[fltsim.0]
title=AH-64J
sim=AH-64J
model=
panel=
sound=
texture=
checklists=
description=The original Hughes model 77 entered the US Army competition for a Advanced Attack Helicopter (AAH).  Having been successful it was selected by the US Army in December 1976 and formally named the Apache in 1981.\n  There are around 827 in service with the US Army to date of varying types. \n
atc_airline=Army
atc_id=20035
atc_flight_number=110
ui_manufacturer=
ui_type=AH-64
ui_variation=AH-64J

atc_heavy=0

[General]
atc_type=BOEINGHELICOPTER
performance=Cruise Speed \t\n115 kts            132 mph          213 km\/h\n\nEngine\nAllison 250-C20J   420 shp\n\nMaximum Range\n435 nm   \t        500 m            805 km\n\nService Ceiling\n20,000 ft        6,096 m\n\nHovering Ceiling\n19,600            5,974 m\n\nFuel Capacity\n91 U.S. gal       344 L\n\nEmpty Weight\n1,640 lb           744 kg\n\nMaximum Gross Weight\n3,200 lb          1,451 kg\n\nMaximum Gross Weight (External Loading)\n3,350 lb          1,519 kg\n\nLength\t\n31.2 ft\t         9.51 m\n\nRotor Span\n33.3 ft\t         10.15 m\n\nHeight\n11.7 ft\t         3.51 m\n\nSeating \t\nUp to 5 \n\nUseful Load\t\n1,498 lb\t          679 kg\n
editable=1
atc_model=


[WEIGHT_AND_BALANCE]
max_gross_weight=13200.000
empty_weight=2100.000

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=0.000000,0.000000,0.000000,0.000000
station_load.1=0,  0.0, 0.0, 0.0              //Co-Pilot        Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)


;Moments of Inertia
empty_weight_pitch_MOI=6000.000
empty_weight_roll_MOI=4000.000
empty_weight_yaw_MOI=10000.000
empty_weight_coupled_MOI=0.000
CG_forward_limit=0.000
CG_aft_limit=1.000

[turboprop_engine]
power_scalar=1.0

[propeller]
thrust_scalar=1.0

[Helicopter]
low_realism_stability_scale=1.0, 1.0, 1.0             //Pitch , Bank, Yaw Scalars on Stability in Low Realism Settings

[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
gear_motor=0, 5 , 17.0
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



//0  Class                        <0=none,1=wheel, 2=scrape, 3=skid>
//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
//14 Airspeed limit for retraction     (KIAS)
//15 Airspeed that gear gets damage at (KIAS)

[contact_points]
point.0=1.000, -14.167, 0.000, -2.000, 1652.034, 0.000, 0.587, 40.200, 0.410, 2.500, 2.361, 3.000, 3.000, 0.000, 0.000, 0.000
point.1=1.000, 2.500, -7.333, -4.000, 1652.034, 1.000, 0.587, 0.000, 0.793, 2.500, 1.448, 3.000, 3.000, 2.000, 0.000, 0.000
point.2=1.000, 2.500, 7.333, -4.000, 1652.034, 2.000, 0.587, 0.000, 0.793, 2.500, 1.448, 3.000, 3.000, 3.000, 0.000, 0.000
point.3=2.000, 0.917, -20.917, 7.583, 0.000, 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, 0.917, 20.917, 7.583, 0.000, 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, -21.333, 0.000, 6.250, 787.402, 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, 12.500, 0.000, 6.250, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=0.000
static_cg_height=4.267

[Views]
eyepoint=6.471969,0.000000,5.613312

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

[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.
//NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque
elevator=100,  180
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=3,0

 [EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks

[fuel]
Center1=0.000, 0.000, 0.000, 91.000, 0.000
fuel_type=2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1


[GeneralEngineData]
engine_type=3
Engine.0=8.300, 0.000, 0.400
fuel_flow_scalar=1.000000

[Reference Speeds]
flaps_up_stall_speed=0.0                   //Knots True (KTAS)
full_flaps_stall_speed=0.0                   //Knots True (KTAS)
cruise_speed=115.0                 //Knots True (KTAS)

[autopilot]
autopilot_available=0
flight_director_available=0