;*****************************************************
;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