[fltsim.0]
title=AI C-124
sim=Boeing737-400
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Douglas
ui_type=C-124 C
ui_variation=
description=Douglas C-124 AIP.2a, only ai model
atc_heavy=0
atc_id=20976
atc_airline=AIR FORCE
atc_flight_number=20976


[General]
performance=Four P&W R-2800-CB16\neach 2400hp for take off\n1800hp METO to 8500feet\n1700hp to 14,500 feet
atc_type=DOUGLAS
atc_model=C-124 C

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0 //original = 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

[WEIGHT_AND_BALANCE]
;load assumed symetrical versus CoG 

reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=2
empty_weight=93200	//orig=63200		;including oil, catering etc.
station_load.0=1000,0,0,0		;5 crew and bags
station_load.1=10000,0,0,0		;50 pax and bags (maximum payload with full fuel)

max_gross_weight=103800			;with -CB16 engines or 107,000 with -CB17

;103800 - 29600 fuel=74200 and 74200 - 63200 = 11000 / 200 = 55 crew plus pax plus bags

;default ramp weight is 103,800lbs with max fuel and weight limited payload

;MLW=88,200 with -CB16 engines and MTOW originally only 100,000lbs

;Moments of Inertia
;
empty_weight_roll_MOI=1920000
empty_weight_pitch_MOI=805000
empty_weight_yaw_MOI=2640000
empty_weight_coupled_MOI=0.0

[fuel]
;max fuel 4934 USG=29600lbs with -CB16 engines
;
LeftMain=0,-15,0,1414,0
RightMain=0,15 ,0,1414,0
Leftaux=0,-15,0,1053,0
Rightaux=0,15 ,0,1053,0
fuel_type=1.000000
number_of_tank_selectors=1

[GeneralEngineData]
engine_type=0
Engine.0=8.33,-11.5,-0.41
Engine.1=6.91,-8.83,-0.83
Engine.2=6.91,8.83,-0.83
Engine.3=8.33,11.5,-0.41
fuel_flow_scalar=0.97

[piston_engine]
;
;P&W R-2800-CB16=2400bhp for take off & 1800bhp at 8500 feet (low blower = METO) and 1700bhp at 14500 feet (high blower)
;
cylinder_displacement=155.78
compression_ratio=6.7
number_of_cylinders=18
max_rated_rpm=2800.000000		;for take off only
max_rated_hp=2000.000000		;for take off only
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.035000	
turbocharged=1
max_design_mp=59.5			
min_design_mp=5.0			
critical_altitude=5000              
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=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
propeller_type=0
propeller_blades=3
gear_reduction_ratio=1.0			
propeller_diameter=8.8				
propeller_moi=26.8				
beta_max=65.0					
beta_min=15.0					
prop_sync_available=1                         
prop_deice_available=1                       
prop_feathering_available=1    
prop_reverse_available=0                                
min_rpm_for_feather=700.0                       
beta_feather=96.0                               
power_absorbed_cf=0.9                           
minimum_on_ground_beta=15.0				
minimum_reverse_beta=0                  
defeathering_accumulators_available=0            
prop_auto_feathering_available=1              
min_gov_rpm=650.000000
prop_tc=0.010000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000

[airplane_geometry]
oswald_efficiency_factor=0.8
wing_area=1463  //original = 1463
wing_span=117.5
wing_root_chord=12.45
wing_dihedral=7.0
wing_incidence=4.0
wing_twist=0.0
htail_area=180.0
htail_span=37
htail_pos_lon=-38
htail_pos_vert=0.0
htail_incidence=0.0
htail_sweep=0.0
htail_area=210.9
vtail_area=93.4
vtail_span=19
vtail_sweep=0.0
vtail_pos_lon=-36
vtail_pos_vert=3
wing_winglets_flag=0
wing_sweep=0.0
wing_pos_apex_lon=0.0
wing_pos_apex_vert=0.0
elevator_area=108.9
aileron_area=43.82
rudder_area=49
elevator_up_limit=27.5
elevator_down_limit=20.0
aileron_up_limit=19.5
aileron_down_limit=15.0
rudder_limit=23.5
elevator_trim_limit=19.5
spoiler_limit=60.0			 ;for cowl flap drag
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[Flaps.0]
type=1
span-outboard=0.5
extending-time=40.0
flaps-position.0=0,0
flaps-position.1=10,174
flaps-position.2=20,174
flaps-position.3=30,174
flaps-position.4=40,152
flaps-position.5=50,152
lift_scalar=1
drag_scalar=0.9
pitch_scalar=1.0

[autopilot]
autopilot_available=1
use_no_default_bank=1
use_no_default_pitch=1 
flight_director_available=0
default_vertical_speed=100		 ;default is zero IRL - 100 is closest available value in FS2002
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=0.000000
pitch_takeoff_ga=8.000000

[Reference Speeds]		;all KIAS - Pitot error not known so IAS set=CAS
flaps_up_stall_speed=135  //orig=115
full_flaps_stall_speed=81
cruise_speed=230

[exits]
number_of_exits=1
exit_rate.0=0.1

[Radios]
Audio.1=1
Com.1=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[contact_points]

static_pitch=0.5
static_cg_height=8.3

point.0=1,30.5 ,0.00,-8.5,1800,0,0.83,52,0.39,2.5,0.90,10,10,0,174,174
point.1=1,-2.5,-12.4,-8.3,1500,1,0.83,0 ,0.39,2.5,0.55,10,10,2,174,174
point.2=1,-2.5,12.40,-8.3,1500,2,0.83,0 ,0.39,2.5,0.55,10,10,3,174,174

point.3=2,-5.166667,-57,3.5,1574,0,0,0,0,0,0,0,0,5,0,0
point.4=2,-5.166667, 57,3.5,1574,0,0,0,0,0,0,0,0,6,0,0
point.5=2,-56.833333,0,-1.2,1574,0,0,0,0,0,0,0,0,9,0,0
point.6=2,30.5,0,-0.66,1574,0,0,0,0,0,0,0,0,4,0,0

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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit 5= landing
light.0=3,  -4.4, -58.61, 3.78, fx_navred
light.1=3,  -4.4,  58.61, 3.78, fx_navgre
light.2=3, -67.45,   0.00, 2.35, fx_navwhi
light.3=1, -58.52,   0.00, 20.40, fx_beacon
light.4=5, -9.8, -18.5, -1.3, fx_landing
light.5=5, -9.8, 18.5, -1.3, fx_landing

[SMOKESYSTEM]
smoke.0=-0.417, 6.333, -26.500, fx_smoke_w
smoke.1=-0.833, 4.917, -13.833, fx_smoke_w
smoke.2=-0.833, 4.917, 13.833, fx_smoke_w
smoke.3=-0.417, 6.333, 26.500, fx_smoke_w

[direction_indicators]
direction_indicator.0=1,0

[keyboard_response]
elevator=450.000000,1000.000000
aileron=450.000000,1000.000000
rudder=450.000000,1000.000000

[Views]
eyepoint=0.000000,0.000000,0.000000