// L1049H FDE beta v1.00
// last modifications 8 May 2009: snubnose 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] // _s 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
