[fltsim.0]
title=MB-AI Navio Patrulha P40
sim=AI Navio Patrulha
model=
panel=
sound=
texture=p40
atc_id=
atc_id_enable=1
atc_id_color=0xffffffff
atc_airline=Marinha
atc_flight_number=
atc_heavy=0
ui_manufacturer=MB-AI
ui_type=Navio Patrulha Classe Grajau
ui_variation=Grajau P40
visual_damage=0
atc_parking_types=DOCK
atc_parking_codes=NPa
description= Código Internacional de Chamada: PWGJ. NPa Grajaú - P 40 - Classe Grajaú. Dimensões: 46.5 m de comprimento, 7.5 m de boca e 2.3 m de calado. Equipamentos: 1 lancha de casco semi-rigido (RHIB), com capacidade para 10 homens e 1 bote inflável para seis homens, usados para salvamentos e abordagens. Um guindaste eletro-hidráulico com capacidade para 620kg. Tripulação: 29 homens, sendo 4 oficiais e 25 praças. Foi subordinado ao 3º Distrito Naval, integrando o Grupamento Naval do Nordeste  (GrupNNE), tendo como área de atuação o litoral dos Estados de Pernambuco, Rio Grande do Norte, Paraíba e Ceará, operando a partir de Natal-RN.

[fltsim.1]
title=MB-AI Navio Patrulha P45
sim=AI Navio Patrulha
model=
panel=
sound=
texture=p45
atc_id=
atc_id_enable=1
atc_id_color=0xffffffff
atc_airline=Marinha
atc_flight_number=
atc_heavy=0
ui_manufacturer=MB-AI
ui_type=Navio Patrulha Classe Grajau
ui_variation=Guaporé P45
visual_damage=0
atc_parking_types=DOCK
atc_parking_codes=NPa
description= Código Internacional de Chamada: PWGD. NPa Guaporé - P 45 - Classe Grajaú. Dimensões: 46.5 m de comprimento, 7.5 m de boca e 2.3 m de calado. Equipamentos: 1 lancha de casco semi-rigido (RHIB), com capacidade para 10 homens e 1 bote inflável para seis homens, usados para salvamentos e abordagens. Um guindaste eletro-hidráulico com capacidade para 620kg. Tripulação: 29 homens, sendo 4 oficiais e 25 praças. Foi subordinado ao 1º Distrito Naval, integrando o Grupamento Naval do Sudeste (GrupNSE), tendo como área de atuação o litoral dos Estados do Rio de Janeiro, São Paulo e Espírito Santo, operando a partir do Rio de Janeiro-RJ.

[fltsim.2]
title=MB-AI Navio Patrulha P46
sim=AI Navio Patrulha
model=
panel=
sound=
texture=p46
atc_id=
atc_id_enable=1
atc_id_color=0xffffffff
atc_airline=Marinha
atc_flight_number=
atc_heavy=0
ui_manufacturer=MB-AI
ui_type=Navio Patrulha Classe Grajau
ui_variation=Gurupá P46
visual_damage=0
atc_parking_types=DOCK
atc_parking_codes=NPa
description= Código Internacional de Chamada: PWGE. NPa Gurupá - P 46 - Classe Grajaú. Dimensões: 46.5 m de comprimento, 7.5 m de boca e 2.3 m de calado. Equipamentos: 1 lancha de casco semi-rigido (RHIB), com capacidade para 10 homens e 1 bote inflável para seis homens, usados para salvamentos e abordagens. Um guindaste eletro-hidráulico com capacidade para 620kg. Tripulação: 29 homens, sendo 4 oficiais e 25 praças. Esta subordinado ao 1º Distrito Naval e é baseado no Rio de Janeiro-RJ.

[fltsim.3]
title=MB-AI Navio Patrulha P47
sim=AI Navio Patrulha
model=
panel=
sound=
texture=p47
atc_id=
atc_id_enable=1
atc_id_color=0xffffffff
atc_airline=Marinha
atc_flight_number=
atc_heavy=0
ui_manufacturer=MB-AI
ui_type=Navio Patrulha Classe Grajau
ui_variation=Gurupi P47
visual_damage=0
atc_parking_types=DOCK
atc_parking_codes=NPa
description= Código Internacional de Chamada: PWGF. NPa Gurupi - P 47 - Classe Grajaú. Dimensões: 46.5 m de comprimento, 7.5 m de boca e 2.3 m de calado. Equipamentos: 1 lancha de casco semi-rigido (RHIB), com capacidade para 10 homens e 1 bote inflável para seis homens, usados para salvamentos e abordagens. Um guindaste eletro-hidráulico com capacidade para 620kg. Tripulação: 29 homens, sendo 4 oficiais e 25 praças. Esta subordinado ao 1º Distrito Naval, integrando o Grupamento Naval do Sudeste (GrupNSE), tendo como área de atuação o litoral dos Estados do Rio de Janeiro, São Paulo e Espírito Santo, operando a partir do Rio de Janeiro-RJ.

[fltsim.4]
title=MB-AI Navio Patrulha P48
sim=AI Navio Patrulha
model=
panel=
sound=
texture=p48
atc_id=
atc_id_enable=1
atc_id_color=0xffffffff
atc_airline=Marinha
atc_flight_number=
atc_heavy=0
ui_manufacturer=MB-AI
ui_type=Navio Patrulha Classe Grajau
ui_variation=Guanabara P48
visual_damage=0
atc_parking_types=DOCK
atc_parking_codes=NPa
description= NPa Guanabara - P 48 - Classe Grajaú. Dimensões: 46.5 m de comprimento, 7.5 m de boca e 2.3 m de calado. Equipamentos: 1 lancha de casco semi-rigido (RHIB), com capacidade para 10 homens e 1 bote inflável para seis homens, usados para salvamentos e abordagens. Um guindaste eletro-hidráulico com capacidade para 620kg. Tripulação: 29 homens, sendo 4 oficiais e 25 praças. Tem como área de atuação o litoral dos Estados do Pará, Maranhão, Amapá e também os rios da Amazônia, operando a partir de Belém-PA.

[fltsim.5]
title=MB-AI Navio Patrulha P49
sim=AI Navio Patrulha
model=
panel=
sound=
texture=p49
atc_id=
atc_id_enable=1
atc_id_color=0xffffffff
atc_airline=Marinha
atc_flight_number=
atc_heavy=0
ui_manufacturer=MB-AI
ui_type=Navio Patrulha Classe Grajau
ui_variation=Guarujá P49
visual_damage=0
atc_parking_types=DOCK
atc_parking_codes=NPa
description= Código Internacional de Chamada: PWGP. NPa Guarujá - P 49 - Classe Grajaú. Dimensões: 46.5 m de comprimento, 7.5 m de boca e 2.3 m de calado. Equipamentos: 1 lancha de casco semi-rigido (RHIB), com capacidade para 10 homens e 1 bote inflável para seis homens, usados para salvamentos e abordagens. Um guindaste eletro-hidráulico com capacidade para 620kg. Tripulação: 29 homens, sendo 4 oficiais e 25 praças. Esta subordinado ao 4º Distrito Naval, e integra o Grupamento Naval do Norte (GrupNNorte), tendo como área de atuação o litoral dos Estados do Pará, Maranhão, Amapá e também os rios da Amazônia, operando a partir da Base Naval de Val-de-Cães em Belém-PA.

[fltsim.6]
title=MB-AI Navio Patrulha P50
sim=AI Navio Patrulha
model=
panel=
sound=
texture=p50
atc_id=
atc_id_enable=1
atc_id_color=0xffffffff
atc_airline=Marinha
atc_flight_number=
atc_heavy=0
ui_manufacturer=MB-AI
ui_type=Navio Patrulha Classe Grajau
ui_variation=Guaratuba P50
visual_damage=0
atc_parking_types=DOCK
atc_parking_codes=NPa
description= Código Internacional de Chamada: PWUR. NPa Guaratuba - P 50 - Classe Grajaú. Dimensões: 46.5 m de comprimento, 7.5 m de boca e 2.3 m de calado. Equipamentos: 1 lancha de casco semi-rigido (RHIB), com capacidade para 10 homens e 1 bote inflável para seis homens, usados para salvamentos e abordagens. Um guindaste eletro-hidráulico com capacidade para 620kg. Tripulação: 29 homens, sendo 4 oficiais e 25 praças. Em 28 de janeiro de 2000, passou a subordinação do 2º Distrito Naval, tendo como área de atuação o litoral dos Estados da Bahia, Sergipe e Alagoas, operando a partir de Salvador (BA).

[fltsim.7]
title=MB-AI NPa Navio Patrulha P51
sim=AI Navio Patrulha
model=
panel=
sound=
texture=p51
atc_id=
atc_id_enable=1
atc_id_color=0xffffffff
atc_airline=Marinha
atc_flight_number=
atc_heavy=0
ui_manufacturer=MB-AI
ui_type=Navio Patrulha Classe Grajau
ui_variation=Gravataí P51
visual_damage=0
atc_parking_types=DOCK
atc_parking_codes=NPa
description= Código Internacional de Chamada: PWGT. NPa Guaratuba - P 50 - Classe Grajaú. Dimensões: 46.5 m de comprimento, 7.5 m de boca e 2.3 m de calado. Equipamentos: 1 lancha de casco semi-rigido (RHIB), com capacidade para 10 homens e 1 bote inflável para seis homens, usados para salvamentos e abordagens. Um guindaste eletro-hidráulico com capacidade para 620kg. Tripulação: 29 homens, sendo 4 oficiais e 25 praças. Em 28 de janeiro de 2000, passou a subordinação do 2º Distrito Naval, tendo como área de atuação o litoral dos Estados da Bahia, Sergipe e Alagoas, operando a partir de Salvador (BA).
              

[General]
atc_type=MARINHA BRASILEIRA 
atc_model=Navio Patrulha 
editable=0
performance="Maximum Speed\n175 kts            324 km\/hr\n\nCruise Speed\n164 kts \t        305 km\/hr at 20,000 ft\n\nEngine\nPratt & Whitney Canada, Inc., PT6A-114A Free Turbine Flat Rated at 675 Shaft hp  \n\nPropeller\nThree-Bladed, Constant Speed, Full Feathering, Reversible  McCauley, 106-inch diameter\n\nMaximum Endurance\n5.1 hours maximum cruise at 10,000 ft\n6.6 hours maximum cruise at 18,000 ft\n6.4 hours maximum range at 10,000 ft\n7.2 hours maximum range at 18,000 ft\n\nService Ceiling\n22,800 ft            6,949 m\n\nFuel Capacity\n335  gal              1,268 L\n\nEmpty Weight\n4,575 lb              2,075 kg\n\nMaximum Gross Weight\n8,785 lb\t            3,985 kg\n\nUseful Load\n4,000 lb\t            1,814 kg\n\nLength\n41 ft, 7 in             12.7 m\n\nWingspan\n52 ft, 1 in\t            15.8 m\n\nHeight\n15 ft, 5-1\/2 in      4.8 m\n\nSeating\nUp to 14"
Category=airplane


[WEIGHT_AND_BALANCE]
max_gross_weight=8000                         // (pounds)
empty_weight=4895                             // (pounds)

reference_datum_position=61.0, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-120.5, 0, 0     // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50


;Moments of Inertia
empty_weight_pitch_MOI=60000.00
empty_weight_roll_MOI=6618.57
empty_weight_yaw_MOI=10431.43
empty_weight_coupled_MOI=0.0

[Flaps.0]
type=1
span-outboard=0.5       // Percent span for flap position
extending-time=5.7      // Seconds, time to fully extend
system_type=0           // 0 = electrical
damaging-speed=175                                  // KIAS
blowout-speed=175                                  // KIAS
flaps-position.0=0     // degrees
flaps-position.1=10,175     // degrees
flaps-position.2=20,150     // degrees
flaps-position.3=30,125     // degrees

[flight_tuning]
cruise_lift_scalar=0
parasite_drag_scalar=0
induced_drag_scalar=0
elevator_effectiveness=0
aileron_effectiveness=0
rudder_effectiveness=1.0
pitch_stability=0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=0
aileron_trim_effectiveness=0
rudder_trim_effectiveness=1.0

[GeneralEngineData]
engine_type=5                                //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-1.3, 0.0, 0.0                       //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.12                  //Scalar for fuel flow efficiency
min_throttle_limit=-0.25                      //Minimum percent throttle.  Generally negative for turbine reverser

[propeller]
thrust_scalar=1.0                   //Propeller thrust scalar
propeller_type=0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=8.8                   //Propeller Diameter, (feet)
propeller_blades=3                     //Number of propeller blades
propeller_moi=19                    //Propeller moment of inertia
beta_max=45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.6                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520                 //Miminum governed RPM
prop_tc=0.004                 //Prop time-constant
gear_reduction_ratio=17.4                  //Propeller gear reduction ratio
fixed_pitch_beta=0                     //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=1                     //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=1               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=700                   //Minimum RPM for prop feathering
beta_feather=88.0                  //Feathering pitch angle (degrees)
power_absorbed_cf=0.9                   //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0          //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=1                     //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0                 //Minimum pitch angle in reverse, (degrees)

[TurbineEngineData]
fuel_flow_gain=0.011                 //Gain on fuel flow
inlet_area=1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm=33000                 //RPM, second stage compressor rated value
static_thrust=158                   //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar=0.85                   //Scalar on Turboprop power
maximum_torque=1865                  //Maximum torque available (ft-lbs)

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 5 , 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 2 , 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0

[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 / Water Rudder Effectiveness  (0=Undamped, 1=Critically Damped) / 1.0 = normal
;/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)
point.0=1,  -11.15, 0.00, -5.300, 1600, 0, 1.40, 30.0, 0.3,  2.5, 0.8, 0.0, 0.0, 0, 175.0, 175.0
point.1=1, -124.40, -5.250, -5.500, 1600, 1, 1.50,  0.0, 0.4,  2.5, 0.8, 0.0, 0.0, 2, 175.0, 175.0
point.2=1, -124.40,  5.250, -5.500, 1600, 2, 1.50,  0.0, 0.4,  2.5, 0.8, 0.0, 0.0, 2, 175.0, 175.0

point.3=4,  -37.0,  -4.5, -6.0, 1000.0, 0, 2.0, 0.0, 0.5, 3.5, 0.900,  0.0,  0.0, 0, 220, 250
point.4=4,  -37.0,  4.5, -6.0, 1000.0, 0, 2.0, 0.0, 0.5, 3.5, 0.900,  0.0,  0.0, 0, 220, 250
point.5=4, -121.0, -5.0, -2.3, 2000.0, 1, 2.0, 10.0, 1.0, 2.5, 0.900, 0.0,  0.0, 2, 220, 250
point.6=4, -121.0, 5.0, -2.3, 2000.0, 2, 2.0, 10.0, 1.0, 2.5, 0.900, 0.0,  0.0, 3, 220, 250






max_number_of_points=21

static_pitch=0.983             //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=5.344         //feet, altitude of CG when at rest on the ground
gear_system_type=1             //Hydraulic

[gear_warning_system]
gear_warning_available=2     //Amphib
pct_throttle_limit=0.1     //Percent throttle that activates warning
flap_limit_idle=20.1     //Flap angle that activates warning at idle
flap_limit_power=13.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake=1        //Parking brake available
toe_brakes_scale=0.68  //Brake scalar

[hydraulic_system]
normal_pressure=3000.0    //PSI
electric_pumps=0         //no electric pumps
engine_map=1,0,0,0   //pump on Eng1


[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

[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit            
light.4=1, 25.00, 0.00,  -6.00,flytampa_aiship_wake_large,


[EFFECTS]
wake=fx_wake_m
water=fx_spray1
dirt=fx_tchdrt
concrete=fx_AI_smoke_Grajau
touchdown=fx_tchdwn_s, 1


[SMOKESYSTEM]
smoke.1=0, -265.0, 11.0, fx_spray1.fx,
smoke.2=0, -265.0, -11.0, fx_spray1.fx,


[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=100,  180
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=3,0

[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

[airspeed_indicators]
airspeed_indicator.0=1.16, -22.0


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

[fuel]
LeftMain=-15.3, -1.1, 2.5, 166.0, 3.6     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-15.3,  1.1, 2.5, 166.0, 3.6     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1

[airplane_geometry]
wing_area=279.0                 //Square feet
wing_span=52.1                  //Feet
wing_root_chord=6.4                   //Feet
wing_dihedral=3.9                   //Degrees
wing_incidence=2.5                   //Degrees
wing_twist=-1.7                  //Degrees
oswald_efficiency_factor=0.7                   //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=2.96                   //Degrees, wing leading edge
wing_pos_apex_lon=-12.3                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_area=39.0                  //Square feet
htail_span=11.7                  //Feet
htail_pos_lon=-27.8                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence=2.0                   //Degrees
htail_sweep=5.0                   //Degrees, horizontal tail leading edge
vtail_area=18.0                  //Square feet
vtail_span=4.8                   //Feet, tip to body
vtail_sweep=45.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-25.7                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=1.5                   //Feet, vertical distance from reference point, positive going up
elevator_area=16.6                  //Square feet
aileron_area=18.3                  //Square feet
rudder_area=6.6                  //Square feet
elevator_up_limit=28.0                  //Degrees
elevator_down_limit=21.0                  //Degrees
aileron_up_limit=20.0                  //Degrees
aileron_down_limit=15.0                  //Degrees
rudder_limit=15.5                 //Degrees
elevator_trim_limit=19.5                  //Degrees
spoiler_limit=20.0                  //Degrees
spoilerons_available=1                     //Spoilerons Available?
aileron_to_spoileron_gain=1                   //Aileron to spoileron gain
min_ailerons_for_spoilerons=0                 //Degrees
min_flaps_for_spoilerons=0                    //Minimum flap handle position when spoilerons activate
spoiler_handle_available=0                    //Defaults to True if spoiler limit > 0, else False.  Should be False for spoilerons only

[Reference Speeds]
flaps_up_stall_speed=72.0                  //Knots True (KCAS)
full_flaps_stall_speed=58.0                  //Knots True (KCAS)
cruise_speed=143.0                 //Knots True (KTAS)
max_mach=0.60
max_indicated_speed=175                   //Red line (KIAS)

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.0
autothrottle_available=0
pitch_takeoff_ga=8.0
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
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.0

[forcefeedback]
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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

[stall_warning]
type=2

[Views]
eyepoint=-36.100000,0.000000,0.000000