[fltsim.0] title=Boeing 737-500_CSA sim=Boeing737-400 model= panel= sound= texture=OKDGL visual_damage=1 kb_checklists=Boeing737-400_check kb_reference=Boeing737-400_ref atc_id=OKDGL atc_airline=CSA atc_flight_number=1123 ui_manufacturer=Boeing ui_type=737-500 - FFX ui_variation=CSA 80th Anniversary description=One should hardly be surprised that the world's most prolific manufacturer of commercial aircraft is also the producer of the world's most popular jetliner. The 737 became the best-selling commercial jetliner worldwide when orders for it hit 1,831 in June 1987 (surpassing Boeing's own 727 as the previous champ). However, it wasn't always that way\s in the first few years of production, there were so few orders that Boeing considered canceling the program. They didn't, and the airplane has more than proven itself in over three decades of service. [General] performance=Power: 2\/ CFM56-3C @ 22,000 lbs\/thrust\nMTOW: 124,500 lbs\nMLW: 114,000 lbs (70% fuel)\nZFW: 89,445 lbs\nV1\/VR\/V2: 135\/145\/165 kts (MTOW)\nVref: 135-140 kts (MLW)\nNormal Cruise: M.78-M.80\nRange: 2300nm atc_type= atc_model= [pitot_static] vertical_speed_time_constant=0.5 //Increasing this value will cause a more instantaneous reaction in the VSI [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=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight= 89445.000 empty_weight_roll_MOI= 1854568.000 empty_weight_pitch_MOI= 1794268.000 empty_weight_yaw_MOI= 2209567.000 empty_weight_coupled_MOI= 1300.000 max_gross_weight= 125021.999 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=0.70 parasite_drag_scalar=0.20 induced_drag_scalar=1.10 ELEVATOR_EFFECTIVENESS=3.5 // ADJUST THIS VALUE TO MEET PITCHCRITERIA AILERON_EFFECTIVENESS=6.0 // ADJUST THIS VALUE TO MEET ROLLCRITERIA rudder_effectiveness=3.0 pitch_stability=2.0 roll_stability=1.5 yaw_stability=0.7 elevator_trim_effectiveness=2.2 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=4.75, -16.1, -2.5 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=4.75, 16.1, -2.5 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.59 //Scalar for fuel flow efficiency [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=19.6 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=22000 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=0.95 [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) [fuel] Center1=0, 0, 0, 2313, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-3, -19, 0, 1500, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-3, 19, 0, 1500, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 //[fuel] //LeftMain= -3.000, -19.000, 0.000, 2655.000, 0.000 //RightMain= -3.000, 19.000, 0.000, 2655.000, 0.000 //fuel_type=2.000000 //number_of_tank_selectors=1 [airplane_geometry] wing_area= 1136.000 wing_span= 94.750 wing_root_chord= 10.500 wing_dihedral= 5.999 wing_incidence= -0.494 wing_twist= 1.000 oswald_efficiency_factor= 0.754 wing_winglets_flag= 0 wing_sweep= 25.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 353.000 htail_span= 41.667 htail_pos_lon= -47.917 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 284.000 vtail_span= 19.215 vtail_sweep= 0.000 vtail_pos_lon= -34.167 vtail_pos_vert= 5.833 elevator_area= 84.250 aileron_area= 39.200 rudder_area= 42.330 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.481 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 [contact_points] point.0=1.000000,32.833333,0.000000,-8.000000,1574.803150,0.000000,1.366704,53.640000,0.308233,2.500000,0.638547,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-3.750000,-10.833333,-8.750000,1574.803150,1.000000,1.366704,0.000000,0.308234,2.500000,0.638543,5.000000,5.000000,2.000000,0.000000,0.000000 point.2=1.000000,-3.750000,10.833333,-8.750000,1574.803150,2.000000,1.366704,0.000000,0.308234,2.500000,0.638543,5.000000,5.000000,3.000000,0.000000,0.000000 point.3=2.000000,0.000000,-46.500000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,0.000000,46.500000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-54.166667,0.000000,2.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,45.750000,0.000000,-2.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=0.126343 static_cg_height=7.785956 [Reference Speeds] flaps_up_stall_speed=156.0 //Knots True (KTAS) full_flaps_stall_speed=110.0 //Knots True (KTAS) cruise_speed=477.0 //Knots True (KTAS) [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=37.152949,-1.499446,4.165129 [autopilot] use_no_default_pitch=1 use_no_default_bank=1 autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 nav_proportional_control=16.00 nav_integrator_control=0.17 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control = 25.0 gs_integrator_control = 0.33 gs_derivative_control = 0.00 gs_integrator_boundary = 0.70 gs_derivative_boundary = 0.00 yaw_damper_gain = 1.0 [direction_indicators] direction_indicator.0=3,0 [Flaps.0] type= 1 span-outboard=0.500 extending-time=25.00 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 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 ///Note - this section is only here to make the LEDs animate. It does not affect flying characterisitics. [flaps.1] //Inboard Leading Edge Flaps type=2 // 1 - tail, 2 - lead span-outboard=0.0 // 0.0 .. 1.0 extending-time=6 // seconds flaps-position.0=0 // flaps-position.1=1.0 // flaps-position.2=2.0 // damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=0.0 drag_scalar=0.0 pitch_scalar=0.0 system_type=1 //Hydraulic [flaps.2] //Inboard Leading Edge Flaps type=2 // 1 - tail, 2 - lead span-outboard=0.0 // 0.0 .. 1.0 extending-time=6 // seconds flaps-position.0=0 // flaps-position.1=1.0 // damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=0.0 drag_scalar=0.0 pitch_scalar=0.0 system_type=1 //Hydraulic [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=1.0 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=1.5 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [LIGHTS] light.0 =3, -8.54, -49.74, 1.90, fx_navred , light.1 =3, -8.54, 49.74, 1.90, fx_navgre , light.2 =3, -8.94, -49.74, 1.90, fx_navred , light.3 =3, -8.94, 49.74, 1.90, fx_navgre , light.4 =3, -49.52, 0.00, 6.30, fx_navwhih , light.5 =2, -10.14, -49.84, 1.90, fx_strobe , light.6 =2, -10.14, 49.84, 1.90, fx_strobe , light.7 =1, 2.20, 0.00, 10.30, fx_beaconh , light.8 =3, -13.60, -49.22, 1.90, fx_navwhi , light.9 =3, -13.60, 49.22, 1.90, fx_navwhi , [Radios] // Radio Type=availiable, standby frequency, has glide slope // Radio Type=availiable, 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 [TailHook] tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=0.7 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.12,0.11 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdr5 concrete=fx_sparks touchdown=fx_tchdwn, 1
