[fltsim.0] title=Cessna 337 N337DD sim=Cessna337 model= panel= sound= texture= checklists= description=Cessna 337 Super Skymaster,\nregistration G-AXFG.\n ui_manufacturer=Cessna ui_type=337 Super Skymaster ui_variation=yellow-white atc_heavy=0 atc_id=N337DD atc_airline= atc_flight_number= [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 2.2b)\n\nFS-DESIGN BERLIN\n(c) 2002 FREEWARE\nwww.fsdesign-berlin.da.ru\n atc_type=CESSNA atc_model=C185 [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 = 0.8 aileron_effectiveness = 1.1 rudder_effectiveness = 0.9 pitch_stability = 1.4 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 = 176.0 //Square feet wing_span = 36.0 //Feet wing_root_chord = 4.9 //Feet wing_dihedral = 1.7 //Degrees wing_incidence = 1.5 //Degrees wing_twist = -3.0 //Degrees oswald_efficiency_factor= 0.7 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 0.0 //Degrees, wing leading edge wing_pos_apex_lon = -2.4 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_area = 39.0 //Square feet htail_span = 11.7 //Feet htail_pos_lon = -18.3 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_incidence = 3.2 //Degrees htail_sweep = 10.0 //Degrees, horizontal tail leading edge vtail_area = 18.0 //Square feet vtail_span = 4.8 //Feet, tip to body vtail_sweep = 40.0 //Degrees, vertical tail leading edge vtail_pos_lon = -16.2 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going up elevator_area = 16.6 //Square feet aileron_area = 18.3 //Square feet rudder_area = 6.7 //Square feet elevator_up_limit = 28.0 //Degrees elevator_down_limit = 21.0 //Degrees aileron_up_limit = 20.0 //Degrees aileron_down_limit = 15.0 //Degrees rudder_limit = 24.0 //Degrees elevator_trim_limit = 19.5 //Degrees spoiler_limit = 0.0 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 0 //Aileron to spoileron gain min_ailerons_for_spoilerons = 0 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate [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=2850.000 max_rated_hp=225.000 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.300 turbocharged=1 max_design_mp=37.50 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=900.000000 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=100.000000 use_no_default_pitch=1 use_no_default_bank=1 pitch_takeoff_ga=8.000000 [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=1250 ; 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=28.499, 0.000
