[fltsim.0]
title=Grumman Goose
sim=goose
model=
panel=
sound=
texture=
panel_alias =
sound_alias =
kb_checklists=
kb_reference=
atc_id=NTEP
ui_manufacturer=Grumman
ui_type=G21 Goose
ui_variation=Private
description=Enter your description here.
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=Grumman
atc_model=G21
editable=1
performance=Enter your performance information here.
[WEIGHT_AND_BALANCE]
max_gross_weight = 8000.00
empty_weight = 5425.00
reference_datum_position = 0.00, 0.00, 0.00
empty_weight_CG_position = 0.00, 0.00, 0.00
max_number_of_stations = 50
station_load.0 = 800.00, 0.00, 0.00, 0.00
station_load.4 = 0, -12.67, -1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 0, -12.67, 1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 0, -15.00, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 20000.00
empty_weight_roll_MOI = 13000.00
empty_weight_yaw_MOI = 26000.00
empty_weight_coupled_MOI= 0.00
CG_forward_limit= 0.00
CG_aft_limit= 1.00
[flight_tuning]
cruise_lift_scalar =1.00
parasite_drag_scalar =1.00
induced_drag_scalar =1.00
elevator_effectiveness =1.00
aileron_effectiveness =1.00
rudder_effectiveness =1.00
pitch_stability =1.00
roll_stability =1.00
yaw_stability =1.00
elevator_trim_effectiveness =1.00
aileron_trim_effectiveness =1.00
rudder_trim_effectiveness =1.00
[GeneralEngineData]
engine_type = 0
Engine.0 = 6.90,-7.0, 2.90
Engine.1 = 6.90, 7.0, 2.90
fuel_flow_scalar = 0.90
min_throttle_limit=-0.250
[piston_engine]
power_scalar =1.00
cylinder_displacement= 109.0
compression_ratio= 6.00
number_of_cylinders= 9
max_rated_rpm= 2200.00
max_rated_hp= 450.00
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.30
turbocharged= 0
max_design_mp= 0.00
min_design_mp= 0.00
critical_altitude= 0.00
emergency_boost_type= 0
emergency_boost_mp_offset= 0.00
emergency_boost_gain_offset= 0.00
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.00
idle_rpm_mechanical_efficiency_scalar=1.00
max_rpm_friction_scalar=1.00
idle_rpm_friction_scalar=1.00
[propeller]
thrust_scalar =1.00
propeller_type= 0
propeller_diameter= 8.00
propeller_blades= 3
propeller_moi= 13.00
beta_max= 45.00
beta_min= 15.20
min_gov_rpm= 1100.00
prop_tc= 0.100
gear_reduction_ratio= 1.00
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.00
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.00
beta_feather= 82.50
power_absorbed_cf= 0.90
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.00
minimum_reverse_beta= 0.00
[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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
//GEAR
point.0 = 1, -14.30, 0.00, -3.40, 3200.00, 0.00, 0.50, 40.00, 0.20, 2.50, 0.95, 3.00, 3.00, 0.00, 0.00, 0.00
point.1 = 1, 2.50, -3.50, -5.70, 3200.00, 1.00, 1.10, 0.00, 0.30, 2.50, 0.850, 4.10, 4.30, 2.00, 0.00, 0.00
point.2 = 1, 2.50, 3.50, -5.70, 3200.00, 2.00, 1.10, 0.00, 0.30, 2.50, 0.850, 4.30, 4.10, 3.00, 0.00, 0.00
//SCRAPES
point.3= 2, 0.00, -22.00, 2.00, 3200.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00
point.4= 2, 0.00, 22.00, 2.00, 3200.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00
point.5= 2, -22.00, 0.00, 2.00, 3200.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00
point.6= 2, 12.00, 0.00, 0.00, 3200.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
static_pitch = 7.00
static_cg_height = 5.00
point.7= 4, 4.00, -2.00, -4.50, 10000.00, 0.00, 0.00, 0.00, 1.00, 2.50, 0.650, 0.00, 0.00, 0.00, 0.00, 0.00
point.8= 4, 4.00, 2.00, -4.50, 10000.00, 0.00, 0.00, 0.00, 1.00, 2.50, 0.650, 0.00, 0.00, 1.00, 0.00, 0.00
point.9= 4, -2.00, 0.00, -4.00, 10000.00, 0.00, 0.00, 0.00, 1.00, 2.50, 0.650, 0.00, 0.00, 1.00, 0.00, 0.00
point.10= 4, -12.00, 0.00, -3.00, 10000.00, 0.00, 0.00, 0.00, 1.00, 2.50, 0.650, 0.00, 0.00, 1.00, 0.00, 0.00
point.11= 4, -2.50, -16.00, -2.0, 10000.00, 0.00, 0.00, 0.00, 1.00, 2.50, 0.650, 0.00, 0.00, 1.00, 0.00, 0.00
point.12= 4, -2.50, 16.00, -2.0, 10000.00, 0.00, 0.00, 0.00, 1.00, 2.50, 0.650, 0.00, 0.00, 1.00, 0.00, 0.00
gear_system_type=0
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[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
[Views]
eyepoint = 3.70, -1.20, 1.30 //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, 0.10, -24.58, 3.05, fx_navred ,
light.1 = 3, 0.10, 24.58, 3.05, fx_navgre ,
light.2 = 3, -20.10, 0.00, -0.50, fx_navwhi ,
light.3 = 2, 0.20, -24.58, 3.05, fx_strobe ,
light.4 = 2, 0.20, 24.58, 3.05, fx_strobe ,
light.5 = 1, -20.67, 0.00, 8.65, fx_beacon ,
light.7 = 4, 3.55, 0.00, 2.32, fx_vclight,
[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.
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[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
[fuel]
LeftMain = 0.00,-6.450, 0.00, 71.00, 0.00
RightMain = 0.00, 6.450, 0.00, 71.00, 0.00
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=1
[EFFECTS]
wake=fx_wake
water=fx_spray
//water=fx_waterland
dirt=fx_dirt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[airplane_geometry]
wing_area = 375.00
wing_span = 49.00
wing_root_chord = 9.50
wing_dihedral = 2.00
wing_incidence = 1.00
wing_twist = -1.00
oswald_efficiency_factor= 0.80
wing_winglets_flag = 0
wing_sweep = 1.00
wing_pos_apex_lon = 2.70
wing_pos_apex_vert = 2.50
htail_area = 72.00
htail_span = 17.00
htail_pos_lon = -17.90
htail_pos_vert = 3.40
htail_incidence = 0.50
htail_sweep = 5.00
vtail_area = 50.00
vtail_span = 8.00
vtail_sweep = 20.00
vtail_pos_lon = -16.40
vtail_pos_vert = 1.40
elevator_area = 36.00
aileron_area = 18.00
rudder_area = 20.00
elevator_up_limit = 17.00
elevator_down_limit = 15.50
aileron_up_limit = 18.00
aileron_down_limit = 18.00
rudder_limit = 30.00
elevator_trim_limit = 15.00
spoiler_limit = 0.00
spoilerons_available = 0
aileron_to_spoileron_gain = 0.00
min_ailerons_for_spoilerons = 0.00
min_flaps_for_spoilerons = 0.00
[Reference Speeds]
flaps_up_stall_speed = 90.00
full_flaps_stall_speed = 70.00
cruise_speed = 150.00
max_indicated_speed=259.00
max_level_speed=172
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga= 8.00
max_pitch=10.00
max_pitch_acceleration=1.00
max_pitch_velocity_lo_alt=2.00
max_pitch_velocity_hi_alt=1.500
max_pitch_velocity_lo_alt_breakpoint=20000.00
max_pitch_velocity_hi_alt_breakpoint=28000.00
max_bank=25.00
max_bank_acceleration=1.80
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.250
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.520
gs_integrator_control=0.260
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.00
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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
[Flaps.0]
type= 1
span-outboard= 0.50
extending-time= 6.00
system_type= 0
damaging-speed= 150.00
blowout-speed= 250.00
flaps-position.0= 0.00, 0.00
flaps-position.1= 10.00, 0.00
flaps-position.2= 20.00, 0.00
flaps-position.3= 30.00, 0.00
[brakes]
toe_brakes_scale=0.70
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=31.512679
flap_limit_idle=31.512679
[hydraulic_system]
normal_pressure=0.00
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
