[fltsim.0] title=Boeing 737-800 West Indies sim=Boeing737-800 model= panel= sound= texture= visual_damage=1 checklists=Boeing737-400_check reference=Boeing737-400_ref atc_heavy=0 atc_id=N951AA atc_airline=West Indian atc_flight_number=249 ui_manufacturer=Boeing ui_type=B-737-800 ui_variation=West Indies description=BWIA West Indies Airways, called "Bwee" by locals, is the national airline of Trinidad and Tobago.\nOriginal Model: FFX/SGA\nRepaint: Alejandro Hurtado [General] atc_heavy=0 atc_type=BOEING AIRCRAFT atc_model=B737 performance=Power: 2x CFM56-7B26 @ 26300 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\nLength: 129 ft 6 in (33.6 m)\nHeight: 41 ft 2 in (12.5 m)\nWingspan: 112 ft 7 in (34.4 m). 737-800 FDE by Mike Baumann FFX-Flight FX Group [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=2.00 pitch_stability=1.10 roll_stability=1.00 yaw_stability=1.00 parasite_drag_scalar=1.20 induced_drag_scalar=1.20 elevator_effectiveness=1.20 aileron_effectiveness=0.90 rudder_effectiveness=0.90 elevator_trim_effectiveness=1.00 aileron_trim_effectiveness=1.00 rudder_trim_effectiveness=1.00 [jet_engine] thrust_scalar=1.10 [WEIGHT_AND_BALANCE] reference_datum_position=0.00,0.00,0.00 empty_weight_CG_position=0.00,0.00,0.00 max_number_of_stations=60 station_load.0=200,60.00,-1.90,4.00 station_load.1=190,60.00, 1.90,4.00 station_load.2=5216,14.50,-17.30,-4.10 station_load.3=5216,14.50, 17.30,-4.10 station_load.4=600,55.50,-2.50,3.80 station_load.5=600,55.50, 2.50,3.80 station_load.6=600,52.16,-2.50,3.80 station_load.7=340,48.82,-2.50,4.00 station_load.8=170,48.82,2.50,4.00 station_load.9=170,45.48,-2.50,4.00 station_load.10=170,45.48,2.50,4.00 station_load.11=170,42.14,-2.50,4.00 station_load.12=340,42.14,2.50,4.00 station_load.13=340,38.80,-2.50,4.00 station_load.14=510,38.80,2.50,4.00 station_load.15=170,35.46,-2.50,4.00 station_load.16=170,35.46,2.50,4.00 station_load.17=340,32.12,-2.50,4.00 station_load.18=510,28.78,-2.50,4.00 station_load.19=170,28.78,2.50,4.00 station_load.20=340,25.44,2.50,4.00 station_load.21=510,22.10,-2.50,4.00 station_load.22=340,22.10,2.50,4.00 station_load.23=170,18.76,-2.50,4.00 station_load.24=170,18.76,2.50,4.00 station_load.25=340,15.42,2.50,4.00 station_load.26=510,12.08,-2.50,4.00 station_load.27=170,12.08,2.50,4.00 station_load.28=170,8.74,-2.50,4.00 station_load.29=170,8.74,2.50,4.00 station_load.30=340,5.40,-2.50,4.00 station_load.31=510,5.40,2.50,4.00 station_load.32=510,2.06,-2.50,4.00 station_load.33=170,2.06,2.50,4.00 station_load.34=170,-1.28,-2.50,4.00 station_load.35=340,-1.28,2.50,4.00 station_load.36=170,-4.62,2.50,4.00 station_load.37=510,-7.96,-2.50,4.00 station_load.38=510,-7.96,2.50,4.00 station_load.39=170,-11.30,-2.50,4.00 station_load.40=170,-11.30,2.50,4.00 station_load.41=340,-14.64,-2.50,4.00 station_load.42=170,-17.98,2.50,4.00 station_load.43=510,-21.32,-2.50,4.00 station_load.44=170,-21.32,2.50,4.00 station_load.45=340,-24.66,2.50,4.00 station_load.46=340,-28.00,-2.50,4.00 station_load.47=340,-28.00,2.50,4.00 station_load.48=510,-31.34,-2.50,4.00 station_load.49=170,-31.34,2.50,4.00 station_load.50=170,-34.68,-2.50,4.00 station_load.51=340,-38.02,2.50,4.00 station_load.52=340,-41.36,-2.50,4.00 station_load.53=510,-41.36,2.50,4.00 station_load.54=170,-44.70,-2.50,4.00 station_load.55=170,-44.70,2.50,4.00 station_load.56=170,-48.04,2.50,4.00 station_load.57=1200,-51.50,0.00,3.80 station_load.58=5600,35.00,0.00,-1.00 station_load.59=4800,-25.00,0.00,-1.00 empty_weight=126200.00 empty_weight_roll_MOI=1854568.00 empty_weight_pitch_MOI=1794268.00 empty_weight_yaw_MOI=2209567.00 empty_weight_coupled_MOI=1300.00 [GeneralEngineData] engine_type=1 Engine.0=13.50, -17.30, -4.10 Engine.1=13.50, 17.30, -4.10 fuel_flow_scalar=1.0 [TurbineEngineData] fuel_flow_gain=0.0035 inlet_area=20.3320 rated_N2_rpm=29920.0000 static_thrust=26300.0000 afterburner_available=0 reverser_available=1 [airplane_geometry] wing_area=1341.000 wing_span=112.700 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=0 wing_sweep=25.000 wing_pos_apex_lon=11.600 wing_pos_apex_vert=0.000 htail_area=348.000 htail_span=47.100 htail_pos_lon=-52.150 htail_pos_vert=7.000 htail_incidence=0.697 htail_sweep=30.000 vtail_area=308.000 vtail_span=27.200 vtail_sweep=35.000 vtail_pos_lon=-44.600 vtail_pos_vert=10.300 elevator_area=70.500 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 NO EFFECT ON ACTUAL FLYING flaps_up_stall_speed=140 full_flaps_stall_speed=115 cruise_speed=475 //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, 55.00, 0.00, -9.90, 1574.80, 0, 1.650, 78.0, 0.400, 2.3, 0.700, 5.10, 5.30,0, 200, 280 //nose gear point.1=1, -0.75, -9.50, -9.10, 1574.80, 1, 2.000, 0.0, 0.400, 2.5, 0.600, 5.30, 5.70,2, 200, 280 //left main point.2=1, -0.75, 9.50, -9.10, 1574.80, 2, 2.000, 0.0, 0.400, 2.5, 0.600, 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 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 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=-1.50 static_cg_height=8.70 [Flaps.0] type=1 span-outboard=0.800 extending-time=12.00 system_type=1 damaging-speed=280.000 blowout-speed=320.000 lift_scalar=2.0 drag_scalar=1.2 pitch_scalar=0.5 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=0.8 extending-time=2 system_type=1 damaging-speed=280 blowout-speed=320 lift_scalar=2.0 drag_scalar=1.0 pitch_scalar=0.2 flaps-position.0=0.000 flaps-position.1=2.000 [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 //Increasing this value will cause a more instantaneous reaction in the VSI [exits] number_of_exits=1 exit_rate.0=0.28 [TailHook] tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=0.5 [folding_wings] wing_fold_system_type=4 fold_rates=0.15,0.15 [Views] eyepoint=60.00,-1.90,5.10 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=1, 2.20, 0.00, 10.30, fx_beaconh , light.1=1, 0.00, 0.00, -4.20, fx_beaconb , light.2=3, -12.00, -58.00, 4.65, fx_navredm , light.3=3, -17.95, -58.80, 4.21, fx_navwhi , light.4=2, -13.00, -58.80, 4.65, fx_strobeh , light.5=3, -12.00, 58.00, 4.65, fx_navgrem , light.6=3, -17.95, 58.80, 4.21, fx_navwhi , light.7=2, -13.00, 58.80, 4.65, fx_strobeh , light.8=3, -64.50, 0.00, 7.00, fx_navwhi , light.9=2, -64.50, 0.00, 7.00, fx_strobeh , light.10=4, 61.00, 0.00, 5.50, fx_vclight , [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, 4302.00, 7.00 LeftMain=4.50, -20.00, 0.00, 1288.00, 8.00 RightMain=4.50, 20.00, 0.00, 1288.00, 8.00 fuel_type=2 number_of_tank_selectors=1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=800.0 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 [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