[fltsim.0] title=PC-12_Medical sim=PC-12_Medical model= panel= sound= texture= prop_anim_ratio=1.3 kb_checklists= ui_manufacturer=Pilatus ui_type=PC12 atc_id_color=0000000000 visual_damage=0 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. 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=N623MS ui_variation=Medical 1 [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 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 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 empty_weight = 5800 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 28000 empty_weight_roll_MOI = 24000 empty_weight_yaw_MOI = 29000 empty_weight_coupled_MOI = 0 max_number_of_stations = 1 station_load.0 = 200, 4.11, 0, 0.05 station_load.1 = 1200, 0, 0, 0 [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 = 1.000000 engine.0 = 15.333333, 0, 0, [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, -4.5, -2, 200, 0 RightMain = -2, 4.5, -2, 200, 0 [contact_points] static_pitch = 0 static_cg_height = 5.9 max_number_of_points = 7 point.0 = 1, 8.4959, 0, -6.123, 2181.102, 0, 0.8, 70, 0.447, 2.5, 0.9, 10, 12, 0, 200, 250 point.1 = 1, -2.4649, -7.5, -6.2, 1574.803, 1, 1.1, 0, 0.507, 2.5, 0.95, 10, 12, 2, 0, 0 point.2 = 1, -2.4649, 7.5, -6.2, 1574.803, 2, 1.1, 0, 0.507, 2.5, 0.95, 10, 12, 3, 0, 0 point.3 = 2, -1.3329, -25.8512, -0.0996, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -1.3329, 25.8512, -0.0996, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -26.0425, 0, -0.0697, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 14.0031, 0, -1.9375, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 [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 = 350.000000 wing_span = 57.166667 wing_root_chord = 5.416667 wing_dihedral = 5.998535 wing_incidence = 0.999756 wing_twist = -1.499634 oswald_efficiency_factor = 0.75 wing_winglets_flag = 1 wing_sweep = 0.000000 wing_pos_apex_lon = 0.000000 wing_pos_apex_vert = 0.000000 htail_area = 67.000000 htail_span = 17.166667 htail_pos_lon = -24.583333 htail_pos_vert = 0.000000 htail_incidence = 0.499878 htail_sweep = 0.000000 vtail_area = 42.000000 vtail_span = 7.389181 vtail_sweep = 0.000000 vtail_pos_lon = -20.500000 vtail_pos_vert = 4.083333 elevator_area = 16.985000 aileron_area = 13.477000 rudder_area = 7.275000 elevator_up_limit = 16.999658 elevator_down_limit = 15.498508 aileron_up_limit = 18.002334 aileron_down_limit = 18.002334 rudder_limit = 30.000070 elevator_trim_limit = 15.000035 spoiler_limit = 59.988681 aileron_to_spoileron_gain = 0.000000 min_ailerons_for_spoilerons = 0.000000 min_flaps_for_spoilerons = 0.000000 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 electric_always_available = 0 [Flaps.0] type=1 span-outboard=0.700000 extending-time=5.000000 system_type=0 lift_scalar=0.9 drag_scalar=1.2 pitch_scalar=0.3 flaps-position.0=0.000000,0.000000 flaps-position.1=15.330818,0.000000 flaps-position.2=30.661636,0.000000 flaps-position.3=45.992454,0.000000 [TurbineEngineData] fuel_flow_gain=0.011000 inlet_area=1.000000 rated_N2_rpm=29920.000000 static_thrust=180.000000 afterburner_available=0 [propeller] thrust_scalar=1.180 propeller_type=0 propeller_diameter=8.8 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=3270.000000 [Reference Speeds] flaps_up_stall_speed=70.000000 full_flaps_stall_speed=65.800000 cruise_speed=234.253499
