[fltsim.0]
title=Cessna 337 (D-IDPA)
sim=Cessna337
model=
panel=
sound=
texture=
checklists=
description=Cessna 337 Super Skymaster,\nregistration D-IDPA.\nRepainted by Chris Grabow (using creaTEXtor by Arik Hohmeyer)\nAP2.2c, December 2002
ui_manufacturer=Cessna
ui_type=337 Super Skymaster
ui_variation=blue-white (D-IDPA)
atc_heavy=0
atc_id=D-IDPA
atc_airline=
atc_flight_number=105

[General]
performance=Wing span: 11.63 m\nLength: 9.07 m \nWeight: 2100 kg (max)\nPower: 2x 213 PS \/ 157 kW \nIO-360-GB\nSpeed: 315 km\/h\n\nDesign & Textures: \nArik Hohmeyer\n\nAnimation:\nChris Grabow\n\nFlightdynamic: \nbased on Donn E. Bohde's\n0-2A-air-file\n\nDate: September 2002, \nVersion FS2002.0 (AP 2.2)\n\nFS-DESIGN BERLIN\n(c) 2002 FREEWARE\nwww.fsdesign-berlin.da.ru\n
atc_type=CESSNA
atc_model=C337

[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=0.000000,0.000000,0.000000,0.000000
empty_weight=3022.000
empty_weight_roll_MOI=6333.000
empty_weight_pitch_MOI=4100.000
empty_weight_yaw_MOI=8929.000
empty_weight_coupled_MOI=0.000
max_gross_weight=3922.000
CG_forward_limit=0.000
CG_aft_limit=1.000

[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

[fuel]
LeftMain=0.000, -15.583, 0.000, 75.000, 0.000
RightMain=0.000, 15.583, 0.000, 75.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=203.000
wing_span=38.167
wing_root_chord=4.917
wing_dihedral=2.999
wing_incidence=0.000
wing_twist=4.499
oswald_efficiency_factor=1.087
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=1.229
wing_pos_apex_vert=0.000
htail_area=33.000
htail_span=10.000
htail_pos_lon=-14.500
htail_pos_vert=0.000
htail_incidence=3.246
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=14.190
aileron_area=20.900
rudder_area=14.350
elevator_up_limit=28.000
elevator_down_limit=20.999
aileron_up_limit=19.996
aileron_down_limit=15.000
rudder_limit=23.995
elevator_trim_limit=19.498
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, 5.833, 0.000, -4.917, 1574.803, 0.000, 0.527, 34.200, 0.190, 2.500, 0.812, 5.000, 5.000, 0.000, 0.000, 0.000
point.1=1.000, -2.333, -4.333, -4.500, 1574.803, 1.000, 0.527, 0.000, 0.191, 2.500, 0.812, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1.000, -2.333, 4.333, -4.500, 1574.803, 2.000, 0.527, 0.000, 0.191, 2.500, 0.812, 5.000, 5.000, 3.000, 0.000, 0.000
point.3=2.000, -0.917, -20.333, 2.500, 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, -0.917, 20.333, 2.500, 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, -18.417, 0.000, 0.083, 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, 0.083, 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=2.911
static_cg_height=4.501

[GeneralEngineData]
engine_type=0
Engine.0=10.000, 0.000, -0.500
Engine.1=-8.000, 0.000, 1.250
fuel_flow_scalar=1.000

[piston_engine]
cylinder_displacement=60.000
compression_ratio=7.500
number_of_cylinders=6
max_rated_rpm=2800.000
max_rated_hp=225.000
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.300
turbocharged=1
max_design_mp=37.000
min_design_mp=0.000
critical_altitude=20000.000
emergency_boost_type=0
emergency_boost_mp_offset=0.000
emergency_boost_gain_offset=0.000
fuel_air_auto_mixture=0
auto_ignition=0
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=1.0
propeller_type=0
propeller_diameter=6.833
propeller_blades=2
propeller_moi=5.500
beta_max=43.000
beta_min=15.000
min_gov_rpm=1100.000
prop_tc=0.100
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=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

[Reference Speeds]
flaps_up_stall_speed=70.000
full_flaps_stall_speed=56.000
cruise_speed=167.399

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

[Views]
eyepoint=-0.884289,-0.986815,-0.192237

[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=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
use_no_default_bank=1

use_no_default_pitch=0


[direction_indicators]
direction_indicator.0=1,0

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

[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

[Flaps.0]
type=1
span-outboard=0.500
extending-time=5.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
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=18.999, 0.000
flaps-position.3=28.499, 0.000
flaps-position.4=37.999, 0.000