[fltsim.0] title=Boeing 737-800 bare sim=737800 model= panel= sound= texture=bare atc_id=G-HZB atc_airline= atc_flight_number=7378 kb_checklists=737-800_check kb_reference=737-800_ref ui_manufacturer=Boeing ui_type=737-800 ui_variation=bare description=Model by Erik Cantu of FlightFX, Textures by Garry J. Smith, GJSmith.net (www.gjsmith.net) [General] atc_type=BOEING atc_model=B738 performance=Power: 2x CFM56-7B24 @ 24200 lbs\/thrust\nMTOW: 174,200 lbs\nMLW: 144,009 lbs (70% fuel)\nZFW: 126,200 lbs\nV1\/VR\/V2: 135\/145\/165 kts (MTOW)\nVref: 135-140 kts (MLW)\nNormal Cruise: M.78-M.80\nRange: 3383nm (MAX PAYLOAD RANGE: 2926nm\nLength: 129 ft 6 in (33.6 m)\nHeight: 41 ft 2 in (12.5 m)\nWingspan: 112 ft 7 in (34.4 m)(117ft 2in with winglets)\/Vmo-Mmo: 340IAS (0.82MACH). 737-800 FDE by Mike Baumann FFX-Flight FX Group\/Special thanks to Chris Trott for his help with fuel and other misc data [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 [flight_tuning] cruise_lift_scalar = 1.050 parasite_drag_scalar = 1.200 induced_drag_scalar = 1.200 elevator_effectiveness = 1.000 aileron_effectiveness = 0.900 rudder_effectiveness = 0.900 pitch_stability = 1.200 roll_stability = 1.100 yaw_stability = 1.100 elevator_trim_effectiveness = 1.000 aileron_trim_effectiveness = 1.000 rudder_trim_effectiveness = 1.000 [jet_engine] thrust_scalar=1.00 [WEIGHT_AND_BALANCE] max_gross_weight = 174200 // (pounds) empty_weight = 90560 // (pounds) reference_datum_position= 0.00, 0.00, 0.00 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position= 0.00, 0.00, 0.00 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0 = "185.0, 60.0, -1.9, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "185.0, 60.0, 1.9, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "500.0, 55.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "1200.0, 52.0, 0.0, 3.8, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "3500.0, 42.0, 0.0, 3.8, Coach 3-8" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = "3500.0, 18.0, 0.0, 3.8, Coach 9-15" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = "4000.0, -6.0, 0.0, 3.8, Coach 16-22" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = "4000.0, -34.0, 0.0, 3.8, Coach 23-28" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8 = "10500.0, 15.0, 0.0,-4.1, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.9 = "5600.0, -25.0, 0.0,-1.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) empty_weight_pitch_MOI = 3309775.603 //Moments of Inertia empty_weight_roll_MOI = 1937410.657 empty_weight_yaw_MOI = 4120327.737 empty_weight_coupled_MOI = 824.066 CG_forward_limit = 0.000 CG_aft_limit = 1.000 [GeneralEngineData] engine_type= 1 Engine.0= 13.50, -17.30, -4.10 Engine.1= 13.50, 17.30, -4.10 fuel_flow_scalar=1 min_throttle_limit=-0.399902 [SMOKESYSTEM] smoke.0=13.50, -5.50, -17.3, fx_737_jetsmoke12v6 smoke.1=13.50, -5.50, 17.3, fx_737_jetsmoke12v6 smoke.2=// 0, -19.00, -58.00, fx_WingVortex //left wing vortex smoke.3=// 0, -19.00, 58.00, fx_WingVortex //right wing vortex [TurbineEngineData] Bypass_Ratio= 5.3000 //Boeing specs fuel_flow_gain= 0.0020 inlet_area= 20.3320 rated_N2_rpm= 29920.0000 static_thrust= 24200.0000 //CFM56-7B24 -7B26's are used on the 900 series afterburner_available=0 reverser_available= 1 [airplane_geometry] wing_area= 1341.000 //Boeing specs wing_span= 117.200 //span set for winglet version-will not effect non winglet version wing_root_chord= 11.910 wing_dihedral= 6.200 wing_incidence= 1.000 wing_twist= -0.500 oswald_efficiency_factor= 0.882 wing_winglets_flag= 1 wing_sweep= 25.000 //Boeing specs wing_pos_apex_lon= 11.600 wing_pos_apex_vert= 0.000 htail_area= 353.100 //Boeing specs htail_span= 153.900 //Boeing specs htail_pos_lon= -52.150 htail_pos_vert= 7.000 htail_incidence= 0.697 htail_sweep= 30.000 vtail_area= 284.200 //Boeing specs vtail_span= 27.200 //Boeing specs vtail_sweep= 35.000 //Boeing specs vtail_pos_lon= -44.600 vtail_pos_vert= 10.300 elevator_area= 70.500 //Boeing specs aileron_area= 26.900 rudder_area= 56.200 elevator_up_limit= 22.500 elevator_down_limit= 19.500 aileron_up_limit= 20.000 aileron_down_limit= 20.000 rudder_limit= 26.000 elevator_trim_limit= 20.000 spoiler_limit= 60.000 spoilerons_available= 1 aileron_to_spoileron_gain=3.000 min_ailerons_for_spoilerons=6.000 min_flaps_for_spoilerons=0.000 [Reference Speeds] //ONLY FOR AI USE, HAS ABSOLUTLY NO EFFECT ON YOUR ACTUAL FLYING flaps_up_stall_speed = 140 full_flaps_stall_speed = 115 cruise_speed = 475 max_indicated_speed=340.000000 max_mach=0.820000 [contact_points] point.0= 1, 51.00, 0.00, -8.70, 1574.80, 0, 2.251, 78.0, 0.308, 2.5, 0.639, 5.10, 5.30,0, 200, 280 //nose gear point.1= 1, -1.75, -9.50, -8.90, 1574.80, 1, 3.333, 0.0, 0.308, 2.5, 0.639, 5.30, 5.70,2, 200, 280 //left main point.2= 1, -1.75, 9.50, -8.90, 1574.80, 2, 3.333, 0.0, 0.308, 2.5, 0.639, 5.20, 5.60,3, 200, 280 //right main point.3= 2, -13.00, -58.85, 4.65, 787.80, 0. 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0, 0 //left wing NOT SET FOR WINGLETS point.4= 2, -13.00, 58.85, 4.65, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0, 0 //right wing NOT SET FOR WINGLETS point.5= 2, -69.15, 0.00, 9.50, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0, 0 //tail(set for hstab strike) point.6= 2, 69.55, 0.00, 1.00, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //nose point.7= 2, -45.15, 0.00, -1.50, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0, 0, 0 //aft fuse scrape point static_pitch=-0.90 static_cg_height=8.60 gear_system_type=0 [Flaps.0] //Trailing edge flaps type= 1 span-outboard=0.599 extending-time=25.00 system_type=1 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.200 drag_scalar= 1.000 pitch_scalar= 0.800 flaps-position.0= 0.000 flaps-position.1= 1.000 flaps-position.2= 2.000 flaps-position.3= 5.000 flaps-position.4= 10.000 flaps-position.5= 15.000 flaps-position.6= 25.000 flaps-position.7= 30.000 flaps-position.8= 40.000 [flaps.1] //Leading Edge slats type=2 span-outboard=0.800 extending-time=6.00 system_type=1 damaging-speed=280 blowout-speed=320 lift_scalar=1.000 drag_scalar=0.800 pitch_scalar=0.500 flaps-position.0=0.000 flaps-position.1=5.000 flaps-position.2=8.000 flaps-position.3=10.000 //3rd position added for later upgrade [electrical] //BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) 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 pitot_heat = 0, 15, 17.0 additional_system = 0, 20, 17.0 marker_beacon = 1, 2, 17.0 starter1 = 0, 20, 17.0 starter2 = 0, 20, 17.0 auto_brakes = 0, 15, 17.0 hydraulic_pump = 0, 2, 17.0 fuel_transfer_pump = 0, 5, 17.0 max_battery_voltage = 28.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps= 60.0 electric_always_available = 1 [pitot_static] vertical_speed_time_constant = 999 [exits] //L1 main exit door (shift+E) number_of_exits = 1 exit_rate.0 = 0.28 [TailHook] //under fuselage landing lights (shift+T) tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=0.5 [folding_wings] //airstairs (shift+F) wing_fold_system_type=4 fold_rates=0.15,0.15 [Views] eyepoint=60.00,-1.90,5.10 //pilots correct viewpoint from cockpit-for passengers perspective views see readme file in //American base package release. instructions there for panel config modifications [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 =1, 17.20, 0.00, 10.30, fx_beaconh , //upper beacon light.1 =1, 0.00, 0.00, -4.30, fx_beaconh , //lower beacon light.2 =3, -12.00, -58.00, 4.65, fx_navredm , //left nav light.3 =4, -17.95, -58.80, 4.21, fx_navwhi , //left id/tail logo light light.4 =2, -13.00, -58.80, 4.65, fx_strobeh , //left wing strobe light.5 =3, -12.00, 58.00, 4.65, fx_navgrem , //right nav light.6 =4, -17.95, 58.80, 4.21, fx_navwhi , //right id/tail logo light light.7 =2, -13.00, 58.80, 4.65, fx_strobeh, //right wing strobe light.8 =3, -64.50, 0.00, 7.00, fx_navwhi , //aft id light.9 =3, -64.50, 0.00, 7.00, fx_strobeh , //aft strobe light.10=4, 61.00, 0.00, 5.50, B738_vclight , //cockpit illumination //light.11=5, 29.40, -6.65, 2.50, fx_navwhih , //left wing inspection light //light.12=5, 29.40, 6.65, 2.50, fx_navwhih , //right wing inspection light [keyboard_response] elevator=150,250 aileron= 150,250 rudder= 150,250 [direction_indicators] direction_indicator.0=3,0 [fuel] Center1= 11.50, 0.00,-1.50, 3437.00, 7.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain= 4.50, -20.00,-0.00, 1719.00, 5.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain= 4.50, 20.00,-0.00, 1719.00, 5.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1800.0 autothrottle_available= 1 autothrottle_arming_required= 1 autothrottle_max_rpm= 98 autothrottle_takeoff_ga= 1 pitch_takeoff_ga= 8 use_no_default_pitch= 1 use_no_default_bank= 1 default_pitch_mode=0 default_bank_mode=0 max_pitch=10.000000 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=10.000000 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=0.360000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=1.000000 [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 Adf.2 = 1 Transponder.1 = 1 Marker.1 = 1 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdr5 concrete=fx_sparks touchdown=fx_tchdwn, 1 [brakes] toe_brakes_scale=0.798702 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=24.637185 flap_limit_idle=5.031985 [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
