[fltsim.0]
title=1US PB4Y-1 Liberator
sim=PB4Y-1_Liberator
model=
panel=
sound=
texture=VB-109
KB_checklists=PB4Y-1_check
KB_reference=PB4Y-1_ref
KB_notes=PB4Y-1_notes
atc_id=08
atc_airline=Navy
atc_flight_number=SAM02
atc_heavy=0
ui_manufacturer=Consolidated
ui_type=PB4Y-1 Liberator
ui_variation='Bus' Millers #8 from VB-109
visual_damage=1
description=Navy Bu.No. # ?8 (AAF S/N # ?) - Pilot - Commander 'Bus' Miller from VB-109

[General]
atc_type=BOEING
atc_model=B24D
editable=no
performance=Wing span: 110 ft.\nLength: 66.4 ft\nWeight: 58,000\nPower:4x 1200 HP \nP&W 1830-94\nSpeed: 303 mph\n\nDesign: \n Textures:Microsoft, Lindsay Watt, Tom Kohler \n \nAnimation: Microsoft\nFlight dynamics: \nTom Kohler\nDate: May 6, 2002\nVersion FS2002\\

[WEIGHT_AND_BALANCE]
// - weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//
empty_weight = 34187

reference_datum_position =  0.0  , 0, 0  // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)

// CoG corrected to 25%
empty_weight_CG_position = 0.111, 0, 0  // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 = 180,  11.7454, -4.0,  2.0  // Pilot
station_load.1 = 180,  11.7454,  4.0,  2.0  // Co-Pilot
station_load.2 = 180,  22.1457,  0.0, -3.4  // Bombardier
station_load.3 = 180,  24.7703,  0.0, -2.4  // Nose gunner
station_load.4 = 180,   5.0853,  0.0,  5.2  // Navigator / top turret gunner
station_load.5 = 180,   8.5302,  0.0,  0.0  // Radio operator / top turret gunner
station_load.6 = 180, -21.8176, -3.3,  0.0  // port waist gunner
station_load.7 = 180, -21.8176,  3.3,  0.0  // starboard waist gunner
station_load.8 = 180, -19.6850,  0.0, -6.5  // Ball turret gunner
station_load.9 = 180, -41.5026,  0.0,  0.8  // Tail gunner

// Moments of Inertia
empty_weight_pitch_MOI  = 125891
empty_weight_roll_MOI  = 337591
empty_weight_yaw_MOI  = 307055
empty_weight_coupled_MOI=0.000000

[flight_tuning]
cruise_lift_scalar          = 1.0
parasite_drag_scalar        = 1.0
induced_drag_scalar         = 1.0
elevator_effectiveness      = 1.0
aileron_effectiveness       = 1.0
rudder_effectiveness        = 1.0
pitch_stability             = 1.0
roll_stability              = 1.0
yaw_stability               = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[electrical]
max_battery_voltage           = 24.0
generator_alternator_voltage  = 28.0
max_generator_alternator_amps = 60.0

[contact_points]
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
//    cls     fb      lr     ud     dmg  bk  dia   str   sat  mcom  damp  ext
point.0=1,  15.50,   0.00, -11.40, 1320, 0, 1.50, 12.0, 0.160, 2.10, 0.70, 6.0, 07.0, 0, 165, 205 // center gear
point.1=1,  -1.50, -13.17, -12.00, 1500, 1, 2.50,  0.0, 1.060, 2.50, 0.86, 9.5, 10.5, 2, 165, 205
point.2=1,  -1.50,  13.17, -12.00, 1500, 2, 2.50,  0.0, 1.060, 2.50, 0.86, 7.0, 08.0, 3, 165, 205
point.3=2,   0.00, -55.83,   1.00, 1020, 0, 0.0,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5
point.4=2,   0.00,  55.83,   1.00, 1020, 0, 0.0,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6
point.5=2, -39.58,   0.00,  -7.50, 1020, 0, 0.0,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9
point.6=2,  17.16,   0.00,  -9.50, 1020, 0, 0.0,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4

static_cg_height = 10.78 	//(feet) altitude of CG when at rest (altitude when loaded on ground)
static_pitch     = 2.41		//degrees (pitch when loaded on ground)

[flaps.0]
type=1							// 1 - tail, 2 - lead
span-outboard    =   0.125		// 0.0 .. 1.0
extending-time   =   8			// seconds
flaps-position.0 =   0			// degrees, KIAS
flaps-position.1 =  10, 150		// degrees, KIAS
flaps-position.2 =  20, 125		// degrees, KIAS
flaps-position.3 =  30, 105		// degrees, KIAS
flaps-position.4 =  45, 105		// degrees, KIAS

damaging-speed   = 165			// KIAS
blowout-speed	 = 185			// KIAS

[Views]
eyepoint = 11.55, -1.4,  1.6

[LIGHTS]
panel=0.00, 0.45, -2.00, fx_vclight

[forcefeedback]
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=27000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=27000          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=27000         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds

[SMOKESYSTEM]
smoke.0=-0.417, 6.333, -26.500, fx_smoke_rx_sm
smoke.1=-0.833, 4.917, -13.833, fx_smoke_rx_sm
smoke.2=-0.833, 4.917, 13.833, fx_smoke_rx_sm
smoke.3=-0.417, 6.333, 26.500, fx_smoke_rx_sm

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[LIGHTS]        
// class, longitudinal, lateral, vertical positions from datum (feet)
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3,   0.0, -54.5,  2.8,  fx_navredm ,
light.1=3,   0.0,  54.5,  2.8,  fx_navgrem ,
light.2=3, -35.0,   0.00, 2.45, fx_navwhih ,
light.3=4,   6.55,  0.00, 3.20, fx_vclight ,
light.4=5,   3.8, -16.4,  0.0,  fx_landing ,
light.5=5,   3.8,  16.4,  0.0,  fx_landing ,
light.6=2,   0.0, -54.5,  2.8,  fx_strobe ,
light.7=2,   0.0,  54.5,  2.8,  fx_strobe ,
light.8=2, -36.0,   0.00, 1.5,  fx_strobe ,
light.9=1, -36.0,   0.00, 1.5,  fx_beacon ,

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 1
Com.2         = 1, 1
Nav.1         = 1, 1, 1
Nav.2         = 1, 1, 0
Adf.1         = 1
Transponder.1 = 1
Marker.1      = 1

[fuel]
Center1=0.000000,0.000000,0.000000,500.000000,0.000000
LeftMain=0.491700,-24.022300,-0.410100,1174.000000,0.000000
RightMain=0.491700,24.022300,-0.410100,1174.000000,0.000000
External1=0.328100,0.000000,-5.610200,800.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=1048.000000
wing_span=110.000000
wing_root_chord=9.500000
wing_dihedral=3.999023
wing_incidence=4.795532
wing_twist=0.000000
oswald_efficiency_factor=0.866563
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=331.000000
htail_span=43.000000
htail_pos_lon=-38.750000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=220.000000
vtail_span=16.911535
vtail_sweep=0.000000
vtail_pos_lon=-38.750000
vtail_pos_vert=7.166667
elevator_area=94.410000
aileron_area=80.250000
rudder_area=39.490000
elevator_up_limit=28.000000
elevator_down_limit=23.000000
aileron_up_limit=26.000000
aileron_down_limit=19.000000
rudder_limit=28.000000
elevator_trim_limit=20.000000
spoiler_limit=0.100000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[GeneralEngineData]
engine_type=0
Engine.0=9.333333,-25.416667,0.250000
Engine.1=10.333333,-11.166667,0.000000
Engine.2=10.333333,11.166667,0.000000
Engine.3=9.333333,25.416667,0.250000
fuel_flow_scalar=1.000000

[piston_engine]
cylinder_displacement=130.714286
compression_ratio=6.700000
number_of_cylinders=14
max_rated_rpm=2700.000000
max_rated_hp=1200.000000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.035000
turbocharged=1
max_design_mp=47.999999
min_design_mp=9.000000
critical_altitude=25000.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.540000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
propeller_type=0
propeller_diameter=11.583000
propeller_blades=3
propeller_moi=31.546380
beta_max=65.000000
beta_min=15.000000
min_gov_rpm=405.000000
prop_tc=0.010000
gear_reduction_ratio=1.777780
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=70.000000
beta_feather=88.500000
power_absorbed_cf=0.900000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=1.000000
minimum_reverse_beta=-14.000000

[Reference Speeds]
flaps_up_stall_speed=118.000000
full_flaps_stall_speed=94.400000
cruise_speed=206.961358

[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=1,0