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//
// AI Transall Transallproject www.Transallproject.de
//
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[fltsim.0]
title=AI Transall C160 LTG61
sim=c160
model=d
panel=
sound=
texture=ltg61
checklists=
ui_manufacturer=AI TransallC160
ui_type=C160 D
ui_variation=German Air Force LTG61 5098
atc_id=
atc_airline=Air Force
atc_flight_number=
atc_heavy=0
atc_parking_types=MIL_CARGO,CARGO,GATE,RAMP
atc_parking_codes=C160
visual_damage=0
description=AI Transall by Transallproject
[fltsim.1]
title=AI Transall C160 LTG61 UN
sim=c160
model=d
panel=
sound=
texture=ltg61_UN
checklists=
ui_manufacturer=AI TransallC160
ui_type=C160 D
ui_variation=German Air Force LTG61 5057 UN Version
atc_id=UN5058
atc_airline=United Nations
atc_flight_number=
atc_heavy=0
atc_parking_types=MIL_CARGO,CARGO,GATE,RAMP
atc_parking_codes=C160
visual_damage=0
description=AI Transall by Transallproject
[fltsim.2]
title=AI Transall C160 LTG62
sim=c160
model=d
panel=
sound=
texture=ltg62
checklists=
ui_manufacturer=AI TransallC160
ui_type=C160 D
ui_variation=German Air Force LTG62 5029
atc_id=
atc_airline=Air Force
atc_flight_number=
atc_heavy=0
atc_parking_types=MIL_CARGO,CARGO,GATE,RAMP
atc_parking_codes=C160
visual_damage=0
description=AI Transall by Transallproject
[fltsim.3]
title=AI Transall C160 LTG63
sim=c160
model=d
panel=
sound=
texture=ltg63
checklists=
ui_manufacturer=AI TransallC160
ui_type=C160 D
ui_variation=German Air Force LTG63 5006
atc_id=
atc_airline=Air Force
atc_flight_number=
atc_heavy=0
atc_parking_types=MIL_CARGO,CARGO,GATE,RAMP
atc_parking_codes=C160
visual_damage=0
description=AI Transall by Transallproject
[fltsim.4]
title=AI Transall C160 LTG62 UN
sim=c160
model=d
panel=
sound=
texture=ltg62_UN
checklists=
ui_manufacturer=AI TransallC160
ui_type=C160 D
ui_variation=German Air Force LTG62 5050 UN Version
atc_id=UN5050
atc_airline=United Nations
atc_flight_number=
atc_heavy=0
atc_parking_types=MIL_CARGO,CARGO,GATE,RAMP
atc_parking_codes=C160
visual_damage=0
description=AI Transall by Transallproject
[fltsim.5]
title=AI Transall C160 LTG63 UN
sim=c160
model=d
panel=
sound=
texture=ltg63_UN
checklists=
ui_manufacturer=AI TransallC160
ui_type=C160 D
ui_variation=German Air Force LTG63 5087 UN Version
atc_id=UN5087
atc_airline=United Nations
atc_flight_number=
atc_heavy=0
atc_parking_types=MIL_CARGO,CARGO,GATE,RAMP
atc_parking_codes=C160
visual_damage=0
description=AI Transall by Transallproject
[General]
atc_type=Transall
atc_model=C160
editable=1
performance=Höchstgeschwindigkeit 510 km\/h\nSpannweite 40.00 m\nLänge 32.40 m\nHöhe 12.36 m\nLeermasse 28 000 kg\nmax. Startgewicht\t 49 150 kg\nmax. Landegewicht 47 000 kg\nmax. Nutzlast 16 000 kg\nmax. Kraftstoffvorrat 13 128 kg\nmax. Nutzladevolumen 139.9 m3
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 108357.0
empty_weight = 61730.0
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 1.500, 0.000, -1.000
empty_weight_pitch_MOI = 995436
empty_weight_roll_MOI = 730165
empty_weight_yaw_MOI = 1184711
empty_weight_coupled_MOI= 0.0
[fuel]
LeftMain = -1.000, -14.000, 9.000, 1336.000, 0.000
RightMain = -1.000, 14.000, 9.000, 1336.000, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
[flight_tuning]
cruise_lift_scalar = 1.200
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
[GeneralEngineData]
engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 14.700, -28.100, -6.000 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 14.700, 28.100, -6.000 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.000 //Scalar for fuel flow efficiency
min_throttle_limit = -0.150 //Minimum percent throttle. Generally negative for turbine reverser
[propeller]
thrust_scalar = 1.200 //Propeller thrust scalar
propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter = 14.800 //Propeller Diameter, (feet)
propeller_blades = 4 //Number of propeller blades
propeller_moi = 24 //Propeller moment of inertia
beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min = 15.200 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm = 25520 //Miminum governed RPM
prop_tc = 0.004 //Prop time-constant
gear_reduction_ratio = 17.600 //Propeller gear reduction ratio
fixed_pitch_beta = 0 //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 = 1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available = 1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather = 700 //Minimum RPM for prop feathering
beta_feather = 78.800 //Feathering pitch angle (degrees)
power_absorbed_cf = 0.900 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta = 1.000 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta = -14.000 //Minimum pitch angle in reverse, (degrees)
[TurbineEngineData]
fuel_flow_gain = 0.011 //Gain on fuel flow
inlet_area = 5.000 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 500 //Lbs, max rated static thrust at Sea Level
[turboprop_engine]
power_scalar = 1.200 //Scalar on Turboprop power
maximum_torque = 11330 //Maximum torque available (ft-lbs)
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
point.0 = 1, 33.15, 0, -11.7, 1500, 0, 1.6, 35, 1.2, 1.2, 0.9, 5, 6, 0, 250, 250
point.1 = 1, -3.5, -8.35, -11.7, 3000, 1, 1.6, 0, 1.2, 1.0, 0.9, 6, 7, 2, 250, 250
point.2 = 1, -3.5, 8.35, -11.7, 3000, 2, 1.6, 0, 1.2, 1.0, 0.9, 6, 7, 3, 250, 250
point.3 = 2, 0, -65, 7.5, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0, 65, 7.5, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -63.5, 0, 3.8, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 43, 0, -6, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
static_pitch = 0.040
static_cg_height = 11.2
gear_system_type=1 //Hydraulic
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 10 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 30 // degrees
flaps-position.4 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -0.1, -65.35, 7.3, fx_navred
light.1 = 3, -0.1, 65.35, 7.3, fx_navgre
light.2 = 3, -63.0, 0.00, 6.5, fx_navwhi
light.3 = 1, -56, 0, 28, fx_beacon
light.4 = 1, 7.0, 8.3, -9.7, fx_beacon
light.5 = 2, -5.30, -28.100, -6.000, fx_exhaust
light.6 = 2, -5.30, 28.100, -6.000, fx_exhaust
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[airplane_geometry]
wing_area = 1720.0 //Square feet
wing_span = 112.0 //Feet
wing_root_chord = 19.9 //Feet
wing_dihedral = 4.0 //Degrees
wing_incidence = 1.5 //Degrees
wing_twist = -0.2 //Degrees
oswald_efficiency_factor= 0.7 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 7.0 //Degrees, wing leading edge
wing_pos_apex_lon = 9.5 //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 = 570.0 //Square feet
htail_span = 47.0 //Feet
htail_pos_lon = -40.0 //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 = 0.0 //Degrees
htail_sweep = 20.0 //Degrees, horizontal tail leading edge
vtail_area = 338.5 //Square feet
vtail_span = 25.0 //Feet, tip to body
vtail_sweep = 25.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -31.5 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 6.0 //Feet, vertical distance from reference point, positive going up
elevator_area = 285.3 //Square feet
aileron_area = 172.7 //Square feet
rudder_area = 200.0 //Square feet
elevator_up_limit = 22.5 //Degrees
elevator_down_limit = 21.5 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 20.0 //Degrees
rudder_limit = 26.0 //Degrees
elevator_trim_limit = 20.0 //Degrees
spoiler_limit = 60.0 //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
auto_spoiler_available=0
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
[Reference Speeds]
flaps_up_stall_speed = 96.0 //Knots True (KTAS)
full_flaps_stall_speed = 76.8 //Knots True (KTAS)
cruise_speed = 245.0 //Knots True (KTAS)
max_mach = 0.58
max_indicated_speed = 263 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
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
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[Views]
eyepoint=0.000000,0.000000,0.000000
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
stick_shaker=0
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=2