;***************************************************** ;Boeing (Stearman) PT-17 Kaydet FDE for FS2002 only ;***************************************************** [fltsim.0] JABIndex=1 title=Stearman sim=Stearman Kaydet model= panel= sound= texture= kb_checklists=stearman_check kb_reference=PT17_ref ui_manufacturer=Stearman ui_type=PT-17 Kaydet ui_variation=Fuerza Aerea Mexicana EMA description=The Stearman prototype (Model 70) designed by Harold Zipp and Jack Clark first appeared in 1933. \n\nThis model depicts a PT-17 with a yellow fuselage and sky blue on wings tips and fuselage sides. This is the typical paint scheme of the Military Air College of the Mexican Air Force. This plane was in service until 1995. [GeneralEngineData] engine_type=0 Engine.0=5.000000,0.000000,0.000000 fuel_flow_scalar=1.10000 ;R-670 SFC about 0.54 [piston_engine] 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 cylinder_displacement=95.4300000 compression_ratio=5.4000000 number_of_cylinders=7 max_rated_rpm=2075.000000 max_rated_hp=220.000000 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=1 turbocharged=0 max_design_mp=0.000000 min_design_mp=0.000000 critical_altitude=0.000000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 ;*************************** ;Jacobs powered PT-18 option ;*************************** ; ;You can turn your 220hp PT-17 into a PT-18 with 225hp Jacobs engine ;by removing the semi colon in front of the power scalar below ; ;power scalar=1.0227 ; ;*************************** [propeller] propeller_type=1 propeller_diameter=9 ;really 102 inches propeller_blades=2 propeller_moi=5 beta_max=15 beta_min=15 min_gov_rpm=1000 prop_tc=0.1 gear_reduction_ratio=1 fixed_pitch_beta=15 ;your engine fitter has adjusted your prop for best climb ;change the value to 25 to get a "cruise prop" low_speed_theory_limit=80 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [fuel] ;43 US gallons of modern unleaded AVGAS is about 258lbs ;the leaded fuel used during WW2 was 7% denser ;to load WW2 fuel change 43 below to 46 LeftMain=0.000000,0.000000,0.000000,43.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 [WEIGHT_AND_BALANCE] reference_datum_position=0,0,0 empty_weight_CG_position=0,0,0 max_number_of_stations=4 station_load.0=200,0,0,0 ;trainee station_load.1=200,0,0,0 ;instructor - set this to 0,0,0,0 to fly solo station_load.2=40,0,0,0 ;oil empty_weight=1936 ;default ramp weight with 258lbs of fuel=2,634lbs cf 2,717lbs max authorised empty_weight_roll_MOI=1825.000000 empty_weight_pitch_MOI=3000.000000 empty_weight_yaw_MOI=3800.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight= 2634.000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=-3.4, 0.0, 2.6 [SMOKESYSTEM] smoke.0= -20.00, +7.70, 0.00, fx_smoke_w [autopilot] autopilot_available=0 ;no trim so no autopilot in FS2002 flight_director_available=0 default_vertical_speed=000.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0 [Reference Speeds] flaps_up_stall_speed=40.000000 KIAS at 2500lbs full_flaps_stall_speed=40.000000 cruise_speed=90 KIAS at low level [airplane_geometry] wing_area=297 wing_span=45.25 ;required to fool MSFS2002 which does not have true biplane code wing_root_chord=4.583333 wing_dihedral=1 wing_incidence=0.000000 wing_twist=0.000000 oswald_efficiency_factor=0.62 ;estimated wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 ;all data below bogus and being taken from air file instead htail_area=20.000000 htail_span=9.000000 htail_pos_lon=-12.500000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=12.000000 vtail_span=3.949684 vtail_sweep=0.000000 vtail_pos_lon=-12.500000 vtail_pos_vert=1.500000 elevator_area=8.600000 aileron_area=8.900000 rudder_area=4.200000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=20 spoiler_limit=0 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] ;real life u/c strength nearer 600/800/800 than 1200/1500/1500 ;change only if you have substantial tailwheel experience ; point.0=1,-16.666667,0 ,-1.755 ,1200,0.0 ,0.52, 1,0.7,2.5,0.59,0,0,0,0,0 point.1=1,2.25 ,-3.166667,-5.7 ,1500,1.0 ,0.52, 0,0.5,2.5,0.63,0,0,2,0,0 point.2=1,2.25 , 3.166667,-5.7 ,1500,2.0 ,0.52, 0,0.5,2.5,0.63,0,0,3,0,0 point.3=2,0.5 ,-21 ,-0.166667,1574,0 ,0,0,0,0,0,0,0,5,0,0 point.4=2,0.5 , 21 ,-0.166667,1574,0 ,0,0,0,0,0,0,0,6,0,0 point.5=2,-16.66667 ,0 ,-1.755 ,1574,0 ,0,0,0,0,0,0,0,9,0,0 point.6=2,8.166667 ,0 ,-0.583333,1574,0 ,0,0,0,0,0,0,0,4,0,0 static_pitch=11.3 static_cg_height=4.9 [General] performance=220hp Continental R-670-5 with a\/p prop.\nRated at 2075 rpm at sea level. 124 mph.\nClimb at full throttle and 70 mph.\nCruise at 1825-1850 rpm to yield.\n106 mph (TAS) burning 80lbs\/hr..\nRange with no reserves 340 miles.\n4.75 hours endurance at low speed.\nService ceiling 11,200\nFor greater detail press F10 in flight.\n\n atc_type=BOEING atc_model=ST75