// 4 December 2009. Folder Lockheed_L749_0. 2-stack variants. [General] atc_type=LOCKHEED atc_model=connie editable=0 performance="Max takeoff weight: 107,000 lbs.\nMax landing weight: 89,500 lbs.\nMax Zero Fuel Weight: 82,000 lbs.\nMax Payload: 25,000 lbs.\nMax speed: 338 knots (TAS)\nCruise speed: 297 knots (TAS)\nRange (max fuel): 5500 nm\nRange (max payload): 3619 nm\nService ceiling: 22,800 ft.\nCrew: 3-5 cockpit, 4 cabin\nPassengers: 60-81\nEngines: Four Wright Cyclone 749C18BD-1 (civil) or R-3350-75 (military).\nFuel capacity: 5820 gallons.\nSee http://calclassic.proboards55.com for further detail." Category=airplane [fltsim.0] title=C-121A USAF 48-609 1998 sim=749 model=usaf panel= sound= texture=609 kb_checklists=L749_check kb_reference= ui_manufacturer=Lockheed ui_type=L-749 Constellation ui_variation=C-121A USAF 48-609 1998 atc_heavy=0 atc_id=8609 atc_id_enable=1 atc_airline=USAF atc_flight_number=2601 description=C/n 2601, AF serial 48-609 entered service with MATS Atlantic Division 31 Dec 1948. Modified to VC-121A configuration 1951, serial 80609, 1254 Air Transport Group, later 89 MAW. Withdrawn from military service Mar 1968. Used as budworm sprayer aircraft with Conifair Aviation until 1980. Acquired by Avra Valley Constellation Group, repainted in MATS colors, and flying airshow circuits until 2005 (serial N494TW). Flown to Korea and preserved at the Korean Air training facility on Jeju Island. prop_anim_ratio=0.99 atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 [fltsim.1] title=L-749 Eastern N118A sim=749 model=EAL panel= sound= texture=EAL-N118A kb_checklists=L749_check kb_reference= ui_manufacturer=Lockheed ui_type=L-749 Constellation ui_variation=Eastern Air Lines N118A atc_heavy=0 atc_id=N118A atc_id_enable=1 atc_airline=EASTERN atc_flight_number=2615 description=Eastern Air Lines N118A (c/n 2615) 1949-60. Sold to Air Haiti Feb 1961. Disappeared without trace en route San Juan-Managua 11 Nov 1961. prop_anim_ratio=0.99 atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 [fltsim.2] title=L-749 Eastern N118A Speedpak sim=749_SP model=EAL_SP panel= sound= texture=EAL-N118A kb_checklists=L749_check kb_reference= ui_manufacturer=Lockheed ui_type=L-749 Constellation ui_variation=Eastern Air Lines N118A Speedpak atc_heavy=0 atc_id=N118A atc_id_enable=1 atc_airline=EASTERN atc_flight_number=2615 description=Eastern Air Lines N118A fitted with Speedpak freight pannier (1949-60). prop_anim_ratio=0.99 atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 [fltsim.3] title=L-749 KLM-FLE sim=749 model=MATS panel= sound= texture=KLM-FLE kb_checklists=L749_check kb_reference= ui_manufacturer=Lockheed ui_type=L-749 Constellation ui_variation=KLM Flevoland atc_heavy=0 atc_id=N749NL atc_id_enable=1 atc_airline=KLM atc_flight_number=2604 description=N749NL (c/n2604) in her vintage 1950's KLM livery. A regular guest at airshows since 2004, her home base is the Dutch National Aviation Museum "Aviodrome" at Lelystad, the Netherlands. Paint by Jaap de Baare. See readme_Flevoland.txt in folder texture.KLM-FLE for more information on the Dutch Connie project. 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 //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= 0.400, 0.000, 0.000 //0.900, 0.000, 0.000 max_number_of_stations= 50 // Use the following lines for L-749A weight configuration station_load.0= "2167.000, -30.000, 0.000, 0.000, Pax-load rear" station_load.1= "3363.000, 22.000, 0.000, 0.000, Pax-load front" station_load.2= "3761.000, -8.000, 0.000, 0.000, Pax-load center" station_load.3= "1789.000, 0.000, 0.000, 0.000, Cabin crew" // Use the following lines for L-749 configuration //station_load.0= "1834.000, -30.000, 0.000, 0.000, Pax-load rear" //station_load.1= "1638.000, 22.000, 0.000, 0.000, Pax-load front" //station_load.2= "1050.000, -8.000, 0.000, 0.000, Pax-load center" //station_load.3= "871.000, 0.000, 0.000, 0.000, Cabin crew" empty_weight= 61000 //73016 empty_weight_roll_MOI= 737000.0 //was2343290.000 empty_weight_pitch_MOI= 468000.0 //was4634852.000 empty_weight_yaw_MOI= 1145000.0 empty_weight_coupled_MOI= 10.000 max_gross_weight= 107000.0 // L749: 102000.0; L749A: 107000.0 max_landing_weight=89500.0 // L749: 84500.0; L749A: 89500.0 CG_forward_limit= 1.000 CG_aft_limit= 0.5 // B 0.5 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -4.750, -61.650, 3.880, fx_navred light.1 = 3, -4.650, 61.600, 4.000, fx_navgre light.2 = 3, -61.100, 0.00, 3.40, fx_navwhi light.3 = 4, 30.25, 0.00, 1.20, fx_749_vclight light.4 = 4, 30.50, -1.44, 1.20, fx_vclight light.5 = 4, 30.50, 1.44, 1.20, fx_vclight light.6 = 7, 12.250, -13.8, -1.75, fx_749_2SX // 2 light.7 = 8, 12.250, 13.95, -1.85,fx_749_2SX // 3 light.8 = 2, 10.650, -29.90, 0.125,fx_749_2SX //1 light.9 = 9, 10.650, 29.90, 0.220,fx_749_2SX //4 light.10 = 1, -6.950, 0.0, 7.050, fx_749_beaconb light.11 = 1, 7.951, -0.0095, -5.425, fx_749_beaconb light.12 = 5, -4.40, -38.385, -0.575, fx_749_landing, light.13 = 5, -4.40, 38.350, -0.575, fx_749_landing, light.14= 5, 4.000, -40.500, 0.000, fx_749_nacelle_refl // Opensky with permission light.15= 5, 4.000, 40.500, 0.000, fx_749_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, -30.417, 0.000 //-31.417 Engine.1= 8.858, -14.701, -1.969 Engine.2= 8.858, 14.701, -1.969 Engine.3= 6.562, 30.417, 0.000 //31.417 fuel_flow_scalar= 1.0320 min_throttle_limit=0.0300 // was 0.00990 master_ignition_switch= 0 //Master Ignition Switch max_contrail_temperature=-20 //choose temp c below which contrails occur [smokesystem] //vert(inop),long,lat smoke.0 = 0.00, -18.10, 38.10, fx_749_fueldumpoutbrd //for existing trails smoke.1 = 0.00, -18.10, -38.10, fx_749_fueldumpoutbrd smoke.2 = 0.00, -22.00, 7.750, fx_749_fueldumpinbrd //for optional wing root trails smoke.3 = 0.00, -22.00, -7.750, fx_749_fueldumpinbrd [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 startup = fx_749_engstrt //startup = fx_749_jet_engstrt windshield_rain_effect_available = 1 [fuel] fuel_type = 1 number_of_tank_selectors = 4 electric_pump = 1 //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 //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 = 12.139 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 12 point.0 = 1.000, 31.96, 0.000, -13.6, 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, -12.9, 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, -12.9, 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, -2.5, -61, 3.7999, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -2.5, 61, 3.7999, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -61.5, 0, 3.657, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 41, 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, -24.1401, 0, -4.6709, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.9 = 2, 10, 0, 7, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.10 = 2, -57, -21.3, 14, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.11 = 2, -57, 21.3, 14, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 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= 0.76 //0.760 //0.780 wing_winglets_flag= 0 wing_sweep= 7.680 wing_pos_apex_lon= 7.0 //6.5 //4.0 // fr 3.281 wing_pos_apex_vert= -2.000 htail_area= 343.00 // M 450-106.8(elev) htail_span= 50.000 // M htail_pos_lon= -52.000 htail_pos_vert= 7.000 htail_incidence= 0.750 // ? was -1.7 htail_sweep= 7.170 //3 view vtail_area= 154.0 // M 210.6 -91.2 rudder = 119.4; B=328 vtail_span= 15.00 // B:20.650 vtail_sweep= 0.000 vtail_pos_lon= -51.000 vtail_pos_vert= 10.000 elevator_area= 106.800 //Marson p. 72; Beckert: 215.000 aileron_area= 99.600 // M; B: 90 rudder_area= 88.2 // 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= 29 //FAA: 29; 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= 0.000 pitch_scalar= 0.4 //0.990 flaps-position.0= 0.000, 0.000 flaps-position.1= 26.000, 174.000 //flaps-position.2= 29.000, 0.000 //66% flaps-position.2= 35.000, 127.000 flaps-position.3= 41.000, 127.000 [Flaps.1] type=1 span-outboard=0.65 extending-time=26.0 system_type=1 flaps-position.0=0,0 flaps-position.1=7.0,0.0 //flaps-position.2=15,0.0 //66% flaps-position.2=30,0.0 flaps-position.3=41,0.0 lift_scalar=0.1 drag_scalar=0.95 pitch_scalar=1.6 //1.00 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=0.800 // 1.00 cylinder_displacement=186.000 // real world 186=3350/18 cuin compression_ratio=6.700 number_of_cylinders=18 max_rated_rpm=2800.000 max_rated_hp=2500.000 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=51.500 min_design_mp=6.60 //6.800 critical_altitude=9200.000 // 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 // 749 and 1049 Hamilton S; 15.0 for Curtiss-E propeller_blades=3 propeller_moi=70 // adjusted MJ SCFA: B: keep rpm above 800, below 900 at idle beta_max=47.000 beta_min=15.000 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=28.00 //80.000 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=0 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 = 1700.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,1,1 //pumps on all Engines [Views] // eyepoint=31.37, -1.00, 2.43 //Bill 291009 eyepoint=29.37, -1.00, 2.43 //FSX eyepoint [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=100.000 full_flaps_stall_speed=80.000 cruise_speed=270.000 // KTAS max_indicated_speed=282.000 // HJN 0506 B: 280 Red Line KIAS max_mach= 0.54 // 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 = 3 exit_rate.0 = 0.4 ; Percent per second [vacuum_system] // max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=4.9 engine_map=0,1,1,0 // [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] // structural_deice_type=3 [airspeed_indicators] airspeed_indicator.0=1.0, 0.0