[fltsim.0]
title =Cri-Cri MC-15
sim =cricri
model =
panel =
sound =
texture =
panel_alias =
sound_alias =
kb_checklists =
kb_reference =
atc_id = f-palu
atc_id_color = 0xffffffff
atc_parking_types =
atc_parking_code =
ui_manufacturer =Colomban
ui_type =Cri-Cri MC-15
ui_variation =Blanc et bleu
description =Le plus petit bi-moteur du monde, plus leger que son pilote et capable de faire de la voltige.\nConcu par Michel Colomban en 1973, cet incroyable petit appareil reste inegalй dans beaucoup de domaines.
atc_heavy=
atc_airline=
atc_flight_number=

[General]
atc_type =EXPERIMENTAL
atc_model =
editable = 1
performance =Flight Dynamics Workbook V2.84.50\n+ Weight: 180 lbs    Max 400 lbs \n+ Power: 15 hp \n+ Max speed @ SL: 127 mph \n+ Max speed: 115 mph @ 8000 ft \n+ Climb rate: 1200 ft\/min @ 115 mph

[pitot_static]
vertical_speed_time_constant = 2

[WEIGHT_AND_BALANCE]
max_gross_weight = 400.000
empty_weight = 180.000

reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position  = -0.200, 0.000, 0.000
CG_forward_limit = 0.000
CG_aft_limit = 1.000

max_number_of_stations = 2
station_load.0 =170.000000, -0.100000, 0.000000, 0.000000, Pilot

empty_weight_pitch_MOI = 100.000
empty_weight_roll_MOI = 90.000
empty_weight_yaw_MOI = 130.000
empty_weight_coupled_MOI = 0.000

[flight_tuning]
cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1
elevator_effectiveness = 2.2
aileron_effectiveness = 1
rudder_effectiveness = 1
pitch_stability = 1
roll_stability = 1
yaw_stability = 1
elevator_trim_effectiveness = 1
aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1
hi_alpha_on_roll = 1
hi_alpha_on_yaw = 1
p_factor_on_yaw = 1
torque_on_roll = 1
gyro_precession_on_roll = 1
gyro_precession_on_yaw = 1

[GeneralEngineData]
engine_type = 0
Engine.0 = 3.000, 1.500, 0.650
Engine.1 = 3.000, -1.500, 0.650
fuel_flow_scalar = 1.000
min_throttle_limit = 0

[piston_engine]
power_scalar = 1
cylinder_displacement = 129.000
compression_ratio = 8.300
number_of_cylinders = 1
max_rated_rpm = 6000.000
max_rated_hp = 15.000
fuel_metering_type = 2
cooling_type = 0
normalized_starter_torque = 0.339
turbocharged = 1
max_design_mp = 29.900
min_design_mp = 9.000
critical_altitude = 8000.000
emergency_boost_type = 0
emergency_boost_mp_offset = 0.000
emergency_boost_gain_offset = 0.000
fuel_air_auto_mixture = 1
auto_ignition = 0
emergency_boost_duration = 0
max_rpm_mechanical_efficiency_scalar = 1
idle_rpm_mechanical_efficiency_scalar = 1
max_rpm_friction_scalar = 1
idle_rpm_friction_scalar = 0.4

[propeller]
thrust_scalar = 1
propeller_type = 1
propeller_diameter = 2.300
propeller_blades = 2
propeller_moi = 0.200
beta_max = 25.000
beta_min = 5.000
min_gov_rpm = 900.000
prop_tc = 0.010
gear_reduction_ratio = 1.000
fixed_pitch_beta = 15.000
low_speed_theory_limit = 79.733
prop_sync_available = 1
prop_deice_available = 1
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 = 0.000
minimum_on_ground_beta = 1.000
minimum_reverse_beta = -14.000
rotation = 1, 1


[folding_wings]
wing_fold_system_type =  0
fold_rates =  0.12, 0.11


[contact_points]
max_number_of_points = 7
point.0 = 1.000, 4.000, 0.000, -1.650, 2165.354, 0.000, 0.200, 20.000, 0.100, 2.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000
point.1 = 1.000, -1.000, -2.000, -1.800, 2165.354, 1.000, 0.220, 0.000, 0.100, 2.500, 0.650, 0.000, 0.000, 2.000, 0.000, 0.000
point.2 = 1.000, -1.000, 2.000, -1.800, 2165.354, 2.000, 0.220, 0.000, 0.100, 2.500, 0.650, 0.000, 0.000, 3.000, 0.000, 0.000
point.3 = 2.000, 4.500, 0.000, 0.000, 2100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.4 = 2.000, -8.000, 0.000, -0.500, 3000.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.5 = 2.000, -1.000, 8.000, 0.000, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.6 = 2.000, -1.000, -8.000, 0.000, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000

static_pitch= 0.000
static_cg_height= 1.850
gear_system_type = 1


[Views]
eyepoint= 0, 0, 2




[electrical]
max_battery_voltage = 12
generator_alternator_voltage = 28
max_generator_alternator_amps = 160
electric_always_available = 1


avionics = 1, 5, 17
additional_system = 0, 20, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17


[LIGHTS]

[keyboard_response]
elevator = 350, 500
aileron  = 450, 1000
rudder   = 200, 1000

[direction_indicators]
direction_indicator.0 = 1, 0

[exits]
number_of_exits = 1
exit_rate.0 = 0.4

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

[autopilot]
autopilot_available = 0
flight_director_available = 0
autothrottle_available = 0

[fuel]
Center2 = 0.500, 0.000, 0.000, 6.000, 0.000
fuel_type =  1
number_of_tank_selectors = 1
electric_pump=0

[airplane_geometry]
wing_area = 32.000
wing_span = 16.000
wing_root_chord = 2.000
wing_dihedral = 3.000
wing_incidence = 0.000
wing_twist = 0.000
oswald_efficiency_factor = 0.863
wing_winglets_flag = 0
wing_sweep  = 0.000
wing_pos_apex_lon = 0.500
wing_pos_apex_vert = 0.000
htail_area = 4.500
htail_span = 6.600
htail_pos_lon = -22.700
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 2.500
vtail_span = 2.900
vtail_sweep = 0.000
vtail_pos_lon  = -22.300
vtail_pos_vert = 0.000
elevator_area = 4.500
aileron_area = 2.300
rudder_area = 1.000
elevator_up_limit = 17.000
elevator_down_limit = 12.000
aileron_up_limit = 16.000
aileron_down_limit = 16.000
rudder_limit = 20.000
elevator_trim_limit = 18.000
spoiler_limit = 0.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000

[Reference Speeds]
flaps_up_stall_speed    = 46.900
full_flaps_stall_speed  = 40.000
cruise_speed            = 105.000
max_indicated_speed = 141
max_mach = 0.2129

[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 = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[gear_warning_system]
gear_warning_available = 0

[brakes]
toe_brakes_scale = 0.640888698995941
parking_brake = 0

[stall_warning]
type = 1

[hydraulic_system]
electric_pumps = 0
engine_map = 1, 1, 0, 0
normal_pressure = 998

[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 3.000
system_type= 3
damaging-speed= 148.000
blowout-speed= 162.000
lift_scalar= 0.000
drag_scalar= 0.000
pitch_scalar= 1.200
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 27.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.500
extending-time= 3.000
system_type= 3
damaging-speed= 148.000
blowout-speed= 162.000
lift_scalar= 1.600
drag_scalar= 0.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 27.000, 0.000
flaps-position.2= 13.500, 0.000
[Flaps.2]
type= 2
span-outboard= 0.500
extending-time= 3.000
system_type= 3
damaging-speed= 148.000
blowout-speed= 162.000
lift_scalar= 0.000
drag_scalar= 1.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 2.000, 0.000
flaps-position.2= 27.000, 0.000