[fltsim.0]
title=Ford 4-AT-E Tri-Motor
sim=Ford_Trimotor
model=
panel=
sound=
texture=
kb_checklists=Ford_Trimotor_check
kb_reference=Ford_Trimotor_ref
atc_id=NC8407
ui_manufacturer=Ford
ui_type="Tri-Motor"
ui_variation="EAA Tri-Motor"
visual_damage=1
description="Nicknamed the "Tin Goose," the Ford 4-AT Tri-Motor pioneered early airline and air transport routes. In 1925, the Ford Motor Company bought the Stout Metal Plane Company to gain rights to the Tri-Motor design. In all, 198 Ford Tri-Motors were built. During its years of regular service in the late 1920s and early 1930s, the Ford Tri-Motor helped popularize commercial flight and promote the safety of flying to travelers."

[fltsim.1]
title=World Travel Airlines Tri-Motor
sim=Ford_Trimotor
model=
panel=
sound=
texture=1
kb_checklists=Ford_Trimotor_check
kb_reference=Ford_Trimotor_ref
atc_id=NC8407
ui_manufacturer=Ford
ui_type="Tri-Motor"
ui_variation="World Travel Airlines"
visual_damage=1
description="Nicknamed the "Tin Goose," the Ford 4-AT Tri-Motor pioneered early airline and air transport routes. In 1925, the Ford Motor Company bought the Stout Metal Plane Company to gain rights to the Tri-Motor design. In all, 198 Ford Tri-Motors were built. During its years of regular service in the late 1920s and early 1930s, the Ford Tri-Motor helped popularize commercial flight and promote the safety of flying to travelers."

[fltsim.2]
title=Emerald Harbor Air Tri-Motor
sim=Ford_Trimotor
model=
panel=
sound=
texture=2
kb_checklists=Ford_Trimotor_check
kb_reference=Ford_Trimotor_ref
atc_id=NC8407
atc_id_color=0xffffffff
ui_manufacturer=Ford
ui_type="Tri-Motor"
ui_variation="Emerald Harbor Air"
visual_damage=1
description="Nicknamed the "Tin Goose," the Ford 4-AT Tri-Motor pioneered early airline and air transport routes. In 1925, the Ford Motor Company bought the Stout Metal Plane Company to gain rights to the Tri-Motor design. In all, 198 Ford Tri-Motors were built. During its years of regular service in the late 1920s and early 1930s, the Ford Tri-Motor helped popularize commercial flight and promote the safety of flying to travelers."

[fltsim.3]
title=Ford 3M Army C-9 90th AS Paint3
sim=Ford_Trimotor
model=
panel=
sound=
texture=3
kb_checklists=Ford_Trimotor_check
kb_reference=Ford_Trimotor_ref
atc_type=C9
atc_airline=Army
atc_id=C9
ui_manufacturer=Ford
ui_type=4-AT Trimotor
ui_variation=US Army C-9, 90th Attack Squadron
ui_typerole="Tri-Motor-Prop"
ui_createdby="Microsoft Corporation" 
description=This C-9 belonged to the U.S. Army Air Corps' 90th Attack Squadron, serving  as a hack during the squadron's 1930 winter maneuvers.  Nicknamed the "Tin Goose," the Ford 4-AT Tri-Motor pioneered early airline and air transport routes. In 1925, the Ford Motor Company bought the Stout Metal Plane Company to gain rights to the Tri-Motor design. In all, 198 Ford Tri-Motors were built. During its years of regular service in the late 1920s and early 1930s, the Ford Tri-Motor helped popularize commercial flight and promote the safety of flying to travelers
Repaint by Mick Morrissey.

[fltsim.4]
title=Ford 3M Army C-9 Bolling Field Paint4
sim=Ford_Trimotor
model=
panel=
sound=
texture=4
kb_checklists=Ford_Trimotor_check
kb_reference=Ford_Trimotor_ref
atc_type=Ford
atc_airline=Army
atc_id=C9
ui_manufacturer=Ford
ui_type=4-AT Trimotor
ui_variation=US Army C-9, Bolling Field Detachment
ui_typerole="Tri-Motor-Prop"
ui_createdby="Microsoft Corporation"  
description=This C-9 belonged to the U.S. Army Air Corps' Bolling Field Detachment, serving  the Army Air Corps Headquarters at the War Department in Washington, D.C.  Nicknamed the "Tin Goose," the Ford 4-AT Tri-Motor pioneered early airline and air transport routes. In 1925, the Ford Motor Company bought the Stout Metal Plane Company to gain rights to the Tri-Motor design. In all, 198 Ford Tri-Motors were built. During its years of regular service in the late 1920s and early 1930s, the Ford Tri-Motor helped popularize commercial flight and promote the safety of flying to travelers
Textures modified by Mick Morrissey"

[fltsim.5]
title=Ford 3M Army C-9 60th SS Paint5
sim=Ford_Trimotor
model=
panel=
sound=
texture=5
kb_checklists=Ford_Trimotor_check
kb_reference=Ford_Trimotor_ref
atc_type=C9
atc_airline=Army
atc_id=C9
ui_manufacturer=Ford
ui_type=4-AT Trimotor
ui_variation=US Army C-9, 60th Service Squadron
ui_typerole="Tri-Motor-Prop"
ui_createdby="Microsoft Corporation"  
description=This C-9 belonged to the U.S. Army Air Corps' 60th Service Squadron.  Nicknamed the "Tin Goose," the Ford 4-AT Tri-Motor pioneered early airline and air transport routes. In 1925, the Ford Motor Company bought the Stout Metal Plane Company to gain rights to the Tri-Motor design. In all, 198 Ford Tri-Motors were built. During its years of regular service in the late 1920s and early 1930s, the Ford Tri-Motor helped popularize commercial flight and promote the safety of flying to travelers.

[fltsim.6]
title=Island Airlines Trimotor Paint6
sim=Ford_Trimotor
model=
panel=
sound=
texture=6
kb_checklists=Ford_Trimotor_check
kb_reference=Ford_Trimotor_ref
atc_id=N7584
atc_flight_number=78
ui_manufacturer=Ford
ui_type="Tri-Motor"
ui_variation="Isalnd Airlines"
ui_typerole="Tri-Motor-Prop"
ui_createdby="Microsoft Corporation"  
description="Nicknamed the "Tin Goose," the Ford 4-AT Tri-Motor pioneered early airline and air transport routes. In 1925, the Ford Motor Company bought the Stout Metal Plane Company to gain rights to the Tri-Motor design. In all, 198 Ford Tri-Motors were built. During its years of regular service in the late 1920s and early 1930s, the Ford Tri-Motor helped popularize commercial flight and promote the safety of flying to travelers."

[fltsim.7]
title=Pan American Trimotor Paint7
sim=Ford_Trimotor
model=
panel=
sound=
texture=7
kb_checklists=Ford_Trimotor_check
kb_reference=Ford_Trimotor_ref
atc_id=NC9637
atc_airline=Pan Am
atc_flight_number=34
ui_manufacturer=Ford
ui_type="Tri-Motor"
ui_variation="Pan American"
ui_typerole="Tri-Motor-Prop"
ui_createdby="Microsoft Corporation"  
description="Nicknamed the "Tin Goose," the Ford 4-AT Tri-Motor pioneered early airline and air transport routes. In 1925, the Ford Motor Company bought the Stout Metal Plane Company to gain rights to the Tri-Motor design. In all, 198 Ford Tri-Motors were built. During its years of regular service in the late 1920s and early 1930s, the Ford Tri-Motor helped popularize commercial flight and promote the safety of flying to travelers."

[fltsim.8]
title=Amercian Airways Trimotor Paint8
sim=Ford_Trimotor
model=
panel=
sound=
texture=8
kb_checklists=Ford_Trimotor_check
kb_reference=Ford_Trimotor_ref
atc_id=N9683
atc_airline=American
atc_flight_number=067
ui_variation=American Airlines
ui_manufacturer=Ford
ui_type="Tri-Motor"
ui_variation="American Airways"
ui_typerole="Tri-Motor-Prop"
ui_createdby="Microsoft Corporation"  
description="Nicknamed the "Tin Goose," the Ford 4-AT Tri-Motor pioneered early airline and air transport routes. In 1925, the Ford Motor Company bought the Stout Metal Plane Company to gain rights to the Tri-Motor design. In all, 198 Ford Tri-Motors were built. During its years of regular service in the late 1920s and early 1930s, the Ford Tri-Motor helped popularize commercial flight and promote the safety of flying to travelers.(Repaint By:Ed Knapp)

[fltsim.9]
title=United Airlines Trimotor Paint9
sim=Ford_Trimotor
model=
panel=
sound=
texture=9
kb_checklists=Ford_Trimotor_check
kb_reference=Ford_Trimotor_ref
atc_id=NC 4364
atc_airline=United
atc_flight_number=56
ui_manufacturer=Ford
ui_type="Tri-Motor"
ui_variation="United Airlines"
ui_typerole="Tri-Motor-Prop"
ui_createdby="Microsoft Corporation" 
description="Nicknamed the "Tin Goose," the Ford 4-AT Tri-Motor pioneered early airline and air transport routes. In 1925, the Ford Motor Company bought the Stout Metal Plane Company to gain rights to the Tri-Motor design. In all, 198 Ford Tri-Motors were built. During its years of regular service in the late 1920s and early 1930s, the Ford Tri-Motor helped popularize commercial flight and promote the safety of flying to travelers."Repaint by Ed Knapp"

[fltsim.10]
title=Ford 3M USMC RR-2 Paint10
sim=Ford_Trimotor
model=
panel=
sound=
texture=10
kb_checklists=Ford_Trimotor_check
kb_reference=Ford_Trimotor_ref
atc_type=C9
atc_model=C9
atc_airline=Army
atc_flight_number=27
atc_id=C9
ui_manufacturer=Ford
ui_type=4-AT Trimotor
ui_variation=US Marines RR-2, VJ-7M 
ui_typerole="Tri-Motor-Prop"
ui_createdby="Microsoft Corporation"
description=This RR2 belonged to the Marine Corps' Utility Squadron Seven (VJ-7M), a unit of the West Coast Expeditionary Force based at Naval Air Station San Diego, California in the early 1930s.  Nicknamed the "Tin Goose," the Ford 4-AT Tri-Motor pioneered early airline and air transport routes. In 1925, the Ford Motor Company bought the Stout Metal Plane Company to gain rights to the Tri-Motor design. In all, 198 Ford Tri-Motors were built. During its years of regular service in the late 1920s and early 1930s, the Ford Tri-Motor helped popularize commercial flight and promote the safety of flying to travelers.

[fltsim.11]
title=Ford 3M USN RR-2 Paint11
sim=Ford_Trimotor
model=
panel=
sound=
texture=11
kb_checklists=Ford_Trimotor_check
kb_reference=Ford_Trimotor_ref
atc_type=C9
atc_model=RR2
atc_airline=Navy
atc_id=RR2
ui_manufacturer=Ford
ui_type=4-AT Trimotor
ui_variation=US Navy RR-2, NAS Pensacola
description=This RR2 belonged to the US. Navy's Naval Air Station Pensacola, Florida in the early 1930s.  Nicknamed the "Tin Goose," the Ford 4-AT Tri-Motor pioneered early airline and air transport routes. In 1925, the Ford Motor Company bought the Stout Metal Plane Company to gain rights to the Tri-Motor design. In all, 198 Ford Tri-Motors were built. During its years of regular service in the late 1920s and early 1930s, the Ford Tri-Motor helped popularize commercial flight and promote the safety of flying to travelers.


[General]
atc_type=Trimotor
atc_model=
editable=0
performance="Maximum Speed\n130 mph	113 kts	209 km/hr\n\nCruise Speed\n110 mph    96 kts	177 km/hr\n\nEngine\nThree 300-hp Wright Whirlwind J-6\n\nPropeller\nTwo-bladed, metal\n\nMaximum Range\n670 mi	1,078 km\n\nService Ceiling\n14,500 ft	4,420 m\n\nFuel Capacity\n231 gal	874 L\n\nEmpty Weight\n6,600 lb	2,994 kg\n\nMaximum Gross Weight\n10,130 lb	4,595 kg\n\nLength\n49 ft, 10  in    15 m\n\nWingspan\n74 ft	22.55 m\n\nHeight\n12 ft, 8  in	3.89 m\n\nSeating\n9\n\nUseful Load\n3,530 lb	1,601 kg"
Category=airplane

[WEIGHT_AND_BALANCE]
max_gross_weight = 10130                         // (pounds)
empty_weight =  6600                            // (pounds)

reference_datum_position     =   1.00, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -1.64, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations =50

station_load.0  = "170.0,   4.9, -1.5, 1.0, Pilot"              //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1  =   "0.0,   4.9,  1.5, 1.0, Co-Pilot"           //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2  = "170.0,   1.2, -1.5, 0.0, Passenger 1"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3  = "170.0,   1.2,  1.5, 0.0, Passenger 2"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4  =   "0.0,  -2.0, -1.5, 0.0, Passenger 3"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5  = "170.0,  -2.0,  1.5, 0.0, Passenger 4"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6  = "170.0,  -4.4, -1.5, 0.0, Passenger 5"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7  = "170.0,  -4.4,  1.5, 0.0, Passenger 6"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8  =   "0.0,  -6.8, -1.5, 0.0, Passenger 7"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9  =   "0.0,  -6.8,  1.5, 0.0, Passenger 8"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 =   "0.0,  -7.9, -1.5, 0.0, Passenger 9"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = "250.0, -10.2,  0.0, 0.0, Baggage"            //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI   = 14885.4
empty_weight_roll_MOI    = 13264.7
empty_weight_yaw_MOI     = 28402.6
empty_weight_coupled_MOI = 0.0

[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
p_factor_on_yaw          = 0.5

[Flaps.0]
type= 0
span-outboard= 0.5
extending-time= 0.0
system_type= 0
flaps-position.0= 0.0, 0.0
flaps-position.1= 0.0, 0.0

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 =  3.5, -9.6, 0.0                      //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 12.2,  0.0, 0.0                      //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 =  3.5,  9.6, 0.0                      //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0                           //Fuel flow scalar
min_throttle_limit = 0.0                        //Minimum percent throttle.  Generally negative for turbine reverser
master_ignition_switch = 1                      //Master Ignition Switch

[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 108.33                    //Cubic inches per cylinder
compression_ratio= 5.1                          //Compression ratio
number_of_cylinders=9                           //Number of cylinders
max_rated_rpm= 2000                             //Max rated RPM
max_rated_hp= 300                               //Max rated HP
fuel_metering_type= 1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3                  //Starter torque factor
turbocharged= 0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0                                //Max design manifold pressure, (inHg)
min_design_mp= 0                                //Min design manifold pressure, (inHg)
critical_altitude= 0                            //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0                   //Scalar on idle RPM friction

[propeller]
thrust_scalar = 1.0                             //Propeller thrust scalar
propeller_type= 1                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 8.9                         //Propeller Diameter, (feet)
propeller_blades= 2                             //Number of propeller blades
propeller_moi= 12.3                             //Propeller moment of inertia
beta_max= 0                                     //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 0                                     //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1400                               //Miminum governed RPM
prop_tc= 0.0                                    //Prop time-constant
gear_reduction_ratio= 1.0                       //Propeller gear reduction ratio
fixed_pitch_beta= 25                            //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80                      //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 0                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 0                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather= 0                          //Minimum RPM for prop feathering
beta_feather= 0                                 //Feathering pitch angle (degrees)
power_absorbed_cf= 0                            //Coefficient of friction for power absorbed by propeller by feathered prop
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                       //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0                         //Minimum pitch angle in reverse, (degrees)


        //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]
point.0=1, -36.5,   0.0,  0.5, 1200.0, 0, 0.74, 180.0, 0.240, 2.5, 0.695, 0.0, 0.0, 0.0, 0.0, 0.0
point.1=1,   0.1,  -9.3, -8.2, 1600.0, 1, 1.53,   0.0, 0.504, 2.5, 0.686, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=1,   0.1,   9.3, -8.2, 1600.0, 2, 1.53,   0.0, 0.504, 2.5, 0.682, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=2,  -1.6, -38.5,  5.0,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2,  -1.6,  38.5,  5.0,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2, -36.0,   0.0, 10.2,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2,  11.0,   0.0, -3.0,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4.0, 0.0, 0.0

static_pitch = 13.4
static_cg_height = 7.26

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.5  //Brake scalar
differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected

[hydraulic_system]
normal_pressure = 0.0    //PSI

[Views]
eyepoint = 4.731, -1.012, 3.771

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3,  -2.05, -38.9,  4.91, fx_navred ,
light.1 = 3,  -2.05,  38.9,  4.91, fx_navgre ,
light.2 = 4,  5.95, 0.00, 2.65, fx_vclight,
light.3 = 4,  -2.00,   0.00,  2.50, fx_vclighth,
light.4 = 5, +2.8, -19.5, 3.7, fx_Shockwave_landing_light // Shockwave light
light.5 = 5, +2.8, +19.5, 3.7, fx_Shockwave_landing_light // Shockwave light

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

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator =200, 1000
aileron  =200, 1000
rudder   =200, 1000

[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=0,0

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 0

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_jenny
touchdown=fx_tchdwn_s, 1

[electrical]
max_battery_voltage = 12
generator_alternator_voltage = 13
max_generator_alternator_amps = 25
engine_generator_map= 0,1,0

[fuel]
LeftMain = -1.0, -5.9, 3.6, 100.0, 0.0  //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain= -1.0,  5.9, 3.6, 100.0, 0.0  //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1  = -1.0,  0.0, 3.6,  31.0, 0.0  //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 3                    
electric_pump=0

[airplane_geometry]
wing_area               = 785.0                 //Square feet
wing_span               = 74.0                  //Feet
wing_root_chord         = 12.84                 //Feet
wing_dihedral           = 0.0                   //Degrees
wing_incidence          = 2.0                   //Degrees
wing_twist              = 0.0                  //Degrees
oswald_efficiency_factor= 0.6                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 1.5                   //Degrees, wing leading edge
wing_pos_apex_lon       = 1.50                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 4.3                   //Feet, vertical distance from reference point, positive going up

htail_area              = 114.0                  //Square feet
htail_span              = 21.7                  //Feet
htail_pos_lon           = -32.4                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 3.9                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.0                   //Degrees
htail_sweep             = 0.0                   //Degrees, horizontal tail leading edge

vtail_area              = 61.0                  //Square feet
vtail_span              = 9.4                   //Feet, tip to body
vtail_sweep             = 44.0                   //Degrees, vertical tail leading edge
vtail_pos_lon           = -32.4                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 6.1                   //Feet, vertical distance from reference point, positive going up

elevator_area           = 52.8                  //Square feet
aileron_area            = 33.8                  //Square feet
rudder_area             = 23.0                  //Square feet
elevator_up_limit       = 30.0                  //Degrees
elevator_down_limit     = 20.0                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 20.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 19.5                  //Degrees
spoiler_limit           = 0.0                   //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate
auto_spoiler_available=0
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

[Reference Speeds]
flaps_up_stall_speed    = 50.4                  //Knots True (KTAS)
full_flaps_stall_speed  = 50.4                  //Knots True (KTAS)
cruise_speed            = 76.5                  //Knots True (KTAS)
max_indicated_speed     = 145                   //Red line (KIAS)

[autopilot]
use_no_default_bank=1
use_no_default_pitch=1
autopilot_available= 0
flight_director_available= 0

[forcefeedback]
ground_bumps_magnitude1=2600            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200            ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000                 ; in microseconds

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

[stall_warning]
type=1
stick_shaker=0


[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