[fltsim.0]
title=AirbusA300-B4600ST Airbus
sim=Boeing737-400
model=600st
panel=
sound=
texture=600st
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
ui_manufacturer=Airbus
ui_type=A300B4600ST Beluga
ui_variation=Airbus Industries
atc_heavy=1
atc_id=FWUAB
atc_type=Airbus
atc_model=A300
atc_airline=Airbus
atc_flight_number=1123
description=Airbus A300 B4600 converted into oversized Freighter. Only 5 build.

[WEIGHT_AND_BALANCE]
max_gross_weight = 150000                      // (pounds)
empty_weight = 74170                           // (pounds)

reference_datum_position     =  0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -5, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 =   "170.0,  41.0, -1.5,	0.0, Pilot"              //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)        
station_load.1 =   "170.0,  41.0,  1.5,	0.0, Kopilot"           //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2 =   "510.0,   0.0,  0.0,	0.0, Besatzung"               //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3 =  "1360.0,  25.5,  0.0,	0.0, Erste Klasse"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.4 =  "8160.0,  11.0,  0.0,	0.0, Sitz 3-10"         //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.5 =  "8160.0,  -10.0,  0.0,	0.0, Sitz 11-18"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.6 =  "7140.0, -30.5,  0.0,	0.0, Sitz 19-25"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.7 = "10000.0,  20.5,  0.0,	0.0, Gepck vorne"    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.8 =  "4000.0, -27.5,  0.0,	0.0, Gepck hinten"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

;Moments of Inertia
empty_weight_pitch_MOI  = 3172439
empty_weight_roll_MOI   = 2262183
empty_weight_yaw_MOI    = 3337024
empty_weight_coupled_MOI = 0

        
[contact_points]
point.0=1,   50.17,   0,   -13.6,   9181.1, 0, 1.442, 55.92, 0.6, 2.5, 0.9, 4.0, 4.0, 0, 220.0, 250.0
point.1=1,  -9.75,  -16.25,   -14.6,   9574.8, 1, 1.442,  0.00, 1.0, 2.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0
point.2=1,   -9.75,  16.25,   -14.6,   9574.8, 2, 1.442,  0.00, 1.0, 2.5, 0.9, 7.1, 7.1, 3, 220.0, 250.0
point.3=2,   -28.1,  -74.1,   2.6,   787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2,   -28.1,  74.1,   2.6,   787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2,   -79.7,   0,   1.3,   787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2,   56.4,   0,   1.3,   787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
point.7=5, -50.90, -19.250, -19.300, 1600, 0, 0.00, 70.0, 0.0,  0.0, 5.00, 3.0, 3.2, 0, 0.0, 0.0
point.8=5, -50.90,  19.250, -19.300, 1600, 0, 0.00, 70.0, 0.0,
max_number_of_points = 21

static_pitch=-0.94       //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=18.67   //feet, altitude of CG when at rest on the ground
gear_system_type=1      //Hydraulic


[LIGHTS]        
light.0 = 3, -101.42,   0.00,  9.40, fx_navwhih ,
light.1 = 2, -101.42,   0.00,  9.40, fx_strobeh ,
//Fuselageshort light.0 = 3, -95.74,   0.00,  9.40, fx_navwhih ,
//fuselageshort light.1 = 2, -95.74,   0.00,  9.40, fx_strobeh ,
light.2 = 1,  -31.14,   0.00, -7.05, fx_beaconb ,
light.3 = 1,   -9.77,   0.00,  27.02, fx_beaconh ,

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.9

[folding_wings]
wing_fold_system_type=4                    
fold_rates=0.11,0.13                         ;Percent per second

