[fltsim.0] title=Pilatus PC-12 sim=PC-12_Combi model= panel= sound= texture= prop_anim_ratio=1.3 kb_checklists= ui_manufacturer=Pilatus ui_type=PC12 atc_id=N1776C ui_variation=Deer Valley Flying Club description=Pilatus aircraft are known for their innovative design, precision engineering, and quality craftmanship. The PC-12 continues this reputation, offering a business aircraft that is Swiss-built and -engineered, and completed with the highest quality materials, finishes, and craftmanship.Integrating a single turboprop engine into an aerodynamically advanced airframe, the Pilatus PC-12 combines excellent economy and reliability with the inherent safety of single-engine turboprop operation. It offers multiple configurations, ranging from executive-level transportation in spacious, pressurized cabin comfort to long-distance delivery of cargo and oversized equipment. The business aircraft also offers some unique special mission capabilites. atc_id_color=0000000000 visual_damage=0 atc_heavy=0 atc_airline= atc_flight_number= [Views] eyepoint=3.67, -1.23, 2.30 //(feet) longitudinal, lateral, vertical distance from reference datum [General] performance=Max Cruise Speed 270 KTAS Max Range (30,000 ft., VFR reserves) 2,261 nm \/ 4,190 km Max Operating Altitude 30,000 ft \/ 9,150 m Cabin Altitude at 25,000 ft. 8,000 ft \/ 2,440 m Takeoff Distance Over 50 ft Obstacle (MTOW)* 2,300 ft \/ 700 m Rate of Climb (MTOW)* 1,680 ft\/min Landing Distance Over 50 ft Obstacle (MTOW)* 1,830 ft \/ 560 m Stall Speed (landing configuration)* 65 KCAS atc_type=PILATUS atc_model=PC12 editable=1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=99.000 pitch_takeoff_ga=8.000 use_no_default_pitch=0 use_no_default_bank=1 [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 [flight_tuning] cruise_lift_scalar=1.0 pitch_stability=1.0 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=0.8 induced_drag_scalar=0.8 elevator_effectiveness=1.000 aileron_effectiveness=1.100 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.400 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [direction_indicators] direction_indicator.0=3,0 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [weight_and_balance] // ACM V2.0 max_gross_weight= 9625.000 empty_weight= 5800.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 empty_weight_pitch_MOI= 28000.000 empty_weight_roll_MOI= 24000.000 empty_weight_yaw_MOI= 29000.000 empty_weight_coupled_MOI= 0.000 max_number_of_stations=1 station_load.0= 200.000, 4.110, 0.000, 0.050 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=1, -29.80, 0, 8.59, fx_beaconbS3 light.1=1, -2.81, 0, -2.7, fx_beaconbS3 light.2=3, -31.00, 0, 8.04, fx_navwhi light.3=3, -0.86, -25.80, 0.45, fx_navred light.4=2, -4.55, -27.08, 2.21, fx_strobe light.5=2, -4.55, 27.08, 2.21, fx_strobe light.6=3, -1.29, 26.24, 0.69, fx_navgre light.7=4, 3.03, 0, 2.71, fx_vclight light.8=4, -5.40, 0, 3.10, fx_vclight [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type= 5 fuel_flow_scalar= 1.000 engine.0= 15.333, 0.000, 0.000 [effects] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 number_of_tank_selectors=1 LeftMain= -2.000, -4.500, -2.000, 200.000, 0.000 RightMain= -2.000, 4.500, -2.000, 200.000, 0.000 [contact_points] static_pitch= 0.000 static_cg_height= 5.900 max_number_of_points=7 point.0= 1.000, 8.496, 0.000, -6.123, 2181.102, 0.000, 0.800, 70.000, 0.447, 2.500, 0.900, 10.000, 12.000, 0.000, 200.000, 712.383 point.1= 1.000, -2.465, -7.500, -6.200, 1574.803, 1.000, 1.100, 0.000, 0.507, 2.500, 0.950, 10.000, 12.000, 2.000, 0.000, 0.000 point.2= 1.000, -2.465, 7.500, -6.200, 1574.803, 2.000, 1.100, 0.000, 0.507, 2.500, 0.950, 10.000, 12.000, 3.000, 0.000, 0.000 point.3= 2.000, -1.333, -25.851, -0.100, 787.402, 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, -1.333, 25.851, -0.100, 787.402, 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, -26.043, 0.000, -0.070, 787.402, 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, 14.003, 0.000, -1.938, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 [keyboard_response] elevator=150.000000, 250.000000 aileron=150.000000, 250.000000 rudder=150.000000, 250.000000 [forcefeedback] [airplane_geometry] //ACM_AREAW1// 0,0,0,1.6510,0.9678,0.9678,0,1.5684,1.9358,1.9358 //ACM_AREAW2// 0,1.4859,2.9040,2.9040,0,1.4033,3.8719,3.8719,0,1.3207 //ACM_AREAW3// 4.8400,4.8400,0,1.2381,5.8081,5.8081,0,1.1555,6.7761,6.7761 //ACM_AREAW4// 0,1.0729,7.7441,7.7441,0,0.9904,8.7122,8.7122,0,0.9078 //ACM_AREAH1// 0,0,0,1.7439,0.2906,0.2906,0,1.6569,0.5813,0.5813 //ACM_AREAH2// 0,1.5697,0.8719,0.8719,0,1.4823,1.1627,1.1627,0,1.3953 //ACM_AREAH3// 1.4534,1.4534,0,1.3079,1.7439,1.7439,0,1.2208,2.0348,2.0348 //ACM_AREAH4// 0,1.1334,2.3255,2.3255,0,1.0463,2.6161,2.6161,0,0.9592 //ACM_AREAV1// 0,0,0,2.2520,0.2502,0.2502,0,2.0720,0.5004,0.5004 //ACM_AREAV2// 0,1.8918,0.7505,0.7505,0,1.7115,1.0009,1.0009,0,1.5313 //ACM_AREAV3// 1.2510,1.2510,0,1.3513,1.5012,1.5012,0,1.1711,1.7517,1.7517 //ACM_AREAV4// 0,0.9908,2.0018,2.0018,0,0.8108,2.2520,2.2520,0,0.6305 //ACM_CAREAW1// 4.3561,4.3561,0.8255,1.1555,4.8400,4.8400,0.8255,1.1390,5.3241,5.3241 //ACM_CAREAW2// 0.8255,1.1224,5.8081,5.8081,0.8255,1.1059,6.2919,6.2919,0.8255,1.0894 //ACM_CAREAW3// 6.7761,6.7761,0.8255,1.0729,7.2600,7.2600,0.8255,1.0564,7.7441,7.7441 //ACM_CAREAW4// 0.8255,1.0399,8.2279,8.2279,0.8255,1.0234,8.7122,8.7122,0.8255,1.0069 //ACM_CAREAH1// 0,0,0.8719,1.7439,0.2906,0.2906,0.8719,1.7005,0.5813,0.5813 //ACM_CAREAH2// 0.8719,1.6569,0.8719,0.8719,0.8719,1.6131,1.1627,1.1627,0.8719,1.5697 //ACM_CAREAH3// 1.4534,1.4534,0.8719,1.5261,1.7439,1.7439,0.8719,1.4823,2.0348,2.0348 //ACM_CAREAH4// 0.8719,1.4387,2.3255,2.3255,0.8719,1.3953,2.6161,2.6161,0.8719,1.3516 //ACM_CAREAV1// 0,0,0.5630,1.6891,0.2502,0.2502,0.5630,1.5988,0.5004,0.5004 //ACM_CAREAV2// 0.5630,1.5089,0.7505,0.7505,0.5630,1.4189,1.0009,1.0009,0.5630,1.3286 //ACM_CAREAV3// 1.2510,1.2510,0.5630,1.2387,1.5012,1.5012,0.5630,1.1484,1.7517,1.7517 //ACM_CAREAV4// 0.5630,1.0585,2.0018,2.0018,0.5630,0.9684,2.2520,2.2520,0.5630,0.8783 wing_area= 350.000 wing_span= 57.167 wing_root_chord= 5.417 wing_dihedral= 5.999 wing_incidence= 1.000 wing_twist= -1.500 oswald_efficiency_factor= 0.750 wing_winglets_flag= 1 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 67.000 htail_span= 17.167 htail_pos_lon= -24.583 htail_pos_vert= 0.000 htail_incidence= 0.500 htail_sweep= 0.000 vtail_area= 42.000 vtail_span= 7.389 vtail_sweep= 0.000 vtail_pos_lon= -20.500 vtail_pos_vert= 4.083 elevator_area= 16.985 aileron_area= 13.477 rudder_area= 7.275 elevator_up_limit= 17.000 elevator_down_limit= 15.499 aileron_up_limit= 18.002 aileron_down_limit= 18.002 rudder_limit= 30.000 elevator_trim_limit= 15.000 spoiler_limit= 59.989 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 spoilerons_available= 0 [electrical] max_battery_voltage=24 generator_alternator_voltage=28 max_generator_alternator_amps=60 electric_always_available=0 [TurbineEngineData] fuel_flow_gain= 0.011 inlet_area= 1.000 rated_N2_rpm= 29920.000 static_thrust= 180.000 afterburner_available= 0 [propeller] thrust_scalar=1.180 propeller_type= 0 propeller_diameter= 8.800 propeller_blades= 4 propeller_moi= 19.000 beta_max= 45.000 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 [turboprop_engine] maximum_torque= 3270.000 [Reference Speeds] flaps_up_stall_speed= 70.000 full_flaps_stall_speed= 65.800 cruise_speed= 234.253 [Flaps.0] type= 1 span-outboard= 0.700 extending-time= 5.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 0.900 drag_scalar= 1.200 pitch_scalar= 0.300 flaps-position.0= 0.000, 0.000 flaps-position.1= 15.331, 0.000 flaps-position.2= 30.662, 0.000 flaps-position.3= 45.992, 0.000