[fltsim.0] title=PC9 RTAF sim=PC9 model=base panel= sound= texture=RTAF checklists= description=The PC-9 is a Swiss designed, two-seat turboprop trainer. atc_id=19 ui_manufacturer=Pilatus ui_type=PC9 ui_variation=Royal Thai Air Force atc_airline=Air Force atc_flight_number=19 [fltsim.1] title=PC9 Factory sim=PC9 model=pc9m panel= sound= texture=PIL checklists= description=The PC-9 is a Swiss designed, two-seat turboprop trainer. atc_id=HBHPJ ui_manufacturer=Pilatus ui_type=PC9M ui_variation=Factory Demonstrator [fltsim.2] title=PC9 Swiss sim=PC9 model=tank panel= sound= texture=SW checklists= description=The PC-9 is a Swiss designed, two-seat turboprop trainer. atc_id=C401 ui_manufacturer=Pilatus ui_type=PC9 ui_variation=Swiss Air Force [fltsim.3] title=PC9 Roulettes sim=PC9 model=aus panel= sound= texture=ROUL checklists= description=The PC-9 is a Swiss designed, two-seat turboprop trainer. atc_id=063 ui_manufacturer=Pilatus ui_type=PC9/A ui_variation=RAAF Roulettes atc_airline=Air Force atc_flight_number=063 [fltsim.4] title=PC9 2FTS sim=PC9 model=aus panel= sound= texture=2FTS checklists= description=The PC-9 is a Swiss designed, two-seat turboprop trainer. atc_id=058 ui_manufacturer=Pilatus ui_type=PC9/A ui_variation=RAAF 2FTS atc_airline=Air Force atc_flight_number=058 [fltsim.5] title=PC9 RAAF sim=PC9 model=aus2 panel= sound= texture=RAAF checklists= description=The PC-9 is a Swiss designed, two-seat turboprop trainer. atc_id=032 ui_manufacturer=Pilatus ui_type=PC9/A ui_variation=RAAF Gray scheme atc_airline=Air Force atc_flight_number=032 [fltsim.6] title=PC9 Slovenia sim=PC9 model=pc9m panel= sound= texture=SAF checklists= description=The PC-9 is a Swiss designed, two-seat turboprop trainer. atc_id=66 ui_manufacturer=Pilatus ui_type=PC9M ui_variation=Slovenia atc_airline=Air Force atc_flight_number=66 [fltsim.7] title=PC9 D-EFMT sim=PC9 model=base panel= sound= texture=DEFMT checklists= description=The PC-9 is a Swiss designed, two-seat turboprop trainer. atc_id=DEFMT atc_flight_number=92 ui_manufacturer=Pilatus ui_type=PC9 ui_variation=German Trainer [fltsim.8] title=PC9 Croatia sim=PC9 model=pc9m panel= sound= texture=CAF checklists= description=The PC-9 is a Swiss designed, two-seat turboprop trainer. atc_id=064 atc_flight_number=064 atc_airline=Air Force ui_manufacturer=Pilatus ui_type=PC9M ui_variation=Croatia Air Force [General] atc_type=PILATUS atc_model=PC9 performance=Max Level Speed : 320 kts \nInitial ROC: 4,000 ft\/min\nMax weight: 7,076lb.\nPowerplant: PT6A-62 950 SHP. [WEIGHT_AND_BALANCE] max_gross_weight = 7054.000 empty_weight = 3715.000 reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=200, 0.0, 0.0, 1.7 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=200, -3.4, 0.0, 2.3 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) empty_weight_roll_MOI=2165 empty_weight_pitch_MOI=4997 empty_weight_yaw_MOI=5257 empty_weight_coupled_MOI=0.000000 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=.80 induced_drag_scalar=1.0 elevator_effectiveness=.8 aileron_effectiveness=1.5 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [exits] number_of_exits=2 exit_rate.0=0.6 exit_rate.1=0.4 [GeneralEngineData] engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=10.7, 0.0, 0.7 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=8.0 //Propeller Diameter, (feet) propeller_blades=4 //Number of propeller blades propeller_moi=15.1 //Propeller moment of inertia beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=5.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=25520 //Miminum governed RPM prop_tc=0.004 //Prop time-constant gear_reduction_ratio=16.5 //Propeller gear reduction ratio fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=700 //Minimum RPM for prop feathering beta_feather=79.3 //Feathering pitch angle (degrees) power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain=0.011 //Gain on fuel flow inlet_area=1.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=33000 //RPM, second stage compressor rated value static_thrust=158 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar=1.0 //Scalar on Turboprop power maximum_torque=2900 //Maximum torque available (ft-lbs) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0=1, 6.6, 0.00, -4.45, 2500, 0, 0.596, 45, .2, 2, 0.9, 4, 4, 0, 180, 225 point.1=1, -1.67, -3.8, -4.4, 2500, 1, 0.596, 0.0, .2, 2.5, 0.9, 4, 4, 2, 180, 225 point.2=1, -1.67, 3.8, -4.4, 2500, 2, 0.596, 0.0, .2, 2.5, 0.9, 4, 4, 3, 180, 225 point.3=2, -1.2, 16.5, 0, 1500, 0, 0, 0.0, 0, 0, 0, 0, 0, 6, 0.0, 0.0 point.4=2, -1.2, -16.5, 0, 1500, 0, 0, 0.0, 0, 0, 0, 0, 0, 5, 0.0, 0.0 point.5=2, -1.2, 0, -1.8, 1500, 0, 0, 0.0, 0, 0, 0, 0, 0, 4, 0.0, 0.0 point.6=2, -16.7, 0, -1.1, 1500, 0, 0, 0.0, 0, 0, 0, 0, 0, 9, 0.0, 0.0 point.7=2, 9.5, 0, -1, 1500, 0, 0, 0.0, 0, 0, 0, 0, 0, 4, 0.0, 0.0 static_pitch=1 static_cg_height=4.3 [Views] eyepoint=0, 0, 2.8 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=4 // seconds flaps-position.0=0 // degrees flaps-position.1=20 // degrees flaps-position.2=40 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS [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 [smokesystem] smoke.0=0, -25, 0, fx_smoke_r [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=150, 250 aileron=150, 250 rudder=150, 250 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.9, -16.4, 0.25, fx_navred , light.1=3, 0.9, 16.4, 0.25, fx_navgre , light.3=2, 0.605, -16.7, .33, fx_strobe , light.4=2, 0.605, 16.7, .33, fx_strobe , light.5=1, -6.65, 0.00, 3.1, fx_beacon , light.7=4, .075, 0.00, 1.60, fx_vclight, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain=0.0, -8.9, -0.6, 70.6, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=0.0, 8.9, -0.6, 70.6, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area=175.3 //Square feet wing_span=33.5 //Feet wing_root_chord=5.16 //Feet wing_dihedral=7.0 //Degrees wing_incidence=1.0 //Degrees wing_twist=-2. //Degrees oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=3.5 //Degrees, wing leading edge wing_pos_apex_lon=1.29 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=-1.5 //Feet, vertical distance from reference point, positive going up htail_area=19.38 //Square feet htail_span=11 //Feet htail_pos_lon=-16.3 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.5 //Feet, vertical distance from reference point, positive going up htail_incidence=-.5 //Degrees htail_sweep=13.0 //Degrees, horizontal tail leading edge vtail_area=9.26 //Square feet vtail_span=3.7 //Feet, tip to body vtail_sweep=15.0 //Degrees, vertical tail leading edge vtail_pos_lon=-13.7 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=1.5 //Feet, vertical distance from reference point, positive going up elevator_area=17.22 //Square feet aileron_area=16.9 //Square feet rudder_area=9.69 //Square feet elevator_up_limit=18.5 //Degrees elevator_down_limit=16 //Degrees aileron_up_limit=20.0 //Degrees aileron_down_limit=11.0 //Degrees rudder_limit=24.0 //Degrees elevator_trim_limit=15.0 //Degrees spoiler_limit=80.0 //Degrees spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=0 //Aileron to spoileron gain min_ailerons_for_spoilerons=0 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=96.0 //Knots True (KTAS) full_flaps_stall_speed=76.8 //Knots True (KTAS) cruise_speed=300.0 //Knots True (KTAS) [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=2000.0 autothrottle_available=0 pitch_takeoff_ga=15.000000 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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