// Do not remove or edit this section. // This section is for PAI Installer information and will not interfere with aircraft behaviour [Project AI] Version=6.03 // FDE Revision by Oliver Caspers // // End of Project AI specific settings [General] atc_type=BOEING atc_model=B732 editable=1 performance=Cruise Speed\t.74 Mach\nMaximum Range\t2,059 nm\nService Ceiling\t36,089 ft\nMax Takeoff Weight\t138,500 lb\nSeating\t\t147 to 168\nCargo Capacity\t1,373 CU ft\n [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight = 110000.0 empty_weight = 61800.0 reference_datum_position = 0.0, 0.0, 0.0 empty_weight_CG_position = 1.5, 0.0, -1.0 max_number_of_stations =2 station_load.0 =30000.0, 1.0, 0.0, 1.0 ;Moments of Inertia empty_weight_pitch_MOI = 2500000.0 empty_weight_roll_MOI = 1800000.0 empty_weight_yaw_MOI = 3700000.0 empty_weight_coupled_MOI = 0.0 CG_forward_limit= 0.0 CG_aft_limit= 1.0 [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 Engine.0 = 2.1, -15.8, -2.2 Engine.1 = 2.1, 15.8, -2.2 fuel_flow_scalar = 1.0 min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 15.7 rated_N2_rpm = 29920.0 static_thrust = 16000 afterburner_available = 0 reverser_available = 1 [jet_engine] thrust_scalar =1.200 [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 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 5.0 //Flap angle that activates warning at idle flap_limit_power = 25.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.885 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=39.9, -1.31, 4.7 //(feet) longitudinal, lateral, vertical distance from reference datum [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 [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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=2500 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm = 93 autothrottle_takeoff_ga=1 pitch_takeoff_ga = 8; max_pitch=10.0 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=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=12.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=25.0 gs_integrator_control=0.53 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [fuel] Center1 = 0.0, 0.0, -1.0, 1980.0, 0.0 LeftMain = -4.7, -9.4, 0.0, 1400.0, 0.0 RightMain = -4.7, 9.4, 0.0, 1400.0, 0.0 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 980.0 wing_span = 93.0 wing_root_chord = 19.9 wing_dihedral = 5.2 wing_incidence = 1.5 wing_twist = -0.2 oswald_efficiency_factor= 0.73 wing_winglets_flag = 0 wing_sweep = 27.0 wing_pos_apex_lon = 9.5 wing_pos_apex_vert = 0.0 htail_area = 264.6 htail_span = 36.0 htail_pos_lon = -39.9 htail_pos_vert = 8.9 htail_incidence = 0.0 htail_sweep = 39.0 vtail_area = 219.9 vtail_span = 19.9 vtail_sweep = 40.0 vtail_pos_lon = -31.5 vtail_pos_vert = 11.0 elevator_area = 88.2 aileron_area = 29.8 rudder_area = 62.8 elevator_up_limit = 22.5 elevator_down_limit = 21.5 aileron_up_limit = 20.0 aileron_down_limit = 20.0 rudder_limit = 26.0 elevator_trim_limit = 20.0 spoiler_limit = 60.0 spoilerons_available = 1 aileron_to_spoileron_gain = 3.0 min_ailerons_for_spoilerons = 10.0 min_flaps_for_spoilerons = 0.0 [Reference Speeds] flaps_up_stall_speed=133.0 full_flaps_stall_speed=107.0 cruise_speed=470.0 max_indicated_speed=340.0 max_mach=0.82 [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 [stall_warning] type=2 [flaps.0] //Trailing Edge Flaps type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 20 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 1 // degrees flaps-position.2 = 2 // degrees flaps-position.3 = 5 // degrees flaps-position.4 = 10 // degrees flaps-position.5 = 20 // degrees flaps-position.6 = 30 // degrees flaps-position.7 = 40 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.1] //Outboard Leading Edge Slat type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 3 // seconds flaps-position.0 = 0 // flaps-position.1 = 0.5 // flaps-position.4 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -19.0, -46.4, 3.628, fx_navred , light.1=3, -19.0, 46.4, 3.628, fx_navgre , light.2=2, -54.500, 0.00, 8.118, fx_strobeh , light.3=2, -18.5, -46.4, 3.628, fx_strobeh , light.4=2, -18.5, 46.4, 3.628, fx_strobeh , light.5=1, 5.0, 0.00, -3.1, fx_beaconb , light.6=1, 3.0, 0.00, 10.2, fx_beaconh , light.7=3, -20.900, 46.55, 3.628, fx_navwhi , light.8=3, -20.900, -46.55, 3.628, fx_navwhi , light.9=4, 40.2652584, 0.00, 4.0386648, fx_vclighth, //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=1.0, 30.5, 0.0, -6.7, 1181.1, 0.0, 1.0, 55.2, 0.7, 2.5, 0.8, 4.0, 4.0, 0.0, 0.0, 0.0 point.1=1.0, -7.0,-9.6,-7.7, 1574.8, 1.0, 1.6, 0.0, 0.9, 2.5, 0.8, 6.9, 6.9, 2.0, 0.0, 0.0 point.2=1.0, -7.0, 9.6,-7.7, 1574.8, 2.0, 1.6, 0.0, 0.9, 2.5, 0.8, 7.1, 7.1, 3.0, 0.0, 0.0 point.3=2.0, -17.8,-46.5, 4.2, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 point.4=2.0, -17.8, 46.5, 4.2, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 point.5=2.0, -50.4, 0.0, 5.2, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 point.6=2.0, 34.8, 0.0,-3.1, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 max_number_of_points=7 static_pitch=-1.0 static_cg_height=6.8 gear_system_type=1 //Hydraulic [fltsim.0] title=PAI B732 canada3 sim=pai732v6 model= panel= sound= texture=CANA kb_checklists= kb_reference= atc_id=CA-REO atc_id_color=0xffffffff atc_airline=canada atc_flight_number=1468 atc_parking_codes=CAN atc_parking_types=GATE ui_manufacturer=Project AI ui_type=BOEING 737-200 ui_variation=CANADA 3000 atc_heavy=0 description=Project AI B732 Only for use with AI Traffic!