// This file based on L-1049G flight dynamics (L1049G_FS9.AIR) 
// version 2.3 by Wolfram Beckert (Apr 6, 2004)
// modified version for L-1649A Starliner Project by the Starliner Project team
// See Starliner thread at www.calclassic.com 
//Edited 30.7.2008 Data from Howard-->fuelgal/tank
//Edited 8.7.2008 Min Prop rpm for feather 350 -->for new model

[fltsim.0]
title=Lockheed L-1649A Starliner TWA N7307C
sim=L1649A
model=
panel=
sound=
texture=N7307C 
kb_checklists=L-1649A_check 
kb_reference=L-1649A_ref
atc_id=307
atc_id_enable=1
ui_manufacturer=Lockheed
ui_type=L-1649A Starliner
ui_variation=TWA N7307C 1957
description="The Starliner was the last of the long-range piston-engine airliners. Providing accommodation for twenty-six first-class and forty-five tourist-class passengers, N7307C "Star of Montana" entered service with TWA in May 1957 and inaugurated the non-stop polar service San Francisco-London on 2 October 1957. Withdrawn from use by TWA 12 September 1960."
atc_flight_number=307
atc_heavy=0
atc_airline=TWA
atc_parking_codes=TWA
atc_parking_types=GATE
prop_anim_ratio=0.95  
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0

[General]
atc_type=LOCKHEED 
atc_model=STARLINER 
editable=0 
performance="Max takeoff weight: 160.000 lbs.\nMax landing weight: 123,000 lbs.\nPayload: 24,293 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-EA-2.\nFuel capacity: 9844 gallons.\nSee the Starliner thread at www.calclassic.com for further detail."  
Category=airplane

[pitot_static]
vertical_speed_time_constant=2.0		//Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.0					// L-1649A

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000    
max_number_of_stations= 50 
//station_load.0= 3800.000,0.0,0,0  // simplified
station_load.0= "3800.000, -30.000, 0.000, 0.000, Pax-load rear"
station_load.1= "2540.000, 22.000, 0.000, 0.000, Pax-load front"
station_load.2= "2920.000, -8.000, 0.000, 0.000, Pax-load center"
station_load.3= "800.000, 0.000, 0.000, 0.000, Cabin crew"
empty_weight= 90873				// 117.000 FAA doc 4a17
empty_weight_roll_MOI= 2143290.000//was2343290.000
empty_weight_pitch_MOI= 5534852.000 //was4634852.000
empty_weight_yaw_MOI= 3473465.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 160000.000			// L-1649A: 160000.0
max_landing_weight=123000.0			// L-1649A
CG_forward_limit= 0.000
CG_aft_limit= 0.5 // B 0.5

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, 0.303, -74.081, 5.637, fx_navred
light.1 = 3, 0.299, 74.081, 5.571, fx_navgre
light.2 = 3, -65.879, 0, 4.84, fx_navwhi
light.3 = 4, 42.1, 0, 1.45, fx_vclighth // 42.1
light.4 = 6, 41.50, 0.00, -5.180, fx_1649A_landing,
light.5 = 7, 13.758, -18.8, 0.310069, fx_1649A_exh
light.6 = 8, 13.758, 18.8, 0.310069,fx_1649A_exh
light.7 = 2,11.362, -36.56, 1.800,fx_1649A_exh
light.8 = 9,11.362, 36.56,1.800,fx_1649A_exh
light.9 = 1, -11.39, 0.0, 7.21, fx_beacon
light.10 = 1, -11.39, 0.0, -5.45, fx_beacon
light.11 = 1, -11.39, 0.0, 7.21, fx_navred
light.12 = 1, -11.39, 0.0, -5.45, fx_navred
light.13 = 5, -2.0330, -44.260, 0.050, fx_1649A_landing,
light.14 = 5, -2.0330, 44.23, 0.010, fx_1649A_landing,
light.15 = 7, 13.0, 12.0, 0.0, fx_redlight 
light.16 =7, 13.0, -22.0, 0.0, fx_redlight 
light.17 = 7, 13.0, -12.0, 0.0, fx_redlight 
light.18 =7, 13.0, 22.0, 0.0, fx_redlight 

[GeneralEngineData]
engine_type= 0
Engine.0= 6.562, -36.417, 0.000
Engine.1= 8.858, -18.701, -1.969
Engine.2= 8.858, 18.701, -1.969
Engine.3= 6.562, 36.417, 0.000
//fuel_flow_scalar= 1.240			// B: should result in about 630 Gal/h at cruise
fuel_flow_scalar= 0.57000                       // RB from 077oland 04-19
min_throttle_limit=0.000000
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_1649A_fueldump
smoke.1 = 2.00, -10.10, -48.1, fx_1649A_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
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 1
number_of_tank_selectors = 4
electric_pump = 1

Center1 = 0, 0, 0, 1635, 21
Center2 = 0, -8.9, 0, 1365, 5
Center3 = 0, 8.9, 0, 1365, 5
LeftMain = 0, -27, 0, 1375, 10
RightMain = 0, 27, 0, 1375, 10
External1 = 0, -54.7, 0, 1335, 9
External2 = 0, 54.7, 0, 1335, 9


//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

//new points.0-2 HJN 05-10
point.0 = 1.000, 41.788, 0.000, -13.24, 2000.000, 0.000, 1.300, 45.000, 0.147, 2.000, 0.800, 7.000, 7.500, 0.000, 0.000, 0.000
point.1 = 1.000, -4.154, -19.96, -12.10, 2500.000, 1.000, 2.635, 0.000, 0.260, 2.000, 0.800, 4.000, 8.000, 2.000, 0.000, 0.000
point.2 = 1.000, -4.154, 19.96, -12.10, 2500.000, 2.000, 2.635, 0.000, 0.260, 2.000, 0.800,  4.000, 8.500, 3.000, 0.000, 0.000
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: see comments for main changes 
//M= Marson p. 72 f.; 
//3V=Lockheed Three view;
//FAA = FAA Doc 4A17

[airplane_geometry] 
wing_area= 1850.000
wing_span= 150.000
wing_root_chord= 18.1  // M
wing_dihedral= 7.500
wing_incidence= 2.0  // was 2.3		
wing_twist= -1.000
oswald_efficiency_factor= 0.700		
wing_winglets_flag= 0
wing_sweep= 1.000
wing_pos_apex_lon= 4.0   // fr 3.281
wing_pos_apex_vert= -2.000
htail_area= 356.800           // M 463.58-106.8(elev)                 
htail_span= 50.000            // M
htail_pos_lon= -60.000
htail_pos_vert= 7.000
htail_incidence= -1.900          // ? was -1.7
htail_sweep= 7.400               //3 view
vtail_area= 119.4            // 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= 105.000        // M; B: 90
rudder_area= 91.2            // M; B: 114.000
elevator_up_limit= 39.000       //FAA
elevator_down_limit= 20.000     //FAA
aileron_up_limit= 23.000        //FAA
aileron_down_limit= 16.000      //FAA
rudder_limit= 38             //FAA: 29; incremented for nosewheel power steering
elevator_trim_limit= 19.0       //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=8.000000
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
aileron_area=11.300000


[electrical]
max_battery_voltage = 25
generator_alternator_voltage = 28
max_generator_alternator_amps = 100
engine_generator_map = 1,1,1,1
electric_always_available = 0
autopilot = 0, 5, 13
avionics_bus = 0, 10, 13
avionics = 1, 5, 13
pitot_heat = 0, 15, 13
additional_system = 0, 20, 13
marker_beacon = 1, 2, 13
gear_warning = 0, 2, 13
fuel_pump = 0, 5, 13
starter1 = 0, 20, 13
starter2 = 0, 20, 13
starter3 = 0, 20, 13
starter4 = 0, 20, 13
light_nav = 0, 5, 13
light_beacon = 0, 5, 13
light_landing = 0, 5, 13
light_taxi = 0, 5, 13
light_strobe = 0, 5, 13
light_panel = 0, 5, 13
prop_sync = 0, 15, 13
auto_feather = 0, 15, 13
propeller_deice = 0, 5, 13
light_cabin = 0, 5, 13

[flight_tuning]
cruise_lift_scalar=1.8 // MJ 05-30, from 1.0 
pitch_stability=1.000 
roll_stability=1.000 
yaw_stability=1.000 
parasite_drag_scalar=0.945000 // Rol. 04-19
induced_drag_scalar=0.95000  // Rol. 05-12
elevator_effectiveness=0.700 
aileron_effectiveness=1.000 
rudder_effectiveness=1.000 
elevator_trim_effectiveness=1.8000 // from 1.0     
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					// 1 - trail, 2 - lead
span-outboard= 0.700
extending-time= 14.000
system_type= 1
damaging-speed= 210.000
blowout-speed= 230.000
lift_scalar= 0.2//RB was 0.00 50 ft distance
drag_scalar= 1.6         // test 
pitch_scalar= 1.9        // test
flaps-position.0= 0,0
flaps-position.1= 25.0, 185		// L-1649A
flaps-position.2= 38.0, 160		// L-1649A

[Flaps.1] 
type=1 
span-outboard=0.5 
extending-time=15
system_type=0 
flaps-position.0=0,0 
flaps-position.1=0,0 
flaps-position.2=25,185 
lift_scalar=0.5 
drag_scalar=0.0
pitch_scalar=0.0



[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=8.500 
number_of_cylinders=18 
max_rated_rpm=2900.000 
max_rated_hp=3250.000 
fuel_metering_type=0 
cooling_type=0 
normalized_starter_torque=0.050 
turbocharged=1 
max_design_mp=59.500 		// turbocompound chargers and 145 hi-octane fuel
min_design_mp=5.000 
critical_altitude=11500.000 	// limit ceiling alt, not equal to real ceiling !
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=1.000 


[propeller]
propeller_type=0 
propeller_diameter=16.83 	// 1649; 
propeller_blades=3 
propeller_moi=120 		// adjusted MJ SCFA: B: keep rpm above 800, below 900 at idle
beta_max=45.000 
beta_min=10.000 
min_gov_rpm=1000.000 		// was 800
prop_tc=0.004 
gear_reduction_ratio=1.880 	//  keep value to fit BMEP
fixed_pitch_beta=20.000 
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=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=0 
feathering_switches=1 		// Switches which invoke feathering
prop_reverse_available=1               // SCFA=1; B: 0 (off; why?); see kneeboard ref 
minimum_reverse_beta=-14.000              //SCFA; B: -25; 
minimum_on_ground_beta=1.000 
thrust_scalar=1.025                     // was 1.050, fine tune climb and cruise, not real but nice trick


[gear_warning_system]
gear_warning_available=1
pct_throttle_limit =  0.1		//Percent throttle that activates warning
flap_limit_idle    =  25.0		//Flap angle that activates warning at idle
flap_limit_power   =  33.0		//Flap angle that activates warning at above idle

[brakes]
parking_brake = 1			//Parking brake available
toe_brakes_scale = 0.34			//Brake scalar B: 0.8
differential_braking_scale = 0.5        //Delta on the amount of brake when the rudder pedals deflected

[hydraulic_system]
normal_pressure = 1500.0		//PSI
electric_pumps  = 0			//no electric pumps
engine_map      = 1,1,1,1		//pumps on all Engines

[Views]
eyepoint=40.2, -1.73, 1.94 // VC


[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=115.000 
full_flaps_stall_speed=95.000 
cruise_speed=314.000                   // KTAS
max_indicated_speed=294.000		// HJN 0506 B: 280 Red Line KIAS
max_mach= 0.57                          // 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=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
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=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
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