[fltsim.0] title=Cessna Skyhawk 172SP sim=Cessna172SP model= panel= sound= texture= kb_checklists=Cessna172SP_check kb_reference=Cessna172SP_ref atc_id=N172 ui_manufacturer=Cessna ui_type="C172SP Skyhawk" ui_variation="Horizon" description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane. One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots. Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for more than 35 years." [fltsim.1] title=Cessna Skyhawk 172SP IFR sim=Cessna172SP model= panel=ifr sound= texture= kb_checklists=Cessna172SP_check kb_reference=Cessna172SP_ref atc_id=N513TP ui_manufacturer=Cessna ui_type="C172SP Skyhawk" ui_variation="172 Sky - IFR panel" description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane. One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots. Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for more than 35 years." [fltsim.2] title=Cessna Skyhawk 172SP Paint1 sim=Cessna172SP model= panel= sound= texture=1 kb_checklists=Cessna172SP_check kb_reference=Cessna172SP_ref atc_id=N458TP ui_manufacturer=Cessna ui_type="C172SP Skyhawk" ui_variation="Smoothie" description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane. One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots. Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for more than 35 years." [fltsim.3] title=Cessna Skyhawk 172SP Paint2 sim=Cessna172SP model= panel= sound= texture=2 kb_checklists=Cessna172SP_check kb_reference=Cessna172SP_ref atc_id=N1MARK atc_id_color=0xffffffff ui_manufacturer=Cessna ui_type="C172SP Skyhawk" ui_variation="Chlorophila" description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane. One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots. Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for more than 35 years." [fltsim.4] title=Cessna Skyhawk 172SP Paint3 sim=Cessna172SP model= panel= sound= texture=3 kb_checklists=Cessna172SP_check kb_reference=Cessna172SP_ref atc_id=N172AA atc_id_color=0xbbb169 ui_manufacturer=Cessna ui_type="C172SP Skyhawk" ui_variation="Cleo" description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane. One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots. Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for more than 35 years." [fltsim.5] title=Cessna Skyhawk 172SP Paint4 sim=Cessna172SP model= panel= sound= texture=4 kb_checklists=Cessna172SP_check kb_reference=Cessna172SP_ref atc_id=N173BB atc_id_color=0xab1a1a ui_manufacturer=Cessna ui_type="C172SP Skyhawk" ui_variation="Cloud 9" description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane. One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots. Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for more than 35 years." [fltsim.6] title=Cessna Skyhawk 172SP Paint5 sim=Cessna172SP model= panel= sound= texture=5 kb_checklists=Cessna172SP_check kb_reference=Cessna172SP_ref atc_id=N72CBA atc_id_color=0xbbb169 ui_manufacturer=Cessna ui_type="C172SP Skyhawk" ui_variation="Mistique" description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane. One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots. Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for more than 35 years." [General] atc_type=Cessna atc_model=C172 editable=0 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] max_gross_weight = 2550 // (pounds) empty_weight = 1650 // (pounds) reference_datum_position = 3.6, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -3.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "170, -3.0, -1.5, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "170, -3.0, 1.5, 0.0, Front Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "0, -6.2, -1.5, 0.0, Rear Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "0, -6.2, 1.5, 0.0, Rear Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "0, -8.0, 0.0, 0.0, Baggage" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 1400.0 empty_weight_roll_MOI = 1137.0 empty_weight_yaw_MOI = 2360.0 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 [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 2.4, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 0.88 //Fuel flow scalar min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser [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) [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 //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, 0.90, 0.00, -4.09, 1500, 0, 0.5, 22.0, 0.25,2.5, 0.7, 0.0, 0.0, 0 point.1 = 1, -4.70, -4.50, -4.01, 3500, 1, 0.5, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2 point.2 = 1, -4.70, 4.50, -4.01, 3500, 2, 0.5, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3 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 max_number_of_points = 21 static_pitch=3.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=3.765 //feet, altitude of CG when at rest on the ground [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit 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 [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=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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain = -3.9, -2.1, 2.5, 26.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -3.9, 2.1, 2.5, 26.5, 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 = 1 electric_pump=1 [airplane_geometry] wing_area = 174.0 //Square feet wing_span = 36.1 //Feet wing_root_chord = 4.9 //Feet wing_dihedral = 1.7 //Degrees wing_incidence = 1.5 //Degrees wing_twist = -3.0 //Degrees oswald_efficiency_factor= 0.68 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 0 //Degrees, wing leading edge wing_pos_apex_lon = -2.4 //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 = -18.3 //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 = 3.2 //Degrees htail_sweep = 10.0 //Degrees, horizontal tail leading edge vtail_area = 18.0 //Square feet vtail_span = 4.8 //Feet, tip to body vtail_sweep = 40.0 //Degrees, vertical tail leading edge vtail_pos_lon = -16.2 //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 = 6.7 //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 = 24.0 //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 [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 [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 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 [stall_warning] type=1