// FS-DESIGN BERLIN, FD 1.3 by W. Beckert 24-05-2004
// Added fuel tank patch

[fltsim.0]
title=Cessna 337
sim=Cessna337_FS9
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=C337_ref
description=Cessna 337 Super Skymaster, bAIRlin,\nregistration D-BRIK.\nRepainted by Chris Grabow (using creaTEXtor by Arik Hohmeyer)\nAP2.3a1, April 2004\n
ui_manufacturer=Cessna
ui_type=337 Super Skymaster
ui_variation=bAIRlin
atc_heavy=0
atc_id=D-BRIK
atc_airline=
atc_flight_number=23
atc_id_color=0000000000
visual_damage=1

[General]
performance=Wing span: 11.63 m\nLength: 9.07 m \nWeight: 2100 kg (max)\nPower: 2x 210 PS \/ 157 kW \nIO-360-GB\nSpeed: 315 km\/h\n\nBase design & base textures: \nArik Hohmeyer\n\nFSDS2 rework: \nJonathan R. Lueb & Chris Grabow\n\nFlightdynamic: \nbased on Donn E. Bohde's\n0-2A-air-file, reworked for FS2004 by Wolfram Beckert\n\nDate: April 2004, \nVersion AP 2.3\n\nFS-DESIGN BERLIN\n(c) 2004 FREEWARE\nwww.fsdesign-berlin.de.vu\n
atc_type=CESSNA
atc_model=C337
editable=1 

[weight_and_balance]
// ACM V2.3
max_gross_weight = 4200
empty_weight = 2615
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 3100
empty_weight_roll_MOI = 5333
empty_weight_yaw_MOI = 8929
empty_weight_coupled_MOI = 0
max_number_of_stations = 3

station_load.0 = 80.0,-1.0,0.0,0.0, Baggage
station_load.1 = 140.0,-1.0,0.0,0.0, 2 Pax rear
station_load.2 = 140.0, 1.5,0.0,0.0, 2 Crew


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2.38, 11.02, 2.51, fx_landing
light.1 = 3, 1.65, -19.3, 3.1, fx_navredm
light.2 = 2, 1.28, -19.48, 3.1, fx_strobe
light.3 = 2, 1.28, 19.48, 3.1, fx_strobe
light.4 = 3, 1.65, 19.3, 3.1, fx_navgrem
light.5 = 1, -16.23, 5.26, 6.92, fx_beaconb
light.6 = 1, 2.69, 0, -3.55, fx_beaconb
light.7 = 4, 4.65, 0, 0.61, fx_vclight
light.8 = 3, 2.31, -11.02, 2.51, fx_landing

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 0.950
engine.0 = 10.000, 0.000, -0.500
engine.1 = -8.000, 0.000, 0.150
min_throttle_limit=0.000000

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

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 1
number_of_tank_selectors = 2    // requires a panel with tank selector
LeftMain = 0, -14.5, 2.8, 46, 0
LeftAux = 0, -3.1, 2, 18, 0
RightMain = 0, 14.5, 2.8, 46, 0
RightAux = 0, 3.1, 2, 18, 0
electric_pump=1


[contact_points]
static_pitch = 2.92
static_cg_height = 4.501
max_number_of_points = 7

point.0 = 1, 8, 0, -4.99, 1374, 0, 0.527, 30, 0.19, 2.5, 0.812, 5, 5, 0, 0, 0
point.1 = 1, -1.4, -3, -4.5, 1574, 1, 0.527, 0, 0.191, 2.5, 0.812, 5, 5, 2, 0, 0
point.2 = 1, -1.4, 3, -4.5, 1574, 2, 0.527, 0, 0.191, 2.5, 0.812, 5, 5, 3, 0, 0
point.3 = 2.000, -0.917, -20.333, 2.500, 1174.0, 0.000, 0.000, 0.000, 0.000, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4 = 2.000, -0.917, 20.333, 2.500, 1174.0, 0.000, 0.000, 0.000, 0.000, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5 = 2.000, -18.417, 0.000, 0.083, 1174.0, 0.000, 0.000, 0.000, 0.000, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6 = 2.000, 5.833, 0.000, 0.083, 1274.0, 0.000, 0.000, 0.000, 0.000, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0
gear_system_type=0


[keyboard_response]
elevator = 100.000000, 180.000000
aileron = 200.000000, 1000.000000
rudder = 200.000000, 1000.000000


[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

[airplane_geometry]
//ACM_AREAW1// 0,0,0,1.2853,0.6462,0.6462,0,1.2210,1.2925,1.2925
//ACM_AREAW2// 0,1.1568,1.9388,1.9388,0,1.0925,2.5851,2.5851,0,1.0282
//ACM_AREAW3// 3.2314,3.2314,0,0.9640,3.8777,3.8777,0,0.8997,4.5240,4.5240
//ACM_AREAW4// 0,0.8354,5.1703,5.1703,0,0.7712,5.8166,5.8166,0,0.7069
//ACM_AREAH1// 0,0,0,1.0160,0.1693,0.1693,0,0.9652,0.3386,0.3386
//ACM_AREAH2// 0,0.9144,0.5080,0.5080,0,0.8636,0.6773,0.6773,0,0.8128
//ACM_AREAH3// 0.8466,0.8466,0,0.7620,1.0160,1.0160,0,0.7111,1.1853,1.1853
//ACM_AREAH4// 0,0.6604,1.3546,1.3546,0,0.6096,1.5240,1.5240,0,0.5588
//ACM_AREAV1// 0,0,0,2.2253,0.2472,0.2472,0,2.0473,0.4945,0.4945
//ACM_AREAV2// 0,1.8692,0.7417,0.7417,0,1.6912,0.9890,0.9890,0,1.5132
//ACM_AREAV3// 1.2363,1.2363,0,1.3352,1.4835,1.4835,0,1.1571,1.7308,1.7308
//ACM_AREAV4// 0,0.9791,1.9780,1.9780,0,0.8011,2.2253,2.2253,0,0.6230
//ACM_CAREAW1// 2.9083,2.9083,0.6426,0.8997,3.2314,3.2314,0.6426,0.8868,3.5546,3.5546
//ACM_CAREAW2// 0.6426,0.8740,3.8777,3.8777,0.6426,0.8611,4.2009,4.2009,0.6426,0.8483
//ACM_CAREAW3// 4.5240,4.5240,0.6426,0.8354,4.8472,4.8472,0.6426,0.8226,5.1703,5.1703
//ACM_CAREAW4// 0.6426,0.8097,5.4935,5.4935,0.6426,0.7969,5.8166,5.8166,0.6426,0.7840
//ACM_CAREAH1// 0,0,0.5080,1.0160,0.1693,0.1693,0.5080,0.9906,0.3386,0.3386
//ACM_CAREAH2// 0.5080,0.9652,0.5080,0.5080,0.5080,0.9398,0.6773,0.6773,0.5080,0.9144
//ACM_CAREAH3// 0.8466,0.8466,0.5080,0.8890,1.0160,1.0160,0.5080,0.8636,1.1853,1.1853
//ACM_CAREAH4// 0.5080,0.8382,1.3546,1.3546,0.5080,0.8128,1.5240,1.5240,0.5080,0.7874
//ACM_CAREAV1// 0,0,0.5563,1.6690,0.2472,0.2472,0.5563,1.5799,0.4945,0.4945
//ACM_CAREAV2// 0.5563,1.4909,0.7417,0.7417,0.5563,1.4019,0.9890,0.9890,0.5563,1.3129
//ACM_CAREAV3// 1.2363,1.2363,0.5563,1.2239,1.4835,1.4835,0.5563,1.1349,1.7308,1.7308
//ACM_CAREAV4// 0.5563,1.0459,1.9780,1.9780,0.5563,0.9568,2.2253,2.2253,0.5563,0.8678
wing_area = 203.000
wing_span = 38.167
wing_root_chord = 4.217
wing_dihedral = 2.5
wing_incidence = 0.000
wing_twist = -0.5
oswald_efficiency_factor = 0.800
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 1.229
wing_pos_apex_vert = 0.000
htail_area = 36.200
htail_span = 10.000
htail_pos_lon = -14.500
htail_pos_vert = 0.000
htail_incidence = 1.000
htail_sweep = 0.000
vtail_area = 41.000
vtail_span = 7.301
vtail_sweep = 0.000
vtail_pos_lon = -14.583
vtail_pos_vert = 1.500
elevator_area = 16.170
aileron_area = 15.440
rudder_area = 10.700
elevator_up_limit = 25.000
elevator_down_limit = 21.000
aileron_up_limit = 17.500
aileron_down_limit = 15.000
rudder_limit = 24.000
elevator_trim_limit = 20.5
spoiler_limit = 0.000
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 25
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
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           = 0.2
gyro_precession_on_yaw   = 1.0
gyro_precession_on_pitch = 1.0

[pitot_static]
vertical_speed_time_constant=10
//Increasing this value will cause a more instantaneous reaction in the VSI

[piston_engine]
cylinder_displacement=60.160    // real IO-360, 361 cuin/6cylinders
compression_ratio=8.500        // real IO-360 Continental
number_of_cylinders=6 
max_rated_rpm=2800.000 
max_rated_hp=212.000 
fuel_metering_type=0         // fuel injection
cooling_type=0 
normalized_starter_torque=0.200 
turbocharged=1 
max_design_mp=36.000 
min_design_mp=5.000 
critical_altitude=10000.000   // altitude to which full power is provided
emergency_boost_type=0 
emergency_boost_mp_offset=0.000 
emergency_boost_gain_offset=0.000 
fuel_air_auto_mixture=0 
auto_ignition=0 
max_rpm_mechanical_efficiency_scalar=1.000000 
idle_rpm_mechanical_efficiency_scalar=1.000000 
max_rpm_friction_scalar=1.000000 
idle_rpm_friction_scalar=1.000000 

[propeller]
thrust_scalar=1.02       // pusher prop improve thrust
propeller_type=0 
propeller_diameter=6.33  // McCauley 2 blade CS full feathering
propeller_blades=2 
propeller_moi=9.500 
beta_max=38.000 
beta_min=15.000 
min_gov_rpm=1100.000 
prop_tc=0.030 
gear_reduction_ratio=1.000 
fixed_pitch_beta=20.000 
low_speed_theory_limit=80.000 
prop_sync_available=0 
prop_deice_available=0 
prop_feathering_available=1 
prop_auto_feathering_available=0 
min_rpm_for_feather=500.000 
beta_feather=87.000 
power_absorbed_cf=0.400 
defeathering_accumulators_available=0 
prop_reverse_available=0 
minimum_on_ground_beta=0.000 
minimum_reverse_beta=0.000 

[Reference Speeds]
flaps_up_stall_speed=65.000 
full_flaps_stall_speed=55.000 
cruise_speed=167.0            // KTAS at 75% power
max_indicated_speed=190.0     // max permissible in dive

[Views]
eyepoint=2.4,-0.9,1.0    // Pilot view

[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 

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=700.000000 
autothrottle_available=0 
pitch_takeoff_ga=8.000000 
use_no_default_bank=1
use_no_default_pitch=0
default_bank_mode=0
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
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000

[direction_indicators]
direction_indicator.0=1,0 

[Flaps.0]
type=1
span-outboard=0.500
extending-time=5.000
system_type=0
damaging-speed=150.000
blowout-speed=170.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=9.500, 0.000
flaps-position.2=19.0, 0.000
flaps-position.3=28.0, 0.000
flaps-position.4=38.0, 0.000

[brakes]
toe_brakes_scale=1.000000
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=15.9
flap_limit_idle=0.000000

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0