[fltsim.0]
title=Piper Cub 71H
sim=PiperCub
model=
panel=1
sound=
texture=N4971H
checklists=
atc_id=N4971H
ui_manufacturer=Piper
ui_type=PA-11
ui_variation=71 Hotel
atc_heavy=0
atc_airline=
atc_flight_number=
description="The Piper PA-11 'Cub Special' was the successor of the original J3-Cub. With its stronger framework, a more powerful engine and the closed cowling the PA-11 was a link between the original J3-Cub and the PA-18 Super-Cub. The N4971H was the plane that carried Kern and Rinker Buck from coast to coast in Summer 1966 on their famous 'Flight of Passage'"

[fltsim.1]
title=Piper Cub 11U
sim=PiperCub
model=
panel=
sound=
texture=N4711U
checklists=
atc_id=N4711U
ui_manufacturer=Piper
ui_type=PA-11
ui_variation=JeffAir
atc_heavy=0
atc_airline=
atc_flight_number=
description="The Piper PA-11 'Cub Special' was the successor of the original J3-Cub. With its stronger framework, a more powerful engine and the closed cowling the PA-11 was a link between the original J3-Cub and the PA-18 Super-Cub. N4711U is a new PA-11 that Cub-Pilot Jeff Russell (JeffAir, Hampden/Maine) has built himself.


[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

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_beacon=0, 5 , 17.0
light_panel=0, 5 , 17.0

[LIGHTS]
light.0 = 4,  -2.27,   0.00,  1.40, fx_vclight

[General]
atc_type=PIPER
atc_model=PA11
editable=1
performance=Maximum Speed\n110 mph    96 kts\t175 km\/hr\n\nEngine\nContinental 85-hp air cooled\n\nService Ceiling\n12,000 ft\t3,660 m\n\nMaximum Range\n210 nm    390 km\n\nFuel Capacity\n12 gal\t45.4 L\n\nEmpty Weight\n660 lb\t300 kg\n\nGross Weight\n1,140 lb \t500 kg\n\nLength\n22 ft \t6.7 m\n\nWingspan\n35 ft\t10.6 m\n\nHeight\n6.7 ft\t2 m\n\nSeating\n2\n\nUseful Load\n540 lb \t245 kg

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations= 50
station_load.0= 0.000, 0.000, 0.000, 0.000, Pilot1
station_load.1= 170.000, -2.000, 0.000, 0.000, Pilot2
station_load.2= 35.000, -3.000, 0.000, 0.000, Baggage
empty_weight= 660.000
empty_weight_roll_MOI= 2000.000
empty_weight_pitch_MOI= 2000.000
empty_weight_yaw_MOI= 4000.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 1140.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[fuel]
LeftMain= 0.000, 0.000, 0.000, 6.000, 0.000
RightMain= 0.000, 0.000, 0.000, 6.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area= 185.000
wing_span= 35.167
wing_root_chord= 5.250
wing_dihedral= 1.000
wing_incidence= 0.000
wing_twist= -1.000
oswald_efficiency_factor= 0.870
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 40.000
htail_span= 9.500
htail_pos_lon= -14.000
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 18.000
vtail_span= 4.837
vtail_sweep= 0.000
vtail_pos_lon= -14.000
vtail_pos_vert= 1.500
elevator_area= 12.470
aileron_area= 18.500
rudder_area= 6.300
elevator_up_limit= 27.502
elevator_down_limit= 20.626
aileron_up_limit= 19.481
aileron_down_limit= 14.897
rudder_limit= 23.491
elevator_trim_limit= 19.481
spoiler_limit= 59.989
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.0, -14.90,   0.0, -1.610, 1500.000, 0.00, 0.30,  80.0, 0.25, 2.50, 0.70, 0.00, 0.00, 0.00, 0.00, 0.00
point.1= 1.0,   1.00,  -4.5, -4.430, 2500.000, 1.00, 0.50,   0.0, 0.30, 2.50, 0.70, 0.00, 0.00, 2.00, 0.00, 0.00
point.2= 1.0,   1.00,   4.5, -4.430, 2500.000, 2.00, 0.50,   0.0, 0.30, 2.50, 0.70, 0.00, 0.00, 3.00, 0.00, 0.00
point.3= 2.000, -0.833, -18.000, 3.417, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -0.833, 18.000, 3.417, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -15.417, 0.000, 0.167, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 5.833, 0.000, -2.167, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 11.000
static_cg_height= 4.000

[GeneralEngineData]
engine_type= 0
Engine.0= 8.333, 0.000, 0.417
fuel_flow_scalar= 1.100
min_throttle_limit=0.000000

[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=0.900
cylinder_displacement= 87.0
compression_ratio= 8.800
number_of_cylinders= 4
max_rated_rpm= 2400.000
max_rated_hp= 85.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
power_scalar=1.000

[propeller]
propeller_type= 1
propeller_diameter= 6.200   // was 6.2
propeller_blades= 2
propeller_moi= 1.900   // was 2.9
beta_max= 0
beta_min= 0
min_gov_rpm= 1400.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 18.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
thrust_scalar=1.000

[Reference Speeds]
flaps_up_stall_speed= 33.000
full_flaps_stall_speed= 26.400
cruise_speed= 70.000
max_indicated_speed=108.000000

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint = -0.25, 0.000, 0.90

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[direction_indicators]
direction_indicator.0=1,0

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[Flaps.0]
type= 0

[brakes]
toe_brakes_scale=1.0000
parking_brake=1

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

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