// L1049H FDE beta v1.00 // last modifications 8 May 2009: rsf: radar no tip tanks [General] atc_type=LOCKHEED atc_model=CONI editable=0 performance="Lockheed L1049H/06-03 \nMax takeoff weight: 142,100 lbs.\nMax landing weight: 114,500 lbs.\nMax Zero Fuel Weight: 109,500 lbs.\nMax Payload: 29,590 lbs.\nMax speed: 338 knots (TAS)\nCruise speed: 297 knots (TAS)\nRange (max fuel): 4570 nm\nRange (max payload): 3619 nm\nService ceiling: 22,800 ft.\nCrew: 5 cockpit, 4 cabin\nPassengers: 75-99\nEngines: Four Curtiss-Wright Turbo Compound R-3350-EA3.\nFuel capacity(with tip tanks): 7768 gallons.\nSee http://calclassic.proboards55.com for further detail." Category=airplane [fltsim.0] title=Lockheed L-1049H Capitol N5401V sim=L1049H model=1049vc_rsf panel= sound= texture=CAP-N5401V kb_checklists=L1049_check_EA kb_reference=L1049G_ref atc_id=689 atc_id_enable=1 ui_manufacturer=Lockheed ui_type=L-1049H Super Constellation ui_variation=Capitol N5401V description="Super H Constellation N5401V, c/n 4839, entered service with TWA 23 April 1958. Sold to Capitol International Airways November 1961. In service with Capitol until 1968. From 1965 to 1967 Capitol had a contract for IT flights from Berlin Tempelhof, and the planes carried Berliner Flug Ring titling and the Berlin bear emplem on the nose." atc_flight_number=380 atc_heavy=0 atc_airline=Capitol atc_parking_codes= atc_parking_types=GATE prop_anim_ratio=0.99 atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 [fltsim.1] title=Lockheed L-1049H No Markings sim=L1049H model=1049vc_rstf panel= sound= texture=H-no_markings kb_checklists=L1049_check_EA kb_reference=L1049G_ref atc_id=689 atc_id_enable=1 ui_manufacturer=Lockheed ui_type=L-1049H Super Constellation ui_variation=H No Markings description="L1049H natural metal texture. By Maarten Brouwer." atc_flight_number=380 atc_heavy=0 atc_airline=Blank atc_parking_codes= atc_parking_types=GATE prop_anim_ratio=0.99 atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 [pitot_static] vertical_speed_time_constant=2.0 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.0 [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 1.000, 0.000, 0.000 //0.900, 0.000, 0.000 max_number_of_stations= 50 //station_load.0= "5690.000, -30.000, 0.000, 0.000, Pax-load rear" // tip tank version //station_load.1= "2800.000, 22.000, 0.000, 0.000, Pax-load front" // tip tank version //station_load.2= "5994.000, -8.000, 0.000, 0.000, Pax-load center" // tip tank version //station_load.3= "800.000, 0.000, 0.000, 0.000, Cabin crew" // tip tank version station_load.0= "5734.000, -30.000, 0.000, 0.000, Pax-load rear" //no tip tanks station_load.1= "4638.000, 22.000, 0.000, 0.000, Pax-load front" //no tip tanks station_load.2= "6650.000, -8.000, 0.000, 0.000, Pax-load center" //no tip tanks station_load.3= "1271.000, 0.000, 0.000, 0.000, Cabin crew" //no tip tanks empty_weight= 79907 //73016 empty_weight_roll_MOI= 950000.0 //was2343290.000 empty_weight_pitch_MOI= 910000.0 //was4634852.000 empty_weight_yaw_MOI= 1790000.0 empty_weight_coupled_MOI= 10.000 max_gross_weight= 142100.0 max_landing_weight=114500.0 CG_forward_limit= 1.000 CG_aft_limit= 0.5 // B 0.5 [lights] // _rs lights //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //light.0 = 3, -2.200, -62.390, 3.871, fx_navred // tip tanks //light.1 = 3, -2.100, 62.285, 3.871, fx_navgre // tip tanks light.0 = 3, -4.750, -61.650, 3.880, fx_navred // no tip tanks light.1 = 3, -4.650, 61.600, 4.000, fx_navgre //no tip tanks light.2 = 3, -67.750, 0, 4.84, fx_navwhi light.3 = 4, 41.25, 0, 1.20, fx_vclighth light.4 = 6, 39.60, 0.00, -5.280, fx_1049_taxiR, // Radar nose //light.4 = 6, 46.10, 0.50, -2.780, fx_1049_taxi, //Snub nose light.5 = 7, 11.250, -13.8, -2.05, fx_1049_exh2_1r9 // 2 light.6 = 8, 11.250, 13.8, -2.05,fx_1049_exh2_1r9 // 3 light.7 = 2, 9.750, -29.90, 0.100,fx_1049_exh2_1r9 //1 light.8 = 9, 9.750, 29.90, 0.100,fx_1049_exh2_1r9//4 light.9 = 1, -8.025, 0.0, 7.075, fx_beaconb light.10 = 1, 10.5, 0.0, -5.425, fx_beaconb light.11 = 5, -4.65, -38.385, -0.590, fx_1049_landing, light.12 = 5, -4.65, 38.350, -0.590, fx_1049_landing, light.13 = 5, 1.500, -40.560, 0.450, fx_1049_nacelle_refl // Opensky light.14 = 5, 1.500, 40.530, 0.410, fx_1049_nacelle_refl [electrical] // HJN 7 Dec max_battery_voltage = 1000 generator_alternator_voltage = 25.5 max_generator_alternator_amps = 100 engine_generator_map = 1,1,1,1 electric_always_available = 0 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 15, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 22 starter2 = 0, 20, 22 starter3 = 0, 20, 22 starter4 = 0, 20, 22 light_nav = 0, 5, 22 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_recognition = 0, 0, 0 light_wing = 0, 0, 0 light_logo = 0, 0, 0 light_strobe = 0, 0, 0 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 propeller_deice = 0, 5, 17 light_cabin = 0, 5, 17 [GeneralEngineData] engine_type= 0 Engine.0= 6.562, -31.417, 0.000 Engine.1= 8.858, -14.701, -1.969 Engine.2= 8.858, 14.701, -1.969 Engine.3= 6.562, 31.417, 0.000 fuel_flow_scalar= 1.0150 min_throttle_limit=0.00990 master_ignition_switch= 0 //Master Ignition Switch max_contrail_temperature=-20 //choose temp c below which contrails occur [smokesystem] smoke.0 = 2.00, -10.10, 48.10, fx_1049_fueldump smoke.1 = 2.00, -10.10, -48.1, fx_1049_fueldump [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 //contrail = fx_1649a_contrail //startup = fx_1649a_engstrt startup = fx_1049_engstrt windshield_rain_effect_available = 1 [fuel] fuel_type = 1 number_of_tank_selectors = 4 electric_pump = 1 // Super Constellation tank config (L-1049, C-121C) //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) External1=-0.5, -27, 0, 1555, 5 // tank 1 Center2= -0.5, -9.0, 0, 790, 10 // tank 2 Center3= -0.5, 9.0, 0, 790, 10 // tank 3 External2=-0.5, 27, 0, 1555, 5 // tank 4 LeftMain= -0.5, -49, 0, 565, 5 // tank 2A RightMain=-0.5, 49, 0, 565, 5 // tank 3A Center1= -1.5, 0, 0, 730, 11 // tank 5 // // additional wing-tip tanks (L-1049G, L-1049H, C-121G) //LeftTip= 2.0, -60, 0, 609, 0 // tank 2B //RightTip= 2.0, 60, 0, 609, 0 // tank 3B // // additional fuselage tank (EC-121G) // LeftAux= 0, 0, 0, 1000, 1 // tank 6 // CAUTION: With FS2004, EITHER use Tank 6 OR Tanks 2B,3B! // VNCON30 Panel does not support more than nine tanks in FS2004 //Gear and scrape section //0 Class //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 [contact_points] static_pitch = 1.6 static_cg_height = 11.839 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 12 point.0 = 1.000, 40.288, 0.000, -13.30, 2000.000, 0.000, 1.300, 50.000, 0.52, 1.80, 0.999, 7.000, 10.500, 0.000, 180.0, 220.0 point.1 = 1.000, -3.860, -15.08, -12.5, 2500.000, 1.000, 2.635, 0.000, 0.70, 1.430, 0.940, 8.000, 12.000, 2.000, 180.0, 220.0 point.2 = 1.000, -3.860, 15.08, -12.5, 2500.000, 2.000, 2.635, 0.000, 0.70, 1.430, 0.940, 9.000, 13.500, 3.000, 180.0, 220.0 point.3 = 2, -1.5513, -74.0185, 3.7999, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -1.5513, 74.0185, 3.7999, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -66, 0, 4.88, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 50, 0, -1.5, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.7 = 2, 20, 0, -5.5, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.8 = 2, -35, 0, -4, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.9 = 2, 20, 0, 6.6, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.10 = 2, -62, -21, 16, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.11 = 2, -62, 21, 16, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 [keyboard_response] elevator = 150.000000, 190.000000 aileron = 150.000000, 190.000000 rudder = 150.000000, 170.000000 [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 = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2700 gear_bump_right_direction = 00500 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 //airplane geometry //FAA = FAA Doc 4A17 [airplane_geometry] wing_area= 1650.000 wing_span= 123.000 wing_root_chord= 18.33 // M wing_dihedral= 7.600 wing_incidence= 3.0 // was 2.3 wing_twist= -2.000 oswald_efficiency_factor= 0.780 wing_winglets_flag= 0 wing_sweep= 7.680 wing_pos_apex_lon= 6.5 //4.0 // fr 3.281 wing_pos_apex_vert= -2.000 htail_area= 347.800 // M 463.58-106.8(elev) htail_span= 50.000 // M htail_pos_lon= -60.000 htail_pos_vert= 7.000 htail_incidence= 0.750 // ? was -1.7 htail_sweep= 7.170 //3 view vtail_area= 210.6 // M 210.6 -91.2 rudder = 119.4; B=328 vtail_span= 15.00 // B:20.650 vtail_sweep= 0.000 vtail_pos_lon= -60.000 vtail_pos_vert= 10.000 elevator_area= 106.800 //Marson p. 72; Beckert: 215.000 aileron_area= 99.600 // M; B: 90 rudder_area= 91.2 // M; B: 114.000 elevator_up_limit= 40.000 //FAA elevator_down_limit= 20.000 //FAA aileron_up_limit= 25.000 //FAA aileron_down_limit= 10.000 //FAA rudder_limit= 36 //FAA: 29; incremented for nosewheel power steering elevator_trim_limit= 22.0 //Beckert; was 20.5 spoiler_limit = 70.000 aileron_to_spoileron_gain = 0.000 spoiler_handle_available = 1 // HJN 0503 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 spoilerons_available = 0 auto_spoiler_available=0 spoiler_extension_time=4.000000 positive_g_limit_flaps_up=4.068376 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-2.106838 negative_g_limit_flaps_down=-2.000000 [flight_tuning] cruise_lift_scalar=1.0 // pitch_stability=1.00 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 // induced_drag_scalar=1.0000 // elevator_effectiveness=1.00 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.000 // aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 p_factor_on_yaw = 0.5 torque_on_roll = 1.0 gyro_precession_on_yaw = 1.0 gyro_precession_on_pitch = 1.0 [Flaps.0] type= 1 span-outboard= 0.650 extending-time= 26.000 system_type= 1 damaging-speed= 210.000 blowout-speed= 230.000 lift_scalar= 0.9500 drag_scalar= 0.100 pitch_scalar= 0.990 flaps-position.0= 0.000, 0.000 flaps-position.1= 26.000, 0.000 //flaps-position.2= 29.000, 0.000 //66% flaps-position.2= 35.000, 0.000 flaps-position.3= 41.000, 0.000 [Flaps.1] type=1 span-outboard=0.65 extending-time=26.0 system_type=1 flaps-position.0=0,0 flaps-position.1=12.0,0.0 //flaps-position.2=15,0.0 //66% flaps-position.2=28,0.0 flaps-position.3=41,0.0 lift_scalar=0.1 drag_scalar=0.95 pitch_scalar=0.80 damaging-speed= 210.000 blowout-speed= 230.000 [piston_engine] 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 cylinder_displacement=186.000 // real world 186=3350/18 cuin compression_ratio=6.700 number_of_cylinders=18 max_rated_rpm=2900.000 max_rated_hp=3400.000 fuel_metering_type=1 // 1=Gravity Carburetor, the only way to have CARB HEAT active cooling_type=0 normalized_starter_torque=0.0185 //0.0125 use the smaller number for manual engine starts using the FE controls or assigned keyboard keys for a slightly more realistic visual animation of a radial engine start. turbocharged=1 max_design_mp=58.500 // turbocompound chargers and 145 hi-octane fuel min_design_mp=7.40 //6.800 critical_altitude=10550.000 // not equal to real ceiling, set to reproduce HB METO power with altitude ! emergency_boost_type=0 emergency_boost_mp_offset=0.000 emergency_boost_gain_offset=0.000 fuel_air_auto_mixture=0 // 1 = automix on, 0 = manual mixture set auto_ignition=0 power_scalar=1.00 [propeller] propeller_type=0 propeller_diameter=15.100 // 1049; propeller_blades=3 propeller_moi=70 // adjusted MJ SCFA: B: keep rpm above 800, below 900 at idle beta_max=47.000 beta_min=14.000 min_gov_rpm=1400.000 // was 800 prop_tc=0.004 gear_reduction_ratio=2.285 // 16:7 gear box fixed_pitch_beta=20.000 low_speed_theory_limit=26.00 //80.000 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=350.0 // Gibson 05-05; was 0.0 beta_feather=-44.0 // HJN 0518; B: 83.0 power_absorbed_cf=0.100 defeathering_accumulators_available=1 feathering_switches=1 // Switches which invoke feathering prop_reverse_available=1.000000 minimum_reverse_beta=-14.000000 minimum_on_ground_beta=1.000 thrust_scalar=1.030 // fine tune climb and cruise, not real but nice trick [gear_warning_system] gear_warning_available=1 pct_throttle_limit = 0.10 //Percent throttle that activates warning flap_limit_idle = 25.0 //Flap angle that activates warning at idle flap_limit_power = 28.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.50 //Brake scalar B: 0.8 differential_braking_scale = 0.78 //Delta on the amount of brake when the rudder pedals deflected [hydraulic_system] normal_pressure = 2700.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,1,1 //pumps on all Engines [Views] //eyepoint=39.7, -1.730, 1.94 // LH Pilot's seat position - use with panel.cfg "BT" option. eyepoint=38.7, -1.55, 2.09 // Slightly higher and further back - use with panel.cfg "AP" or "eyepoint back" options [Radios] // Radio Type=available, 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, 1 Adf.1=1 Adf.2=1 Transponder.1=1 Marker.1=1 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=1,0 [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=98.000 cruise_speed=290.000 // KTAS max_indicated_speed=294.000 // HJN 0506 B: 280 Red Line KIAS max_mach= 0.56 // HJN 0506 B: 0.52 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700 // keep this low to avoid excessive VS when A/P is engaged autothrottle_available=0 //unclear if real AC had AT autothrottle_arming_required=0 autothrottle_max_rpm=90 autothrottle_takeoff_ga=0 default_pitch_mode=0 // 0=None, 1=Pitch Hold, 2=Altitude hold pitch_takeoff_ga=8 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=0.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=24000.0 default_bank_mode=0 // 0=None, 1=Wing Level Hold, 2=Heading Hold max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=18.00 nav_integrator_control=0.25 nav_derivative_control=0.10 nav_integrator_boundary=2.50 nav_derivative_boundary=0.50 gs_proportional_control=25.0 gs_integrator_control=0.53 gs_derivative_control=0.10 gs_integrator_boundary=0.70 gs_derivative_boundary=0.20 yaw_damper_gain=1.0 // yaw damper on [stall_warning] type=1 stick_shaker=0 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ; Percent per second [vacuum_system] // L-1649A max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=4.9 engine_map=0,1,1,0 // L-1649A [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] // L-1649A structural_deice_type=3 [airspeed_indicators] airspeed_indicator.0=1.02, -5.0