[fltsim.0] title=Lockheed Model 14-WF62 Super Electra, G-AFGN sim=L14-WF62 model=WF62 panel= sound=cw texture=G-AFGN checklists=L14-WF62_check description=Lockheed Model 14-WF62 was the export configuration of the Model 14. This particular aircraft, G-AFGN was used to transport Prime Minister Sir Neville Chamberlain to Munich for his conference with Adolf Hitler in September 1938.\n\n ui_manufacturer=Lockheed ui_type=Model 14 ui_variation=WF62 - Performance Testing atc_heavy=0 atc_id=G-AFGN atc_airline=British Airways Ltd. atc_flight_number= [General] performance=Max Spd 250 mph @ 5,000 ft\nCrs Spd 215 mph @ 5,800 ft\nMax End 10 hrs\nSrvc Clng 24,500 ft\nMax GWT 17,500 lb\nEmpty Wt 10,750 lbs\nUsfl Ld 6,850 lb\nWng Area 551 sq ft\nWng Ldng 31.8 lbs\/sq ft\nPwr Ldng 9.7 lbs\/hp\nFuel Cap 644 gal\nOil Cap. 60 gal\nCrew 2 Passengers 14\nEngine Wright Cyclone SGR-1820-F62 900 HP Max TO, 750 HP at 6700 Ft \nModel Design Dave Carroll\n\n atc_type=LOCKHEED atc_model=L14 [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 1.500, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, 4.200, -1.200, 0.000 empty_weight= 10750.000 empty_weight_roll_MOI= 31780.000 empty_weight_pitch_MOI= 55297.000 empty_weight_yaw_MOI= 101209.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 17500.000 CG_forward_limit= 1.500 CG_aft_limit= 1.000 station_load.1= 170.000, 4.200, 1.200, 0.000 station_load.2= 170.000, 0.600, -1.200, 0.000 station_load.3= 170.000, 0.600, 1.200, 0.000 station_load.4= 170.000, -2.000, -1.200, 0.000 station_load.5= 170.000, -2.000, 1.200, 0.000 station_load.6= 170.000, -4.000, -1.200, 0.000 station_load.7= 170.000, -4.000, 1.200, 0.000 station_load.8= 170.000, -6.000, -1.200, 0.000 station_load.9= 170.000, -6.000, 1.200, 0.000 station_load.10= 170.000, -8.000, -1.200, 0.000 station_load.11= 170.000, -8.000, 1.200, 0.000 station_load.12= 170.000, -10.000, -1.200, 0.000 station_load.13= 170.000, -10.000, 1.200, 0.000 station_load.14= 170.000, -12.000, -1.200, 0.000 station_load.15= 170.000, -12.000, 1.200, 0.000 station_load.16= 300.000, -0.500, 0.000, 0.000 [fuel] fuel_type=1.000000 number_of_tank_selectors=1 LeftMain= -2.210, -4.940, 0.000, 182.000, 10.000 LeftAux= 1.480, -4.940, 0.000, 140.000, 10.000 RightMain= -2.210, 4.940, 0.000, 182.000, 10.000 RightAux= 1.480, 4.940, 0.000, 140.000, 10.000 [airplane_geometry] wing_area= 551.000 wing_span= 65.500 wing_root_chord= 8.400 wing_dihedral= 5.208 wing_incidence= 0.000 wing_twist= 1.000 oswald_efficiency_factor= 0.690 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 2.600 wing_pos_apex_vert= 0.000 htail_area= 130.000 htail_span= 25.917 htail_pos_lon= -23.300 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 58.000 vtail_span= 17.400 vtail_sweep= 0.000 vtail_pos_lon= -24.600 vtail_pos_vert= 2.700 elevator_area= 42.508 aileron_area= 35.400 rudder_area= 25.892 elevator_up_limit= 28.000 elevator_down_limit= 22.999 aileron_up_limit= 26.001 aileron_down_limit= 18.999 rudder_limit= 25.783 elevator_trim_limit= 19.996 spoiler_limit= 90.000 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, -26.583, 0.000, 0.250, 1181.102, 0.000, 0.682, 49.140, 0.050, 2.500, 0.712, 5.000, 5.000, 0.000, 0.000, 0.000 point.1= 1.000, 2.167, -7.667, -6.500, 1574.803, 1.000, 1.578, 0.000, 0.415, 2.500, 1.321, 8.000, 8.000, 2.000, 0.000, 0.000 point.2= 1.000, 2.167, 7.667, -6.500, 1574.803, 2.000, 1.578, 0.000, 0.415, 2.500, 1.321, 10.000, 10.000, 3.000, 0.000, 0.000 point.3= 2.000, -1.000, -32.833, 2.917, 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, -1.000, 32.833, 2.917, 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, -27.477, 0.000, 3.099, 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, 9.667, 0.000, -5.000, 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= 13.211 static_cg_height= 5.700 [GeneralEngineData] engine_type= 0 Engine.0= 9.667, -7.667, 0.000 Engine.1= 9.667, 7.667, 0.000 fuel_flow_scalar= 0.620 [piston_engine] cylinder_displacement= 202.222 compression_ratio= 6.700 number_of_cylinders= 9 max_rated_rpm= 2700.000 max_rated_hp= 900.000 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 0.600 turbocharged= 1 max_design_mp= 42.000 min_design_mp= 1.000 critical_altitude= 27000.000 emergency_boost_type= 0 emergency_boost_mp_offset= 4.000 emergency_boost_gain_offset= 0.401 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 power_scalar=1.000 [propeller] propeller_type= 0 propeller_diameter= 13.000 propeller_blades= 3 propeller_moi= 86.500 beta_max= 65.000 beta_min= 18.500 min_gov_rpm= 1100.000 prop_tc= 0.010 gear_reduction_ratio= 2.000 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 thrust_scalar=1.000 [Reference Speeds] flaps_up_stall_speed= 82.000 full_flaps_stall_speed= 48.000 cruise_speed= 187.000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=4.148000,-1.027000,4.152000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=900.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 10.000 system_type= 0 damaging-speed= 180.000 blowout-speed= 220.000 lift_scalar= 1.000 drag_scalar= 2.000 pitch_scalar= 0.200 flaps-position.0= 0.000, 0.000 flaps-position.1= 15.000, 0.000 flaps-position.2= 30.000, 0.000