// cessna l-19e (o-1e)designed by massimo taccoli //fd files ver 1.2 by dennis seeley, 28 jan 04 [fltsim.0] title=GA-AI cessna l-19e canadian army sim=l-19e model= panel= sound= sound= texture=can kb_checklists= kb_reference=l-19e_ref ui_manufacturer=cessna ui_type=l-19e bird dog ui_variation=canadian army atc_id_enable=1 atc_1d_color=0x00000000 atc_id=724 atc_parking_types=ramp visual_damage=0 description=cessna's model 305 was developed from the model 170 as a private venture which, in 1950, was chosen as the new standard liason and observation aircraft for the us army, which named it the l-19.the us military designation was changed to o-1 in 1962. the canadian army bought 16 l-19as in 1953 and 9 l-19es in 1957 for use by artillery observers. this fs aircraft represents an o-1e (cessna model 305c) in canadian army markings. atc_id_color=000000 [fltsim.1] title=GA-AI cessna l-19e rok marine corps sim=l-19e model= panel= sound= texture=rokaf kb_checklists= kb_reference=l-19e_ref ui_manufacturer=cessna ui_type=l-19e bird dog ui_variation=republic of korea marine corps. atc_id_enable=1 atc_1d_color=0x00000000 atc_id=650 atc_parking_types=ramp description=cessna's model 305 was developed from the model 170 as a private venture which, in 1950, was chosen as the new standard liason and observation aircraft for the us army, which named it the l-19.the us military designation was changed to o-1 in 1962. this fs aircraft represents an l-19e (cessna model 305c) used by the republic of korea marine corps in 1969. [general] performance=length: 25 ft 10 in.\nheight: 7 ft 4 in.\nwing span: 36 ft 0 in.\nwing area: 174 sq ft.\nengine: continental o-470-11 6-cyl air-cooled.\nmilitary power: 213 hp at 2,600 rpm at sea level.\nnormal power: 190 hp at 2,300 rpm.\nprop: mccauley 90 in fixed pitch.\nempty weight: 1,614 lb.\nmto weight: 2,400 lb.\nmax speed: 145 mph at sea level.\nmax cruise speed: 117 mph at 10,000 ft.\nstall speed (full flaps): 54 mph ias.\ninitial climb rate: 1,230 fpm at sea level.\nservice ceiling: 18,500 ft.\nrange (max cruise): 491 mi.\nfuel consumption (max cruise): 7.8 gph. atc_type=cessna atc_model=l-19e editable=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 [weight_and_balance] max_gross_weight = 2400 empty_weight = 1614 reference_datum_position = 0.39, 0, 3.4 empty_weight_cg_position = 0.107, 0, -2.9 empty_weight_pitch_moi = 1577.4 empty_weight_roll_moi = 1141.2 empty_weight_yaw_moi = 2217.4 empty_weight_coupled_moi = 0 max_number_of_stations = 2 station_load.0 = 170.0, 0.107, 0.0, -3.5, pilot station_load.1 = 0.0, -3.000, 0.0, -3.5, passenger [lights] //types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -0.69, -19.05, 0.50, fx_navred light.1 = 3, -0.70, 19.00, 0.5, fx_navgre light.2 = 2, -1.00, -19.00, 0.5, fx_strobe light.3 = 2, -1.00, 19.00, 0.5, fx_strobe light.4 = 1, -8.7, 0, -1.9, fx_beacon light.5 = 4, 1.25, -0.84, -2.53, fx_vclight light.6 = 4, 1.25, 0.84, -2.53, fx_vclight [generalenginedata] //0=piston, 1=jet, 2=none, 3=helo-turbine, 4=rocket, 5=turboprop engine_type = 0 fuel_flow_scalar = 0.942 engine.0 = 6.67, 0.0, -2.9 min_throttle_limit=0.000000 [smokesystem] smoke.0 = 3.1, -0.9, -5.8, fx_engsmoke smoke.1 = 3.1, 0.9, -5.8, fx_engsmoke [effects] dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 [fuel] //longitudinal (feet), lateral (feet), vertical (feet), usable(gallons), unusable (gallons) fuel_type = 1 number_of_tank_selectors = 1 leftmain = 0.107, -2.1, 0, 22, 3 rightmain = 0.107, 2.1, 0, 22, 3 electric_pump=1 [contact_points] static_pitch = 10.1 static_cg_height = 4.75 max_number_of_points = 8 point.0 = 1,-19.20, 0.00, -5.10, 1501, 0, 0.25,30.0,0.28,2.5,0.85,0.0,0.0,0 point.1 = 1, 1.58, -3.90, -8.80, 1574, 1, 0.85, 0.0,0.33,2.5,0.85,0.0,0.0,2 point.2 = 1, 1.58, 3.90, -8.80, 1574, 2, 0.85, 0.0,0.33,2.5,0.85,0.0,0.0,3 point.3 = 2, -0.91,-18.92, 0.40, 1574, 0, 0.00, 0.0,0.00,0.0,0.00,0.0,0.0,5 point.4 = 2, -0.91, 18.92, 0.40, 1574, 0, 0.00, 0.0,0.00,0.0,0.00,0.0,0.0,6 point.5 = 2,-20.30, 0.00, -2.00, 1574, 0, 0.00, 0.0,0.00,0.0,0.00,0.0,0.0,9 point.6 = 2, 6.20, 0.00, -4.70, 1574, 0, 0.00, 0.0,0.00,0.0,0.00,0.0,0.0,4 point.7 = 2,-17.80, 0.00, 1.80, 1574, 0, 0.00, 0.0,0.00,0.0,0.00,0.0,0.0,9 [keyboard_response] elevator = 100.0, 180.0 aileron = 100.0, 180.0 rudder = 100.0, 180.0 [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 = 1500 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5.0 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 350 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 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] wing_area = 174.0 wing_span = 36.0 wing_root_chord = 5.33 wing_dihedral = 2.13 wing_incidence = 1.5 wing_twist = -3.0 oswald_efficiency_factor = 0.75 wing_winglets_flag = 0 wing_sweep = 0.0 wing_pos_apex_lon = 1.3325 wing_pos_apex_vert = 0.0 htail_area = 35.28 htail_span = 10.54 htail_pos_lon = -16.67 htail_pos_vert = -2.75 htail_incidence = 0.0 htail_sweep = 20.0 vtail_area = 19.4 vtail_span = 4.0 vtail_sweep = 33.0 vtail_pos_lon = -16.5 vtail_pos_vert = -2.33 elevator_area = 15.0 aileron_area = 16.74 rudder_area = 9.58 elevator_up_limit = 26.0 elevator_down_limit = 20.0 aileron_up_limit = 20.0 aileron_down_limit = 14.0 rudder_limit = 16.0 elevator_trim_limit = 24.0 spoiler_limit = 0.0 aileron_to_spoileron_gain = 0.0 min_ailerons_for_spoilerons = 0.0 min_flaps_for_spoilerons = 0.0 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 24 max_generator_alternator_amps = 50 electric_always_available = 0 flap_motor = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 10, 17 marker_beacon = 1, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 light_nav = 0, 3, 17 light_beacon = 0, 3, 17 light_landing = 0, 3, 17 light_taxi = 0, 3, 17 light_strobe = 0, 3, 17 light_panel = 0, 3, 17 [brakes] toe_brakes_scale=0.35 parking_brake=1 differential_braking_scale=1.0 [views] eyepoint=-0.75, 0.0, -1.5 [flaps.0] type=1 span-outboard=0.41 extending-time=3.0 system_type=0 damaging-speed= 87.0 blowout-speed =120.0 lift_scalar =1.0 drag_scalar =1.0 pitch_scalar=1.0 flaps-position.0= 0.0,0.0 flaps-position.1=30.0,0.0 flaps-position.2=45.0,0.0 flaps-position.3=60.0,0.0 [piston_engine] cylinder_displacement=78.5 compression_ratio=7.0 number_of_cylinders=6 max_rated_rpm=2600.0 max_rated_hp=213.0 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.3 turbocharged=0 max_design_mp=0.0 min_design_mp=0.0 critical_altitude=0.0 emergency_boost_type=0 emergency_boost_mp_offset=0.0 emergency_boost_gain_offset=0.0 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.0 idle_rpm_mechanical_efficiency_scalar=1.0 max_rpm_friction_scalar=1.0 idle_rpm_friction_scalar=1.0 [propeller] propeller_type=1 propeller_diameter=7.5 propeller_blades=2 propeller_moi=6.0 beta_max=0.0 beta_min=0.0 min_gov_rpm=1400.0 prop_tc=0.1 gear_reduction_ratio=1.0 fixed_pitch_beta=45.4 low_speed_theory_limit=80.0 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.0 beta_feather=0.0 power_absorbed_cf=0.0 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.0 minimum_reverse_beta=0.0 thrust_scalar=1.0 [radios] audio.1=1 com.1=1, 1 com.2=1, 1 nav.1=1, 0, 1 nav.2=1, 0, 1 adf.1=1 transponder.1=1 marker.1=1 [hydraulic_system] electric_pumps=0 engine_map=0,0,0,0 normal_pressure=0.0 [exits] number_of_exits = 2 exit_rate.0 = 0.4 [direction_indicators] direction_indicator.0=1,0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [stall_warning] type=1 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 autothrottle_available=0 autothrottle_arming_required=0 max_throttle_rate=0.1 autothrottle_takeoff_ga=0 autothrottle_max_rpm=99.0 default_pitch_mode=0 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 default_bank_mode=0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.0 nav_proportional_control=9.0 nav_integrator_control=0.25 nav_derivative_control=0.0 nav_integrator_boundary=2.5 nav_derivative_boundary=0.0 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.0 gs_integrator_boundary=0.70 gs_derivative_boundary=0.0 yaw_damper_gain=0.0 [reference speeds] flaps_up_stall_speed=55.0 full_flaps_stall_speed=44.0 cruise_speed=125.0 max_indicated_speed =165.0