[fltsim.0]
title=Ju52/3m
sim=Ju52_3m
model=
panel=
sound=
texture=
checklists=
KB_checklists=Ju52_3m_check
description=Lufthansa Version\nImproved version of the Junkers Ju52\/3m g4e. It had modern radio equipment, and was powered by 3 × BMW 132A-3 radials, rated at 725 hp (541 kW) each. The internal fuel capacity of 544 Imp gal (654 US gal, 2.475 liters) made a range radius of 1000 km possible at cruising speed at 4500 m.
ui_manufacturer=Junkers
ui_type=Ju-52/3m g4e
ui_variation=Lufthansa J.1935
atc_heavy=0
atc_airline=Lufthansa
atc_id=D-AJAN
atc_flight_number=1123
visual_damage=1
[fltsim.1]
title=Ju52/3m Modern
sim=Ju52_3m
model=
panel=1
sound=
texture=1
checklists=
KB_checklists=Ju52_3m_check
description=Lufthansa Version\nImproved version of the Junkers Ju52\/3m g4e. It had modern radio equipment, and was powered by 3 × BMW 132A-3 radials, rated at 725 hp (541 kW) each. The internal fuel capacity of 544 Imp gal (654 US gal, 2.475 liters) made a range radius of 1000 km possible at cruising speed at 4500 m.
ui_manufacturer=Junkers
ui_type=Ju-52/3m g4e
ui_variation=Lufthansa Moderne Instrumente
atc_heavy=0
atc_airline=LUFTHANSA
atc_id=D-CDLH
atc_flight_number=1123
visual_damage=1
[General]
atc_type=Ju52_3m
atc_model=Ju52_3m
editable=1
performance=Power:\t 3 x 725hp 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\nApril 2002
[contact_points]
static_pitch= 11.850
static_cg_height= 5.835
point.0= 1.000, -42.500, 0.000, 2.655, 1574.803, 0.000, 0.642, 60.600, 0.326, 2.500, 0.707, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, 3.417, -6.833, -6.233, 1574.803, 1.000, 0.642, 0.000, 0.342, 2.500, 0.797, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, 3.417, 6.833, -6.233, 1574.803, 2.000, 0.642, 0.000, 0.342, 2.500, 0.797, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -0.083, -48.333, 4.583, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -0.083, 48.333, 4.583, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -38.333, 0.000, 2.500, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 18.333, 0.000, 1.667, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
[WEIGHT_AND_BALANCE]
max_gross_weight= 23146.000
empty_weight= 12346.000
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= 170.000, 7.400, -1.800, 0.000
station_load.1= 170.000, -7.400, 1.800, 0.000
station_load.2= 4800.000, 0.000, 0.000, 0.000
;station_load.3=170, -4.2, -1.80, 0.0
;station_load.4=170, -2.0, 1.80, 0.0
;station_load.5=170, -2.0, -1.80, 0.0
;station_load.6=170, -0.8, 1.80, 0.0
;station_load.7=170, -0.8, -1.80, 0.0
;station_load.8=170, -3.4, 1.80, 0.0
;station_load.9=170, -3.8, -1.80, 0.0
;station_load.10=170, -6.0, 1.80, 0.0
;station_load.11=170, -6.0, -1.80, 0.0
;station_load.12=170, -8.0, 1.80, 0.0
;station_load.13=170, -8.0, -1.80, 0.0
;station_load.14=170, -10.3, 1.80, 0.0
;station_load.15=170, -10.3, -1.80, 0.0
;station_load.16=170, -13.7, 1.80, 0.0
;station_load.17=170, -13.7, -0.80, 0.0
;station_load.18=1020, -37.2, 0.0, 0.0
;station_load.19=170, -4.2, 1.80, 0.0
;Moments of Inertia
empty_weight_roll_MOI= 141677.000
empty_weight_pitch_MOI= 70636.000
empty_weight_yaw_MOI= 172848.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=0.7
induced_drag_scalar=0.7
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
[piston_engine]
power_scalar=1.0
cylinder_displacement= 410.700
compression_ratio= 6.000
number_of_cylinders= 9
max_rated_rpm= 2050.000
max_rated_hp= 725.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.050
turbocharged= 1
max_design_mp= 38.000
min_design_mp= 1.000
critical_altitude= 14500.000
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=1
idle_rpm_mechanical_efficiency_scalar=0.2
max_rpm_friction_scalar=4.5
idle_rpm_friction_scalar=0.0500000
[propeller]
thrust_scalar=1.0
propeller_type= 0
propeller_diameter= 10.400
propeller_blades= 2
propeller_moi= 33.700
beta_max= 45.500
beta_min= 12.500
min_gov_rpm= 1200.000
prop_tc= 0.010
gear_reduction_ratio= 1.700
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 1
min_rpm_for_feather= 700.000
beta_feather= 79.300
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[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
[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
autopilot=0, 5 , 17.0
avionics_bus=0, 0, 17.0
avionics=1, 0 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 0, 17.0
marker_beacon=1, 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_landing=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 0 , 17.0
[General]
performance=Length: 18,90 m ( 62 ft )\nWing span: 29,25 m ( 96 ft )\nWeight: 6500 kg emp.(12610 pf.) \nPower: 3x 725hp BMW\nAccomodation: Aircrew 4\nMulti-res model\nDesigner: Pierino Primavesi\nArtwork: Pierino Primavesi\nDate:April 2002\nVersion FS2002 \n
[fuel]
LeftMain= 0.000, -9.000, 0.000, 330.000, 0.000
RightMain= 0.000, 9.000, 0.000, 330.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
[airplane_geometry]
wing_area= 1189.400
wing_span= 95.900
wing_root_chord= 12.000
wing_dihedral= 6.500
wing_incidence= 0.000
wing_twist= 5.000
oswald_efficiency_factor= 0.700
wing_winglets_flag= 0
wing_sweep= 2.500
wing_pos_apex_lon= -2.200
wing_pos_apex_vert= 1.000
htail_area= 169.000
htail_span= 32.800
htail_pos_lon= -35.900
htail_pos_vert= 6.500
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 69.900
vtail_span= 8.500
vtail_sweep= 5.000
vtail_pos_lon= -39.400
vtail_pos_vert= 8.500
elevator_area= 57.850
aileron_area= 25.250
rudder_area= 43.000
elevator_up_limit= 17.000
elevator_down_limit= 15.500
aileron_up_limit= 18.000
aileron_down_limit= 18.000
rudder_limit= 30.000
elevator_trim_limit= 15.000
spoiler_limit= 60.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
[GeneralEngineData]
engine_type= 0
Engine.0= 8.333, -13.333, 1.250
Engine.1= 12.500, 0.000, 4.167
Engine.2= 8.333, 13.333, 1.250
fuel_flow_scalar= 1.000
[Reference Speeds]
flaps_up_stall_speed= 51.000
full_flaps_stall_speed= 41.000
cruise_speed= 105.000
[keyboard_response]
elevator=75.000000,120.000000
aileron=75.000000,120.000000
rudder=75.000000,120.000000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=600.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
[direction_indicators]
direction_indicator.0=1,0
[Views]
//eyepoint=7.891810,-1.699446,6.704022
eyepoint=8.1,-1.7,7.0
[LIGHTS]
light.0=5, 4.59, -4.00, -1.08, fx_landing ,
light.1=5, 4.59, 4.00, -1.08, 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, -24.51, 0.00, 1.21, fx_strobe ,
light.7=1, -38.48, 0.00, 15.25, fx_beacon ,
light.2=4, 9.84, 0.00, 6.30, fx_vclight ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[SMOKESYSTEM]
smoke.0=3.576,6.266,-12.598, fx_smoke_bju
smoke.1=4.50,12.86,-3.28, fx_smoke_bju
smoke.2=3.576,6.266,12.598, fx_smoke_bju
smoke.3=4.50,12.86,3.28, fx_smoke_bju
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 5.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 30.000, 0.000
flaps-position.3= 40.000, 0.000
[Radios]
Audio.1= 1
Com.1= 1, 0
Com.2= 1, 0
Nav.1= 1, 1, 1
Nav.2= 1, 1, 0
Adf.1= 1
Transponder.1= 1
Marker.1= 1
