[fltsim.0] title=AIA DC-9-50 Northwest sim=aia_dc_9_50 model=no_refl panel= sound= texture=northwest kb_checklists= kb_reference= atc_id= atc_airline=Northwest atc_flight_number=1123 ui_manufacturer=Aardvark ui_type=dc-9-50 ui_variation=Northwest Airlines description=AI Aardvark DC-9-50 atc_id_color=0000000000 visual_damage=0 [fltsim.1] title=AIA DC-9-50 AVE sim=aia_dc_9_50 model=no_refl panel= sound= texture=AVE kb_checklists= kb_reference= atc_id= atc_airline=AVE atc_flight_number=1123 ui_manufacturer=Aardvark ui_type=dc-9-50 ui_variation=Avensa description=AI Aardvark DC-9-50 atc_id_color=0000000000 visual_damage=0 [General] atc_type=MCDONNELDOUGLAS atc_model=DC9 editable=1 performance=Only experienced AI pilots should attempt to fly this aircraft. [weight_and_balance] // ACM V1.0 pl4 max_gross_weight = 120000 empty_weight = 79686 reference_datum_position = 77, 0, 0 empty_weight_CG_position = -72, 0, 0 empty_weight_pitch_MOI = 951967 empty_weight_roll_MOI = 465681 empty_weight_yaw_MOI = 1447094 empty_weight_coupled_MOI = 0 max_number_of_stations = 1 station_load.0 = 33000, -69.5, 0.0, 0.0 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 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=1.0 [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-103.6, -8.5, 0.6 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-103.6, 8.5, 0.6 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=10.4 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=19000 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=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, 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] static_pitch = -0.5 static_cg_height = 4.1 max_number_of_points = 7 point.0 = 1, -16.1697, 0, -4.4134, 1500, 0, 1.08, 25, 1, 2.5, 0.9, 7, 5, 0, 0, 0 point.1 = 1, -83.0959, -8.3297, -5.4231, 3000, 1, 1.85, 0, 1.5, 2.5, 0.8, 7, 7, 2, 0, 0 point.2 = 1, -83.1, 8.33, -5.4231, 3000, 2, 1.85, 0, 1.5, 2.5, 0.8, 7, 7, 3, 0, 0 point.3 = 2, -92.3227, -47.3471, 3.0831, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -92.3227, 47.3471, 3.0831, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -129.6882, 0, 6.8754, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, -14.574, 0, 1.8174, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 gear_system_type=0 [Views] eyepoint=-13.3, -1.82, 5.0 //(feet) longitudinal, lateral, vertical distance from reference datum [Flaps.0] type= 1 span-outboard= 0.800 extending-time= 20.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.5 drag_scalar=1.0 pitch_scalar= 1.0 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 2.000, 0.000 flaps-position.3= 5.000, 0.000 flaps-position.4= 10.000, 0.000 flaps-position.5= 15.000, 0.000 flaps-position.6= 25.000, 0.000 flaps-position.7= 30.000, 0.000 flaps-position.8= 40.000, 0.000 [Flaps.1] type= 2 span-outboard= 0.800 extending-time= 2.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.00 drag_scalar= .00 pitch_scalar= 0.00 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 [Flaps.2] type= 2 span-outboard= 0.800 extending-time= 3.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.00 drag_scalar= 0.00 pitch_scalar= 0.00 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.500, 0.000 flaps-position.2= 1.000, 0.000 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -87.77, 46.78, 3.41, fx_navgrem light.1 = 3, -87.77, -46.78, 3.41, fx_navredm light.2 = 2, -87.97, -46.96, 3.34, fx_strobeh light.3 = 2, -87.97, 46.96, 3.34, fx_strobeh light.4 = 3, -91.41, 47.43, 3.13, fx_navwhi light.5 = 3, -91.41, -47.43, 3.13, fx_navwhi light.6 = 1, -71, 0, 10.29, fx_beaconb light.7 = 1, -76.5, 0, -1.24, fx_beacon [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 Center1 = -76.2, 0, -6, 580, 3 Center2 = -78.2, 0, -6, 580, 3 LeftMain = -78.7, -12.1, -4, 2920, 3 RightMain = -78.7, 12.1, -4, 2920, 3 electric_pump=0 [airplane_geometry] wing_area=1209.0 //Square feet wing_span=107.8 //Feet wing_root_chord=23.1 //Feet wing_dihedral=3.0 //Degrees wing_incidence=1.3 //Degrees wing_twist=0.0 //Degrees oswald_efficiency_factor=0.8 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=24.5 //Degrees, wing leading edge wing_pos_apex_lon=-61.0 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_area=341.0 //Square feet htail_span=40.0 //Feet htail_pos_lon=-134.0 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=0.0 //Degrees htail_sweep=30.0 //Degrees, horizontal tail leading edge vtail_area=168.0 //Square feet vtail_span=14.8 //Feet, tip to body vtail_sweep=25.0 //Degrees, vertical tail leading edge vtail_pos_lon=-131.8 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=10.9 //Feet, vertical distance from reference point, positive going up elevator_area=145.0 //Square feet aileron_area=38.0 //Square feet rudder_area=65.3 //Square feet elevator_up_limit=26.0 //Degrees elevator_down_limit=26.0 //Degrees aileron_up_limit=30.0 //Degrees aileron_down_limit=30.0 //Degrees rudder_limit=30.0 //Degrees elevator_trim_limit=20.0 //Degrees spoiler_limit=60.0 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=3 //Aileron to spoileron gain min_ailerons_for_spoilerons=10 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=142.0 //Knots True (KTAS) full_flaps_stall_speed=113.6 //Knots True (KTAS) cruise_speed=477 //Knots True (KTAS) max_indicated_speed=340.000000 max_mach=0.820020 [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=150.0, 250.0 aileron=150.0, 250.0 rudder=150.0, 250.0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8 ; 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 [forcefeedback] 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=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 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 [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=0.885037 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0