//////////////////////////////////////////////////////////////////////// //FLIGHT DYNAMICS CONFIGURATION FILE: EnigmaSim 737-300SP // //FOR FS9 (CFM563B1). FDE COPYRIGHT ENIGMA SIMULATIONS, JAN2010 // //MARTYN BECKER 23OCT10 v3.1 thebecken@hotmail.com // // // //REALISTIC DYNAMICS - ACCURATE DIMENSIONS, LOAD WEIGHTS, // //FUEL, SPEED, ENGINE POWER AND RANGE // //////////////////////////////////////////////////////////////////////// //Insert [fltsim] sections between the dotted lines ------------------------------------------------------------------------ [fltsim.0] title=Enigma Boeing 737-300SP sim=Enigma733_fs9 model= panel= sound= texture= kb_checklists= kb_reference=Enigma737_fuel_ref atc_id=N532AU atc_id_color=0xffffffff atc_airline= atc_flight_number=9999 ui_manufacturer=Boeing ui_type=737-300SP Enigma ui_variation= description=ENIGMASIM B737-300\nModel\nAndrew Quintal\n\nMaster Textures\n - Ron Waite\n - Andrew Quintal\n\nFlight Dynamics\n - Martyn Becker\n\nBeta Team\n - Enigma Staff\n atc_heavy=0 ------------------------------------------------------------------------- [General] performance=SP version - Power: 2 x CFM56-3B1 rated at 20,000 lbs thrust\nMTOW: 124,500 lbs\nMLW: 112,000 lbs \nZFW: 71,412 lbs\nV1\/VR\/V2: 135\/145\/165 kts (MTOW)\nVref: 135-140 kts (MLW)\nNormal Cruise: M.75 (Max M.82)\nMax alt. FL370\nTypical two-class passenger configuration - 128\nRange with maximum payload (15% safety margin): 1815nm\nFuel capacity 5,311 US gallons. atc_type=Boeing atc_model=B733 category=airplane //AERODYNAMICS [airplane_geometry] wing_area= 1136.00 wing_span= 94.75 wing_root_chord= 18.50 wing_dihedral= 6.00 wing_incidence= 2.50 wing_twist= 0.000 oswald_efficiency_factor= 0.754 wing_winglets_flag= 1 wing_sweep= -25.000 wing_pos_apex_lon= -5.00 wing_pos_apex_vert= 0.00 htail_area= 408.000 htail_span= 42.650 htail_pos_lon= -43.921 htail_pos_vert= 8.796 htail_incidence= -0.600 htail_sweep= -30.000 vtail_area= 305.000 vtail_span= 21.125 vtail_sweep= -35.000 vtail_pos_lon= -32.654 vtail_pos_vert= 10.873 elevator_area= 102.500 aileron_area= 39.000 rudder_area= 51.850 elevator_up_limit= 24.000 elevator_down_limit= 24.000 aileron_up_limit= 20.000 aileron_down_limit= 20.000 rudder_limit= 23.500 elevator_trim_limit= 12.000 spoiler_limit= 59.989 spoilerons_available= 1 aileron_to_spoileron_gain= 3.000 min_ailerons_for_spoilerons= 9.969 min_flaps_for_spoilerons= 0.000 auto_spoiler_available=1 spoiler_extension_time=0.60 //1.200000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 [Flaps.0] type= 1 //trailing edge span-outboard=0.500 extending-time=32 //25.00 system_type= 0 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.60 drag_scalar= 1.000 pitch_scalar= 1.000 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 //leading edge span-outboard=0.0 extending-time=6 flaps-position.0=0 flaps-position.1=1.0 flaps-position.2=1.0 flaps-position.3=1.0 flaps-position.4=1.0 flaps-position.5=2.0 damaging-speed=250 blowout-speed=300 lift_scalar=0.75 drag_scalar=0.0 pitch_scalar=0.0 system_type=1 [flaps.2] type=2 //leading edge span-outboard=0.0 extending-time=6 flaps-position.0=0 flaps-position.1=1.0 damaging-speed=250 blowout-speed=300 lift_scalar=0.75 drag_scalar=0.0 pitch_scalar=0.0 system_type=1 [flight_tuning] cruise_lift_scalar=1.300 pitch_stability=2.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.880 induced_drag_scalar=1.000 elevator_effectiveness=1.9 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.500 aileron_trim_effectiveness=1.200 rudder_trim_effectiveness=1.000 [Reference Speeds] flaps_up_stall_speed= 120.00 full_flaps_stall_speed= 96.00 cruise_speed= 335.17 max_indicated_speed=341.23 max_mach=0.82 [WEIGHT_AND_BALANCE] //Alternative MOI figures supplied below for use with Johan Dees' modification of the default sim1.dll file (avsim.com) reference_datum_position=0, 0, 0 empty_weight_CG_position=0, 0, 0 max_number_of_stations=50 station_load.0="840.0, 30.0, 0.0, 0.0, Crew" station_load.1="800.0, 28.0, 0.0, 0.0, Business 1" station_load.2="800.0, 25.0, 0.0, 0.0, Business 2" station_load.3="8400.0, 0.0, 0.0, 0.0, Economy 1" station_load.4="8400.0, -10.0, 0.0, 0.0, Economy 2" station_load.5="4000.0, 40.0, 0.0, 0.0, Forward cargo" station_load.6="3000.0, -20.0, 0.0, 0.0, Rear cargo" empty_weight= 71412.00 empty_weight_pitch_MOI= 2395873 //11794268.00 empty_weight_roll_MOI= 958349 //2954568.00 empty_weight_yaw_MOI= 2831486 //8009567.00 empty_weight_coupled_MOI= 0.00 max_gross_weight= 124500.00 CG_forward_limit= 0.000 CG_aft_limit= 1.000 //INSTRUMENTS/SYSTEMS [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1200.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=96 pitch_takeoff_ga=8 use_no_default_pitch=1 use_no_default_bank=1 default_pitch_mode=0 default_bank_mode=0 max_pitch=10 max_pitch_acceleration=1 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.00 max_pitch_velocity_hi_alt_breakpoint=28000.00 max_bank=25 max_bank_acceleration=1.80 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=1 [brakes] toe_brakes_scale=0.60 parking_brake=1 differential_braking_scale=1 auto_brakes=4 [direction_indicators] direction_indicator.0=3,0 [electrical] //BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) //Amended to extend battery life at startup max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 1 flap_motor= 0, 1 , 1 gear_motor = 4, 1 , 1 light_wing = 0, 1 , 1 light_logo = 0, 1 , 1 autopilot = 0, 5 , 1 avionics_bus = 0, 5, 1 avionics = 1, 5 , 1 pitot_heat= 0, 2 , 1 additional_system = 2, 1, 1 marker_beacon = 1, 1 , 1 gear_warning = 0, 1 , 1 fuel_pump = 0, 1 , 1 starter1 = 0, 1, 1 light_nav = 0, 1 , 1 light_beacon = 0, 1 , 1 light_landing = 0, 1 , 1 light_taxi = 0, 1 , 1 light_strobe = 0, 1 , 1 light_panel = 0, 1 , 1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.10 flap_limit_power=25.50 flap_limit_idle=5.00 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.00 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cabin light.0 = 3, -65.25, 0.00, 8.42, fx_strobeh , light.1 = 1, -0.65, 0.00, -3.50, fx_beaconb , light.2 = 1, 4.20, 0.00, 9.95, fx_beaconh , light.3 = 4, 44.41, 0.00, 3.00, fx_vclight , light.4 = 5, 1.0, -7.75, 0.2 , fx_Enigma_3Dlanding , light.5 = 5, 1.0, 7.75, 0.2 , fx_Enigma_3Dlanding , light.6 = 6, 28.3, 0.00, -4.10 , fx_Enigma_3Dtaxi , light.7 = 6, -21.0, -29.80, 0.5 , fx_Enigma_3Dwing , light.8 = 6, -21.0, 29.80, 0.5 , fx_Enigma_3Dwing , light.9=7, -9.0, -16.0, -2.8, fx_fanengine_light_idle , light.10=8, -9.0, 16.0, -2.8, fx_fanengine_light_idle , light.11=9, -9.0, -16.0, -2.8, fx_fanengine_light , light.12=9, -9.0, 16.0, -2.8, fx_fanengine_light , light.13 = 3, 1.5, 0.0, 0.2 , fx_Enigma_733_strobe_FS9 , light.14 = 10, -66.50, 0.00, 5.50, fx_APU , //ENGINES [fuel] Center1= 0.000, 0.000, 0.000, 2079.000, 3.000 LeftMain= -10.000, 19.000, 0.000, 1600.000, 3.000 RightMain= -10.000, -19.000, 0.000, 1600.000, 3.000 fuel_type=2 number_of_tank_selectors=1 electric_pump=1 [GeneralEngineData] engine_type= 1 Engine.0= -5.00, -16.00, -2.30 Engine.1= -5.00, 16.00, -2.30 fuel_flow_scalar= 0.71 min_throttle_limit=-0.21 ;max_contrail_temperature =-30 [jet_engine] thrust_scalar=1.10 [TurbineEngineData] fuel_flow_gain= 0.0045 inlet_area= 21.240 rated_N2_rpm= 29920.000 static_thrust= 20000.000 afterburner_available= 0 reverser_available= 1 //MISCELLANEOUS SIMULATOR [attitude_indicators] attitude_indicator.0=1 [contact_points] //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) //Gear point.0= 1, 27.417, 0.000, -6.800, 2000.000, 0.000, 0.904, 40.000, 0.900, 1.033, 0.900, 7.000, 9.000, 0.000, 240.000, 260.000 //nose point.1= 1, -13.291, -10.706, -7.450, 2000.000, 1.000, 1.678, 0.000, 0.922, 1.334, 0.95000, 8.000, 10.000, 2.000, 240.000, 260.000 //main port point.2= 1, -13.291, 10.706, -7.450, 2000.000, 2.000, 1.678, 0.000, 0.922, 1.334, 0.9500, 9.000, 11.000, 3.000, 240.000, 260.000 //main starboard // Scrape Points point.3=2,-24.00, -48.50, 2.60,1574.80,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,5.00,0.00,0.00 //left wingtip point.4=2,-24.00, 48.50, 2.60,1574.80,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,6.00,0.00,0.00 //right wingtip point.5=2,-45.00, 0.00, -1.50,1574.80,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,9.00,0.00,0.00 //tail point.6=2,30.00, 0.00, -3.50,1574.80,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00 //nose point.7=2,-4.500, -16.200, -2.800,1574.80,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00 //left engine point.8=2,-4.500, 16.200, -2.800,1574.80,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00 //right engine max_number_of_points = 10 static_pitch= -1.000 static_cg_height=6.30 gear_system_type=1 [forcefeedback] gear_bump_nose_magnitude=8000 //3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=9000 //2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=9000 //2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=8000 //1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=8000 //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 [ground_reaction] main_gear_static_compression=0.8 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.8 // (feet), The distance the center gear strut is compressed when at rest on the ground main_gear_damping_ratio=2.00 //1.0 // Main gear strut damping, 0 = undamped oscillations, 1 = critically damped center_gear_damping_ratio=1.5 // Center gear strut damping, 0 = undamped oscillations, 1 = critically damped [keyboard_response] elevator=150.00,250.00 aileron=150.00,250.00 rudder=150.00,250.00 [pitot_static] vertical_speed_time_constant=99 pitot_heat=1.0 [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 [stall_warning] type=1 stick_shaker=0 [turn_indicators] turn_indicator.0=1,0 [Views] eyepoint=43.7, -1.31, 3.55 //VISUAL EFFECTS [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits=5 exit_rate.0=0.4 ;Percent/second exit_rate.1=0.2 ;Percent/second exit_rate.2=0.4 ;Percent/second exit_rate.3=0.4 ;Percent/second exit_rate.4=0.4 ;Percent/second [folding_wings] wing_fold_system_type=4 fold_rates=0.15,0.15 [smokesystem] //Wing tip vortices smoke.0=0, -25.167, -34.567, VortexEnigmaFlap smoke.1=0, -25.167, 34.567, VortexEnigmaFlap [TailHook] tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=0.7
