[fltsim.0] title=Pacific Sun Airways Boeing 737-200ADV sim=737-200adv model= panel= sound= texture= kb_checklists=Boeing737-200_check kb_reference=Boeing737-200_ref atc_id= atc_airline= atc_flight_number=291 ui_manufacturer=Boeing ui_type="737-200" ui_variation= description="Boeing 737-247 ADV with JT8D-17 engines, Paint by Alexander Ho [General] atc_type=BOEING atc_model=B732 performance=Cruise Speed\t.72 - .78 MachMaximum Range\t2,100 nmService Ceiling\t35,000 ftMax Takeoff Weight124,000 lbSeating\t\t112 to 118Cargo Capacity\txxxx CU ft editable=0 Category=airplane [pitot_static] vertical_speed_time_constant=999 pitot_heat=1.000000 [weight_and_balance] max_gross_weight = 117000 empty_weight = 61890 reference_datum_position = 0.0, 0.0, 0.0 empty_weight_CG_position = 1.20, 0, 0 empty_weight_pitch_MOI = 571131 empty_weight_roll_MOI = 384600 empty_weight_yaw_MOI = 930732 empty_weight_coupled_MOI = 2000 max_number_of_stations = 30 station_load.0 = 110, 43.5, -1.36, 5.5, Captain station_load.1 = 165, 43.5, 1.361, 5.5, First Officer station_load.2 = 165, 36, -3, 4, Flight Attendant station_load.3 = 165, 36, -1.44, 4, Flight Attendant station_load.4 = 660, 30, 0, 4, 1A to 1F //6 seats per row 660 = 4 of 6 occupied per row x 165 station_load.5 = 660, 27, 0, 4, 2A to 2F station_load.6 = 660, 24, 0, 4, 3A to 3F station_load.7 = 660, 21, 0, 4, 4A to 4F station_load.8 = 660, 18, 0, 4, 5A to 5F station_load.9 = 660, 15, 0, 4, 6A to 6F station_load.10 = 660, 12, 0, 4, 7A to 7F station_load.11 = 660, 9, 0, 4, 8A to 8F station_load.12 = 660, 6, 0, 4, 9A to 9F station_load.13 = 660, 2, 0, 4, 10A to 10F station_load.14 = 660, -1, 0, 4, 11A to 11F station_load.15 = 660, -4, 0, 4, 12A to 12F station_load.16 = 660, -7, 0, 4, 13A to 13F station_load.17 = 660, -10, 0, 4, 14A to 14F station_load.18 = 660, -13, 0, 4, 15A to 15F station_load.19 = 660, -16, 0, 4, 16A to 16F station_load.20 = 660, -19, 0, 4, 17A to 17F station_load.21 = 660, -22, 0, 4, 18A to 18F station_load.22 = 660, -25, 0, 4, 19A to 19F station_load.23 = 660, -28, 0, 4, 20A to 20F station_load.24 = 165, -33, -3, 4, Flight Attendant station_load.25 = 165, -33, -1.44, 4, Flight Attendant station_load.26 = 1200, 27, 0, -0.98, Cargo Hold 1FWD //Maximum 2146 lbs station_load.27 = 2000, 18, 0, -0.98, Cargo Hold 2FWD //Maximum 3340 lbs station_load.28 = 1700, -7, 0, -0.98, Cargo Hold 1AFT //Maximum 4040 lbs station_load.29 = 1500, -16, 0, -0.98, Cargo Hold 2AFT //Maximum 3459 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 1, 8.3558, 0.0000, 9.4058, fx_beacon, light.1 = 1, 11.3558, 0.0000, -3.9672, fx_beacon, light.2 = 3, -13.1086, -46.3622, 2.5446, fx_navred , light.3 = 3, -13.1086, 46.3622, 2.5446, fx_navgre , light.4 = 3, -48.5807, 0.0000, 7.1568, fx_navwhi , light.5 = 3, -17.3041, -46.1595, 2.3199, fx_navwhi , light.6 = 3, -17.3041, 46.1595, 2.3199, fx_navwhi , light.7 = 2, -12.5919, -46.2687, 2.5669, fx_strobeh, light.8 = 2, -12.5919, 46.2687, 2.5669, fx_strobeh, [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 1.64 engine.0 = 0, -17, -2.5 engine.1 = 0, 17, -2.5 min_throttle_limit=-0.25 [smokesystem] // lon/vert/lat smoke.0 = -16.5, -2.5, -17, fx_smoke_JT8D.fx smoke.1 = -16.5, -2.5, 17, fx_smoke_JT8D.fx [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 contrail = fx_contrail_l [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 Center1 = 6.25, 0, -0.2, 2303.7, 0 // 15433 lbs max LeftMain = 1.5, -9.6, -0.2, 1428.15, 0 // 9567 lbs max RightMain = 1.5, 9.6, -0.2, 1428.15, 0 RightTip = 0.0, 0.0, 0.0, 1.0, 0 //DO NOT REMOVE presence of this tank used to identify Terry Gaff/Flight1 model electric_pump=0 [contact_points] static_pitch = -0.4 static_cg_height = 7.45 max_number_of_points = 8 point.0 = 1.000, 37.94, 0.0000, -7.6000, 900.00, 0.000, 1.000, 78.000, 0.3047, 1.900, 0.867, 4.600, 4.5, 0, 285, 310 point.1 = 1.000, -1.81, -9.8248, -9.5892, 1500.00, 1.000, 3.333, 0.000, 1.9410, 1.000, 0.879, 5.500, 5.9, 2, 285, 310 point.2 = 1.000, -1.81, 9.8248, -9.5892, 1500.00, 2.000, 3.333, 0.000, 1.9410, 1.000, 0.879, 5.500, 5.9, 3, 285, 310 point.3 = 2.000, 5.66, -48.4500, 3.0000, 787.80, 0. 0.0, 0.000, 0.000, 0.0000, 0.000, 0.000, 0.000, 5.0, 0, 0 point.4 = 2.000, 5.66, 48.4500, 3.0000, 787.80, 0, 0.0, 0.000, 0.000, 0.0000, 0.000, 0.000, 0.000, 6.0, 0, 0 point.5 = 2.000, -44.66, 0.0000, 7.6000, 787.80, 0, 0.0, 0.000, 0.000, 0.0000, 0.000, 0.000, 0.000, 9.0, 0, 0 point.6 = 2.000, 58.94, 0.0000, 1.7500, 787.80, 0, 0.0, 0.000, 0.000, 0.0000, 0.000, 0.000, 0.000, 4.0, 0, 0 point.7 = 2.000, -15.76, 0.0000, -2.3000, 787.80, 0, 0.0, 0.000, 0.000, 0.0000, 0.000, 0.000, 0.000, 4.0, 0, 0 gear_system_type=0 [keyboard_response] elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [forcefeedback] gear_bump_nose_magnitude = 1000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 450 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 2000 crash_direction1 = 1000 crash_magnitude2 = 2000 crash_direction2 = 9000 crash_period2 = 7500 crash_duration2 = 2500000 stick_shaker_magnitude = 2000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] wing_area = 980.000 wing_span = 93.000 wing_root_chord = 10.54 wing_dihedral = 0.000 wing_incidence = 1 wing_twist = 0 oswald_efficiency_factor = 0.77 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 4.6376 wing_pos_apex_vert = 0 htail_area = 312.00 htail_span = 30.000 htail_pos_lon = -40.0 htail_pos_vert = 7.112 htail_incidence = 1.50 htail_sweep = 35.000 vtail_area = 224.000 vtail_span = 22.5 vtail_sweep = 0.000 vtail_pos_lon = -37 vtail_pos_vert = 9.25 elevator_area = 70.46 aileron_area = 13.4 rudder_area = 56.2 elevator_up_limit = 22.00 elevator_down_limit = 18.00 aileron_up_limit = 30.000 aileron_down_limit = 20.000 rudder_limit = 25.000 elevator_trim_limit = 17.000 spoiler_limit = 60.000 aileron_to_spoileron_gain = 3.00 min_ailerons_for_spoilerons = 12.50 min_flaps_for_spoilerons = 0.0000 spoilerons_available = 1 auto_spoiler_available=0 spoiler_extension_time=1.500000 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 [electrical] max_battery_voltage = 28 generator_alternator_voltage = 28 max_generator_alternator_amps = 400 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 0, 5, 17 pitot_heat = 0, 2, 17 additional_system = 1, 2, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 2, 20, 17 starter2 = 2, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 [flight_tuning] cruise_lift_scalar=1.00 parasite_drag_scalar=1.00 induced_drag_scalar=1.00 elevator_effectiveness=1.00 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.200 yaw_stability=1.000 elevator_trim_effectiveness=1.00 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [gear_warning_system] gear_warning_available=1 //Normal pct_throttle_limit=0.1 //Percent throttle that activates warning flap_limit_idle=1.0 //Flap angle that activates warning at idle flap_limit_power=15.0 //Flap angle that activates warning at above idle [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=1.0 //Brake scalar auto_brakes=4 [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=44.45, -2.25, 6.25 //(feet) longitudinal, lateral, vertical distance from reference datum [Radios] // 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 Adf.2=1 Transponder.1=1 Marker.1=1 [direction_indicators] direction_indicator.0=3,0 //Electric-Mag gyros [attitude_indicators] attitude_indicator.0=2,2 [turn_indicators] turn_indicator.0=1,0 [Airspeed_indicators] airspeed_indicator.0=0.9826, 0.0 //Calibrates IAS to CAS [exits] //Exits number_of_exits=2 exit_rate.0=0.2 ;Percent per second exit_rate.1=0.2 ;Percent per second [TailHook] //Leading Flaps Landing Lights tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=0.7 [folding_wings] //Ground Spoilers wing_fold_system_type = 4 ;0=None fold_rates = 3.0,3.0 ;Percent per second [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=2500 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=100 autothrottle_takeoff_ga=1 pitch_takeoff_ga=12 max_pitch=10.0 max_pitch_acceleration=2.5 max_pitch_velocity_lo_alt=4.0 max_pitch_velocity_hi_alt=2.0 max_pitch_velocity_lo_alt_breakpoint=15000.0 max_pitch_velocity_hi_alt_breakpoint=25000.0 max_bank=25.0 max_bank_acceleration=2.0 max_bank_velocity=3.0 max_throttle_rate=5.0 nav_proportional_control=15.00 nav_integrator_control=0.125 nav_derivative_control=9.0 nav_integrator_boundary=0.50 nav_derivative_boundary=5.0 gs_proportional_control=25.00 gs_integrator_control=1.00 gs_derivative_control=0.00 gs_integrator_boundary=0.50 gs_derivative_boundary=0.00 yaw_damper_gain=1.0 use_no_default_pitch=1 default_bank_mode=2 default_pitch_mode=0 [Reference Speeds] flaps_up_stall_speed=175.000 full_flaps_stall_speed=140.000 cruise_speed=430.000 max_mach=0.84 max_indicated_speed=350 //Red line (KIAS) [stall_warning] type=1 stick_shaker=1 [Flaps.0] // trailing edge flaps - Inboard flaps between root chord wing and turbine type=1 span-outboard=0.800 extending-time=40.000 system_type=1 damaging-speed=250.000 blowout-speed=280.000 lift_scalar=0.40 drag_scalar=0.25 pitch_scalar=1.250 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] // trailing edge flaps - outboard flaps between turbine and tip chord wing type=1 span-outboard=0.800 extending-time=40.000 system_type=1 damaging-speed=250.000 blowout-speed=280.000 lift_scalar=0.50 drag_scalar=0.25 pitch_scalar=1.450 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.2] // leading edge Slats setting - Inboard flaps between root chord wing and turbine type= 2 span-outboard= 0.800 extending-time=15.000 system_type= 1 damaging-speed= 280.000 blowout-speed= 320.000 lift_scalar= 0.50 drag_scalar= 0.10 pitch_scalar=0.10 flaps-position.0= 0.000 flaps-position.1= 0.500 flaps-position.4= 1.000 [Flaps.3] // leading edge flap setting - outboard devices between turbine and tip chord wing type= 2 span-outboard= 0.800 extending-time=5.000 system_type= 1 damaging-speed= 280.000 blowout-speed= 320.000 lift_scalar= 0.50 drag_scalar= 0.20 pitch_scalar=0.500 flaps-position.0= 0.000 flaps-position.1= 1 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=9.850 rated_N2_rpm=12250 //HPC maximum RPM static_thrust=17000 //Static Thrust for JT8D-17 (-15 and -9 are derated internally by the panel) afterburner_available=0 reverser_available=1 [jet_engine] thrust_scalar=1 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0
