[fltsim.0]
title=AA-5A
sim=AA-5A
model=
panel=
sound=
texture=
panel_alias =
sound_alias =
kb_checklists=
kb_reference=
atc_id= N26118
atc_id_color=0x00000000
atc_parking_code =
atc_airline=
atc_flight_number=
ui_manufacturer=Grumman American
ui_type=AA-5A
ui_variation=U.S. Civil Register
description=First introduced in 1974, the AA-5 series were unique in their bonded honeycomb airframes, producing a simple, smooth, and strong structure. With a sliding canopy and quick controls, the AA-5 were a breed apart. The later AA-5B series had more powerful engines, giving a needed boost in performance. 
ui_typerole="Single Engine Prop"
ui_createdby="Piglet's Peculiar Planes"
visual_damage=1
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0

[CameraDefinition.0]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0, 2.0, -3.9
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title = "Nose"
Guid = {8A1987D0-09B6-7E48-B4E1-62C5DBE2A720}
Description =Looking back from the nose of the engine toward the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0, 1.1, 4.0
InitialPbh = 20, 0, 180
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum

[CameraDefinition.2]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 6, 0.3, 0
InitialPbh = 0, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.3]
Title = "Left Wing"
Guid = {7a91803e-898b-435a-8391-725be6a48203}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -6, 0.3, 0
InitialPbh = 0, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[General]
atc_type=Grumman 
atc_model=AA-5A 
performance=+ Empty Weight: 1200 lbs + Max Power: 115 Hp + Maneuver speed: 75 mph @ 2.0 g + Max speed: 130 mph @ 5000 ft + Max speed at sea-level: 130 mph + Climb rate: 1750 ft/min @ 55 mph Flight Dynamics By: Tim Piglet Conrad Piglet's Peculiar Planes FD Build 12 - 4/20/05 11:08 PM Flight Dynamics Workbook V3.00.03                                                
editable=1 
prop_anim_ratio = 1
Category=airplane

[pitot_static]
vertical_speed_time_constant = 2
pitot_heat=1.000000

[weight_and_balance]

// ACM V2.5
max_gross_weight =2200.0
empty_weight =1360.00000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.000, 0.000, 0.000
empty_weight_pitch_MOI =813.00000
empty_weight_roll_MOI =722.00000
empty_weight_yaw_MOI =1264.00000
empty_weight_coupled_MOI =0.00000
CG_forward_limit = 0
CG_aft_limit = 1
max_number_of_stations =2
station_load.0= 170, -0.510, -0.750, 0.000, Pilot
station_load.1= 170, -0.510, 0.750, -0.030, Passenger



[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 0.59, -15.49, -0.03, fx_navred
light.1 = 3, 0.59, 15.49, -0.03, fx_navgre
light.2 = 1, -12.85, 0, 5.15, fx_beacon
light.3 = 2, 0.36, -15.54, -0.02, fx_strobe
light.4 = 2, 0.35, 15.44, -0.03, fx_strobe
light.5 = 3, -14.80, 0, 0.31, fx_navwhi
light.6 = 4, -0.48, 0, 0.33, fx_vclight_deepred

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type =0
fuel_flow_scalar =1.00000
min_throttle_limit = 0
engine.0 =5.400, 0.000, 0.100

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

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type =1
number_of_tank_selectors =1
electric_pump =1

LeftMain = -0.350, -4.340, -1.080, 26.000, 0.000
RightMain = -0.350, 4.340, -1.080, 26.000, 0.000


[contact_points]
static_pitch = 0.000
static_cg_height = 3.820
tailwheel_lock =0
gear_system_type =4
max_number_of_points =7
point.0= 1, 5.741, 0.000, -3.698, 1800, 0, 0.500, 40.000, 0.150, 1.500, 0.800, 0.000, 0.000, 0
point.1= 1, -0.691, -3.819, -3.724, 1800, 1, 0.600, 0.000, 0.250, 1.300, 0.700, 0.000, 0.000, 2
point.2= 1, -0.691, 3.858, -3.724, 1800, 2, 0.600, 0.000, 0.250, 1.300, 0.700, 0.000, 0.000, 3
point.3= 2, 0.000, -15.627, -0.276, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, 0.000, 15.627, -0.276, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, 3.550, 0.000, -3.070, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.6= 2, -13.361, 0.000, -0.418, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9



[keyboard_response]
elevator = 350, 500
aileron = 450, 1000
rudder = 200, 1000


[forcefeedback]
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 =500
gear_bump_right_duration =250000
ground_bumps_magnitude1 =3250
ground_bumps_angle1 =8900
ground_bumps_intercept1 =5
ground_bumps_slope1 =0.48
ground_bumps_magnitude2 =750
ground_bumps_angle2 =9100
ground_bumps_intercept2 =0.075
ground_bumps_slope2 =1
crash_magnitude1 =10000
crash_direction1 =1000
crash_magnitude2 =10000
crash_direction2 =9000
crash_period2 =75000
crash_duration2 =2500000
stick_shaker_magnitude =5000
stick_shaker_direction =0
stick_shaker_period =111111

[airplane_geometry]
//ACM_AREAW1// 0.0335,0.0335,-0.6041,1.0576,0.5856,0.5856,-0.5817,1.0455,0.9116,0.9116
//ACM_AREAW2// -0.3356,0.9024,1.6896,1.6896,-0.3356,0.8988,2.3505,2.3505,-0.3356,0.9115
//ACM_AREAW3// 2.6452,2.6452,-0.3468,0.9160,3.1078,3.1078,-0.3580,0.9203,4.5206,4.5206
//ACM_AREAW4// -0.3520,0.9084,4.6422,4.6422,-0.3222,0.8966,4.7415,4.7415,-0.1901,0.8847
//ACM_AREAH1// 0.1080,0.1080,-0.0405,0.0047,0.2288,0.2288,-0.6799,0.0016,0.3137,0.3137
//ACM_AREAH2// -0.4142,0.0078,0.4346,0.4346,-0.4142,0.0046,0.5735,0.5735,-0.4142,0.0064
//ACM_AREAH3// 0.7347,0.7347,-0.4142,0.0078,0.8557,0.8557,-0.4187,0.0050,0.9539,0.9539
//ACM_AREAH4// -0.4142,0.0156,1.2866,1.2866,-0.4097,0.0082,1.6461,1.6461,-0.4007,0.0141
//ACM_AREAV1// -0.0035,-0.0035,0.0989,0.1219,0.3262,0.3262,-2.3466,0.1348,0.3702,0.3702
//ACM_AREAV2// -0.5018,0.1370,0.4246,0.4246,-0.4382,0.1325,0.5956,0.5956,-0.3887,0.1315
//ACM_AREAV3// 0.7666,0.7666,-0.3110,0.1337,0.9306,0.9306,-0.2544,0.1292,1.1686,1.1686
//ACM_AREAV4// -0.1802,0.1245,1.2090,1.2090,-0.1555,0.3707,1.2919,1.2919,-0.0811,0.3281
//ACM_CAREAW1// 2.7461,2.7461,0.6154,0.9097,2.9972,2.9972,0.6111,0.8993,3.2076,3.2076
//ACM_CAREAW2// 0.6152,0.9080,3.3985,3.3985,0.6152,0.8976,3.6106,3.6106,0.6111,0.9067
//ACM_CAREAW3// 3.7729,3.7729,0.6111,0.9091,3.9157,3.9157,0.6070,0.9116,4.0454,4.0454
//ACM_CAREAW4// 0.6152,0.9074,4.2363,4.2363,0.6152,0.9101,4.4745,4.4745,0.6152,0.9254
//ACM_CAREAH1// 0.0872,0.0872,0.0065,0.3622,0.2219,0.2219,0.0259,0.3669,0.2984,0.2984
//ACM_CAREAH2// 0.0211,0.3764,0.3847,0.3847,0.0162,0.3764,0.5001,0.5001,0.0114,0.3667
//ACM_CAREAH3// 0.6443,0.6443,0.0065,0.3666,1.2058,1.2058,0.0162,0.3760,1.6361,1.6361
//ACM_CAREAH4// 0.0211,0.3760,1.6499,1.6499,-0.4007,0.3760,1.7167,1.7167,-0.3619,0.3760
//ACM_CAREAV1// 0.0122,0.0122,0.1428,0.4778,0.1674,0.1674,0.1428,0.4723,0.2504,0.2504
//ACM_CAREAV2// 0.1387,0.4675,0.3190,0.3190,0.1346,0.4628,0.4414,0.4414,0.1346,0.4432
//ACM_CAREAV3// 0.5692,0.5692,0.1346,0.4324,0.6766,0.6766,0.1387,0.4247,0.8011,0.8011
//ACM_CAREAV4// 0.1387,0.4140,1.0507,1.0507,0.1387,0.3978,1.1774,1.1774,0.1346,0.3811
wing_area =140.10000
wing_span =31.50000
wing_root_chord =4.50000
wing_dihedral =5.00000
wing_incidence =0.00000
wing_twist =0.00000
oswald_efficiency_factor =0.84894
wing_winglets_flag =0
wing_sweep =0.00000
wing_pos_apex_lon =1.11196
wing_pos_apex_vert =-1.25000
htail_area =13.83000
htail_span =11.50000
htail_pos_lon =-13.40000
htail_pos_vert =0.00000
htail_incidence =0.00000
htail_sweep =0.00000
vtail_area =9.64000
vtail_span =4.28000
vtail_sweep =8.00000
vtail_pos_lon =-13.07000
vtail_pos_vert =0.70000
elevator_area =13.00000
aileron_area =9.20000
rudder_area =3.74000
elevator_up_limit =30.00000
elevator_down_limit =20.00000
aileron_up_limit =15.00000
aileron_down_limit =15.00000
rudder_limit =30.00000
elevator_trim_limit =18.00000
spoiler_limit =0.00000
aileron_to_spoileron_gain =0.00000
spoiler_handle_available = 0
min_ailerons_for_spoilerons =0.00000
min_flaps_for_spoilerons =0.00000
spoilerons_available =0
auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.799145
negative_g_limit_flaps_up=-3.199786
negative_g_limit_flaps_down=-2.399573

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 160
engine_generator_map = 1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
starter3 = 0, 20, 17
starter4 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
prop_sync = 0, 15, 17
auto_feather = 0, 15, 17
auto_brakes = 0, 15, 17
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17

[flight_tuning]
cruise_lift_scalar=1.00000 
parasite_drag_scalar=1.00000 
induced_drag_scalar=1.00000 
elevator_effectiveness=1.00000 
aileron_effectiveness=1.00000 
rudder_effectiveness=1.00000 
pitch_stability=1.00000 
roll_stability=1.00000 
yaw_stability=1.00000 
elevator_trim_effectiveness=1.00000 
aileron_trim_effectiveness=1.00000 
rudder_trim_effectiveness=1.00000 
hi_alpha_on_roll =1.00000
hi_alpha_on_yaw =1.00000
p_factor_on_yaw =1.00000
torque_on_roll =1.00000
gyro_precession_on_roll =1.00000
gyro_precession_on_yaw =1.00000

[piston_engine]
power_scalar=1.00000 
cylinder_displacement=90.00000 
compression_ratio=8.50000 
number_of_cylinders=4 
max_rated_rpm=2700.00000 
max_rated_hp=180.00000 
fuel_metering_type=1 
cooling_type=0 
normalized_starter_torque=0.32000 
turbocharged=0 
max_design_mp=29.92000 
min_design_mp=9.00000 
critical_altitude=0.00000 
emergency_boost_type=0 
emergency_boost_mp_offset=0.00000 
emergency_boost_gain_offset=0.00000 
fuel_air_auto_mixture=0 
auto_ignition=0 
emergency_boost_duration=0.00000 
max_rpm_mechanical_efficiency_scalar=1.00000 
idle_rpm_mechanical_efficiency_scalar=1.00000 
max_rpm_friction_scalar=1.00000 
idle_rpm_friction_scalar=1.00000 

[propeller]
thrust_scalar=1.00000 
propeller_type=1 
propeller_diameter=6.00000 
propeller_blades=2 
propeller_moi=3.10000 
beta_max=26.00000 
beta_min=24.00000 
min_gov_rpm=420.00000 
prop_tc=0.01000 
gear_reduction_ratio=1.00000 
fixed_pitch_beta=25.00000 
low_speed_theory_limit=77.91534 
prop_sync_available=0 
prop_deice_available=1 
prop_feathering_available=0 
prop_auto_feathering_available=0 
min_rpm_for_feather=700.00000 
beta_feather=88.50000 
power_absorbed_cf=0.90000 
defeathering_accumulators_available=0 
prop_reverse_available=0 
minimum_on_ground_beta=1.00000 
minimum_reverse_beta=-14.00000 
rotation = 1

[Views]
eyepoint=-.64, -0.88, 1.71 

[flaps.0]       //Trailing Edge Flaps
type= 1
system_type=0
span-outboard= 0.500
extending-time= 5.0
damaging-speed=347.0
blowout-speed=354.0
flaps-position.0=0.00
flaps-position.1=15.00
flaps-position.2=30.00
flaps-position.3=45.00
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=1.00

[Radios] // 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 

[direction_indicators]
direction_indicator.0=1, 0 

[exits]
number_of_exits = 2
exit_rate.0 = 0.8
exit_rate.1 = 0.8

[autopilot]
autopilot_available=1 
use_no_default_bank =1
use_no_default_pitch =1
flight_director_available=0 
default_vertical_speed=1000.00000 
autothrottle_available=0 
autothrottle_arming_required =0
autothrottle_takeoff_ga =1.00000
autothrottle_max_rpm =90.00000
pitch_takeoff_ga=8.00000 
default_pitch_mode =0
default_bank_mode =0
max_pitch =10.00000
max_pitch_acceleration =1.00000
max_pitch_velocity_lo_alt =2.00000
max_pitch_velocity_hi_alt =1.50000
max_pitch_velocity_lo_alt_breakpoint =20000.00000
max_pitch_velocity_hi_alt_breakpoint =28000.00000
max_bank=25.00000
max_bank_acceleration =1.80000
max_bank_velocity =3.00000
max_throttle_rate =0.10000
nav_proportional_control =9.00000
nav_integrator_control =0.25000
nav_derivative_control =0.00000
nav_integrator_boundary =2.50000
nav_derivative_boundary =0.00000
gs_proportional_control =9.52000
gs_integrator_control =0.26000
gs_derivative_control =0.00000
gs_integrator_boundary =0.70000
gs_derivative_boundary =0.00000
yaw_damper_gain =0.00000

[Reference Speeds]
flaps_up_stall_speed=48.74956 
full_flaps_stall_speed=46.05574 
cruise_speed=120.78769 
max_indicated_speed =175.00000
max_mach =0.22300

[gear_warning_system]
gear_warning_available =1
pct_throttle_limit =0.10000
flap_limit_idle =33.75000
flap_limit_power =16.87500
[brakes]
toe_brakes_scale =0.75000
parking_brake = 1
[stall_warning] //  0 = None, 1 = Suction, 2 = Electric.
type = 1
stick_shaker=1
[hydraulic_system]
electric_pumps = 0
engine_map = 1, 0, 0, 0
normal_pressure =1000.00000
[attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0 = 1, 0
[direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind
direction_indicator.0=1, 0 

[airspeed_indicators]
airspeed_indicator.0 = 1, 0
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=4.900000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[deice_system]
structural_deice_type=2
[smokesystem]
smoke.0=0
[AirWrench]
Aircraft_Length=22.00000
Vmax_sl=148.00000
Vmax_ca=148.00000
V_rc=60.90000
Climb_Rate=853.70000
Climb_Weight=2012.00000
Max_gforce=4.00000
Emergency_hp=180.00000
nose_position_lon=9.37000
ActualIncidence=1.00000
ActualTwist=0.00000
ActualTailIncidence=0.00000
Aircraft_Type=2
FlowCorrection=1.00000
Power_Correction=1.11111
JetAltitude=0.00000
turboprop_critical_altitude=0.00000
target_roll_Vopt=336.70000
target_roll_rate=63.50000
pitch_damping=1.00000
yaw_damping=1.00000
elevator_scalar=1.00000
rudder_scalar=1.00000
dihedral_scalar=1.00000
Elevator_FF=50.00000
Aileron_FF=-50.00000
Roll_Response=30.00000
Adverse_Yaw=100.00000
Control_Response=40.00000
V_Max_Control=149.60127
V_Zero_Control=299.20254
Spin_Stability=100.00000
Stall_Stability=100.00000
Elevator_Propwash=1.00000
Rudder_Propwash=1.00000
spoiler_time=0.00000
afterburner_thrust=0.00000
mach_scale=1.00000
spoiler_type=0
spoiler_cd=0.00000
spoiler_cl=0.00000
spoiler_cm=0.00000
flaps_type=1
flaps_cd_scalar=0.93177
flaps_cm_scalar=0.00000
vfe_enabled=0
gear_cd_scalar=0.00000
gear_cm_scalar=0.00000
cylinder_head_temperature=501.00000
exhaust_gas_temperature=1201.00000
fuel_pressure=20.00000
oil_pressure=60.00000
oil_temperature=241.00000
radiator_temperature=211.00000
exhaust_pressure_ratio=0.00000
interstage_turbine_temperature=-459.00000
knots_flag=0
cfs1_flag=0
laminar_flow=0
fixed_wing_pos=0
AirWrenchVersion=1.01.34
cfs2_ai_flag=0
fs8_flag=1
direct_edit_mach=0