// O. Fischer

[fltsim.0]
title=Junkers 52/3m D-ALYL 
sim=Ju_52
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=D-ALYL
atc_parking_types=GATE,RAMP
ui_manufacturer=Junkers
ui_type=Ju-52 
ui_variation=XI.Olympiade D-ALYL
atc_heavy=0
atc_airline=Lufthansa
atc_flight_number=
description=Pionierflьge und neue Flugverbindungen bis ins ferne Asien wurden durch die Ju 52 mцglich. Unter der Leitung von Dipl.Ing. Ernst Zindel wurde in den Dessauer Junkers-Flugzeugwerken 1930 zuerst eine einmotorige Version als Frachtflugzeug konstruiert. Wenige Monate spдter, auf Wunsch einiger Fluggesellschaften, konzentrierten sich die Ingenieure jedoch auf die bekannte, dreimotorige Version Ju 52\/3m, die 1932 zum ersten verkehrsmдЯigen Einsatz kam.\n\nThe Ju52 made many experimental flights all over the world and routes into the Far East were made possible by this aircraft. The "Junkers-Flugzeugwerke" in Dessau developed it originally as a single engine cargo aircraft in 1930, under chief constructor Ernst Zindel (Dipl. Ing). A few months later construction began on the well known three-engined JU 52\/3m,the change was triggered by several interested airlines looking for a reliable design. This version saw commercial service first in 1932.

[fltsim.1]
title=Junkers 52/3m D-ASIS
sim=Ju_52
model=
panel=
sound=
texture=1
kb_checklists=
kb_reference=
atc_id=D-ASIS
atc_parking_types=GATE,RAMP
ui_manufacturer=Junkers
ui_type=Ju-52 
ui_variation=Wilhelm Cuno D-ASIS
atc_heavy=0
atc_airline=Lufthansa
atc_flight_number=
description=Pionierflьge und neue Flugverbindungen bis ins ferne Asien wurden durch die Ju 52 mцglich. Unter der Leitung von Dipl.Ing. Ernst Zindel wurde in den Dessauer Junkers-Flugzeugwerken 1930 zuerst eine einmotorige Version als Frachtflugzeug konstruiert. Wenige Monate spдter, auf Wunsch einiger Fluggesellschaften, konzentrierten sich die Ingenieure jedoch auf die bekannte, dreimotorige Version Ju 52\/3m, die 1932 zum ersten verkehrsmдЯigen Einsatz kam.\n\nThe Ju52 made many experimental flights all over the world and routes into the Far East were made possible by this aircraft. The "Junkers-Flugzeugwerke" in Dessau developed it originally as a single engine cargo aircraft in 1930, under chief constructor Ernst Zindel (Dipl. Ing). A few months later construction began on the well known three-engined JU 52\/3m,the change was triggered by several interested airlines looking for a reliable design. This version saw commercial service first in 1932.

[fltsim.2]
title=Junkers 52/3m G-AHOF
sim=Ju_52
model=1
panel=
sound=
texture=2
kb_checklists=
kb_reference=
atc_id=G-AHOF
atc_parking_types=GATE,RAMP
ui_manufacturer=Junkers
ui_type=Ju-52 
ui_variation=British European Airways G-AHOF
atc_heavy=0
atc_airline=British European Airways
atc_flight_number=
description=Pionierflьge und neue Flugverbindungen bis ins ferne Asien wurden durch die Ju 52 mцglich. Unter der Leitung von Dipl.Ing. Ernst Zindel wurde in den Dessauer Junkers-Flugzeugwerken 1930 zuerst eine einmotorige Version als Frachtflugzeug konstruiert. Wenige Monate spдter, auf Wunsch einiger Fluggesellschaften, konzentrierten sich die Ingenieure jedoch auf die bekannte, dreimotorige Version Ju 52\/3m, die 1932 zum ersten verkehrsmдЯigen Einsatz kam.\n\nThe Ju52 made many experimental flights all over the world and routes into the Far East were made possible by this aircraft. The "Junkers-Flugzeugwerke" in Dessau developed it originally as a single engine cargo aircraft in 1930, under chief constructor Ernst Zindel (Dipl. Ing). A few months later construction began on the well known three-engined JU 52\/3m,the change was triggered by several interested airlines looking for a reliable design. This version saw commercial service first in 1932.

[fltsim.3]
title=Junkers 52/3m ZS-AFB
sim=Ju_52
model=
panel=
sound=
texture=3
kb_checklists=
kb_reference=
atc_id=ZS-AFB
atc_parking_types=GATE,RAMP
ui_manufacturer=Junkers
ui_type=Ju-52 
ui_variation=Lord Charles Somerset ZS-AFB
atc_heavy=0
atc_airline=South African Airways
atc_flight_number=
description=Pionierflьge und neue Flugverbindungen bis ins ferne Asien wurden durch die Ju 52 mцglich. Unter der Leitung von Dipl.Ing. Ernst Zindel wurde in den Dessauer Junkers-Flugzeugwerken 1930 zuerst eine einmotorige Version als Frachtflugzeug konstruiert. Wenige Monate spдter, auf Wunsch einiger Fluggesellschaften, konzentrierten sich die Ingenieure jedoch auf die bekannte, dreimotorige Version Ju 52\/3m, die 1932 zum ersten verkehrsmдЯigen Einsatz kam.\n\nThe Ju52 made many experimental flights all over the world and routes into the Far East were made possible by this aircraft. The "Junkers-Flugzeugwerke" in Dessau developed it originally as a single engine cargo aircraft in 1930, under chief constructor Ernst Zindel (Dipl. Ing). A few months later construction began on the well known three-engined JU 52\/3m,the change was triggered by several interested airlines looking for a reliable design. This version saw commercial service first in 1932.

[fltsim.4]
title=Junkers 52/3m D-ABIK
sim=Ju_52
model=
panel=
sound=
texture=4
kb_checklists=
kb_reference=
atc_id=D-ABIK
atc_parking_types=GATE,RAMP
ui_manufacturer=Junkers
ui_type=Ju-52 
ui_variation=Manfred von Richthofen D-ABIK
atc_heavy=0
atc_airline=Lufthansa
atc_flight_number=
description=Pionierflьge und neue Flugverbindungen bis ins ferne Asien wurden durch die Ju 52 mцglich. Unter der Leitung von Dipl.Ing. Ernst Zindel wurde in den Dessauer Junkers-Flugzeugwerken 1930 zuerst eine einmotorige Version als Frachtflugzeug konstruiert. Wenige Monate spдter, auf Wunsch einiger Fluggesellschaften, konzentrierten sich die Ingenieure jedoch auf die bekannte, dreimotorige Version Ju 52\/3m, die 1932 zum ersten verkehrsmдЯigen Einsatz kam.\n\nThe Ju52 made many experimental flights all over the world and routes into the Far East were made possible by this aircraft. The "Junkers-Flugzeugwerke" in Dessau developed it originally as a single engine cargo aircraft in 1930, under chief constructor Ernst Zindel (Dipl. Ing). A few months later construction began on the well known three-engined JU 52\/3m,the change was triggered by several interested airlines looking for a reliable design. This version saw commercial service first in 1932.


[General]
atc_type=Junkers
atc_model=Ju52
editable=0
performance=Hцchstgeschwindigkeit\/max. speed\n161 mph          260 km\/h\n\nReisegeschwindigkeit\/cruise speed\n118 mph          190 km\/h\n\nTriebwerke\/engines\n3 BMW 132 A (bzw. 132 E)  mit je 660-PS\n\nLuftschrauben\/props\nZweiblatt,Junkers Ju PAK aus Dural 2,9m\n\nMaximale Reichweite\/max. range\n745 Meilen          1.200 km\n\nDienstgipfelhцhe\/service ceiling\n16.730 FuЯ          5.100 m\n\nTreibstoffmenge\/fuel quantity\n667 Gallonen          2.450 l\n\nLeergewicht\/empty weight\n14.500 lbs          6.590 kg\n\nMaximales Bruttogewicht\/max. weight\n23.150 lbs          10.500 kg\n\nLдnge\/lenght\n62 FuЯ          18,9 m\n\nSpannweite\/wingspan\n96 FuЯ          29,25 m\n\nHцhe\/height\n20FuЯ          6,10 m\n\nSitzplдtze\/seats\n17\n\nZuladung\/load\n8.620 lbs          3.910 kg\n\nModell\nO.Fischer
Category=airplane

[WEIGHT_AND_BALANCE]
max_gross_weight = 23148.500
empty_weight = 14528.500

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations =50

station_load.0  =190.000000, 7.250000, -1.800000, 0.000000, Pilot         
station_load.1  =165.000000, 7.250000, 1.800000, 0.000000, Kopilot        
station_load.2  =360.000000, 0.000000, 0.000000, 0.000000, Passagierreihe        
station_load.3  =360.000000, 1.200000, 0.000000, 0.000000, Passagierreihe         
station_load.4  =360.000000, -1.700000, 0.000000, 0.000000, Passagierreihe         
station_load.5  =360.000000, -4.700000, 0.000000, 0.000000, Passagierreihe
station_load.6  =360.000000, -7.700000, 0.000000, 0.000000, Passagierreihe         
station_load.7  =360.000000, -10.700000, 0.000000, 0.000000, Passagierreihe     
station_load.8  =180.000000, -13.800000, 0.000000, 0.000000, Passagierreihe         
station_load.9  =500.000000, -16.000000, 0.000000, 0.000000, Gepдck 

;Moments of Inertia
empty_weight_pitch_MOI = 105705.000
empty_weight_roll_MOI = 71542.000
empty_weight_yaw_MOI = 140733.000
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 =0.500
aileron_effectiveness  =1.000
rudder_effectiveness   =0.500
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
p_factor_on_yaw          = 0.5
torque_on_roll           = 1.0
gyro_precession_on_yaw   = 1.0
gyro_precession_on_pitch = 1.0

[GeneralEngineData]
engine_type = 0
Engine.0 = 9.000, -11.970, -1.300
Engine.1 = 16.000, 0.000, 0.000
Engine.2 = 9.000, 11.970, -1.300
fuel_flow_scalar= 1.000
min_throttle_limit = 0.0                        //Minimum percent throttle.  Generally negative for turbine reverser
master_ignition_switch = 1                      //Master Ignition Switch

[piston_engine]
power_scalar=1.000
cylinder_displacement= 187.800 
compression_ratio= 6.930
number_of_cylinders= 9
max_rated_rpm= 2050.000
max_rated_hp= 660.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.200
turbocharged= 1
max_design_mp= 35.000    
min_design_mp= 10.000
critical_altitude= 6500.000
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=0.800
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= 9.550
propeller_blades= 2
propeller_moi= 25.000
beta_max= 45.000
beta_min= 12.500
min_gov_rpm= 1400.000
prop_tc= 0.100
gear_reduction_ratio= 1.700
fixed_pitch_beta= 25.000
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, -40.000, 0.000, -0.650, 1200.000, 0.000, 0.820, 180.000, 0.250, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 //Spornrad
point.1= 1.000, 2.250, -6.560, -8.900, 1600.000, 1.000, 1.800, 0.000, 0.545, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000 //Fahrwerk-links
point.2= 1.000, 2.250, 6.560, -8.900, 1600.000, 2.000, 1.800, 0.000, 0.545, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000 //Fahrwerk-rechts
point.3= 2.000, -0.500, -48.500, 1.350, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //Tragflдche-links
point.4= 2.000, -0.500, 48.500, 1.350, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //Tragflдche-rechts
point.5= 2.000, -38.250, -16.000, 4.500, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Horizontale-links
point.6= 2.000, -38.250, 16.000, 4.500, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Horizontale-rechts
point.7= 2.000, 17.000, 0.000, -2.400, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Rumpf-Bug
point.8= 2.000, -38.500, 0.000, 1.445, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Rumpf-Heck

static_pitch = 11.100
static_cg_height = 7.850
gear_system_type = 1
tailwheel_lock = 0 

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.5  //Brake scalar
differential_braking_scale = 1       //Delta on the amount of brake when the gas lever deflected

[hydraulic_system]
normal_pressure = 0.0    //PSI

[Views]
eyepoint = 7.650, -1.700, 3.500 
//eyepoint = 7.500, 1.700, 3.400 //Copilot

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing , ..., 10=cabin
light.0 = 3,  -0.46, -48.54,  1.33, fx_navred,     //Navigationslicht links
light.1 = 3,  -0.46,  48.54,  1.33, fx_navgre,     //Navigationslicht rechts
light.2 = 4,   8.50,  0.00,  3.00, fx_vclight52,         //Cockpit
light.3 = 10,   -10.50,   0.00,  4.5, fx_vclighth52,        //Kabine
light.4 = 10,   -4.00,   0.00,  4.5, fx_vclighth52,        //Kabine
light.5 = 10,   2.00,   0.00,  4.5, fx_vclighth52,        //Kabine

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 0
Nav.1         = 0, 0, 0
Adf.1         = 1
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, 1000
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
direction_indicator.1=2,0

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
attitude_indicator.1 = 2 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0

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

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 55
engine_generator_map= 0,1,0

[fuel]
LeftMain = -3.000, -12.000, -2.000, 317.000, 0.000
RightMain= -3.000, 12.000, -2.000, 317.000, 0.000
Center1  = 5.900, 0.000, 4.000, 13.200, 0.000
fuel_type = 1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 3                    
electric_pump=1
manual_transfer_pump=1

[airplane_geometry]
wing_area               = 1184.000
wing_span               = 95.960
wing_root_chord         = 12.000
wing_dihedral           = 6.000
wing_incidence          = 3.000
wing_twist              = 0.000
oswald_efficiency_factor= 0.650
wing_winglets_flag      = 0
wing_sweep              = 8.000
wing_pos_apex_lon       = 0.500
wing_pos_apex_vert      = 1.300

htail_area              = 125.500
htail_span              = 29.500
htail_pos_lon           = -36.000
htail_pos_vert          = 0.000
htail_incidence         = 0.000
htail_sweep             = 7.000

vtail_area              = 30.750
vtail_span              = 11.000
vtail_sweep             = 60.000
vtail_pos_lon           = -38.000
vtail_pos_vert          = 7.800

elevator_area           = 57.850
aileron_area            = 94.500
rudder_area             = 35.050
elevator_up_limit       = 30.000
elevator_down_limit     = 20.000
aileron_up_limit        = 18.000
aileron_down_limit      = 18.000
rudder_limit            = 30.000
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
auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.666667
negative_g_limit_flaps_up=-3.333333
negative_g_limit_flaps_down=-2.000000

[Reference Speeds]
flaps_up_stall_speed    = 56.000
full_flaps_stall_speed  = 47.000
cruise_speed= 102.590
max_indicated_speed=140.380 //Red line (KIAS)

[autopilot]
autopilot_available= 1
flight_director_available= 0
pitch_takeoff_ga= 0.000
autothrottle_available= 0
direction_indicator=1
use_no_default_pitch= 1
max_bank= 15.000
max_bank_acceleration= 1.800
max_bank_velocity= 3.000
max_throttle_rate= 0.100
nav_proportional_control= 9.000
nav_integrator_control= 0.250
nav_derivative_control= 0.000
nav_integrator_boundary= 2.500
nav_derivative_boundary= 0.000
gs_proportional_control= 9.520
gs_integrator_control= 0.260
gs_derivative_control= 0.000
gs_integrator_boundary= 0.700
gs_derivative_boundary= 0.000
yaw_damper_gain= 0.000
default_bank_mode=2     //Default to Heading Hold
default_pitch_mode=0
default_vertical_speed=700.000000
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

[forcefeedback]
ground_bumps_magnitude1=2600            ; 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=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=3500000                 ; in microseconds

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second  //Hauptausgang
exit_rate.1 = 0.8                               ;Percent per second  //Cockpittьren

[stall_warning]
type=0
stick_shaker=1

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 7.000
system_type= 3
damaging-speed= 100.000
blowout-speed= 120.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000

[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=4.900000
engine_map=1,1,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0