[fltsim.0] title=ET-29C FAA 1965 sim=cv240 model=bn panel= sound= texture=faa-02 checklists=CV240_check kb_reference=CV240_ref ui_manufacturer=Convair ui_type=ET-29C ui_variation=FAA 1965-2 description=The Convair ET-29C with the registration N246 was one of 85 aircrafts T-29C built in 1952. 10 of these Convairs were converted for MATS Air Force Communications Service AFCS as AT-29C for military flight inspection. According to the rules of the unique designation system for military aircraft all AT-29C were redesignated to ET-29C in 1962. N246 was transferred from U.S. Air Force to FAA in 1962 and reallocated to the U.S. Air Force in 1969. Unfortunately more whereabouts are unknown. atc_heavy=0 atc_id=N248 atc_airline=FAA atc_flight_number=245 prop_anim_ratio=0.9 [General] performance=Two P&W R-2800-CA18\neach 2400hp for take off\n1800hp METO to 6000feet\n1675hp to 13,500 feet\n1100hp normal cruise at FL160 atc_type=CONVAIR atc_model=None [WEIGHT_AND_BALANCE] ;load assumed symetrical versus CoG ;Late production CV-240 (therefore long range version) ;To simulate early delivers to e.g. AAL reduce the fuel to 500 USG per side and increase pax to 40 making station load.1=8000 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=27700 ;including oil, catering etc. station_load.0=600,0,0,0 ;3 crew and bags station_load.1=4800,0,0,0 ;24 pax and bags max_gross_weight=42400 ;final certification of long range variant ;MLW=39800 ;42400 - 1550 * 6=33100 and 33100 - 27700 = 5400 / 200 = 27 crew plus pax plus bags ;default ramp weight is 42,400lbs with max fuel and weight limited payload ;Moments of Inertia ; empty_weight_roll_MOI=505000 empty_weight_pitch_MOI=175000 empty_weight_yaw_MOI=635000 empty_weight_coupled_MOI=0.000000 [fuel] ;max fuel 775 USG in each outer wing (many only had 500) ; LeftMain=0,-20,0,772.7,2.3 RightMain=0,20,0,772.7,2.3 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=0.97 [piston_engine] ; ;P&W R-2800-CA18=2400bhp for take off & 1800bhp at 6000 feet (low blower = METO) and 1675bhp at 13500 feet (high blower) ; ;-CA18 has same take off power as -CB16 at lower MAP but less rated power at lower rated and critical altitudes ; 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=56.5 min_design_mp=5.0 critical_altitude=4700 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 propeller_diameter=8.8 propeller_moi=26.8 beta_max=65.0 beta_min=15.0 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_reverse_available=1 min_rpm_for_feather=700.0 beta_feather=96.0 power_absorbed_cf=0.9 minimum_on_ground_beta=15.0 minimum_reverse_beta=-26.0 defeathering_accumulators_available=0 prop_auto_feathering_available=1 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=817 wing_span=91.75 wing_root_chord=8.9 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 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, 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=180 [Views] eyepoint=21.047, -2.077, 3.845 [exits] number_of_exits=1 exit_rate.0=0.1 [Radios] Audio.1=1 Com.1=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [LIGHTS] light.0=3, -3.45, -45.9, 1.5, fx_navred , light.1=3, -3.45, 45.9, 1.5, fx_navgre , light.2=3, -45.3, 0.00, 1.37, fx_navwhi , light.3=1, -35.2, 0.00, 20.4, fx_beacon , light.4=4, 22, -2.50, 2.0, fx_vclight , light.4=4, 22, -2.50, 3.0, fx_vclight , light.5=4, 21.5, -2.50, 1.0, fx_vclight , light.6=4, 21.5, 2.5, 1.0, fx_vclight , light.7=4, 22, 2.50, 2.0, fx_vclight , light.8=4, 21, 2.50, 3.5, fx_vclight , light.9=4, 16.50, 2.50, -0.5, fx_vclight , [SMOKESYSTEM] smoke.0=0.2, -4.67, 12.33, fx_smoke_w smoke.1=0.2, -4.67, -12.33, fx_smoke_w [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