[fltsim.0]
title=mz-d3a1
sim=mz-d3a1
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=NZMAN
ui_manufacturer= Aichi Kokuki KK
ui_type=D3A1 "Val"
ui_variation=Jogakusei Zen Nihongou
description=The Aichi was a carrier-borne bomber responsible for bombing the first targets at Pearl Harbor. Known as the Val to the Allies, the D3A1 had a tapered elliptical wing for aerodynamic efficiency. \nD3A1 (Aichi 99 Dive Bomber Type11 "Val") by Hagochu(Akemi Mizoguchi)\n Coverted to FS9 by R.A.Baum

[General]
atc_type=Aichi 99
atc_model=Val
editable=0
performance=Type:- Aichi D3A1 Dive Bomber\nEngine:-Mitusbishi Kinsei 43, 14 Cylinder Radial 1000 hp\nWingspan:-47 ft 2 in.\nLength:- 33 ft 5 1/2 in\nHeight:- 12 ft 7 1/2 in\nWeight:- 8,047 lb Loaded\nMax Speed:- 240 mph @ 9,840 ft.\nCeiling:- 30,050 ft.\nRange:- 915 miles\nArmament:- 3 Machine Guns; 813 lb. of Bombs



[WEIGHT_AND_BALANCE]
empty_weight = 5309.0				// (pounds)

reference_datum_position     =  0.0, 0, 0	// (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  0.0, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 = 170,  -1.5, 0.0, 1.5		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170,  -3.0, 0.0, 1.5		//Gunner          Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI =  6668.43	//slug-ft^2
empty_weight_roll_MOI  =  5725.72       //slug-ft^2
empty_weight_yaw_MOI   = 10186.09       //slug-ft^2
empty_weight_coupled_MOI=0.000000
max_gross_weight=8473.500000

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
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=140.710000
compression_ratio=6.600000
number_of_cylinders=14
max_rated_rpm=2500.000000
max_rated_hp=1000.000000
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.035000
turbocharged=1
max_design_mp=44.999999
min_design_mp=1.000000
critical_altitude=6500.000000
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]
thrust_scalar = 1.1
propeller_type=0
propeller_diameter=11.000000
propeller_blades=3
propeller_moi=34.940000
beta_max=50.000000
beta_min=18.000000
min_gov_rpm=1400.000000
prop_tc=0.010000
gear_reduction_ratio=1.429000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000

[exits]
number_of_exits = 1
exit_rate.0 = 0.4  				;Percent per second

[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0

[contact_points]
	//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
point.0=1, -22.80,   0.00, -1.69, 1600, 0, 0.25, 90.0, 0.30, 2.5, 0.90, 0.0, 0.0, 0
point.1=1,   1.55,  -5.72, -6.64, 2200, 1, 1.25,  0.0, 0.50, 2.5, 0.79, 0.0, 0.0, 2
point.2=1,   1.55,   5.72, -6.64, 2200, 2, 1.25,  0.0, 0.50, 2.5, 0.79, 0.0, 0.0, 3
point.3=2,   0.00, -20.00, -1.25, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5
point.4=2,   0.00,  20.00, -1.25, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6
point.5=2, -20.25,   0.00, -1.66, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9
point.6=2,   2.41,   0.00, -2.08, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4

static_pitch = 11.74		//degrees (pitch when loaded on ground)
static_cg_height = 6.36         //(feet) altitude of CG when at rest (altitude when loaded on ground)

[Views]
eyepoint=-2.54, 0.0, 2.90481   //(feet) longitudinal, lateral, vertical distance from reference datum

[folding_wings]
wing_fold_system_type = 4			;0=None
fold_rates = 0.12,0.11				;Percent per second

[TailHook]
tailhook_length=4				;(feet)
tailhook_position = -17.5, 0.0, 1.815		;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0

[flaps.0]
type=1								// 1 - tail, 2 - lead
span-outboard=0.125					// 0.0 .. 1.0
extending-time=5					// seconds
flaps-position.0=0					// degrees, KIAS
flaps-position.1=10					// degrees, KIAS
flaps-position.2=20					// degrees, KIAS
flaps-position.3=30					// degrees, KIAS
damaging-speed=203					// KIAS
blowout-speed=307					// KIAS

[forcefeedback]
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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=2500000 ; in microseconds


[General]
performance=Ž©dF2408‚‹‚‡\n‘S’·F10.2‚\n‘S•F14.36‚\nÅ‘呬“xF390‚‹‚\/‚ˆ\næˆõF2–¼\n•‘•F‹@e@7.7‚‚~3\n@@@@”š’e@250‚‹‚‡~1@60‚‹‚‡~2\n
[fuel]
Center1=-2.000000,0.000000,-2.000000,247.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=370.000000
wing_span=47.166667
wing_root_chord=8.333333
wing_dihedral=7.399292
wing_incidence=0.999756
wing_twist=0.000000
oswald_efficiency_factor=0.698501
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=24.000000
htail_span=11.000000
htail_pos_lon=-18.833333
htail_pos_vert=0.000000
htail_incidence=-0.999756
htail_sweep=0.000000
vtail_area=15.000000
vtail_span=4.415880
vtail_sweep=0.000000
vtail_pos_lon=-18.833333
vtail_pos_vert=0.583333
elevator_area=13.000000
aileron_area=20.400000
rudder_area=13.060000
elevator_up_limit=26.000825
elevator_down_limit=26.000825
aileron_up_limit=21.497376
aileron_down_limit=20.345731
rudder_limit=28.997394
elevator_trim_limit=19.996227
spoiler_limit=59.988681
spoilerons_available=1
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[GeneralEngineData]
engine_type=0
Engine.0=8.500000,0.000000,0.000000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000
[Reference Speeds]
flaps_up_stall_speed=64.000000
full_flaps_stall_speed=51.200000
cruise_speed=182.992812
max_indicated_speed=760.500000
[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
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
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556
[stall_warning]
type=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=1,0