[fltsim.0]
title=Cessna LC-126 AK S&R
sim=Cessna_lc126
panel=
model=
sound=
texture=
checklists=
description=The USAF discovered the Cessna 195 when a bush flyer landed his float plane on a northern ice cap and, in two trips, brought out 12 injured flyers. They ordered twelve LC-126's and put them through hell, the only repairs made to those original 12 was caused by pilot error.
ui_manufacturer=Cessna
ui_type=C195 Shakey Jake
ui_variation=LC-126 Floatplane
atc_heavy=0
atc_id=AR948
visual_damage=1
atc_airline=
atc_flight_number=
[General]
performance=-Dimensions \nSpan : 36.3 ft \nLength : 27.4 ft \nHeight : 7.2 ft \n-Weight \nempty : 2,050 lb \nmax : 3,350 lb \n-Power Plant : 275 Jacobs \n-Performance : 143 cruise\nmax speed : 154 mph, Vne 173 \nceiling : \nrange : \n\nAircraft by:OK Designs\/Lizardo\n
atc_type=Cessna
atc_model=C195
//Note:The following are not intended to reflect actual plane dimensions etc, but just to achive proper flight dynamics. See www.cessna195.org
[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=170.00, 2.75, -1.20, -.50 //Pilot
station_load.1=170.00, 2.75, 1.20, -.50 //Pilot girlfriend and beer
empty_weight=2430.000
empty_weight_roll_MOI=3500.000
empty_weight_pitch_MOI=4400.000
empty_weight_yaw_MOI=5800.000
empty_weight_coupled_MOI=0.000
max_gross_weight=3350.000
CG_forward_limit=0.000
CG_aft_limit=1.000
[fuel]
LeftMain=0.000, 2.000, 2.750, 40.000, 0.000
RightMain=0.000, -2.000, 2.750, 40.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=1
[airplane_geometry]
wing_area=350.0
wing_span=50.0
wing_root_chord=7.0
wing_dihedral=1.000
wing_incidence=1.000
wing_twist=0.00
oswald_efficiency_factor=0.75
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=0.000
wing_pos_apex_vert=3.00
htail_area=29.000
htail_span=10.500
htail_pos_lon=-28.3
htail_pos_vert=0.000
htail_incidence=0.00
htail_sweep=0.000
vtail_area=25.000
vtail_span=6.0
vtail_sweep=0.000
vtail_pos_lon=-28.3
vtail_pos_vert=4.500
elevator_area=20.0
aileron_area=25.00
rudder_area=25.00
elevator_up_limit=25.0
elevator_down_limit=25.0
aileron_up_limit=22.00
aileron_down_limit=22.00
rudder_limit=25.0
elevator_trim_limit=19.5
spoiler_limit=0
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000
[contact_points]
//0 Class
//1 Longitudinal Position (feet, + = fwd)
//2 Lateral Position (feet, + = right)
//3 Vertical Position (feet, + = above)
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
// 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.0=4, 9.0, -5.1, -5.90, 3600, 0, 0.0, 0.0, 0.4, 2.5, 0.85, 0.0, 0.0, 1, 0.0, 0.0
point.1=4, 9.0, 5.1, -5.90, 3600, 0, 0.0, 0.0, 0.4, 2.5, 0.85, 0.0, 0.0, 2, 0.0, 0.0
point.2=4, -6.5, -5.1, -5.40, 3600, 0, 0.0, 0.0, 0.4, 2.5, 0.85, 0.0, 0.0, 3, 0.0, 0.0
point.3=4, -6.5, 5.1, -5.40, 3600, 0, 0.0, 0.0, 0.4, 2.5, 0.85, 0.0, 0.0, 4, 0.0, 0.0
point.4=5, -12.5, 5.1, -6.90, 3600, 0, 0.0, 35.0, 0.0, 0.0, 0.5, 1.0, 1.0, 0, 0.0, 0.0 //water rudder
point.5=5 -12.5 -5.1, -6.90, 3600, 0, 0.0, 35.0, 0.0, 0.0, 0.5, 1.0, 1.0, 0, 0.0, 0.0
// Scrapes
point.5=2, 0.0, -24.0, 4.0, 308.5, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 //left wing
point.6=2, 0.0, 24.0, 4.0, 308.5, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 //right wing
point.7=2, -22.0, 0.0, 0.3, 916.5, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 //tail cone
point.8=2, 6.5, 0.0, -2.2, 1274.5, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 //nose
point.9=2, -19.6, 0.0, 7.5, 308.5, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0 //tail
static_pitch=2.0
static_cg_height=5.168
[GeneralEngineData]
engine_type= 0
Engine.0= 8.000, 0.000, 0.000
fuel_flow_scalar= 0.5
min_throttle_limit=0.000000
[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.72
idle_rpm_mechanical_efficiency_scalar=0.5
max_rpm_friction_scalar=.98
idle_rpm_friction_scalar=.10
cylinder_displacement= 107.85
compression_ratio= 8.000
number_of_cylinders= 7
max_rated_rpm= 2400.000
max_rated_hp= 300.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.500
turbocharged= 0
max_design_mp= 00.000
min_design_mp= 00.000
critical_altitude= 000.000
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=1.12
[propeller]
propeller_type= 0
propeller_diameter= 8.500
propeller_blades= 2
propeller_moi= 8.000
beta_max= 45.000
beta_min= 15.000
min_gov_rpm= 2000.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 0.000
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=1.12
[Reference Speeds]
flaps_up_stall_speed= 64.000
full_flaps_stall_speed= 62.000
cruise_speed= 139.000
max_indicated_speed=190.000000 //
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[Views]
eyepoint= 1.1, -0.85, 1.15
[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, 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
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
[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
yaw_damper_gain=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
[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, -.22, -18.0, 2.119, fx_navred
light.1 = 3, -.22, 18.0, 2.119, fx_navgre
light.2 = 3, -20.36, 0.00, .83, fx_navwhi
light.3 = 2, -.36, -17.85, 2.11, fx_strobe
light.4 = 2, -.36, 17.85, 2.11, fx_strobe
light.5 = 1, -9.13, 0.00, 1.43, fx_beacon
light.6 = 4, 2.00, 0.00, 1.400, fx_vclight
[EFFECTS]
wake=fx_wake
water=fx_waterland
;water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[direction_indicators]
direction_indicator.0=1,0
[SMOKESYSTEM]
smoke.0=0.0, 3.50, 0.00, fx_ICFX_F4U_Startup
smoke.1=0.0, 3.50, -2.50, fx_ICFX_RadialXtra
smoke.2=0.0, 3.50, 2.50, fx_ICFX_RadialXtra
smoke.3=0.0, 2.50, -3.50, fx_ICFX_RadialXtra
smoke.4=0.0, 2.50, 3.50, fx_ICFX_RadialXtra
smoke.5=0.0, 3.50, -2.20, fx_ICFX_F4U_Smoke //optional
smoke.6=0.0, 3.50, 2.20, fx_ICFX_F4U_Smoke //optional
[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.05
roll_stability=1.0
yaw_stability=1.0
parasite_drag_scalar=1.2
induced_drag_scalar=1.0
elevator_effectiveness=1.05
aileron_effectiveness=1.05
rudder_effectiveness=.5
elevator_trim_effectiveness=.82
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
p_factor_on_yaw = .90
torque_on_roll = .80
gyro_precession_on_yaw = 1.0
gyro_precession_on_pitch = 1.0
[Flaps.0]
type=1
span-outboard=0.600
extending-time=5.000
system_type=0
damaging-speed=120.000
blowout-speed=140.000
lift_scalar=.900
drag_scalar=1.40
pitch_scalar=.01
flaps-position.0=0.000, 0.000
flaps-position.1=11.25, 0.000
flaps-position.2=22.5, 0.000
flaps-position.3=33.75, 0.000
flaps-position.4=45.0, 0.000
[folding_wings]
wing_fold_system_type = 4 ;0=None
fold_rates = 0.5,0.5 ;Percent per second
[exits]
number_of_exits = 2
exit_rate.0 = 0.3 ;Percent per second
exit_rate.1 = 0.3 ;Percent per second
[brakes]
toe_brakes_scale=1.4
parking_brake=1
differential_braking_scale = 1.5
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[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
