// 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 Withdrawn from military service Mar 1968.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_2S // 2
light.7 = 8, 12.250, 13.95, -1.85,fx_749_2S // 3
light.8 = 2, 10.650, -29.90, 0.125,fx_749_2S //1
light.9 = 9, 10.650, 29.90, 0.220,fx_749_2S //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 eyxepoint Roland 291109
[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
