// WARNING NEVER TAKE OFF "FREEWARE_COPYRIGHT_TenkuuDevelopersStudio_01JUN2013" from under // If you do those , wings will be gone and other unexpected things will happen. // OPTANT and the following 0 and 1 is for the Option antenna OFF/ON // You can just control by changing the number . 0 = OFF 1 = ON // [fltsim.0] title=Plane0 FREEWARE_COPYRIGHT_TenkuuDevelopersStudio_ OPTANT1110000000_OPTDEC11110 sim=Boeing 787-800 RR model= panel= sound= texture=BA VC checklists= atc_airline= atc_id=G-ZBJB atc_flight_number=3 atc_heavy=1 atc_parking_types=GATE,RAMP,CARGO atc_parking_code=BCA ui_manufacturer=Boeing ui_type=787-8 ui_variation=BA VC visual_damage=1 description=The Boeing 787 Dreamliner is a long-range, mid-size wide-body, twin-engine jet airliner developed by Boeing Commercial Airplanes. It seats 210 to 290 passengers, depending on the variant. Boeing states that it is the company's most fuel-efficient airliner and the world's first major airliner to use composite materials for most of its construction.[4] The 787 consumes 20% less fuel than the similarly-sized Boeing 767.[5] Some of its distinguishing features include a four-panel windshield, noise-reducing chevrons on its engine nacelles, and a smoother nose contour. The aircraft's initial designation was 7E7, prior to its renaming in January 2005.[6] The first 787 was unveiled in a roll-out ceremony on July 8, 2007, at Boeing's Everett assembly factory, by which time it had become the fastest-selling wide-body airliner in history with 677 orders.[7] By October 2011, 797 Boeing 787s had been ordered by 57 customers, with ILFC having the largest number on order.[8] The 787 development and production has involved a large-scale collaboration with numerous suppliers around the globe. Final assembly is at the Boeing Everett Factory in Everett, Washington. Aircraft will also be assembled at a new factory in North Charleston, South Carolina. Both sites will deliver 787s to airline customers. Originally planned to enter service in May 2008, the project has suffered from multiple delays. The airliner's maiden flight took place on December 15, 2009, and completed flight testing in mid-2011. Final Federal Aviation Administration and European Aviation Safety Agency certification was received in late August 2011 and the first model was delivered in late September 2011. It entered commercial service on October 26, 2011. atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 [weight_and_balance] max_gross_weight = 502433 empty_weight = 252499 reference_datum_position = 10, 0, 0 empty_weight_CG_position = -10, 0, 0 empty_weight_pitch_MOI = 18000000 empty_weight_roll_MOI = 5500000 empty_weight_yaw_MOI = 16300000 empty_weight_coupled_MOI = 2048 max_number_of_stations = 5 station_load.0 = 3450, 34.07, 0, -0.24, First station_load.1 = 3450, -8.69, 0, 0, Business station_load.2 = 8400, -54.10, 0, 0, Coach station_load.3 = 7000, 36.44, 0, -5.62, F. Cargo station_load.4 = 7000, -47.88, 0, -5.62, R. Cargo [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 8, 7.7, -27, -1, tdsb8_wing_light light.1 = 8, 7.7, 27, -1, tdsb8_wing_light light.2 = 3, 54.787, 0, -8.5, tdsnose_gearwell light.3 = 3, 54.787, 0, -8.5, fx_beaconb [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 0.50 min_throttle_limit = -0.25 engine.0 = 1, -32.42, -7.95, engine.1 = 1, 32.42, -7.95, [jet_engine] thrust_scalar = 1.24 [TurbineEngineData] bypass_ratio=10.00000 fuel_flow_gain=0.004 inlet_area=56 rated_N1_rpm=2683.000 rated_N2_rpm=13391.000 static_thrust=74511.000 afterburner_available=0 reverser_available=1 [smokesystem] smoke.0 = -6.360, 14.000, -26.060, Opensky_revspray smoke.1 = -6.360, 14.000, 26.060, Opensky_revspray [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt touchdown = fx_tchdwn, 1 windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 2 electric_pump = 1 Center1 = 13.86, 0, -7.01, 22150, 50 LeftMain = 0, -27.61, -2.02, 5542.6, 27.4 RightMain = 0, 27.61, -2.02, 5542.6, 27.4 [contact_points] static_pitch = -1 static_cg_height = 19.0275 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 28 point.0 = 1, 54.75722, 1.2825, -18.5, 1100, 0, 1.66, 70, 1.0, 2.07021, 0.85, 10.0, 13, 0, 270, 285 point.1 = 1, 54.75722, -1.2825, -18.5, 1100, 0, 1.66, 70, 1.0, 2.07021, 0.85, 10.0, 13, 0, 270, 285 point.2 = 1, -17.4028, -18, -18.9, 1100, 1, 2.05, 0, 1.9, 1.0207, 0.95, 9.9, 13, 2, 270, 285 point.3 = 1, -22.6639, -18, -18.9, 1100, 1, 2.05, 0, 1.9, 1.13289, 0.95, 9.9, 13, 2, 270, 285 point.4 = 1, -22.6639, -14.1335, -18.9, 1100, 1, 2.05, 0, 1.9, 1.13289, 0.95, 9.9, 13, 2, 270, 285 point.5 = 1, -17.4028, -14.1335, -18.9, 1100, 1, 2.05, 0, 1.9, 1.13289, 0.95, 9.9, 13, 2, 270, 285 point.6 = 1, -17.4028, 14.1335, -18.9, 1100, 2, 2.05, 0, 1.9, 1.13289, 0.95, 9.9, 13, 3, 270, 285 point.7 = 1, -22.6639, 14.1335, -18.9, 1100, 2, 2.05, 0, 1.9, 1.13289, 0.95, 9.9, 13, 3, 270, 285 point.8 = 1, -22.6639, 18, -18.9, 1100, 2, 2.05, 0, 1.9, 1.13289, 0.95, 9.9, 13, 3, 270, 285 point.9 = 1, -17.4028, 18, -18.9, 1100, 2, 2.05, 0, 1.9, 1.13289, 0.95, 9.9, 13, 3, 270, 285 point.10 = 2, -112.1483, -32.302, 6.1934, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.11 = 2, -112.3419, 32.2605, 6.1525, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.12 = 2, -59.8324, 98.3261, 9.23, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.13 = 2, -59.8324, -98.3261, 9.23, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.14 = 2, -110.6399, 0, 37.3906, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.15 = 2, -110.5517, 0, 1.8579, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.16 = 2, 53.4688, 0, 8.2111, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.17 = 2, 1.9787, 0, -10.6872, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.18 = 2, 46.5784, 0, -10.4012, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.19 = 2, -52.3725, 0, -10.4266, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.20 = 2, -81.4922, 0, -6.4418, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.21 = 2, 14.6689, 32.9365, -13.0471, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.22 = 2, 14.6689, -32.9365, -13.0471, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.23 = 2, 8.4836, 32.9368, -13.9413, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.24 = 2, 8.4836, -32.9368, -13.9413, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.25 = 2, 8.4836, 38.9609, -7.2304, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.26 = 2, 8.4836, -38.9609, -7.2304, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.27 = 2, 72.7294, 0, -4.6621, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 [keyboard_response] elevator = 100.000, 200.000 aileron = 100.000, 200.000 rudder = 100.000, 200.000 [forcefeedback] gear_bump_nose_magnitude = 6000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 6000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 6000 gear_bump_right_direction = 00500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5.0 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1.0 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [airplane_geometry] wing_area = 3501.3926 wing_span = 197.30 wing_root_chord = 36.11 wing_dihedral = 7.80 wing_incidence = 5 wing_twist = 6 oswald_efficiency_factor = 0.600 wing_winglets_flag = 1 wing_sweep = 35 wing_pos_apex_lon = 17.41 wing_pos_apex_vert = -6.05 htail_area = 762.19 htail_span = 64.51 htail_pos_lon = -69.36 htail_pos_vert = 1 htail_incidence = -1.5 htail_sweep = 40 vtail_area = 571.87 vtail_span = 31.45 vtail_sweep = 45.5 vtail_pos_lon = -60.13 vtail_pos_vert = 5.78 elevator_area = 254.000 aileron_area = 115.000 rudder_area = 195.29 elevator_up_limit = 32.54 elevator_down_limit = 26.93 aileron_up_limit = 32.20 aileron_down_limit = 16.94 rudder_limit = 32.10 elevator_trim_limit = 20 spoiler_limit = 63 aileron_to_spoileron_gain = 1.5 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 10.000 min_flaps_for_spoilerons = 0 spoilerons_available = 1 auto_spoiler_available=1 spoiler_extension_time=2.000000 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 = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1,1 electric_always_available = 1 flap_motor = 0, 5, 17 [flight_tuning] cruise_lift_scalar=0.5 parasite_drag_scalar=1.0 induced_drag_scalar=1.1 elevator_effectiveness=1.0 aileron_effectiveness=3.5 rudder_effectiveness=1.5 pitch_stability=1. roll_stability=0.5 yaw_stability=1.00 elevator_trim_effectiveness=0.8 aileron_trim_effectiveness=0.50 rudder_trim_effectiveness=0.50 [pitot_static] vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [Reference Speeds] flaps_up_stall_speed=176.0 full_flaps_stall_speed=120.00 cruise_speed=485.00 max_indicated_speed=360.000000 max_mach=0.89 [Views] eyepoint=37.50, -1.46, 2.15 //eyepoint=72.50, -1.86, 2.25 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000 autothrottle_available=1 use_no_default_pitch= 1 use_no_default_bank= 1 pitch_takeoff_ga=18 autothrottle_arming_required= 1 autothrottle_takeoff_ga= 1 autothrottle_max_rpm= 105.00 default_pitch_mode=0 default_bank_mode=0 max_pitch= 10.00 max_pitch_acceleration= 2.00 max_pitch_velocity_lo_alt= 4.00 max_pitch_velocity_hi_alt= 1.50 max_pitch_velocity_lo_alt_breakpoint= 20000 max_pitch_velocity_hi_alt_breakpoint= 24000 max_bank= 25.00 max_bank_acceleration= 2.0 max_bank_velocity= 3.0 max_throttle_rate= 0.030 nav_proportional_control= 12.00 nav_integrator_control= 0.05 nav_derivative_control= 0.01 nav_integrator_boundary= 0.5 nav_derivative_boundary= 0.35 gs_proportional_control= 15.0 gs_integrator_control= 0.30 gs_derivative_control= 0.00 gs_integrator_boundary= 0.7 gs_derivative_boundary= 0.00 yaw_damper_gain= 1.00 [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 [Flaps.0] type=1 span-outboard=0.800000 extending-time=20 lift_scalar=0.5 drag_scalar=.3 pitch_scalar=0.5 span-outboard = 0.8 damaging-speed= 260.0 blowout-speed = 280.0 flaps-position.0=0.0,0.000000 flaps-position.1=0.0,0.000000 flaps-position.2=5,0.000000 flaps-position.3=15.0,0.000000 flaps-position.4=20.0,0.000000 flaps-position.5=25.0,0.000000 flaps-position.6=30.0,0.000000 [Flaps.1] type=2 span-outboard=0.800000 extending-time=10.800000 system_type=1 lift_scalar=0.6 drag_scalar=0.3 pitch_scalar=0.6 flaps-position.0=0.0,0.000000 flaps-position.1=17.0,0.000000 flaps-position.2=17.0,0.000000 flaps-position.3=17.0,0.000000 flaps-position.4=17.0,0.000000 flaps-position.5=35.0,0.000000 flaps-position.6=35.0,0.000000 [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=0.580 parking_brake=1 auto_brakes=4 [hydraulic_system] electric_pumps=1 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [exits] number_of_exits = 4 exit_rate.0 = 0.10 ;Percent per second exit_rate.1 = 0.08 ;Percent per second exit_rate.2 = 0.10 ;Percent per second exit_rate.3 = 0.10 ;Percent per second [General] performance=Passengers\n3-class conf: 300 \n2-class conf: 400 \n1-class conf: 440\n\nCargo\n32 LD-3 containers aft \n600 cubic Ft (17 cubic m)\nTotal lower hold volume: 5,656 cu ft \n\nDimensions\nSpan 199 ft 11 in\nLength 209 ft 1 in\nHeight 64 ft 7 in \n (--max 58 ft 8 in--min)\n\nEngines: RR Trent 895\nTO Thrust Rating: 93,400 lb\n\nMax Fuel Cap.: 45,220 gal\nMaxTOW: 656,000 lb\nZFW: 429,110 lb\n\nMax Range: 7,695 nm (14,260 km)\nTypical Cruise Speed \n @ FL350: M.84 Category=airplane [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