[fltsim.0] title=Great Lakes CV-440 sim=cv440 model= panel= sound= texture= kb_checklists=CV440_check kb_reference=CV440_ref ui_manufacturer=Convair ui_type=Convair 440 ui_variation=Great Lakes description=Notes: While the Convair Liner series was begun by American Air Lines, ordering the CV-240, United Air Lines was the prime mover behind the CV-340. The 340's fuselage was longer to seat 1 more row of passengers, and was owned by many major airlines. atc_heavy=0 atc_id=CFGLT atc_airline=Great Lakes atc_flight_number=374 prop_anim_ratio=0.9 [General] performance=Length: 79' Span 105'\nWeight: 47,000 lbs. max.\nPower: 2,400 h.p., R-2800-CB16 radials\nDetails: Convair CV-340\nDate: 3\/99\nRevised airframe by Dave McQueen\nOriginal and Mov Pts by Tom Gibson\nRadar nose by Frank Safranek atc_type=CONVAIR atc_model=None [WEIGHT_AND_BALANCE] ;load assumed symetrical versus CoG for the time being. reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=2 empty_weight=30400 ;including oil, catering etc. station_load.0=600,0,0,0 ;3 crew and bags station_load.1=5600,0,0,0 ;28 pax and bags max_gross_weight=47000 ;47000 - 1730 * 6 = 36620 and 36620 - 30400 = 6220 / 200 = 31 crew plus pax plus bags ;default ramp weight is 46,980lbs ;Moments of Inertia ; empty_weight_roll_MOI=710000 empty_weight_pitch_MOI=210000 empty_weight_yaw_MOI=830000 empty_weight_coupled_MOI=0.000000 [fuel] ;max fuel 865 USG in each outer wing. ;with max payload 600 USG in each wing ; LeftMain=0,-30,0,862.7,2.3 RightMain=0,30,0,862.7,2.3 fuel_type=1.000000 number_of_tank_selectors=1 [GeneralEngineData] engine_type=0 Engine.0=-6.0,-12.5,-1.0 Engine.1=-6.0,12.5,-1.0 fuel_flow_scalar=1.000000 [piston_engine] ; ;P&W R-2800-CB16=2400bhp for take off & 1800bhp at 8500 feet (low blower = METO) and 1700bhp at 14500 feet (high blower) ;FS2002 does not support ehp v eshp variation in supercharged piston engines leading to unavoidable inaccuracy ;this is being rectified as far as possible by variation of induced drag in lieu of thrust ; cylinder_displacement=155.78 compression_ratio=6.7 number_of_cylinders=18 max_rated_rpm=2800.000000 ;for take off only max_rated_hp=2400.000000 ;for take off only fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=59.5 min_design_mp=5.0 critical_altitude=7000 ; ;data below not really relevant emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 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] propeller_type=0 propeller_blades=3 gear_reduction_ratio=1.0 ;really 0.45 but set to 1.0 with smaller prop for same thrust propeller_diameter=8.8 ;really 13.4 and 8.8 required propeller_moi=26.8 ;estimated for the real prop beta_max=65.0 ;unknown so look up table given full range beta_min=15.0 ;uncertain so look up table given full range prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_reverse_available=1 min_rpm_for_feather=700.0 ;estimate beta_feather=96.0 power_absorbed_cf=0.9 ;estimate minimum_on_ground_beta=15.0 ;estimate minimum_reverse_beta=-26.0 defeathering_accumulators_available=0 prop_auto_feathering_available=1 ; ;data below non functional or FS required data min_gov_rpm=650.000000 prop_tc=0.010000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 [airplane_geometry] oswald_efficiency_factor=0.805 wing_area=920 wing_span=105.33 wing_root_chord=8.7 wing_dihedral=3.8 wing_incidence=4.0 wing_twist=0.0 htail_area=180.0 htail_span=37 htail_pos_lon=-38 htail_pos_vert=0.0 htail_incidence=0.0 htail_sweep=0.0 htail_area=200.0 vtail_area=110.0 vtail_span=19 vtail_sweep=0.0 vtail_pos_lon=-36 vtail_pos_vert=3 wing_winglets_flag=0 wing_sweep=0.0 wing_pos_apex_lon=0.0 wing_pos_apex_vert=0.0 elevator_area=72 aileron_area=43.82 rudder_area=36 elevator_up_limit=27.5 elevator_down_limit=20.0 aileron_up_limit=19.5 aileron_down_limit=15.0 rudder_limit=23.5 elevator_trim_limit=19.5 spoiler_limit=59.988681 ;for the landing lights - time set to 5 seconds spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [Flaps.0] type=1 span-outboard=0.3 extending-time=20.0 flaps-position.0=0,0 flaps-position.1=11,174 flaps-position.2=17,174 flaps-position.3=28,156 flaps-position.4=40,148 lift_scalar=0.9 drag_scalar=0.1 pitch_scalar=0.5 [Flaps.1] type=1 span-outboard=0.6 extending-time=20.0 system_type=0 flaps-position.0=0,0 flaps-position.1=0,174 flaps-position.2=5,174 flaps-position.3=28,156 flaps-position.4=40,148 lift_scalar=0.1 drag_scalar=0.9 pitch_scalar=0.5 [contact_points] static_pitch=0.0 static_cg_height=8.5 ;gear strength set to about double real world to safeguard use from taxiways with no smoothing polygon point.0=1,24.0,0.0000,-8.65,1200,0,0.83,63.0,0.10,2.5,1.00,6.5,9.5,0,174,174 point.1=1,-0.5,-12.66,-8.70,1500,1,0.83,0.00,0.39,2.5,0.66,6.0,9.0,2,174,174 point.2=1,-0.5,12.66 ,-8.70,1500,2,0.83,0.00,0.39,2.5,0.66,6.0,9.0,3,174,174 point.3=2,-2.83,-54,1.83,500,0.0,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2,-2.83,54 ,1.83,500,0.000000,0.000000,0,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2,-33.0,0.0,-1.5,500,0.0,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2,28.4,0.00,-1.5,500,0.000000,0,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.7= 5, -30.90, -5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 3.0, 3.2, 0, 0.0, 0.0 point.8= 5, -30.90, 5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 3.1, 3.5, 0, 0.0, 0.0 [autopilot] autopilot_available=1 use_no_default_bank=1 use_no_default_pitch=1 flight_director_available=0 default_vertical_speed=100 ;default is zero IRL - 100 is closest available value in FS2002 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=0.000000 pitch_takeoff_ga=8.000000 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [direction_indicators] direction_indicator.0=1,0 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [Reference Speeds] ;all KIAS - Pitot error not known so IAS set=CAS flaps_up_stall_speed=105 full_flaps_stall_speed=85 cruise_speed=195 [Views] eyepoint= 22.24, -2.115, 3.816 [exits] number_of_exits=1 exit_rate.0=0.1 [TailHook] tailhook_length=4 ;(feet) tailhook_position = -15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust = 1.0 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -3.45, -52.65, 2.2, fx_navred , light.1=3, -3.45, 52.65, 2.2, fx_navgre , light.2=3, -47.6, 0.00, 1.77, fx_navwhi , light.3=1, -38.6, 0.00, 19.9, fx_beacon , light.4=4, 24, -2.50, 2.0, fx_vclight , light.4=4, 24, -2.50, 3.0, fx_vclight , light.5=4, 23.5, -2.50, 1.0, fx_vclight , light.6=4, 23.5, 2.5, 1.0, fx_vclight , light.7=4, 24, 2.50, 2.0, fx_vclight , light.8=4, 23, 2.50, 3.5, fx_vclight , light.9=4, 17.00, -2.0, 1.5, fx_vclight , [SMOKESYSTEM] smoke.0=0.2, -4.67, 12.33, fx_smoke_rx smoke.1=0.2, -4.67, -12.33, fx_smoke_rx [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=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 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