,0.5109,0.2642,1.6188,0.6812,0.6812,0.3269,1.5779 //ACM_AREAV3// 0.8517,0.8517,0.3898,1.5750,1.0219,1.0219,0.4336,1.5532,1.1921,1.1921 //ACM_AREAV4// 0.5343,1.5123,1.3624,1.3624,0.5971,1.4903,1.6275,1.6275,0.6790,1.4305 //ACM_CAREAW1// 2.6289,2.6289,1.3414,1.8413,2.9210,2.9210,1.3516,1.8265,3.2130,3.2130 //ACM_CAREAW2// 1.3617,1.8114,3.5051,3.5051,1.3717,1.7969,3.7973,3.7973,1.3822,1.7819 //ACM_CAREAW3// 4.0893,4.0893,1.3924,1.7673,4.3814,4.3814,1.4026,1.7525,4.6736,4.6736 //ACM_CAREAW4// 1.4127,1.7378,4.9657,4.9657,1.4227,1.7230,5.2578,5.2578,1.4332,1.7079 //ACM_CAREAH1// 0,0,0.5841,1.1683,0.1947,0.1947,0.6011,1.1562,0.3894,0.3894 //ACM_CAREAH2// 0.6182,1.1440,0.5841,0.5841,0.6352,1.1318,0.7789,0.7789,0.6523,1.1196 //ACM_CAREAH3// 0.9735,0.9735,0.6693,1.1073,1.1683,1.1683,0.6862,1.0951,1.3631,1.3631 //ACM_CAREAH4// 0.7034,1.0829,1.5578,1.5578,0.7203,1.0707,1.7525,1.7525,0.7375,1.0585 //ACM_CAREAV1// 0,0,0.3831,1.1497,0.1703,0.1703,0.3892,1.0944,0.3406,0.3406 //ACM_CAREAV2// 0.3950,1.0391,0.5109,0.5109,0.4011,0.9836,0.6812,0.6812,0.4070,0.9283 //ACM_CAREAV3// 0.8517,0.8517,0.4129,0.8729,1.0219,1.0219,0.4189,0.8173,1.1921,1.1921 //ACM_CAREAV4// 0.4248,0.7620,1.3624,1.3624,0.4307,0.7067,1.5331,1.5331,0.4368,0.6514 wing_area = 192.60000 wing_span = 34.30000 wing_root_chord = 7.74000 wing_dihedral = 1.10000 wing_incidence = 0.00000 wing_twist = 0.00000 oswald_efficiency_factor = 0.84000 wing_winglets_flag = 0 wing_sweep = 3.00000 wing_pos_apex_lon = 1.6585 wing_pos_apex_vert = -2.00000 htail_area = 32.50000 htail_span = 11.50000 htail_pos_lon = -13.50000 htail_pos_vert = 0.00000 htail_incidence = -0.125 htail_sweep = 9.00000 vtail_area = 26.00000 vtail_span = 5.03000 vtail_sweep = 12.00000 vtail_pos_lon = -14.00000 vtail_pos_vert = 0.85000 elevator_area = 6.80000 aileron_area = 6.60000 rudder_area = 6.20000 elevator_up_limit = 25.00000 elevator_down_limit = 18.00000 aileron_up_limit = 25.00000 aileron_down_limit = 12.50000 rudder_limit = 16.00000 elevator_trim_limit = 18.0000 spoiler_limit = 43.00000 aileron_to_spoileron_gain = 0.00000 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 0.00000 min_flaps_for_spoilerons = 0.00000 spoilerons_available = 0 auto_spoiler_available=1 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=9.690171 positive_g_limit_flaps_down=4.273504 negative_g_limit_flaps_up=-4.310897 negative_g_limit_flaps_down=-2.534188 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 2, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 [flight_tuning] cruise_lift_scalar =1.00000 pitch_stability =1.00000 roll_stability =1.00000 yaw_stability =1.00000 parasite_drag_scalar= 1.0000 induced_drag_scalar = 1.0000 elevator_effectiveness=1.00000 aileron_effectiveness =1.00000 rudder_effectiveness =1.00000 elevator_trim_effectiveness=1.00000 aileron_trim_effectiveness =1.00000 rudder_trim_effectiveness =1.00000 hi_alpha_on_roll =1.00000 hi_alpha_on_yaw =1.00000 p_factor_on_yaw =1.00000 torque_on_roll =1.00000 gyro_precession_on_roll=1.00000 gyro_precession_on_yaw =1.00000 [propeller] thrust_scalar=1.00000 propeller_type=0 propeller_diameter=9.5 propeller_blades=4 propeller_moi=54 beta_max=45.0000 // full power beta_min=9.5000 // park min_gov_rpm=24000.00000 prop_tc=0.00800 gear_reduction_ratio=16.0000 fixed_pitch_beta=0.00000 low_speed_theory_limit=65.00000 //eq.Vrot prop_sync_available=0 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=700.00000 beta_feather=79.80000 power_absorbed_cf=0.90000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.00000 minimum_reverse_beta=0.0000 [TurbineEngineData] fuel_flow_gain=0.0120 inlet_area=1.02000 rated_N2_rpm=33000.00000 static_thrust=192.0000 //dont change reverser_available=0 afterburner_available=0 [turboprop_engine] power_scalar=1.00000 maximum_torque=3500 //lim M=0.6 [pitot_static] vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [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=1,0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [Reference Speeds] flaps_up_stall_speed=57.5 //c.air full_flaps_stall_speed=48.6 cruise_speed=280.00000 max_indicated_speed=360.00000 max_mach=0.54300 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=900 autothrottle_available=0 max_pitch=8 max_pitch_acceleration=1 max_pitch_velocity_lo_alt=2 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000 max_pitch_velocity_hi_alt_breakpoint=28000 max_bank=25 max_bank_acceleration=1.8 max_bank_velocity=3 max_throttle_rate=0.1 nav_proportional_control=9 nav_integrator_control=0.25 nav_derivative_control=0 nav_integrator_boundary=2.5 nav_derivative_boundary=0 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0 gs_integrator_boundary=0.7 gs_derivative_boundary=0 yaw_damper_gain =1 pitch_takeoff_ga=8 default_pitch_mode=0 default_bank_mode=0 autothrottle_arming_required=0 autothrottle_takeoff_ga=1 autothrottle_max_rpm=80 use_no_default_bank=1 use_no_default_pitch=1 [stall_warning] type=1 stick_shaker=1 [gear_warning_system] gear_warning_available =1 pct_throttle_limit =0.10000 flap_limit_idle =18.75000 flap_limit_power =16.00000 [brakes] parking_brake =1.05 toe_brakes_scale =0.98000 auto_brakes=0 hydraulic_system_scalar=0.51000 differential_braking_scale=0.00000 [hydraulic_system] normal_pressure =3000.00000 electric_pumps = 0 //no electric pumps engine_map = 1,0,0,0 //pumps on Eng1 [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 [Flaps.0] type= 1 system_type=0 span-outboard= 0.526 extending-time= 11 damaging-speed=240.0 blowout-speed=260.0 flaps-position.0=0.00 flaps-position.1=15.00 flaps-position.2=30.00 lift_scalar= 0.5200 //dont change drag_scalar= 1.0000 pitch_scalar=0.985 [GPWS] max_warning_height=250 sink_rate_fpm=-1200 excessive_sink_rate_fpm=-1500 climbout_sink_rate_fpm=-100 flap_and_gear_sink_rate_fpm=-150 [AirWrench] Aircraft_Length=28.98000 Vmax_sl=379.75707 Vmax_ca=384.70542 V_rc=230.50103 Climb_Rate=2500.20000 Climb_Weight=3096.00000 Max_gforce=9.50000 Emergency_hp=180.00000 VSI_Weight=3416.00000 static_margin=0.09500 nose_position_lon=10.24000 ActualIncidence=1.50000 ActualTwist=-3.00000 ActualTailIncidence=-0.01000 Aircraft_Type=7 FlowCorrection=1.00000 ReheatCutoff=1.20000 OptimumMach=0.60000 Power_Calibration=1.00000 IdleRPM=0.00000 piston_research=0.00000 JetAltitude=0.00000 turboprop_critical_altitude=19964.00000 target_roll_Vopt=345.69401 target_roll_rate=53.10000 pitch_damping=1.10000 yaw_damping=0.90000 weathervane=1.00000 elevator_scalar=1.00000 aileron_scalar=1.00000 rudder_scalar=1.00000 dihedral_scalar=1.00000 sideslip_scalar=1.00000 prop_yaw_damping_scalar=1.00000 Elevator_FF=130.00000 Aileron_FF=-150.00000 Roll_Response=25.00000 Adverse_Yaw=100.00000 Control_Response=97.00000 V_Max_Control=379.75707 V_Zero_Control=759.51414 V_Max_RdrControl=379.75707 V_Zero_RdrControl=759.51414 Spin_Stability=98.00000 Roll_Off=0.00000 glide_ratio=14.12337 CritAoA=12.00000 ClAoA_k0=0.10000 ClAoA_k1=0.10000 ClAoA_k2=0.15000 ClAoA_k3=0.15000 Elevator_Propwash=1.10000 Rudder_Propwash=1.00000 afterburner_thrust=875.00000 prop_design_altitude=5000.00000 prop_material_type=1 protect_airfile=0 spoiler_type=1 spoiler_cd=0.06010 spoiler_cl=-0.02200 spoiler_cm=-0.00220 auto_flaps_enabled=0 flaps_type=1 flaps_cd_scalar=0.30700 flaps_cm_scalar=0.00500 vfe_enabled=0 gear_cd_scalar=0.38000 gear_cm_scalar=-0.00000 critical_mach_number=0.80000 max_mach_cd0=60 direct_edit_drag=0 cylinder_head_temperature=501.00000 exhaust_gas_temperature=826.00000 fuel_pressure=16.50000 oil_pressure=66.00000 oil_temperature=141.00000 radiator_temperature=211.00000 lo_rpm_friction=1.00000 hi_rpm_friction=1.00000 exhaust_pressure_ratio=1.40000 interstage_turbine_temperature=1682.00000 knots_flag=1 cfs1_flag=0 cfs2_flag=0 AI_flag=0 edit_tp_torque=1 direct_edit_mach=0 direct_edit_2dtab=0 fixed_wing_pos=1 range_est_alt=0.00000 range_est_rpm=0.00000 range_est_mp=29.92000 range_est_fuel=129.40000 contact_light_flags=0 AirWrenchVersion=1.01.64 [Views] eyepoint=0.558657,0.000000,3.444919 //eyepoint=-0.758657,0.000000,3.344919 [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