[fltsim.0]
title=Junkers Ju-52 Ju-Air 
sim=ju52_ver40
model=
panel=
sound=
texture=
KB_checklists=ju52_ver40_check
kb_reference=ju52_ver40_ref
description=Today: Ju-Air. Improved version \nof the Junkers Ju52\/3m g4e. \nIt had modern radio equipment, \nand was powered by 3 × BMW 132A-3 \nradials, rated at 660 hp each. \nThe internal fuel capacity of \n544 Imp gal (654 US gal, 2.475 liters) \nmade a range radius of 1000 km \npossible at cruising speed at 4500 m.
ui_manufacturer=Junkers
ui_type=Ju-52/3m g4e 
ui_variation=Ju-air HB-HOS
atc_heavy=0
atc_airline=Ju-Air
atc_id=HBHOS
atc_flight_number=1939
visual_damage=1

[fltsim.1]
title=Junkers Ju-52 "Where eagles dare"
sim=ju52_ver40
model=wed
panel=
sound=
texture=
checklists=
KB_checklists=ju52_ver40_check
description=Swiss Army version, today Ju-Air\nThis aircraft was used in the motion \npicture "Where Eagles Dare" \n(1968, Metro-Goldwyn-Mayer)
ui_manufacturer=Junkers
ui_type=Ju-52/3m g4e
ui_variation=Where eagles dare
atc_heavy=0
atc_airline="Where Eagles Dare"
atc_id=CN+4V
atc_flight_number=1939
visual_damage=1

[General]
atc_type=ju52_ver40
atc_model=ju52_ver40
editable=0
performance=Power:\t         3 x 660 hp BMW 132A \nWingspan:         29,25 m  ( 96 ft )\nLength:\t         18,90 m  ( 62 ft )\nHeight:\t         6,10 m\nWing Area:         110,50 m^2\nWeight Empty:    6'500 kg\nMTOW:\t          10,50 tonnes\nFuel capacity:    2'475 l\nFuel consumption: 450 l\/h\nTake off sp.:    ap. 120 km\/h \nCruise sp.:       ap. 170 km\/h\nTop speed:            250 km\/h\nRange:\t       ap. 1'000 km\s  ap. 5 h\nTake off run:    ap. 500 m\nLanding run:    ap. 350 m\nCeiling:\t       5'500 m (ap. 18'000 ft)\nInitial climb:     208 m (680 ft) p. min.\nFlap limit sp.: 10 deg....170 km\/h\n                         25 deg....160 km\/h\n                         40 deg....150 km\/\nAircrew            4\nPassengers    14\n\nVersion FS2002\nDesigner: Pierino Primavesi\nDecember 2002

[Reference Speeds]
flaps_up_stall_speed=55.0                  
full_flaps_stall_speed=45.0                  
cruise_speed=105.0

[GeneralEngineData]
engine_type=0
Engine.0=8.333333,-13.333333,1.250000
Engine.1=12.500000,0.000000,4.166667
Engine.2=8.333333,13.333333,1.250000
fuel_flow_scalar=1.0000

[fuel]
LeftMain=0.000000,-9.000000,0.000000,330.000000,0.000000
RightMain=0.000000,9.000000,0.000000,330.000000,0.000000
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  
empty_weight = 14617                            
max_gross_weight = 23100
max_number_of_stations=50
station_load.0=170,  7.4, -1.80, 0.0         
station_load.1=170,  7.4, 1.80, 0.0         
station_load.2=2000.000,0.000000,0.000000,0.000000
empty_weight_roll_MOI= 54758.000
empty_weight_pitch_MOI= 48676.000
empty_weight_yaw_MOI= 99972.000
empty_weight_coupled_MOI= 0.000      

[piston_engine]
power_scalar = 1
cylinder_displacement = 187.8
compression_ratio = 6.93
number_of_cylinders = 9
max_rated_rpm = 2050
max_rated_hp = 660
fuel_metering_type = 0
cooling_type = 0
normalized_starter_torque = 0.030
turbocharged = 1
max_design_mp = 35
min_design_mp = 1
critical_altitude = 15500
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar = 0.8
idle_rpm_mechanical_efficiency_scalar = 0.82
max_rpm_friction_scalar = 1.4
idle_rpm_friction_scalar = 1.6

[propeller]
thrust_scalar = 1
propeller_type = 0
propeller_diameter = 10.4
propeller_blades = 2
propeller_moi = 33.7
beta_max = 45
beta_min = 12.5
min_gov_rpm = 1400
prop_tc = 0.01
gear_reduction_ratio = 1.7
fixed_pitch_beta = 0
low_speed_theory_limit = 80
prop_sync_available = 0
prop_deice_available = 0
prop_feathering_available = 0
prop_auto_feathering_available = 1
min_rpm_for_feather = 700
beta_feather = 79.3
power_absorbed_cf = 0.9
defeathering_accumulators_available = 0
prop_reverse_available = 0
minimum_on_ground_beta = 0
minimum_reverse_beta = 0

[electrical]
autopilot=0,5,17.0
avionics_bus=0,10,17.0
avionics=1,5,17.0
pitot_heat=0,2,17.0
additional_system=0,20,17.0
marker_beacon=1,2,17.0
gear_warning=0,2,17.0
fuel_pump=0,5,17.0
starter1=0,20,17.0
starter2=0,20,17.0
starter3=0,20,17.0
light_nav=0,5,17.0
light_beacon=0,5,17.0
light_landin0,5,17.0
light_taxi=0,5,17.0
light_strobe=0,5,17.0
light_panel=0,5,17.0

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=1
pitch_takeoff_ga=8.000000
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=95.000000
use_no_default_pitch=1 
use_no_default_bank=1 

[direction_indicators]
direction_indicator.0=1,0

[LIGHTS]
light.0=5, 5.39, -7.175, -0.68, fx_landing ,
light.1=5, 5.39, 7.175, -0.68, fx_landing ,
light.2=3, -2.56, -49.04, 3.94, fx_navred ,
light.3=3, -2.56, 49.04, 3.94, fx_navgre ,
light.4=2, -2.63, -49.04, 3.94, fx_strobe ,
light.5=2, -2.63, 49.04, 3.94, fx_strobe ,
light.6=2, -25.61, 0.00, 1.37, fx_beacon ,
light.7=1, -38.71, 0.00, 15.07, fx_beacon ,
light.8=4,  7.00,   0.00, 6.00, fx_vclight

[SMOKESYSTEM]
smoke.0=3.576,6.266,-12.598, fx_smoke_ju4 
smoke.1=4.50,12.86,-3.28, fx_smoke_ju4
smoke.2=3.576,6.266,12.598, fx_smoke_ju4
smoke.3=4.50,12.86,3.28, fx_smoke_ju4

[airplane_geometry]
wing_area = 1184
wing_span = 96
wing_root_chord = 12
wing_dihedral = 2
wing_incidence = 3
wing_twist = 0
oswald_efficiency_factor = 0.65
wing_winglets_flag = 0
wing_sweep  = 0
wing_pos_apex_lon = 0
wing_pos_apex_vert = 0
htail_area = 169
htail_span = 32.8
htail_pos_lon = -35.9
htail_pos_vert = 6.5
htail_incidence = 0
htail_sweep = 0
vtail_area = 69.9
vtail_span = 8.5
vtail_sweep = 0
vtail_pos_lon  = -39.4
vtail_pos_vert = 8.5
elevator_area = 57.8
aileron_area = 25.25
rudder_area = 43
elevator_up_limit = 30
elevator_down_limit = 20
aileron_up_limit = 15
aileron_down_limit = 15
rudder_limit = 30
elevator_trim_limit = 18
spoiler_limit = 90
spoilerons_available = 0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0

[contact_points]
static_pitch=11.85
static_cg_height=5.834774
tailwheel_lock = 1

point.0=1.000000,-42.500000,0.000000,2.65533,1574.803200,0.000000,0.641976,60.00000,0.326418,2.500000,0.706510,0,0,0.000000,0.000000,0.000000
point.1=1.000000,3.416667,-6.833333,-6.233333,1574.803200,1.000000,0.641976,0.000000,0.342364,2.500000,0.796592,0,0,2.000000,0.000000,0.000000
point.2=1.000000,3.416667,6.833333,-6.233333,1574.803200,2.000000,0.641976,0.000000,0.342364,2.500000,0.796592,0,0,3.000000,0.000000,0.000000
point.3=2.000000,-0.083333,-48.333333,4.583333,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-0.083333,48.333333,4.583333,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-38.333333,0.000000,2.500000,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,18.333333,0.000000,1.666667,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
point.7=2.000000,0,0.000000,-0.98,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
point.8=2.000000,0,0.000000,8.72,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000

[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

[ground_reaction]
main_gear_static_compression=0.3		// (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.3            // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=0.7		// Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=0.7		// Center gear strut damping, 0 = undamped osciallations, 1 = critically damped

[keyboard_response]
elevator = 120, 200
aileron  = 120, 200
rudder   = 120, 200

[Views]
eyepoint= 7.95, -1.66, 7.3

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[flaps.0]       //Trailing Edge Flaps
type = 1
span-outboard = 0.8
extending-time = 5
system_type= 1
flaps-position.0 = 0
flaps-position.1 = 10
flaps-position.2 = 30
flaps-position.3 = 40
damaging-speed = 92
blowout-speed = 101

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000