[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