[fltsim.0]
title=Cessna 195 red
sim=cessna195
panel=
model=s
sound=
texture=
prop_anim_ratio=2.7
checklists=
description=The last Cessna to maintain the pre-war tradition of the radial engine. High performance is achieved through clean aerodynamics and a lot of Jacobs horsepower. 300 compared to 145 for the Cessna 170. A successful blend of old and new technology. It was also one of the last planes designed to look good.
ui_manufacturer=Cessna
ui_type=C195 Shakey Jake
ui_variation=Default
atc_heavy=0
atc_id=N700MS
visual_damage=1
atc_airline=
atc_flight_number=
[fltsim.1]
title=Cessna 195 dressed red
sim=cessna195
panel=
model=wp
sound=
texture=
prop_anim_ratio=2.7
checklists=
description=The last Cessna to maintain the pre-war tradition of the radial engine. High performance is achieved through clean aerodynamics and a lot of Jacobs horsepower. 300 compared to 145 for the Cessna 170. A successful blend of old and new technology. It was also one of the last planes designed to look good.
ui_manufacturer=Cessna
ui_type=C195 Shakey Jake
ui_variation=wheelpants
atc_heavy=0
atc_id=N700MS
visual_damage=1
atc_airline=
atc_flight_number=
[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
[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
[General]
performance=Length:27.4'\nSpan:36.3'\nWeight:2030 empty\nPower: Jacobs 300 radial engine\nRange: 610NM @max cruise\nDate:Aug 2003\
nDetails: 18,300ceiling, max speed 156kts, cruise 139kts \nDesigner: Lizardo
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= 0.00, 0.000, 0.000
max_number_of_stations=6
station_load.0= 170.000, 1.00, 1.40, -.50,
station_load.1= 170.000, 1.00, -1.40,-.50,
station_load.2= 100.00,-14.0, 0.0, 0.0 //beer ballast
empty_weight= 3730.0
empty_weight_roll_MOI= 20000.000
empty_weight_pitch_MOI= 10000.000
empty_weight_yaw_MOI= 25000.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 5050.0
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= 306.0
wing_span= 42.000
wing_root_chord= 7.300
wing_dihedral= 1.000
wing_incidence= 2.00
wing_twist= 0.000
oswald_efficiency_factor= 0.90
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 2.558
htail_area= 29.000
htail_span= 10.500
htail_pos_lon= -16.000
htail_pos_vert= 1.292
htail_incidence= -0.500
htail_sweep= 0.000
vtail_area= 25.000
vtail_span= 6.000
vtail_sweep= 0.000
vtail_pos_lon= -16.000
vtail_pos_vert= 2.000
elevator_area= 28.000
aileron_area= 22.000
rudder_area= 15.000
elevator_up_limit= 26.500
elevator_down_limit= 26.500
aileron_up_limit= 20.000
aileron_down_limit= 20.000
rudder_limit= 25.000
elevator_trim_limit= 15.500
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
[contact_points]
point.0= 1.000, -18.917, 0.000, -1.37, 1574.803, 0.000, 0.518, 60.000, 0.250, 2.500, 0.900, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 1.800, -4.0, -5.14, 1574.803, 1.000, 0.518, 10.000, 0.250, 2.500, 0.900, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 1.800, 4.0, -5.14, 1574.803, 2.000, 0.518, 10.000, 0.250, 2.500, 0.900, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, -1.000, -18.167, 2.083, 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, -1.000, 18.167, 2.083, 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, -19.917, 0.000, 1.417, 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, 3.583, 0.000, 1.333, 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= 10.000
static_cg_height= 4.168
[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=1.7
idle_rpm_mechanical_efficiency_scalar=0.5
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=.10
cylinder_displacement= 107.85
compression_ratio= 8.000
number_of_cylinders= 7
max_rated_rpm= 2200.000
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=1.48
[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=1.28
[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
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=1.000000
[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_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_ICFX_tiremark_6, 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=1.0
roll_stability=1.0
yaw_stability=1.0
parasite_drag_scalar=1.08
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
[folding_wings]
wing_fold_system_type = 4 ;0=None
fold_rates = 0.5,0.5 ;Percent per second
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 125.000
blowout-speed= 145.000
lift_scalar= .90
drag_scalar= 1.30
pitch_scalar= 0.01
flaps-position.0= 0.000, 0.000
flaps-position.1= 11.250, 0.000
flaps-position.2= 22.500, 0.000
flaps-position.3= 33.750, 0.000
flaps-position.4= 45.000, 0.000
[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