[fltsim.0] title=Cessna O-2A US Army sim=CessnaO2aUSArmy model= panel= sound= texture= checklists= description=Cessna O-2A, US army, registration 11150.\n\n ui_manufacturer=Cessna ui_type=O-2A Super Skymaster ui_variation=US Army atc_heavy=0 atc_id=11150 atc_airline=ARMY atc_flight_number=150 [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: June 2002, \nVersion FS2002.0 (AP 2.0a2)\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=0.000, 0.000, 0.000, 0.000 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