[fltsim.0]
title=MAI T41D HAF
sim=AI_T41
model=
panel=
sound=
texture=HAF
atc_id=
atc_airline=HELLENIC AIR FORCE
atc_flight_number=
ui_manufacturer=cessna
ui_type=t-41d mescalero
ui_variation=Hellenic Air Force Academy Trainer
atc_parking_codes=T41,M000
atc_parking_types=RAMP,GATE
description=Cessna's T-41D mescalero trainer replaces the old harvards as the HAF academy trainer, back in 1968. the T-41D used to be the first aircraft that all the HAF academy cadets fly with. HAF is equiped with a total number of 20 aircrafts.
[general]
atc_type=cessna
atc_model=c172
editable=0
performance="maximum speed\n126 kts 203 km\/hr\n\ncruise speed\n124 kts 200 km\/hr\n\nengine\ntextron lycoming io-360-l2a 180 bhp\n\npropeller\ntwo-bladed macauley fixed pitch\n\nmaximum range\n638 nm 734 mi 1181 km\n\nservice ceiling\n14,000 ft\t 4267 m\n\nfuel capacity\n56 gal\t 212 l\t \n\nempty weight\n1,665 lb\t 1,002 kg\n\nmaximum gross weight\n2,550 lb\t 1,157 kg\n\nlength\n27 ft, 2 in 8.2 m\n\nwingspan\n36 ft, 1 in\t 11 m\n\nheight\n8 ft, 11 in\t 2.72 m\n\nseating\t 4\n\nuseful load\n893 lb\t 405 kg\n"
[weight_and_balance]
max_gross_weight = 2550 // (pounds)
empty_weight = 1650 // (pounds)
reference_datum_position = 3.6, 0, 0 // (feet) distance from flightsim reference position: (1/4 chord, centerline, waterline)
empty_weight_cg_position = -3.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170, -3.0, -1.5, 0.0, pilot" // weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, -3.0, 1.5, 0.0, front passenger" // weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "0, -6.2, -1.5, 0.0, rear passenger" // weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "0, -6.2, 1.5, 0.0, rear passenger" // weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "0, -8.0, 0.0, 0.0, baggage" // weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;moments of inertia
empty_weight_pitch_moi = 1400.0
empty_weight_roll_moi = 1137.0
empty_weight_yaw_moi = 2360.0
empty_weight_coupled_moi= 0.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[generalenginedata]
engine_type = 0 //0=piston, 1=jet, 2=none, 3=helo-turbine, 4=rocket, 5=turboprop
engine.0 = 2.4, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 0.88 //fuel flow scalar
min_throttle_limit = 0.0 //minimum percent throttle. generally negative for turbine reverser
[piston_engine]
power_scalar = 1.0 //piston power scalar
cylinder_displacement= 90.0 //cubic inches per cylinder
compression_ratio= 8.5 //compression ratio
number_of_cylinders=4 //number of cylinders
max_rated_rpm= 2700 //max rated rpm
max_rated_hp= 180 //max rated hp
fuel_metering_type= 0 //0=fuel injected, 1=gravity carburetor, 2=aerobatic carburetor
cooling_type= 0 //0=cooling type air, 1=cooling type liquid
normalized_starter_torque= 0.3 //starter torque factor
turbocharged= 0 //is it turbocharged? 0=false, 1=true
max_design_mp= 0 //max design manifold pressure, (inhg)
min_design_mp= 0 //min design manifold pressure, (inhg)
critical_altitude= 0 //altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=none, 1=water injection, 2=methanol/water injection, 3=war emergency power
emergency_boost_mp_offset= 0 //additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //automixture available? 0=false, 1=true
auto_ignition= 0 //auto-ignition available? 0=false, 1=true
max_rpm_mechanical_efficiency_scalar= 1.0 //scalar on maximum rpm mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //scalar on idle rpm mechanical efficiency
max_rpm_friction_scalar= 1.0 //scalar on maximum rpm friction
idle_rpm_friction_scalar= 1.0 //scalar on idle rpm friction
[propeller]
thrust_scalar = 1.0 //propeller thrust scalar
propeller_type= 1 //0=constant speed, 1=fixed pitch
propeller_diameter= 6.3 //propeller diameter, (feet)
propeller_blades= 2 //number of propeller blades
propeller_moi= 5.0 //propeller moment of inertia
beta_max= 0 //maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 0 //minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 0 //miminum governed rpm
prop_tc= 0 //prop time-constant
gear_reduction_ratio= 1.0 //propeller gear reduction ratio
fixed_pitch_beta= 20 //fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80 //speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 0 //prop synchronization available? 0=false, 1=true
prop_deice_available= 0 //prop de-icing available? 0=false, 1=true
prop_feathering_available= 0 //prop feathering available? 0=false, 1=true
prop_auto_feathering_available= 0 //prop auto-feathering available? 0=false, 1=true
min_rpm_for_feather= 0 //minimum rpm for prop feathering
beta_feather= 0 //feathering pitch angle (degrees)
power_absorbed_cf= 0 //coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0 //defeathering accumulators available? 0=false, 1=true
prop_reverse_available= 0 //prop reverse available? 0=false, 1=true
minimum_on_ground_beta= 0 //miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0 //minimum pitch angle in reverse, (degrees)
[electrical]
;bustype, maxampload, minvoltage bustypes:0=mainbus,1=avionicsbus,2=batterybus,3=hotbatterybus,4-7=generator/alternatorbus(1-4)
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
//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, 0.90, 0.00, -4.09, 1500, 0, 0.5, 22.0, 0.25,2.5, 0.7, 0.0, 0.0, 0
point.1 = 1, -4.70, -4.50, -4.01, 3500, 1, 0.5, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2
point.2 = 1, -4.70, 4.50, -4.01, 3500, 2, 0.5, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3
point.3 = 2, -3.90, -18.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -3.90 18.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.5= 2,-20.23, 0.0, 0.30, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.6= 2, 1.48, 0.0, -2.17, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.7= 2,-22.80, 0.0, 5.83, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7
point.8= 2, -4.90, 0.0, -2.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8
max_number_of_points = 21
static_pitch=3.02 //degrees, pitch when at rest on the ground (+=up, -=dn)
static_cg_height=3.765 //feet, altitude of cg when at rest on the ground
[brakes]
parking_brake = 1 //parking brake available
toe_brakes_scale = 0.68 //brake scalar
[hydraulic_system]
normal_pressure = 0.0 //psi
[views]
eyepoint= -3.95, -0.85, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum
[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, -2.88, -18.11, 2.95, fx_navred
light.1 = 3, -2.88, 18.11, 2.95, fx_navgre
light.2 = 2, -3.15, -18.31, 2.95, fx_strobe
light.3 = 2, -3.15, 18.31, 2.95, fx_strobe
light.4 = 1, -20.60, 0.00, 6.33, fx_beacon
light.5 = 4, -2.27, 0.00, 1.45, fx_vclight
[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=1,0
[attitude_indicators]
//type: 0=none, 1=vacuum gyro, 2=electric gyro
attitude_indicator.0 = 1
[turn_indicators]
//type: 0=none, 1=electric gyro, 2= vacuum gyro
turn_indicator.0=1,1 //turn and bank
[effects]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
leftmain = -3.9, -2.1, 2.5, 26.5, 0.0 //longitudinal (feet), lateral (feet), vertical (feet), usable(gallons), unusable (gallons)
rightmain = -3.9, 2.1, 2.5, 26.5, 0.0 //longitudinal (feet), lateral (feet), vertical (feet), usable(gallons), unusable (gallons)
fuel_type = 1 //fuel type: 1 = avgas, 2 = jeta
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 174.0 //square feet
wing_span = 36.1 //feet
wing_root_chord = 4.9 //feet
wing_dihedral = 1.7 //degrees
wing_incidence = 1.5 //degrees
wing_twist = -3.0 //degrees
oswald_efficiency_factor= 0.68 //measure of lift effeciency of wing
wing_winglets_flag = 0 //are winglets available?
wing_sweep = 0 //degrees, wing leading edge
wing_pos_apex_lon = -2.4 //feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //feet, vertical distance from reference point, positive going up
htail_area = 39.0 //square feet
htail_span = 11.7 //feet
htail_pos_lon = -18.3 //feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //feet, vertical distance from reference point, positive going up
htail_incidence = 3.2 //degrees
htail_sweep = 10.0 //degrees, horizontal tail leading edge
vtail_area = 18.0 //square feet
vtail_span = 4.8 //feet, tip to body
vtail_sweep = 40.0 //degrees, vertical tail leading edge
vtail_pos_lon = -16.2 //feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 1.5 //feet, vertical distance from reference point, positive going up
elevator_area = 16.6 //square feet
aileron_area = 18.3 //square feet
rudder_area = 6.7 //square feet
elevator_up_limit = 28.0 //degrees
elevator_down_limit = 21.0 //degrees
aileron_up_limit = 20.0 //degrees
aileron_down_limit = 15.0 //degrees
rudder_limit = 24.0 //degrees
elevator_trim_limit = 19.5 //degrees
spoiler_limit = 0.0 //degrees
spoilerons_available = 0 //spoilerons available?
aileron_to_spoileron_gain = 0 //aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //degrees
min_flaps_for_spoilerons = 0 //minimum flap handle position when spoilerons activate
[flaps.0] //trailing edge flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 7 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 12.7 // degrees
flaps-position.2 = 25.3 // degrees
flaps-position.3 = 38 // degrees
damaging-speed = 120 // kias
blowout-speed = 150 // kias
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 0 //0=electric, 1=hydraulic, 2=pneumatic, 3=manual, 4=none
[reference speeds]
flaps_up_stall_speed = 53.0 //knots true (ktas)
full_flaps_stall_speed = 48.0 //knots true (ktas)
cruise_speed = 115.0 //knots true (ktas)
max_indicated_speed = 163 //red line (kias)
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0
[forcefeedback]
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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
[stall_warning]
type=1
