[fltsim.0] title=Piper Arrow-III panel 4x3 U.S. sim=Piper Arrow-III-T model= panel=4x3 sound= texture=us kb_checklists=Piper Arrow-III_check kb_reference=Piper Arrow-III_ref atc_id=N1927H ui_manufacturer=Piper ui_type=Arrow-III-T ui_variation=panel 4x3 U.S. description=Flight dynamics derived from FS2004 Mooney Bravo, adapted by Rien Cornelissen to match Arrow-IV flight characteristics\n\n\n atc_heavy=0 atc_airline= atc_flight_number= [fltsim.1] title=Piper Arrow-III panel 16x9 U.S. sim=Piper Arrow-III-T model= panel=16x9 sound= texture=us kb_checklists=Piper Arrow-III_check kb_reference=Piper Arrow-III_ref atc_id=N1927H ui_manufacturer=Piper ui_type=Arrow-III-T ui_variation=panel 16x9 U.S. description=Flight dynamics derived from FS2004 Mooney Bravo, adapted by Rien Cornelissen to match Arrow-IIII turbo flight characteristics\n\n\n atc_heavy=0 atc_airline= atc_flight_number= [fltsim.2] title=Piper Arrow-III panel 4x3 U.K. sim=Piper Arrow-III-T model= panel=4x3 sound= texture=uk kb_checklists=Piper Arrow-III_check kb_reference=Piper Arrow-III_ref atc_id=G-BNNX ui_manufacturer=Piper ui_type=Arrow-III-T ui_variation=panel 4x3 U.K. description=Flight dynamics derived from FS2004 Mooney Bravo, adapted by Rien Cornelissen to match Arrow-IV flight characteristics\n\n\n atc_heavy=0 atc_airline= atc_flight_number= [fltsim.3] title=Piper Arrow-III panel 16x9 U.K. sim=Piper Arrow-III-T model= panel=16x9 sound= texture=uk kb_checklists=Piper Arrow-III_check kb_reference=Piper Arrow-III_ref atc_id=G-BNNX ui_manufacturer=Piper ui_type=Arrow-III-T ui_variation=panel 16x9 U.K. description=Flight dynamics derived from FS2004 Mooney Bravo, adapted by Rien Cornelissen to match Arrow-IIII turbo flight characteristics\n\n\n atc_heavy=0 atc_airline= atc_flight_number= [General] performance=Engine 200 hp at 2,575 RPM, constant speed prop\nMaximum Speed at MSL 140 kts\n75% Power Cruise 138 kts at 6,600 ft\nMax. Rate of Climb 940 ft\/min at MSL, 90 kts,2900 lbs\nMaximum Range\t 1100 nm\nService Ceiling 20,000 ft\nFuel Capacity\t 72 U.S gal\nEmpty Weight 1809 lbs \nMax Gross Weight\t 2900 lbs\nSeating\t\t 4\n atc_type=Arrow atc_model=P28RT Category=airplane [WEIGHT_AND_BALANCE] empty_weight= 1807 max_gross_weight= 2900.0 reference_datum_position= 4.0, 0.0, 0.0 empty_weight_CG_position= -4.0, 0.0, 0.0 max_number_of_stations= 5 station_load.0= 170.0, -4.350, -0.800, -0.045 station_load.1= 170.0, -4.350, 0.800, -0.045 station_load.2= 0.0, -6.600, -0.800, -0.045 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3= 0.0, -6.600, 0.800, -0.045 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4= 0.0, -9.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI= 1400 empty_weight_roll_MOI= 1137 empty_weight_yaw_MOI= 2360 empty_weight_coupled_MOI= 0.0 [flight_tuning] cruise_lift_scalar= 1.0 parasite_drag_scalar= 1.0 induced_drag_scalar= 1.0 elevator_effectiveness= 0.7 aileron_effectiveness= 1.0 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= 0.5 [Flaps.0] type= 1 span-outboard= 0.5 extending-time= 0.2 system_type= 0 damaging-speed= 0.0 blowout-speed= 0.0 lift_scalar= 1.0 drag_scalar= 1.0 pitch_scalar= 1.0 flaps-position.0= 0.0, 0.0 flaps-position.1= 12.7, 0.0 flaps-position.2= 25.3, 0.0 flaps-position.3= 38.0, 0.0 [piston_engine] power_scalar=1.0 cylinder_displacement= 63 compression_ratio= 7.5 number_of_cylinders=6 max_rated_rpm= 2575 max_rated_hp= 200 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 1 turbocharged= 1 max_design_mp= 47 min_design_mp= 1 critical_altitude= 20000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.0 emergency_boost_gain_offset= 0.0 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.2 idle_rpm_mechanical_efficiency_scalar=1.0 max_rpm_friction_scalar=1.0 idle_rpm_friction_scalar=0.7 [propeller] thrust_scalar=1.0 propeller_type= 0 propeller_diameter= 6.1 propeller_blades= 3 propeller_moi= 3 beta_max=38 beta_min= 15 min_gov_rpm= 1100 prop_tc= 0.1 gear_reduction_ratio= 1.0 fixed_pitch_beta= 0 low_speed_theory_limit= 80 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0 beta_feather= 0 power_absorbed_cf= 0 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0 minimum_reverse_beta= 0p [pitot_static] vertical_speed_time_constant= 0.7 pitot_heat=1 [fuel] LeftMain= -5.2, -6.500, 0.850, 36.0, 0.0 RightMain= -5.2, 6.500, 0.850, 36.0, 0.0 fuel_type= 1 number_of_tank_selectors= 1 electric_pump= 1 [airplane_geometry] wing_area= 169.0 wing_span= 35.0 wing_root_chord= 5.3 wing_dihedral= 6.0 wing_incidence= 2.5 wing_twist= -1.5 oswald_efficiency_factor= 0.6 wing_winglets_flag= 0 wing_sweep= 15.0 wing_pos_apex_lon= 5.7 wing_pos_apex_vert= 1.314 htail_area= 39.0 htail_span= 13.0 htail_pos_lon= -19.3 htail_pos_vert= 5.0 htail_incidence= 2.0 htail_sweep= 0.0 vtail_area= 18.0 vtail_span= 4.8 vtail_sweep= 3.0 vtail_pos_lon= -18.5 vtail_pos_vert= 4.5 elevator_area= 35.0 aileron_area= 18.3 rudder_area= 6.7 elevator_up_limit= 28.0 elevator_down_limit= 21.0 aileron_up_limit= 20.0 aileron_down_limit= 15.0 rudder_limit= 24.0 elevator_trim_limit= 19.5 spoiler_limit= 0.0 spoilerons_available= 0 aileron_to_spoileron_gain= 0 min_ailerons_for_spoilerons= 0 min_flaps_for_spoilerons= 0 auto_spoiler_available=0 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-1.500000 negative_g_limit_flaps_down=-1.500000 [contact_points] //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 point.0= 1.0, 1.866, 0.0, -2.89, 3500, 0, 0.500, 22.0, 0.250, 2.5, 0.90, 7.0, 7.0, 0 point.1= 1.0, -5.73, -5.14, -2.7, 3500, 1, 0.517, 0.0, 0.250, 2.5, 0.90, 7.0, 7.0, 2 point.2= 1.0, -5.73, 5.14, -2.7, 3500, 2, 0.517, 0.0, 0.250, 2.5, 0.90, 7.0, 7.0, 3 max_number_of_points= 21 static_pitch= 1.0 static_cg_height= 2.8 gear_system_type= 0 [GeneralEngineData] engine_type= 0 Engine.0= 2.973, 0.800, 0.0 fuel_flow_scalar= 0.80 min_throttle_limit= 0.0 [Reference Speeds] flaps_up_stall_speed= 58.0 full_flaps_stall_speed= 53.0 cruise_speed= 125.0 max_indicated_speed= 190 [keyboard_response] elevator= 100.0, 180.0 aileron= 200.0, 1000.0 rudder= 200.0, 1000.0 [Views] eyepoint= -5.0, -0.82, 2.15 //(feet) longitudinal, lateral, vertical distance from reference datum [autopilot] autopilot_available= 1 flight_director_available= 0 default_vertical_speed= 500 autothrottle_available= 0 pitch_takeoff_ga= 8.0 use_no_default_bank= 0 use_no_default_pitch= 1 default_pitch_mode=0 default_bank_mode= 0 max_pitch= 10.00 max_pitch_acceleration= 1.0 max_pitch_velocity_lo_alt= 2.0 max_pitch_velocity_hi_alt= 1.5 max_pitch_velocity_lo_alt_breakpoint= 20000 max_pitch_velocity_hi_alt_breakpoint= 28000 max_bank= 20.00 max_bank_acceleration= 3.0 max_bank_velocity= 5.0 max_throttle_rate= 0.10 nav_proportional_control= 9.0 nav_integrator_control= 0.25 nav_derivative_control= 0.00 nav_integrator_boundary= 2.5 nav_derivative_boundary= 0.0 gs_proportional_control= 9.5 gs_integrator_control= 0.26 gs_derivative_control= 0.0 gs_integrator_boundary= 0.7 gs_derivative_boundary= 0.0 yaw_damper_gain= 0.0 [direction_indicators] direction_indicator.0= 1, 0 [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, 5 , 17.0 avionics= 1, 5 , 17.0 pitot_heat= 0, 2 , 17.0 additional_system= 0, 2 , 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 [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 //(feet) longitudinal, lateral, vertical distance from reference datum light.0= 2, -5.75, -17.0, 1.0, fx_strobeh light.1= 2, -5.75, 17.0, 1.0, fx_strobeh light.2= 4, -4.26, 0.0, 2.66, fx_vclight light.3= 3, -5.572, -16.831, 0.972, fx_navred3 light.4= 3, -5.572, 16.831, 0.972, fx_navgre3 light.5= 1, -18.20, 0.00, 5.50, fx_beacon light.6= 1, -18.20, 0.00, 5.40, fx_beacon [exits] number_of_exits= 2 exit_rate.0= 0.2 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [brakes] toe_brakes_scale= 1.0 parking_brake= 1 [gear_warning_system] gear_warning_available= 1 pct_throttle_limit= 50 flap_limit_power= 20 flap_limit_idle= 20 [hydraulic_system] normal_pressure= 0.0 [stall_warning] type= 1 stick_shaker=0 [attitude_indicators] attitude_indicator.0= 1 [turn_indicators] turn_indicator.0= 1,0 [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= 00500 gear_bump_right_duration= 250000 ground_bumps_magnitude1= 3250 ground_bumps_angle1= 8900 ground_bumps_intercept1= 5.0 ground_bumps_slope1= 0.48 ground_bumps_magnitude2= 750 ground_bumps_angle2= 9100 ground_bumps_intercept2= 0.075 ground_bumps_slope2= 1.0 crash_magnitude1= 10000 crash_direction1= 01000 crash_magnitude2= 10000 crash_direction2= 9000 crash_period2= 75000 crash_duration2= 25000 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=4.900000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0
