[fltsim.0]
title=Fairchild PT26 RCAF
sim=Fairchild PT26
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=Fairchild Aircraft Co.
ui_type=Cornell PT-26
ui_variation=Royal Canadian Air Force
visual_damage=0
description=Fairchild PT-26 - covered cockpit version of PT-19 primary school plane for WWII pilots.\nIn production between 1938/1956.\nManufacturing in Canada by Fleet Acft. of Canada, Brazil and Chile.\nEngine Ranger L-440 175 hp\nCruise speed 100 mph
atc_heavy=0
atc_id=5360
atc_airline=R.C.A.F.
atc_flight_number=
[General]
atc_type=FAIRCHILD AIRCRAFT
atc_model=PT-26
editable=1
performance=Maximum Speed\n128 mph 111 kts\t205 km\/hr\n\nEngine\n175-hp Ranger L-440\n\nPropeller\nWood\n\nMaximum Range\n372 mi 690 km\n\nService Ceiling\n16,000 ft\t5,300 m\n\nFuel Capacity\n45 gal\t169 L\n\nEmpty Weight\n1,845 lb\t662.25 kg\n\nMaximum Gross Weight\n2,545 lb\t871 kg\n\nLength\n27 ft, 8 in \t8.4 m\n\nWingspan\n35 ft, 1 in\t11.8 m\n\nHeight\n10 ft, 6 in\t3.25 m\n\nSeating\n2\n\nUseful Load\n700 lb\t317 kg
[WEIGHT_AND_BALANCE]
max_gross_weight = 2945.000
empty_weight = 1945.000
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.200, 0.000, 0.000
max_number_of_stations = 50
station_load.0 =170.000000, -1.800000, 0.000000, 0.000000, Pilot
station_load.1 =0.000000, 0.000000, 0.000000, 0.000000, Passenger
;Moments of Inertia
empty_weight_pitch_MOI = 1550.000
empty_weight_roll_MOI = 1130.000
empty_weight_yaw_MOI = 2330.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
hi_alpha_on_roll = 0.300
hi_alpha_on_yaw = 0.300
p_factor_on_yaw = 0.800
torque_on_roll = 0.0
gyro_precession_on_yaw = 0.300
gyro_precession_on_pitch= 0.400
[GeneralEngineData]
engine_type = 0
Engine.0 = 4.000, 0.000, 0.000
fuel_flow_scalar= 1.000
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
starter_type = 1 //1=Manual Starter
[piston_engine]
power_scalar =1.000
cylinder_displacement= 74.000
compression_ratio= 6.500
number_of_cylinders= 6
number_of_magnetos = 2 //Number of magnetos
max_rated_rpm= 2450.000
max_rated_hp= 175.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
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
[propeller]
thrust_scalar =1.000
propeller_type= 1
propeller_diameter= 6.780
propeller_blades= 2
propeller_moi= 5.000
beta_max= 0.000
beta_min= 0.000
min_gov_rpm= 0.000
prop_tc= 0.000
gear_reduction_ratio= 1.000
fixed_pitch_beta= 22.000
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= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
//0 Class
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
[contact_points]
point.0= 1.000, -16.500, 0.000, -0.980, 3500.000, 0.000, 0.400, 180.000, 0.300, 0.800, 0.600, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 1.700, -4.900, -5.570, 2600.000, 1.000, 1.100, 0.000, 0.500, 1.800, 0.600, 0.000, 0.000, 0.000, 0.000, 0.000
point.2= 1.000, 1.700, 4.900, -5.570, 2600.000, 2.000, 1.100, 0.000, 0.500, 1.800, 0.600, 0.000, 0.000, 0.000, 0.000, 0.000
point.3= 2.000, 0.000, -16.600, 2.100, 800.000, 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, 0.000, 16.600, 2.100, 800.000, 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, -18.000, 0.000, 1.000, 800.000, 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, 8.000, 0.000, -0.200, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 14.350
static_cg_height = 4.600
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.85 //Brake scalar
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint = -0.2, 0.0, 2.9
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, 2.0, 0.00, 2.0, fx_vclight,
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 0
Com.1 = 1, 0
Nav.1 = 0, 0, 0
Adf.1 = 0
Transponder.1 = 0
Marker.1 = 0
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator =200, 500
aileron =200, 500
rudder =200, 500
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=0,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 0
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=0,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
touchdown=fx_tchdwn_s, 1
concrete=fx_sparks
startup=fx_engstrt_jenny
windshield_rain_effect_available = 0 //Do not draw rain on this windshield
[electrical]
max_battery_voltage = 0
generator_alternator_voltage = 0
[fuel]
LeftMain = -0.970, -1.800, -0.060, 22.500, 0.000
RightMain= -0.970, 1.800, -0.060, 22.500, 0.000
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 180.600
wing_span = 35.020
wing_root_chord = 6.200
wing_dihedral = 8.300
wing_incidence = 0.900
wing_twist = 0.890
oswald_efficiency_factor= 0.900
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 0.000
wing_pos_apex_vert = 0.000
htail_area = 52.000
htail_span = 12.250
htail_pos_lon = -17.750
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 73.500
vtail_span = 8.620
vtail_sweep = 0.000
vtail_pos_lon = -14.650
vtail_pos_vert = 1.750
elevator_area = 18.760
aileron_area = 10.800
rudder_area = 17.200
elevator_up_limit = 28.000
elevator_down_limit = 25.000
aileron_up_limit = 20.000
aileron_down_limit = 15.000
rudder_limit = 28.000
elevator_trim_limit = 18.000
spoiler_limit = 0.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 49.000
full_flaps_stall_speed = 39.000
cruise_speed = 90.000
max_indicated_speed = 150.0 //Red line (KIAS)
[autopilot]
autopilot_available= 0
flight_director_available= 0
[forcefeedback]
ground_bumps_magnitude1=1600 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
crash_magnitude1=8000 ; 0 - 10000
crash_direction1=01000 ; 0 - 35999 degrees
crash_magnitude2=8000 ; 0 - 10000
crash_direction2=9000 ; 0 - 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=350000 ; in microseconds
[stall_warning]
type=0
[exits]
number_of_exits = 2
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 1.000
system_type= 3
damaging-speed= 150.000
blowout-speed= 180.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 40.000, 0.000
