[fltsim.0]
title=PC9_AI RAFO-Royal Air Force Oman
sim=PC9_AI
model=
panel=
sound=
texture=RAFO-Royal Air Force Oman
checklists=
atc_airline=MAJAN
atc_parking_types=MIL_COMBAT
atc_parking_codes=PC9,M003
description=The Pilatus PC9\/A as used by the Royal Australian Air Force's\n"Rouletts" Aerobatic\/Display team based at RAAF East Sale.
ui_manufacturer =Pilatus
ui_type =Pc-9/A
ui_variation =Royal Air Force Oman
[General]
atc_type=PILATUS
atc_model=PC9
performance=Max Level Speed : 300 kts \/\/ 345 mph\nInitial Rate of Climb: 4,050 ft\/min\nRange : 955 nautical miles with 5% reserve\nWeights : Empty: 3,715lb Max T\/O: 7,055 lb.\nPowerplant: 1x P&WC PT6A-62 Turboprop of 950 SHP (Flat Rated).\n\n \n \n \n \n \n \n
[SMOKESYSTEM]
smoke.0=-0.52, -10.02, 3.09, fx_smoke_w
smoke.1=-0.52, -12.02, 3.09, fx_smoke_w
smoke.2=-0.52, -14.02, 3.09, fx_smoke_w
[WEIGHT_AND_BALANCE]
max_gross_weight = 7055.000
empty_weight = 3607.000
reference_datum_position = 16.200, 0.000, 0.000
empty_weight_CG_position = -16.000, 0.000, 0.000
max_number_of_stations = 50
station_load.0 = 170.000, -16.000, -1.500, 0.000
;Moments of Inertia
empty_weight_pitch_MOI = 4524.000
empty_weight_roll_MOI = 2477.000
empty_weight_yaw_MOI = 6121.000
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 =0.450
induced_drag_scalar =1.200
elevator_effectiveness =1.000
aileron_effectiveness =2.000
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
[GeneralEngineData]
engine_type = 5
Engine.0 = -2.400, 0.000, 0.000
fuel_flow_scalar = 1.120
min_throttle_limit=-0.250000
max_contrail_temperature=-27
[propeller]
thrust_scalar =1.200
propeller_type = 0
propeller_diameter = 8.500
propeller_blades = 4
propeller_moi = 19.000
beta_max = 40.000
beta_min = 5.000
min_gov_rpm = 25520.000
prop_tc = 0.004
gear_reduction_ratio = 17.400
fixed_pitch_beta = 0.000
low_speed_theory_limit = 80.000
prop_sync_available = 0
prop_deice_available = 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather = 700.000
beta_feather = 88.000
power_absorbed_cf = 0.900
defeathering_accumulators_available= 0
prop_reverse_available = 1
minimum_on_ground_beta = 1.000
minimum_reverse_beta = -14.000
[TurbineEngineData]
fuel_flow_gain = 0.011
inlet_area = 1.000
rated_N2_rpm = 33000.000
static_thrust = 158.000
afterburner_available= 0
[turboprop_engine]
power_scalar =1.000
maximum_torque = 3700.000
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
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -16.18, -16.85, -0.21, fx_navred
light.1 = 3, -16.18, 16.85, -0.21, fx_navgre
light.2 = 3, -35.10, 0.00, -0.50, fx_navwhi
light.3 = 2, -16.29, -16.87, -0.21, fx_strobe
light.4 = 2, -16.29, 16.87, -0.21, fx_strobe
light.5 = 1, -22.40, 0.00, 2.53, fx_beacon
light.6 = 4, -22.40, 0.816, -2.59, fx_beacon
[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 = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[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=3,0
//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, -7.10, 0.00, -5.40, 1500, 0, 0.5, 35.0, 0.3, 2.5, 0.7, 3.0, 4.0, 0
point.1 = 1, -17.50, -4.00, -5.25, 2500, 1, 0.5, 0.0, 0.3, 2.5, 0.7, 4.0, 6.0, 2
point.2 = 1, -17.50, 4.00, -5.25, 2500, 2, 0.5, 0.0, 0.3, 2.5, 0.7, 5.0, 6.0, 3
point.3 = 2, -15.90, -26.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -15.90 26.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.5= 2, -39.23, 0.0, 0.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.6= 2, -2.50, 0.0, -2.17, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.7= 2, -42.00, 0.0, 10.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7
max_number_of_points = 21
static_pitch = 0.24 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height= 5.25 //feet, altitude of CG when at rest on the ground
gear_system_type=1
[Views]
eyepoint= -15.0, 0.0, 2.25 //(feet) longitudinal, lateral, vertical distance from reference datum
[fuel]
LeftMain = -18.400, -1.100, 2.500, 79.166, 3.600
RightMain = -18.400, 1.100, 2.500, 79.166, 3.600
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
contrail=fx_contrail_l
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[airplane_geometry]
wing_area = 175.000
wing_span = 33.250
wing_root_chord = 6.400
wing_dihedral = 3.900
wing_incidence = 1.000
wing_twist = -1.000
oswald_efficiency_factor= 0.850
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = -16.000
wing_pos_apex_vert = 0.000
htail_area = 39.000
htail_span = 11.700
htail_pos_lon = -30.900
htail_pos_vert = 0.000
htail_incidence = 2.000
htail_sweep = 5.000
vtail_area = 38.000
vtail_span = 5.800
vtail_sweep = 0.000
vtail_pos_lon = -28.800
vtail_pos_vert = 1.500
elevator_area = 18.360
aileron_area = 12.240
rudder_area = 21.000
elevator_up_limit = 28.000
elevator_down_limit = 28.000
aileron_up_limit = 25.000
aileron_down_limit = 15.000
rudder_limit = 24.000
elevator_trim_limit = 19.500
spoiler_limit = 20.000
spoilerons_available = 0
aileron_to_spoileron_gain = 1.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 80.000
full_flaps_stall_speed = 65.000
cruise_speed = 260.000
max_indicated_speed=324.718750
max_mach=1.000000
[autopilot]
default_bank_mode=0
default_pitch_mode=0
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 2000.0
autothrottle_available= 0
pitch_takeoff_ga= 8.000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
[forcefeedback]
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000 ; 0 - 10000
crash_direction1=01000 ; 0 - 35999 degrees
crash_magnitude2=10000 ; 0 - 10000
crash_direction2=9000 ; 0 - 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=2500000 ; in microseconds
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 4.700
system_type= 0
damaging-speed=155.000
blowout-speed=160.000
lift_scalar= 1.000
drag_scalar= 2.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 40.000, 0.000
[brakes]
toe_brakes_scale=0.640889
parking_brake=1
[gear_warning_system]
gear_warning_available=2
pct_throttle_limit=0.099976
flap_limit_power=20.053523
flap_limit_idle=13.178029
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
