//Aero Commander 560A(HC) for FS2002. Model designed and animated in GMAX by Milton Shupe - October-April 2003. Flight Dynamics by Milton Shupe. [fltsim.0] title=AC560 Spanish Red sim=AC560A1 model=AC560A1 panel=560A1 sound= texture=spanishred description=Beginning in 1955, Aero Design & Engineering Company rolled out the first model 560A. Only 100 units were built between 1955 & 1957. Between 14 and 25 AC560A(HC)'s were produced as modified 560A's. The AC560A(HC) Power : Lycoming GO-480-G1B6 - 295hp at 3400 RPM. kb_checklists=AC560A_Check kb_reference=AC560A_Ref ui_manufacturer=Aero Design & Engineering ui_type=AC56 novc ui_variation=Red novc atc_heavy=0 atc_id=N1946 atc_airline=Private atc_flight_number=1946 atc_type=ROCKWELL [fltsim.1] title=AC560 Orange sim=AC560A1 model=AC560A1 panel=560A1 sound= texture=orange description=Beginning in 1955, Aero Design & Engineering Company rolled out the first model 560A. Only 100 units were built between 1955 & 1957. Between 14 and 25 AC560A(HC)'s were produced as modified 560A's. The AC560A(HC) Power : Lycoming GO-480-G1B6 - 295hp at 3400 RPM. kb_checklists=AC560A_Check kb_reference=AC560A_Ref ui_manufacturer=Aero Design & Engineering ui_type=AC56 novc ui_variation=Orange novc atc_heavy=0 atc_id=N1946 atc_airline=Private atc_flight_number=1946 atc_type=ROCKWELL [fltsim.2] title=AC560 Factory N2649B sim=AC560A1 model=AC560A1 panel=560A1 sound= texture=N2649B description=Beginning in 1955, Aero Design & Engineering Company rolled out the first model 560A. Only 100 units were built between 1955 & 1957. Between 14 and 25 AC560A(HC)'s were produced as modified 560A's. The AC560A(HC) Power : Lycoming GO-480-G1B6 - 295hp at 3400 RPM. kb_checklists=AC560A_Check kb_reference=AC560A_Ref ui_manufacturer=Aero Design & Engineering ui_type=AC56 novc ui_variation=N2649B novc atc_heavy=0 atc_id=N2649B atc_airline=Private atc_flight_number=1946 atc_type=ROCKWELL [General] //Range, maximum cruising power at 60% (2600rpm@22"MP), is 950nm (1150sm/1851km)with 30 minutes reserve //performance=Hi speed cruise: 212 mph/171 kts@10,000'\nVR: 87 mph - Normal climb: 140 mph\nRate of climb (sea level): 1400 fpm\ //nStalls (mph) - clean : 67\s dirty : 40\nPower: 2x 295 hp Lycoming GO-480-C2 \nLanding speed: 82 mph\ //nService ceiling: 22000 ft atc_type=AERO atc_model=AC560A editable=0 performance=Hi speed cruise: 212 mph\nNormal rate of climb (sea level): 140 mph-1400FPM\nStalls (mph) - clean : 67\s dirty : 40\nPower: 2x 295 hp Lycoming GO-480-G1B6\nApproach speed: 98 mph\nService ceiling: 22000 ft\nVR: 87 mph - Best climb: 140 mph\nOEI service ceiling: 9750 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 station_load.3=0.000, 4.200, 1.100, -1.000 station_load.4=170.000, 0.000, -1.100, -1.000 //rear passengers station_load.5=170.000, 0.000, 1.100, -1.000 //rear passengers station_load.6=170.000,-1.500, -1.100, -0.000 //cargo station_load.7=170.000,-1.500, 1.100, -0.000 //cargo empty_weight = 4250 empty_weight_roll_MOI = 8892 empty_weight_pitch_MOI = 3761 empty_weight_yaw_MOI = 10671 empty_weight_coupled_MOI=0.000 max_gross_weight=6000.000 CG_forward_limit=0.150 CG_aft_limit=0.380 [exits] number_of_exits=2 exit_rate.0=0.8 ;Percent per second exit_rate.1=0.8 ;Percent per second [fuel] //Fuel: 100/130 minimum grade aviation gasoline //16 U.S. gallons per engine per hour at 2,600 r.p.m. //Fuel capacity: 156 U.S. gallons (568 litres) total; [5 inter-connected tanks]; 151 U.S. gallons usable LeftMain=-1.000, -3.000, 1.000, 30.000, 0.000 RightMain=-1.000, 3.000, 1.000, 30.000, 0.000 Center1=-1.000, 0.000, 1.000, 96.000, 5.000 fuel_type=1.000000 number_of_tank_selectors=2 [airplane_geometry] wing_area=242.500 wing_span=44.058 wing_root_chord=8.669 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=0.0 wing_pos_apex_vert=0.0 htail_area=27 htail_span=16 htail_pos_lon=-19 htail_pos_vert=0 htail_incidence=0 htail_sweep=0 vtail_area=13 vtail_span=6.0 vtail_sweep=0 vtail_pos_lon=-19 vtail_pos_vert=0.0 elevator_area=18.5 aileron_area=22.4 rudder_area=10 elevator_up_limit=30.002 elevator_down_limit=10.614 aileron_up_limit=23.614 aileron_down_limit=15.614 rudder_limit=20.001 elevator_trim_limit=25.002 rudder_trim_limit=21.0 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, 13.183, 0.000, -5.683 1574.803, 0.000, 0.667, 20.000, 0.20, 4.700, 0.800, 5.000, 4.000, 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, 10.000, 8.000, 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, 6.000, 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 [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 [piston_engine] //Lycoming GO-480-G1B6 //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: 3400/295 //Max Continuous: 3000/275 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 cylinder_displacement=80.000 compression_ratio=8.500 number_of_cylinders=6 max_rated_rpm=3400.000 max_rated_hp=295.000 fuel_metering_type=2 cooling_type=0 normalized_starter_torque=0.035 turbocharged=0 max_design_mp=29.800 min_design_mp=9.000 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-A3MV20-2-MV8833N-2 propeller_type=0 propeller_diameter=7.000 propeller_blades=3 propeller_moi=6.817360 beta_max=38.5 beta_min=17.000 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=83.000 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=60.2219 full_flaps_stall_speed=40.593 cruise_speed=212.0 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=5.774,-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 [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 [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=4, 5.80, 0.0, -2.50, fx_vclight , light.5=1, -19.75, 0.0, 9.9, fx_beacon , light.6=1, -1.1, 0.0, -4.7, fx_beacon , light.7=3, -23.41, 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] 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 flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 starter1=0, 20, 17.0
