
[fltsim.0]
title=CESSNA 172 AI Carpatia
sim=CESSNA 172 AI
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=AI
ui_type=Cessna 172 Carpatia 
ui_variation=OM-ACR
atc_parking_codes=ACR
atc_id_color=0xffffffffff
visual_damage=0
description=staticky model pre sceneriu LZTR\n\nrepaint by Roland Kanik  


[General]
atc_type=Cessna
atc_model=C172
editable=1 
performance="Maximum Speed\n126 kts            203 km\/hr\n\nCruise Speed\n124 kts            200 km\/hr\n\nEngine\nTextron Lycoming IO-360-L2A 180 bhp\n\nPropeller\nTwo-Bladed Macauley Fixed Pitch\n\nMaximum Range\n638 nm            734 mi          1181 km\n\nService Ceiling\n14,000 ft\t         4267 m\n\nFuel Capacity\n56 gal\t          212 L\t \n\nEmpty Weight\n1,665 lb\t          1,002 kg\n\nMaximum Gross Weight\n2,550 lb\t          1,157 kg\n\nLength\n27 ft, 2 in          8.2 m\n\nWingspan\n36 ft, 1 in\t           11 m\n\nHeight\n8 ft, 11 in\t           2.72 m\n\nSeating\t           4\n\nUseful Load\n893 lb\t           405 kg\n" 

[weight_and_balance]
// ACM V2.3
max_gross_weight = 2550
empty_weight = 1650
reference_datum_position = 3.6, 0, 0
empty_weight_CG_position = -3, 0, 0
empty_weight_pitch_MOI = 1400
empty_weight_roll_MOI = 1137
empty_weight_yaw_MOI = 2360
empty_weight_coupled_MOI = 0
max_number_of_stations = 5
station_load.0 = "170, -3.0, -1.5, 0.0, Pilot"
station_load.1 = "170, -3.0,  1.5, 0.0, Front Passenger"
station_load.2 = "0, -6.2, -1.5, 0.0, Rear Passenger"
station_load.3 = "0, -6.2,  1.5, 0.0, Rear Passenger"
station_load.4 = "0, -8.0,  0.0, 0.0, Baggage"

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3,  -2.88, -18.11, 2.95, fx_navred
light.1 = 3,  -2.88,  18.11, 2.95, fx_navgre
light.2 = 2,  -3.15, -18.31, 2.95, fx_strobe
light.3 = 2,  -3.15,  18.31, 2.95, fx_strobe
light.4 = 1, -20.60,   0.00, 6.33, fx_beacon
light.5 = 4,  -2.27,   0.00, 1.45, fx_vclight
light.6 = 5, 0.7, -5.7, -2, fx_Shockwave_landing_light // Shockwave light

[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 0.88
engine.0 = 2.4, 0.0, 0.0
min_throttle_limit=0.000000

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

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 1
LeftMain = -3.9, -2.1, 2.5, 26.5, 0
RightMain = -3.9, 2.1, 2.5, 26.5, 0
electric_pump=0

[contact_points]
static_pitch = 3.02
static_cg_height = 3.765
max_number_of_points = 9
point.0 = 1, 0.9, 0, -3.29, 1500, 0, 0.5, 22, 0.25, 2.5, 0.7, 0, 0, 0, 0, 0
point.1 = 1, -4.7, -4.5, -3.31, 3500, 1, 0.5, 0, 0.3, 2.5, 0.7, 0, 0, 2, 0, 0
point.2 = 1, -4.7, 4.5, -3.31, 3500, 2, 0.5, 0, 0.3, 2.5, 0.7, 0, 0, 3, 0, 0
point.3 = 2, -3.90, -18.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -3.90   18.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.5 = 2,-20.23,   0.0,  0.30, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.6 = 2,  1.48,   0.0, -2.17, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.7 = 2,-22.80,   0.0,  5.83, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7
point.8 = 2, -4.90,   0.0, -2.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8

[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000

[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.0
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[airplane_geometry]
//ACM_AREAW1// 0,0,0,1.4935,0.6112,0.6112,0,1.4188,1.2225,1.2225
//ACM_AREAW2// 0,1.3441,1.8338,1.8338,0,1.2694,2.4451,2.4451,0,1.1948
//ACM_AREAW3// 3.0564,3.0564,0,1.1201,3.6677,3.6677,0,1.0454,4.2790,4.2790
//ACM_AREAW4// 0,0.9707,4.8903,4.8903,0,0.8961,5.5016,5.5016,0,0.8214
//ACM_AREAH1// 0,0,0,1.1887,0.1981,0.1981,0.0349,1.1642,0.3962,0.3962
//ACM_AREAH2// 0.0698,1.1397,0.5943,0.5943,0.1048,1.1152,0.7924,0.7924,0.1397,1.0907
//ACM_AREAH3// 0.9905,0.9905,0.1746,1.0662,1.1887,1.1887,0.2096,1.0417,1.3868,1.3868
//ACM_AREAH4// 0.2445,1.0172,1.5849,1.5849,0.2794,0.9927,1.7830,1.7830,0.3144,0.9682
//ACM_AREAV1// 0,0,0,1.4630,0.1625,0.1625,0.1364,1.4824,0.3251,0.3251
//ACM_AREAV2// 0.2728,1.5017,0.4876,0.4876,0.4092,1.5211,0.6502,0.6502,0.5456,1.5404
//ACM_AREAV3// 0.8128,0.8128,0.6820,1.5598,0.9753,0.9753,0.8184,1.5792,1.1379,1.1379
//ACM_AREAV4// 0.9548,1.5985,1.3004,1.3004,1.0912,1.6179,1.4630,1.4630,1.2276,1.6372
//ACM_CAREAW1// 2.7508,2.7508,0.7467,1.0454,3.0564,3.0564,0.7467,1.0305,3.3621,3.3621
//ACM_CAREAW2// 0.7467,1.0155,3.6677,3.6677,0.7467,1.0006,3.9734,3.9734,0.7467,0.9857
//ACM_CAREAW3// 4.2790,4.2790,0.7467,0.9707,4.5846,4.5846,0.7467,0.9558,4.8903,4.8903
//ACM_CAREAW4// 0.7467,0.9409,5.1959,5.1959,0.7467,0.9259,5.5016,5.5016,0.7467,0.9110
//ACM_CAREAH1// 0,0,0.5943,1.1887,0.1981,0.1981,0.6292,1.1939,0.3962,0.3962
//ACM_CAREAH2// 0.6642,1.1991,0.5943,0.5943,0.6991,1.2043,0.7924,0.7924,0.7340,1.2095
//ACM_CAREAH3// 0.9905,0.9905,0.7690,1.2147,1.1887,1.1887,0.8039,1.2200,1.3868,1.3868
//ACM_CAREAH4// 0.8388,1.2252,1.5849,1.5849,0.8738,1.2304,1.7830,1.7830,0.9087,1.2356
//ACM_CAREAV1// 0,0,0.3657,1.0972,0.1625,0.1625,0.5021,1.1751,0.3251,0.3251
//ACM_CAREAV2// 0.6385,1.2530,0.4876,0.4876,0.7749,1.3309,0.6502,0.6502,0.9113,1.4088
//ACM_CAREAV3// 0.8128,0.8128,1.0477,1.4866,0.9753,0.9753,1.1841,1.5645,1.1379,1.1379
//ACM_CAREAV4// 1.3205,1.6424,1.3004,1.3004,1.4569,1.7203,1.4630,1.4630,1.5933,1.7982
wing_area = 174.0
wing_span = 36.1
wing_root_chord = 4.9
wing_dihedral = 1.7
wing_incidence = 1.5
wing_twist = -3.0
oswald_efficiency_factor = 0.68
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = -2.4
wing_pos_apex_vert = 0.0
htail_area = 39.0
htail_span = 11.7
htail_pos_lon = -18.3
htail_pos_vert = 0.0
htail_incidence = 3.2
htail_sweep = 10.0
vtail_area = 18.0
vtail_span = 4.8
vtail_sweep = 40.0
vtail_pos_lon = -16.2
vtail_pos_vert = 1.5
elevator_area = 16.6
aileron_area = 18.3
rudder_area = 6.7
elevator_up_limit = 28.0
elevator_down_limit = 21.0
aileron_up_limit = 20.0
aileron_down_limit = 15.0
rudder_limit = 24.0
elevator_trim_limit = 19.5
spoiler_limit = 0.0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[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 

[piston_engine]
power_scalar=1.0                              //Piston power scalar
cylinder_displacement=90.0                     //Cubic inches per cylinder
compression_ratio=8.5                          //Compression ratio
number_of_cylinders=4                           //Number of cylinders
max_rated_rpm=2700                             //Max rated RPM
max_rated_hp=180                               //Max rated HP
fuel_metering_type=0                           //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=6.3                         //Propeller Diameter, (feet)
propeller_blades=2                             //Number of propeller blades
propeller_moi=5.0                              //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=0                                  //Miminum governed RPM
prop_tc=0                                      //Prop time-constant
gear_reduction_ratio=1.0                       //Propeller gear reduction ratio
fixed_pitch_beta=20                            //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
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)

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

[hydraulic_system]
normal_pressure = 0.0    //PSI

[Views]
eyepoint=-3.95, -0.85, 2.1         //(feet) longitudinal, lateral, vertical distance from reference datum

[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 

[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=1,1    //Turn AND Bank
[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 7                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 12.7                                 // degrees
flaps-position.2 = 25.3                                 // degrees
flaps-position.3 = 38                                   // degrees
damaging-speed   = 120                                  // KIAS
blowout-speed    = 150                                  // KIAS
lift_scalar = 1.0                                       
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 0                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None

[Reference Speeds]
flaps_up_stall_speed=53.0                  //Knots True (KTAS)
full_flaps_stall_speed=48.0                  //Knots True (KTAS)
cruise_speed=115.0                 //Knots True (KTAS)
max_indicated_speed     = 163                   //Red line (KIAS)

[autopilot]
autopilot_available=1 
flight_director_available=0 
default_vertical_speed=700.0 
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

[stall_warning]
type=1
