[fltsim.0] title=TVA Pelican sim=pelican model= panel= sound= texture=TVA2 kb_checklists= kb_reference= atc_id=N700MS atc_airline=Transload atc_flight_number=1123 atc_parking_types=GATE,RAMP ui_manufacturer=Transload Airlines ui_type=Boeing Pelican ui_variation=Cargo/Boeing Corp. description=The Boeing Pelican ULTRA (Large Transport Aircraft) is a proposed ground effect airplane under study by Boeing Phantom Works. Intended as a large-capacity transport craft for military or civilian use, it would have a wingspan of 500 feet, a cargo capacity of 1,400 tons, and a range of 10,000 miles. Powered by four turboprop engines, its main mode would be to fly 20-50 feet over water, though it would also be capable of overland flight at a higher altitude but lesser range. It would operate from conventional runways, with its weight distributed over 38 fuselage-mounted landing gears with 76 wheels. atc_heavy=1 atc_id_font=Verdana,-11,1,600,0 atc_id_color=0x00000000 visual_damage=0 [fltsim.1] title=TVA_Pelican sim=pelican model= panel= sound= texture=TVA1 kb_checklists= kb_reference= atc_id=N700MS atc_airline=Transload atc_flight_number=1123 atc_parking_types=GATE,RAMP ui_manufacturer=Transload Airlines ui_type=Boeing Pelican ui_variation=Cargo Division description=The Boeing Pelican ULTRA (Large Transport Aircraft) is a proposed ground effect airplane under study by Boeing Phantom Works. Intended as a large-capacity transport craft for military or civilian use, it would have a wingspan of 500 feet, a cargo capacity of 1,400 tons, and a range of 10,000 miles. Powered by four turboprop engines, its main mode would be to fly 20-50 feet over water, though it would also be capable of overland flight at a higher altitude but lesser range. It would operate from conventional runways, with its weight distributed over 38 fuselage-mounted landing gears with 76 wheels. atc_heavy=1 atc_id_font=Verdana,-11,1,600,0 atc_id_color=0x00000000 visual_damage=0 [General] atc_type=BOEING atc_model=Pelican editable=1 performance=Length: 400 ft (122 m)\nWingspan: 500 ft (152 m)\nUseful load: 2,800,000 lb (1400 tons) (1,272,727 kg) Category=airplane [weight_and_balance] // ACM V2.5 max_gross_weight = 4000000.000 empty_weight = 1200000.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 empty_weight_pitch_MOI = 360000000.000 empty_weight_roll_MOI = 420000000.000 empty_weight_yaw_MOI = 770000000.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit = 0.000 CG_aft_limit = 1.000 max_number_of_stations = 3 station_load.0 =800000.000000, -40.000000, 0.000000, 0.000000, Station 1 station_load.1 =800000.000000, 0.000000, 0.000000, 0.000000, Station 2 station_load.2 =800000.000000, 40.000000, 0.000000, 0.000000, Station 3 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 0.00, -250.43, -12.50, fx_navredh , light.1 = 3, 0.00, 250.43, -12.50, fx_navgreh , light.2 = 3, -270.73, 0.00, 23.37, fx_navwhih , light.3 = 3, 0.00, -250.43, -12.50, fx_strobeh , light.4 = 3, 0.00, 250.43, -12.50, fx_strobeh , light.5 = 2, -20.24, 0.00, -23.04, fx_beaconh , light.6 = 1, 7.98, 0.00, 27.50, fx_beaconh , light.7 = 4, 112.87, 0.00, 23.87, fx_vclighth , [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 5 fuel_flow_scalar = 1.000 min_throttle_limit = -0.25 engine.0 = 48.830, -110.340, 20.860 engine.1 = 48.830, -57.000, 20.860 engine.2 = 48.830, 57.000, 20.860 engine.3 = 48.830, 110.340, 20.860 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks 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 = 1 electric_pump = 1 LeftMain = 0.000, -100.000, 6.000, 28000.000, 0.000 RightMain = 0.000, 100.000, 6.000, 28000.000, 0.000 [contact_points] static_pitch = 0.000 static_cg_height = 30.000 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 7 point.0 = 1.000, 83.000, 0.000, -31.000, 3000.000, 0.000, 3.000, 40.000, 0.250, 4.000, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000 point.1 = 1.000, -10.000, -22.000, -31.000, 5000.000, 1.000, 3.000, 0.000, 0.300, 2.500, 0.800, 8.000, 8.000, 2.000, 0.000, 0.000 point.2 = 1.000, -10.000, 22.000, -31.000, 5000.000, 2.000, 3.000, 0.000, 0.300, 2.500, 0.800, 8.200, 8.200, 3.000, 0.000, 0.000 point.3 = 2.000, -12.237, -254.558, -22.814, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4 = 2.000, -11.748, 255.851, -22.815, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5 = 2.000, -269.376, 0.000, 14.521, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6 = 2.000, 129.903, 0.000, -0.305, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 [keyboard_response] elevator = 150.0, 250.0 aileron = 150.0, 250.0 rudder = 150.0, 250.0 [forcefeedback] gear_bump_nose_magnitude = 3000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2700 gear_bump_left_direction = 9000 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2700 gear_bump_right_direction = 27000 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1300 ground_bumps_angle1 = 08900 ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.20 ground_bumps_magnitude2 = 200 ground_bumps_angle2 = 09100 ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] //ACM_AREAW1// 0,0,0,25.3945,8.6902,8.6902,0.3034,25.6102,17.3806,17.3806 //ACM_AREAW2// 0.6068,25.8258,25.4799,25.4799,0.9103,25.8446,34.7613,34.7613,1.2137,25.8633 //ACM_AREAW3// 42.2697,42.2697,1.5173,25.0939,51.7481,51.7481,1.8207,22.9458,61.4234,61.4234 //ACM_AREAW4// 2.1243,20.6007,69.5227,69.5227,2.4277,18.0585,78.2132,78.2132,9.6259,16.6982 //ACM_AREAH1// 0,0,0,15.6935,3.1080,3.1080,0,16.0809,6.8070,6.8070 //ACM_AREAH2// 0,15.0895,9.9152,9.9152,0,15.6738,13.2202,13.2202,0,15.2734 //ACM_AREAH3// 16.5254,16.5254,0,15.4638,19.8304,19.8304,0,15.0631,23.1354,23.1354 //ACM_AREAH4// 0,15.4505,26.4405,26.4405,0,15.6410,29.1546,29.1546,0,15.6344 //ACM_AREAV1// -0.1968,-0.1968,0,17.2203,2.7232,2.7232,0,17.2294,5.4464,5.4464 //ACM_AREAV2// 0,17.2385,8.1695,8.1695,0,17.0508,10.8928,10.8928,0,17.2569 //ACM_AREAV3// 13.6160,13.6160,0,17.0692,16.1422,16.1422,0,16.6844,18.6685,18.6685 //ACM_AREAV4// 0,16.6935,21.7856,21.7856,0,16.8997,24.1149,24.1149,0,16.7119 //ACM_CAREAW1// 44.4253,44.4253,19.5785,23.8696,47.1945,47.1945,18.9423,23.5704,49.5698,49.5698 //ACM_CAREAW2// 18.5032,22.8771,52.5360,52.5360,18.0638,22.3810,56.4873,56.4873,17.4277,21.2938 //ACM_CAREAW3// 60.8324,60.8324,17.1854,20.6007,62.4197,62.4197,15.9582,19.7105,64.4010,64.4010 //ACM_CAREAW4// 15.9130,19.2143,66.5792,66.5792,15.4737,18.7180,68.5606,68.5606,15.4285,18.4188 //ACM_CAREAH1// 3.3487,3.3487,10.9000,15.8906,4.6840,4.6840,10.7032,15.7888,6.6100,6.6100 //ACM_CAREAH2// 11.0971,15.6871,9.9152,9.9152,10.7032,15.3882,13.2202,13.2202,10.9000,15.6805 //ACM_CAREAH3// 16.3283,16.3283,10.9000,15.5787,19.0424,19.0424,10.9000,15.8709,21.3626,21.3626 //ACM_CAREAH4// 10.7032,15.7691,23.6826,23.6826,10.7032,15.2734,27.1847,27.1847,10.5061,15.3685 //ACM_CAREAV1// 2.5608,2.5608,13.2187,17.5937,4.1020,4.1020,13.2187,17.2042,5.4464,5.4464 //ACM_CAREAV2// 13.2187,17.2089,7.5785,7.5785,13.2187,17.0165,10.3018,10.3018,13.2187,17.4151 //ACM_CAREAV3// 13.0250,13.0250,13.0218,17.2227,16.3393,16.3393,13.2187,16.6362,18.2744,18.2744 //ACM_CAREAV4// 12.8248,17.0349,19.4218,19.4218,13.2187,17.0394,20.7660,20.7660,13.0218,16.8470 wing_area = 36500.000 wing_span = 513.210 wing_root_chord = 83.300 wing_dihedral = 0.000 wing_incidence = 0.000 wing_twist = -1.000 oswald_efficiency_factor = 0.500 wing_winglets_flag = 1 wing_sweep = 2.000 wing_pos_apex_lon = 33.000 wing_pos_apex_vert = 17.670 htail_area = 9800.000 htail_span = 195.170 htail_pos_lon = -214.110 htail_pos_vert = 19.790 htail_incidence = 0.000 htail_sweep = 0.000 vtail_area = 1000.000 vtail_span = 40.410 vtail_sweep = 0.000 vtail_pos_lon = -201.870 vtail_pos_vert = 23.340 elevator_area = 1000.000 aileron_area = 1000.000 rudder_area = 775.000 elevator_up_limit = 18.000 elevator_down_limit = 15.000 aileron_up_limit = 18.000 aileron_down_limit = 18.000 rudder_limit = 30.000 elevator_trim_limit = 10.000 spoiler_limit = 0.000 aileron_to_spoileron_gain = 0.000 spoiler_handle_available = 0 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 spoilerons_available = 0 auto_spoiler_available=0 positive_g_limit_flaps_up=3.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-2.000000 negative_g_limit_flaps_down=-2.000000 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1,1,1,1 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 2, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 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 [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 Transponder.1=1 Marker.1=1 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=4.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=4.000 pitch_stability=2.002 roll_stability=1.000 yaw_stability=2.002 elevator_trim_effectiveness=0.505 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [propeller] thrust_scalar=1.000 propeller_type= 0 propeller_diameter= 50.000 propeller_blades= 6 propeller_moi= 5000.000 beta_max= 45.000 beta_min= 18.000 min_gov_rpm= 4000.000 prop_tc= 0.004 gear_reduction_ratio= 17.000 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 1 prop_deice_available= 1 prop_feathering_available= 1 prop_auto_feathering_available= 1 min_rpm_for_feather= 700.000 beta_feather= 80.000 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 0.500 minimum_on_ground_beta= 1.000 minimum_reverse_beta= -14.000 [TurbineEngineData] fuel_flow_gain= 0.011 inlet_area= 60.000 rated_N2_rpm= 29920.000 static_thrust= 1000.000 afterburner_available= 0 [turboprop_engine] power_scalar=1.000 maximum_torque= 1500000.000 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 15.0 //Flap angle that activates warning at idle flap_limit_power = 30.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1.00 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,1,1 //pumps on Eng1,2 [Views] eyepoint=112.32, -1.50, 23.04 //(feet) longitudinal, lateral, vertical distance from reference datum [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=1,0 [Reference Speeds] flaps_up_stall_speed= 120.000 full_flaps_stall_speed= 100.000 cruise_speed= 250.000 max_mach = 0.60 max_indicated_speed = 300 //Red line (KIAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.0 autothrottle_available=0 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [stall_warning] type=2 stick_shaker=1 [direction_indicators] direction_indicator.0=3,0 [exits] number_of_exits = 2 exit_rate.0 = 0.5 ;Percent per second exit_rate.1 = 0.1 ;Percent per second [Flaps.0] type= 1 span-outboard= 0.800 extending-time= 10.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.500 drag_scalar= 1.000 pitch_scalar= 0.100 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 30.000, 0.000 [pitot_static] pitot_heat=1.000000 [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=2