;***************************************************** ;Boeing (Stearman) PT-17 Kaydet FDE for FS2002 only ;***************************************************** [fltsim.0] JABIndex=1 title=Stearman Jet Age Colours sim=stearman kaydet model= panel= sound= texture= kb_checklists=stearman2_check kb_reference=PT17_ref atc_id=GJETAGE ui_manufacturer=Stearman ui_type=Stearman - Civilian ui_variation=Civilian colors description=While most post war surplus Stearmans ended at crop dusters, many found new homes as airshow performers. Turn on the smoke (I key) and let her fly! atc_heavy=0 atc_airline= atc_flight_number= [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=125.4300000 compression_ratio=5.4000000 number_of_cylinders=7 max_rated_rpm=2100.000000 max_rated_hp=225.000000 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 [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=800 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=2950.000 [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_b [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