//Aero Commander 520 for FS2002/FS9. Model designed and animated in GMAX by Milton Shupe - October-February 2003. Flight Dynamics by Milton Shupe. Revised for FS9 8/03. // AC520 TDC 6A1 [fltsim.0] title=AC520 Factory Blue sim=AC520 model= panel=Classic sound= texture=fac520 description=Beginning in 1952, Aero Design & Engineering Company rolled out the first model 520. The 520 proved to be a fantastic design which was vastly ahead of other General Aviation products of the time. 150 units were built between 1951 & 1954. Power : Lycoming GO-435-C2B - 260hp kb_checklists=AC520_Check kb_reference=AC520_Ref ui_manufacturer=Aero Design & Engineering ui_type=AC52 ui_variation=Factory Blue atc_heavy=0 atc_id=CF-DBB atc_airline=Private atc_flight_number=1946 [fltsim.1] title=AC520 Pegasus sim=AC520 model= panel=Classic sound= texture=peg520 description=Serial 520-46 reg# N2649 kb_checklists=AC520_Check kb_reference=AC520_Ref ui_manufacturer=Aero Design & Engineering ui_type=AC52 ui_variation=MobilOilPegasus atc_heavy=0 atc_id=N2649 atc_airline=Private atc_flight_number=1946 [fltsim.2] title=AC520 N2609 sim=AC520 model= panel=Classic sound= texture=n2609 description=N2609B kb_checklists=AC520_Check kb_reference=AC520_Ref ui_manufacturer=Aero Design & Engineering ui_type=AC52 ui_variation=N2609 atc_heavy=0 atc_id=N2609B atc_airline=Private atc_flight_number=1946 [fltsim.3] title=AC520 Texas sim=AC520 model= panel=Classic sound= texture=Texas description=Beginning in 1952, Aero Design & Engineering Company rolled out the first model 520. The 520 proved to be a fantastic design which was vastly ahead of other General Aviation products of the time. 150 units were built between 1951 & 1954. Power : Lycoming GO-435-C2B - 260hp kb_checklists=AC520_Check kb_reference=AC520_Ref ui_manufacturer=Aero Design & Engineering ui_type=AC52 ui_variation=Texas atc_heavy=0 atc_id=N614MS atc_airline=Private atc_flight_number=1946 [fltsim.4] title=AC520 Factory Green sim=AC520 model= panel=Classic sound= texture=factA description=Beginning in 1952, Aero Design & Engineering Company rolled out the first model 520. The 520 proved to be a fantastic design which was vastly ahead of other General Aviation products of the time. 150 units were built between 1951 & 1954. Power : Lycoming GO-435-C2B - 260hp kb_checklists=AC520_Check kb_reference=AC520_Ref ui_manufacturer=Aero Design & Engineering ui_type=AC52 ui_variation=Factory Green atc_heavy=0 atc_id=N1946 atc_airline=Private atc_flight_number=1946 [General] //Range, maximum cruising power at 60% (2600rpm@22"MP), is 999nm (1150sm/1851km)with 30 minutes reserve //performance=Hi speed cruise: 197 mph/171 kts@10,000'\nVR: 82 mph - Best climb: 140 mph\nRate of climb (sea level): 1700 fpm\ //nStalls (mph) - clean : 67\s dirty : 40\nPower: 2x 260 hp Lycoming GO-435-C2 \nApproach speed: 98 mph\ //nService ceiling: 24000 ft atc_type=AERO atc_model=AC520 editable=0 performance=Hi speed cruise: 197 mph\nBest rate of climb (sea level): 140 mph\nStalls (mph) - clean : 67\s dirty : 40\nPower: 2x 260 hp Lycoming GO-435-C2B\nApproach speed: 98 mph\nService ceiling: 24000 ft\nVR: 76 mph - Best climb: 140 mph\nOEI service ceiling: 8700 ft [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=20 station_load.0="170.000, 5.500, -1.100, -1.000, pilot" station_load.1="170.000, 5.500, 1.100, -1.000, copilot" station_load.2="0.000, 4.200, -1.100, -1.000, mid-pass" station_load.3="0.000, 4.200, 1.100, -1.000, mid-pass" station_load.4="170.000, 0.000, -1.100, -1.000, passengers" station_load.5="170.000, 0.000, 1.100, -1.000, passengers" station_load.6="25.000,-1.500, -1.100, -0.000, cargo" station_load.7="25.000,-1.500, 1.100, -0.000, cargo" empty_weight = 3612 empty_weight_roll_MOI = 8892 empty_weight_pitch_MOI = 3761 empty_weight_yaw_MOI = 10671 empty_weight_coupled_MOI=0.000 max_gross_weight=5700.000 [exits] number_of_exits=2 exit_rate.0=0.8 ;Percent per second exit_rate.1=0.8 ;Percent per second [fuel] //Fuel: 80/87 or 91/96 minimum grade aviation gasoline //13.5 U.S. gallons per engine per hour at 2,600 r.p.m. //Fuel capacity: 150 U.S. gallons (568 litres) total; [5 inter-connected tanks]; 145 U.S. gallons (549 litres) usable LeftMain=-1.000, -3.000, 1.000, 30.000, 0.000 RightMain=-1.000, 3.000, 1.000, 30.000, 0.000 Center1=-2.000, 0.000, 1.000, 90.000, 5.000 fuel_type=1.000000 number_of_tank_selectors=2 electric_pump=1 [airplane_geometry] wing_area=242.500 wing_span=44.058 wing_root_chord=6.25 wing_dihedral=4.000 wing_incidence=3.000 wing_twist=-4.000 oswald_efficiency_factor=0.8919 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=2.08 wing_pos_apex_vert=1.0 htail_area=33 htail_span=16.9 htail_pos_lon=-19 htail_pos_vert=0 htail_incidence=1 htail_sweep=0 vtail_area=20.6 vtail_span=8.0 vtail_sweep=0 vtail_pos_lon=-19 vtail_pos_vert=2.0 elevator_area=20.5 aileron_area=22.4 rudder_area=13.4 elevator_up_limit=30.002 elevator_down_limit=10.614 aileron_up_limit=23.614 aileron_down_limit=15.614 rudder_limit=15.001 elevator_trim_limit=25.002 spoiler_limit=59.989 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 [contact_points] point.0=1.000, 12.683, 0.000, -5.723 1574.803, 0.000, 0.667, 20.000, 0.200, 4.700, 0.800, 5.000, 5.000, 0.000, 0.000, 0.000 point.1=1.000, -0.630, -6.166, -5.643, 1574.803, 1.000, 0.917, 0.000, 0.500, 2.000, 0.800, 5.000, 5.000, 2.000, 0.000, 0.000 point.2=1.000, -0.630, 6.166, -5.643, 1574.803, 2.000, 0.917, 0.000, 0.500, 2.000, 0.800, 5.000, 5.000, 3.000, 0.000, 0.000 point.3=2.000, 0.483, -22.100, 4.583, 1574.803, 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, 0.483, 22.100, 4.583, 1574.803, 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, -24.433, 0.000, 2.917, 1574.803, 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, 15.567, 0.000, 2.917, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=1.150 static_cg_height=5.368 gear_system_type=1 [GeneralEngineData] engine_type=0 Engine.0=4.000, -6.333, -0.100 Engine.1=4.000, 6.333, -0.100 fuel_flow_scalar=0.88 min_throttle_limit=0.000000 [piston_engine] //Lycoming GO-435-C2B; Serial numbers 21, 23, & 39 through 150 (114 aircraft) //Oil capacity: 6.0 U.S. gallons (22.71 litres) total (3.0 gallons each engine) // 4.5 U.S. gallons (17.03 litres) usable //Takeoff RPM/HP: 3400/260 //Max Continuous: 3000/240 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.200 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=0.800 cylinder_displacement=72.500 compression_ratio=7.300 number_of_cylinders=6 max_rated_rpm=3400.000 max_rated_hp=260.000 fuel_metering_type=2 cooling_type=0 normalized_starter_torque=0.3 turbocharged=0 max_design_mp=0 min_design_mp=1 critical_altitude=0.000 emergency_boost_type=0 emergency_boost_mp_offset=0.000 emergency_boost_gain_offset=0.000 fuel_air_auto_mixture=1 auto_ignition=0 power_scalar=1.000 [propeller] //Propellers (hub/blade): Hartzell HC-82X20-2/9333C-3 propeller_type=0 propeller_diameter=7.500 propeller_blades=2 propeller_moi=6.817360 beta_max=38.5 beta_min=18.000 min_gov_rpm=1110.000 prop_tc=0.01 gear_reduction_ratio=1.5576 fixed_pitch_beta=0.000 low_speed_theory_limit=80.000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=700.000 beta_feather=89.000 power_absorbed_cf=0.900 defeathering_accumulators_available=1 prop_reverse_available=0 minimum_on_ground_beta=12.000 minimum_reverse_beta=0.000 thrust_scalar=1.00 [Reference Speeds] flaps_up_stall_speed=58.2219 full_flaps_stall_speed=34.7593 cruise_speed=171.188 max_indicated_speed=237.593750 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=4.974,-1.131, -0.229 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1000.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 use_no_default_bank=1 use_no_default_pitch=0 default_bank_mode=0 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [direction_indicators] direction_indicator.0=1,0 [forcefeedback] stick_shaker_magnitude=5000 stick_shaker_direction=0 stick_shaker_period=111111 gear_bump_nose_magnitude=2000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=2700 gear_bump_left_direction=9000 gear_bump_left_duration=250000 gear_bump_right_magnitude=2700 gear_bump_right_direction=27000 gear_bump_right_duration=250000 ground_bumps_magnitude1=1350 ground_bumps_angle1=8900 ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ground_bumps_angle2=9100 ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 p_factor_on_yaw = 0.5 torque_on_roll = 1.0 gyro_precession_on_yaw = 1.0 gyro_precession_on_pitch = 1.0 [Radios] // Radio Type=available, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [pitot_static] vertical_speed_time_constant=2.0 [EFFECTS] dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 water=fx_spray [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.95, -22.6, 1.85, fx_navred , light.1=3, 0.94, 22.6, 1.82, fx_navgre , light.2=2, 0.259, 22.6, 1.85, fx_strobe , light.3=2, 0.275, -22.57, 1.82, fx_strobe , light.4=1, -18.65, 0.0, 9.5, fx_beacon , light.5=1, -1.1, 0.0, -4.5, fx_beacon , light.6=4, 1.50, 0.0, 0.0, fx_vclight, light.7=4, 4.50, 0.0, 0.0, fx_vclight, light.8=3,-23.4, -0.0, 1.0, fx_navwhi , [Flaps.0] type=1 span-outboard=0.320 extending-time=6.000 system_type=1 damaging-speed=250.000 blowout-speed=305.000 lift_scalar=1.00 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=0.000 flaps-position.1=10.000 flaps-position.2=20.000 flaps-position.3=30.000 flaps-position.4=40.000 [electrical] //max_battery_voltage=25.200 //generator_alternator_voltage=28.500 //max_generator_alternator_amps=160.000 //additional_system=0, 0.1, 17.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 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 [brakes] toe_brakes_scale=0.640889 parking_brake=1 [gear_warning_system] gear_warning_available=2 pct_throttle_limit=0.099976 flap_limit_power=20.001957 flap_limit_idle=9.998114 [hydraulic_system] electric_pumps=1 engine_map=1,1,0,0 normal_pressure=13.875000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0