[fltsim.0]
title=JBK Martin 130
sim=JBK Martin 130
model=
panel=
sound=
texture=
kb_checklists=M130_ref
ui_manufacturer=Martin
ui_type=130
ui_variation=China Clipper
atc_heavy=0
atc_id=NC14716
atc_airline=PAN AM
atc_flight_number=1935
description=Martin M130 flying boat, Pan American Airways System, 1935. Only three M130's were built, NC14716 'China Clipper' was the first.
ui_typerole="Propliner"
ui_createdby="JBK"

[General]
atc_type=Martin
atc_model=Clipper
editable=0 
performance=Wingspan: 130' \nLength: 91'\nEmpty weight: 28800 lbs, Max. take-off 51000 lbs\nEngines: 4 P&W Twin Wasp S1A4G, 830 HP each.\nMaximum Speed 180 mph at 7000 ft\/ 160 kts\nCruising speed 157 mph\/ 140 kts\nService ceiling: 17000 ft
Category=airplane

[CameraDefinition.001]
Title = Copilot
Guid = {65C01636-A908-443C-B96B-501185398960}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False 
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.915, 0, 0
InitialPbh=6.0, 0, 0


[weight_and_balance]

max_gross_weight = 51000
empty_weight = 28000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -1, 0, -3
empty_weight_pitch_MOI = 158843
empty_weight_roll_MOI = 484170
empty_weight_yaw_MOI = 642359
empty_weight_coupled_MOI = 0
max_number_of_stations = 8

station_load.0 = 360, 18,0,-5, Pilots (2)
station_load.1 = 540, 12,0,-5, Other crew (3)
station_load.2 = 2040, -8,0,-9, 12 pax (46 max)
station_load.3 = 510, -7,0,-9, Freight and mail


[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1
engine.0 = 10.5, -20.7, 0,
engine.1 = 10.5, -8.6, 0,
engine.2 = 10.5, 8.6, 0,
engine.3 = 10.5, 20.7, 0,

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

[fuel]

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

fuel_type = 1
number_of_tank_selectors = 1

LeftMain = -1, -10, -10, 1550, 0		
RightMain = -1, 10, -10, 1550, 0 	

electric_pump=1

[contact_points]
static_pitch = 3
static_cg_height = 11.5
max_number_of_points = 18

point.0 = 4, -5, -16.1, -13.5, 3500, 0, 0, 0, 0.55, 5.2, 0.4, 0, 0, 2, 0, 0
point.1 = 4, -5, 16.1, -13.5, 3500, 0, 0, 0, 0.55, 5.2, 0.4, 0, 0, 3, 0, 0
point.2 = 4, 25.578, 0, -14.002, 3500, 0, 0, 20, 0.2, 6.5, 0.6, 0, 0, 0, 0, 0
point.3 = 2, 0, -65, 1.5, 900, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0, 65, 1.5, 900, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -61.113, 0, -2.9, 900, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 30.65, 0, -10.005, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0


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

[forcefeedback]
ground_bumps_magnitude1 = 1800
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1900
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000

[airplane_geometry]
wing_area = 2312.0
wing_span = 130
wing_root_chord = 20
wing_dihedral = 2.0
wing_incidence = 2.0
wing_twist = -1.0
oswald_efficiency_factor = 0.65
wing_winglets_flag = 0
wing_sweep = 4.3
wing_pos_apex_lon = 5.0
wing_pos_apex_vert = 0
htail_area = 420.0 
htail_span = 43.0
htail_pos_lon = -46.2
htail_pos_vert = 0
htail_incidence = 0.5
htail_sweep = 12.0
vtail_area = 144.0
vtail_span = 13
vtail_sweep = 18.0
vtail_pos_lon = -46
vtail_pos_vert = 0
elevator_area = 200.0
aileron_area = 200.0
rudder_area = 65.0
elevator_up_limit = 26.0
elevator_down_limit = 18.0
aileron_up_limit = 15.0
aileron_down_limit = 9.0
rudder_limit = 29.0
elevator_trim_limit = 15.0
spoiler_limit = 57.0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
auto_spoiler_available=0
spoiler_extension_time=5.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000


[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0


[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 


[exits]
number_of_exits=2
exit_rate.0=0.4  				;Percent per second
exit_rate.1=0.4  				;Percent per second


[Views]
eyepoint=17.75, -1.5, -4.46      //(feet) longitudinal, lateral, vertical distance from reference datum


[flaps.0]
type=0							// 1 - tail, 2 - lead
span-outboard=0.50					// 0.0 .. 1.0
extending-time=5					// seconds
flaps-position.0=0					// degrees, KIAS


[Reference Speeds]
flaps_up_stall_speed=73.000000 
full_flaps_stall_speed=60.000000 
cruise_speed=147
max_indicated_speed=255.000000


[lights]
light.0 = 3,  1.8, -62.66, 2.13, fx_navred,
light.1 = 3,  1.8,  62.66, 2.13, fx_navgre,
light.2 = 3,  -61.336,  0, -2.75, fx_navwhi,
light.3 = 4,  20.4,   -1.3,  -5, fx_vclighth,
light.4 = 4,  20.4,   1.3,  -5, fx_vclighth,

[autopilot]
autopilot_available=1 
flight_director_available=0 
default_vertical_speed=700.000000 
autothrottle_available=0
pitch_takeoff_ga=8.000000 
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
default_bank_mode=2     //Default to Heading Hold
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000


[piston_engine]
cylinder_displacement=194.77 
compression_ratio=6.5 
number_of_cylinders=9 
max_rated_rpm=2600.0 
max_rated_hp=960.0 
fuel_metering_type=1 
cooling_type=0 
normalized_starter_torque=0.30
turbocharged=1 
max_design_mp=37.5 
min_design_mp=0 
critical_altitude=7000 
emergency_boost_type=0 
emergency_boost_mp_offset=0 
emergency_boost_gain_offset=0.66 
fuel_air_auto_mixture=0 
auto_ignition=0 
max_rpm_mechanical_efficiency_scalar=1.0 
idle_rpm_mechanical_efficiency_scalar=1.0 
max_rpm_friction_scalar=1.0 
idle_rpm_friction_scalar=1.0 


[propeller]
thrust_scalar = 1.0                             //Propeller thrust scalar
propeller_type= 0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 11.23                       //Propeller Diameter, (feet)
propeller_blades= 3                             //Number of propeller blades
propeller_moi= 40.2                             //Propeller moment of inertia
beta_max= 65.0                                  //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 15.0                                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 800                               //Miminum governed RPM
prop_tc= 0.1                                    //Prop time-constant
gear_reduction_ratio= 1.778                     //Propeller gear reduction ratio
fixed_pitch_beta= 0.0                           //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80.0                    //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 1                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 1                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0                      //Minimum RPM for prop feathering
beta_feather= 89.5                              //Feathering pitch angle (degrees)
power_absorbed_cf= 0.9                          //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available= 0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available= 0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta= 0.0                     //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0                       //Minimum pitch angle in reverse, (degrees)
feathering_switches = 1                         //Switches which invoke feathering
rotation=1,1,1,1


[brakes]
toe_brakes_scale=1.0
parking_brake=0


[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=6.930556


[stall_warning]
type=-1
stick_shaker=1


[attitude_indicators]
attitude_indicator.0=1


[turn_indicators]
turn_indicator.0=1,0


[direction_indicators]
direction_indicator.0=1,0 


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

[pitot_static]
pitot_heat=1.000000

[vacuum_system]
max_pressure=5.500000
vacuum_type=3
electric_backup_pressure=0.000000
engine_map=0,0,0,0

[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=1.000000

[deice_system]
structural_deice_type=0