[fltsim.0]
title=PA12
sim=PA12
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=NC77583
atc_id_color=0x00000000
ui_manufacturer="Piper"
ui_type="PA-12"
ui_variation="Factory Paint"
ui_typerole="Single Engine Prop"
ui_createdby="Microsoft Corporation"
description="When Piper dropped the J- designation system in exchange for the PA- system, the J-5C became the PA-12 "Super Cruiser". The earlier J-5s had been powered by either a 100 hp (75 kW) Lycoming O-235 or a 75 hp (56 kW) Lycoming O-145. The newer PA-12 model was initially powered by a 108 hp (81 kW) Lycoming O-235-C engine, was fully cowled, and had a metal spar wing with two 19 gallon fuel tanks. A Lycoming O-235-C1 engine rated at 115 hp (86 kW) for take-off was optional.
The PA-12 was approved for wheels, skis, floats and also for crop spraying.
Cockpit accommodation was provided for the pilot in the front seat and two passengers in the rear seat, side-by-side. Unlike the J-3 Cub the PA-12 was flown solo from the front seat."
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
[General]
atc_type=Piper
atc_model=Super Cruiser
editable=0
performance="Cruising Speed\n103 mph \n\nEngine\nLycoming 0-235-0 100 hp\n\nService Ceiling\n12.600 ft \n\nMaximum Range\n600 mi \n\nFuel Capacity\n38 gal \n\nEmpty Weight\n950 lb\n\nGross Weight\n1,750 lb\n\nLength\n31 ft 1 in\n\nWingspan\n35 ft 5.5 in\n\n\nSeating\n3\n\nUseful Load\n800 lb\n\n Designer: P. Clawson"
Category = airplane
[CameraDefinition.0]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 19.0, 0.38, -2.0
InitialPbh = 5, 0, 270
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.1]
Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -19.0, 0.38, -2.0
InitialPbh = 5, 0, 90
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.2]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
ShowWeather = Yes
InitialXyz = 0, 1.9, -15
InitialPbh = 11, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.001]
Title = "Rear Seat"
Guid = {195EAB58-9E4A-4E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.7
SmoothZoomTime = 2.0
ZoomPanScalar = 0.75
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.0, 0.1, -1.2
InitialPbh=7, 0, 0
[weight_and_balance]
// ACM V2.5
max_gross_weight = 1750
empty_weight = 950
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 313.8
empty_weight_roll_MOI = 313.9
empty_weight_yaw_MOI = 642.2
empty_weight_coupled_MOI = 0
max_number_of_stations = 3
station_load.0 = 170.0, 0.58, 0.00, 0.00
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, 0.86, -17.212, 2.58, fx_navred
light.1 = 3, 0.86, 17.212, 2.58, fx_navgre
light.2 = 3, -14.019, 0, 4.404, fx_navwhi
light.3 = 4, -0.7, 0.00, 1.50, fx_vclight,
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.0
min_throttle_limit = 0.0
engine.0 = 5.0, 0, 0,
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup = fx_engstrt_cub
windshield_rain_effect_available = 1
[fuel]
LeftMain = 0.000, -5.100, 1.000, 19.000, 0.000
RightMain = 0.000, 5.100, 1.000, 19.000, 0.000
fuel_type =1
number_of_tank_selectors =1
electric_pump=0
[contact_points]
static_pitch = 12
static_cg_height = 3.7
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7
point.0 = 1, -15.0077, 0, -1.52, 1800, 0, 0.25, 60, 0.3, 2.5, 0.4, 0, 0, 0, 0, 0
point.1 = 1, 1.135, -3, -4.1, 1600, 1, 0.75, 0, 0.129, 1.25, 0.8, 0, 0, 2, 0, 0
point.2 = 1, 1.135, 3, -4.1, 1600, 2, 0.75, 0, 0.129, 1.25, 0.8, 0, 0, 3, 0, 0
point.3 = 2, -1.00, -17.7, 1.80, 800, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0
point.4 = 2, -1.00, 17.7, 1.80, 800, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0
point.5 = 2, -18.8334, 0, 0.3764, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 6.1379, 0, -1.4776, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
[keyboard_response]
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000
[forcefeedback]
ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
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 = 178.5
wing_span = 35.5
wing_root_chord = 5.25
wing_dihedral = 1.5
wing_incidence = 2.5
wing_twist = -1.0
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 1.45
wing_pos_apex_vert = 2.08
htail_area = 18.2
htail_span = 9.60
htail_pos_lon = -11.44
htail_pos_vert = 0.84
htail_incidence = -0.5
htail_sweep = 20
vtail_area = 13.0
vtail_span = 3.31
vtail_sweep = 30
vtail_pos_lon = -11.19
vtail_pos_vert = 1.09
elevator_area = 10.64
aileron_area = 9.6
rudder_area = 6.55
elevator_up_limit = 25.0
elevator_down_limit = 25.0
aileron_up_limit = 25.0
aileron_down_limit = 25.0
rudder_limit = 28.0
elevator_trim_limit = 10.0
spoiler_limit = 0.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
auto_spoiler_available=0
positive_g_limit_flaps_up=0.000000
positive_g_limit_flaps_down=0.000000
negative_g_limit_flaps_up=0.000000
negative_g_limit_flaps_down=0.000000
[electrical]
max_battery_voltage = 0
generator_alternator_voltage = 0
max_generator_alternator_amps = 60
engine_generator_map = 1
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
p_factor_on_yaw = 0.2
torque_on_roll = 0.3
gyro_precession_on_yaw = 0.3
gyro_precession_on_pitch = 0.3
[Flaps.0]
type= 0
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=58.75 //Cubic inches per cylinder
compression_ratio=7.5 //Compression ratio
number_of_cylinders=4 //Number of cylinders
max_rated_rpm=2600 //Max rated RPM
max_rated_hp=100 //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
magneto_order_left_right_both = 1 //sets the order of the magneto switch direction
[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=3.78 //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=0.1 //Prop time-constant
gear_reduction_ratio=1.0 //Propeller gear reduction ratio
fixed_pitch_beta=52.0 //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=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 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 //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
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.8 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint=0.25, 0.000, 1.3
[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
[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=0,0
[vacuum_system]
max_pressure=0
vacuum_type=0 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
[pneumatic_system]
max_pressure=0
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 0.0 //Scalar on heat effectiveness, 0 = not available
[Reference Speeds]
flaps_up_stall_speed=33.0 //Knots True (KTAS)
full_flaps_stall_speed=33.0 //Knots True (KTAS)
cruise_speed=63.0 //Knots True (KTAS)
max_indicated_speed = 106 //Red line (KIAS)
[autopilot]
autopilot_available=0
flight_director_available=0
[stall_warning]
type=1
stick_shaker=0
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
