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