[fltsim.0] title=O1e Canadian Air Force sim=O1e model= panel= sound_alias=c172\sound texture=2 kb_checklists= kb_reference= atc_id= ui_manufacturer=Cessna ui_type=C305C Bird Dog ui_variation= O1E Canada description=The Model 305, a development of the Model 170 was a private venture which in 1950 won the competition for a new standard liason\/observation aircraft for the US army. [fltsim.1] title=O1e RoKAF sim=O1e model= panel= sound= texture=1 kb_checklists= kb_reference= atc_id= ui_manufacturer=Cessna ui_type=C305C Bird Dog ui_variation= O1E RoKAF description=The Model 305, a development of the Model 170 was a private venture which in 1950 won the competition for a new standard liason\/observation aircraft for the US army. [General] atc_type=Cessna atc_model=C305C editable=0 performance=Length:7.89m (25'10ft) \nWing span:10.97m (36'0ft) \nEmpty Weight:732kg (1614lb) \nMTOW:1088kg (2400lb) \nPower:213hp Continental O-470-11 \nDetails:\nDesign & Paint: Massimo Taccoli\nDate:December 2001\nEmail: maxtaccoli@tiscalinet.it [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=170.0,0.000000,0.000000,0.000000 station_load.1=170.0,-3.0000,0.000000,0.000000 max_gross_weight=2400 empty_weight=1614.000000 ;Moments of Inertia empty_weight_roll_MOI=3900.000000 empty_weight_pitch_MOI=4207.000000 empty_weight_yaw_MOI=5000.000000 empty_weight_coupled_MOI=0.000000 [fuel] LeftMain=-3.9,-2.1,2.5,25.000000,0.000000 RightMain=-3.9,2.1,2.5,25.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=174.000000 wing_span=36.0 wing_root_chord=4.9 wing_dihedral=1.7 wing_incidence=1.5 wing_twist=-3.0 oswald_efficiency_factor=0.69 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=39.000000 htail_span=11.666667 htail_pos_lon=-15.000000 htail_pos_vert=0.000000 htail_incidence=3.2 htail_sweep=0.000000 vtail_area=18.0 vtail_span=5.2 vtail_sweep=40 vtail_pos_lon=-15.000000 vtail_pos_vert=1.500000 elevator_area=6.7 aileron_area=18.3 rudder_area=7.000000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1.0,-18.583, 0.000,-0.246,1574.80,0.00,0.0820, 0.00,0.286,2.50,0.85,5.00, 5.00,0.00,0.00,0.00 point.1=1.0, 2.0801,-3.848,-5.755,1574.80,1.00,0.5938, 0.00,0.333,2.50,0.85,5.00, 5.00,2.00,0.00,0.00 point.2=1.0, 2.0801,3.8484,-5.755,1574.80,2.00,0.5938, 0.00,0.333,2.50,0.85,5.00, 5.00,3.00,0.00,0.00 point.3=2.0, -0.917,-18.917, 3.500,1574.80,0.00,0.0000, 0.00,0.000,0.00,0.00,0.00, 0.00,5.00,0.00,0.00 point.4=2.0, -0.917, 18.917, 3.500,1574.80,0.00,0.0000, 0.00,0.000,0.00,0.00,0.00, 0.00,6.00,0.00,0.00 point.5=2.0,-19.584, 0.000, 0.917,1574.80,0.00,0.0000, 0.00,0.000,0.00,0.00,0.00, 0.00,9.00,0.00,0.00 point.6=2.0, 7.084, 0.000,-2.000,1574.80,0.00,0.0000, 0.00,0.000,0.00,0.00,0.00, 0.00,4.00,0.00,0.00 static_pitch=14.95 static_cg_height=5.0232 [Flaps.0] type=1 span-outboard=0.500000 extending-time=7.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=13.330818,0.000000 flaps-position.2=26.661636,0.000000 flaps-position.3=39.992454,0.000000 [GeneralEngineData] engine_type=0 Engine.0=7.250000,0.000000,0.000000 fuel_flow_scalar=0.9 [piston_engine] 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 cylinder_displacement=89.5 compression_ratio=8.000000 number_of_cylinders=6 max_rated_rpm=2400.000000 max_rated_hp=210.000000 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=0 max_design_mp=0.000000 min_design_mp=0.000000 critical_altitude=0.000000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 [propeller] propeller_type=0 propeller_diameter=7.583333 propeller_blades=2 propeller_moi=11.447476 beta_max=29.217391 beta_min=15.000000 min_gov_rpm=1400.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Reference Speeds] flaps_up_stall_speed=55.000000 full_flaps_stall_speed=44.000000 cruise_speed=90.00 [keyboard_response] elevator=100, 180 aileron=200, 1000 rudder=200, 1000 [Views] eyepoint=0.307579,-0.012816,1.973630 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.20, -18.97, 3.90, fx_navred light.1=3, 0.20, 18.97, 3.90, fx_navgre light.2=2, 0.17, -19.00, 3.90, fx_strobe light.3=2, 0.17, 19.00, 3.90, fx_strobe light.4=1, 0.00, 0.00, -2.51, fx_beacon light.5=1, 0.00, 0.00, 3.69, fx_beacon light.6=4, -2.27, 0.00, 1.40, fx_vclight [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 microsec