[fltsim.0]
title=Grumman Goose G21a Cutters
sim=g21
model=
panel=
sound=
texture=
panel_alias =
sound_alias =
kb_checklists=goose_check
kb_reference=goose_ref
visual_damage=1
atc_id=NC327
prop_anim_ratio=0.45
ui_manufacturer=Grumman
ui_type= Cutters Goose
ui_variation=
description=Grumman Goose N327 as it appeared in the flight scenes in Tales of the Gold Monkey.
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=Grumman
atc_model=G21
editable=1
performance=See Kneeboard Reference
[fltsim.1]
title=Grumman Goose JRF-2
sim=g21
model=
panel=
sound=
texture=1
panel_alias =
sound_alias =
kb_checklists=goosej_check
kb_reference=goosej_ref
visual_damage=1
atc_id=1050
prop_anim_ratio=0.45
ui_manufacturer=Grumman
ui_type= Goose JRF-2
ui_variation=
description=Grumman JRF-2 in WW2 Coastal Patrol colors.
atc_heavy=0
atc_airline=navy
atc_flight_number=1050
[fltsim.2]
title=Grumman Goose G21a Avalon Air Transport
sim=g21
model=
panel=
sound=
texture=2
panel_alias =
sound_alias =
kb_checklists=Goosea_check
kb_reference=Goosea_ref
visual_damage=1
atc_id=N327
prop_anim_ratio=0.45
ui_manufacturer=Grumman
ui_type= Goose Avalon Air Transport
ui_variation=
description=Grumman Goose N327 as it appeared while used by Avalon Air Transport to ferry passengers to Catalina Island.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.3]
title=Grumman Goose G21a Southeast Skyways
sim=g21
model=
panel=
sound=
texture=3
panel_alias =
sound_alias =
kb_checklists=Gooses_check
kb_reference=Gooses_ref
visual_damage=1
atc_id=N327
prop_anim_ratio=0.45
ui_manufacturer=Grumman
ui_type= Goose Southeast Skyways
ui_variation=
description=Grumman Goose N327 as it appeared while used by Southeast Skyways operating out of Juneau Alaska.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.4]
title=Grumman Goose G21a Chrysler Air
sim=g21
model=
panel=
sound=
texture=4
panel_alias =
sound_alias =
kb_checklists=Goosec_check
kb_reference=Goosec_ref
visual_damage=1
atc_id=N327
prop_anim_ratio=0.45
ui_manufacturer=Grumman
ui_type= Goose Chrylsler Air
ui_variation=
description=Grumman Goose N327 as it appeared while used by Chrysler Air in Seattle Washington
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.5]
title=Grumman Goose JRF-2 NAVY2
sim=g21
model=
panel=
sound=
texture=5
panel_alias =
sound_alias =
kb_checklists=goosej_check
kb_reference=goosej_ref
visual_damage=1
atc_id=1050
prop_anim_ratio=0.45
ui_manufacturer=Grumman
ui_type= Goose JRF-2 Navy2
ui_variation=
description=Grumman JRF-2 in WW2 NAVY Colors
atc_heavy=0
atc_airline=navy
atc_flight_number=1050
[fltsim.6]
title=Grumman Goose JRF-2 Peruvian Army Air Force
sim=g21
model=
panel=
sound=
texture=6
panel_alias =
sound_alias =
kb_checklists=goosej_check
kb_reference=goosej_ref
visual_damage=1
atc_id=1050
prop_anim_ratio=0.45
ui_manufacturer=Grumman
ui_type= Goose JRF-2 Peruvian Army Air Force
ui_variation=
description=Grumman JRF-2 in WW2 Peruvian Colors
atc_heavy=0
atc_airline=army
atc_flight_number=1051
[fltsim.7]
title=Grumman Goose G21a Cutters with Sarah
sim=g21
model=1
panel=
sound=
texture=
panel_alias =
sound_alias =
kb_checklists=goose_check
kb_reference=goose_ref
visual_damage=1
atc_id=NC327
prop_anim_ratio=0.45
ui_manufacturer=Grumman
ui_type= Cutters Goose Sarah Copilot
ui_variation=
description=Grumman Goose N327 as it appeared in the flight scenes in Tales of the Gold Monkey.
[forcefeedback]
ground_bumps_magnitude1=2600 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000 ; in microseconds
[flight_tuning]
cruise_lift_scalar=0.34
parasite_drag_scalar=0.22
induced_drag_scalar=1.0
elevator_effectiveness=1.3
aileron_effectiveness=1.1
rudder_effectiveness=2.3
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=0.5
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations = 50
station_load.0 = "170, -4.0, -1.5, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "190, -4.0, 1.5, 0.0, Copilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "10, 0.0, 0.0, 0.0, Rear Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "0, 0.0, 0.0, 0.0, Rear Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum station_load.4 = "0, 0.0, 0.0, 0.0, Rear Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum station_load.5 = "0, 0.0, 0.0, 0.0, Rear Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum station_load.6 = "0, 0.0, 0.0, 0.0, Rear Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum station_load.7 = "0, 0.0, 0.0, 0.0, Rear Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "0, 0.0, 0.0, 0.0, Rear Passenger"
station_load.5 = "0, 0.0, 0.0, 0.0, Rear Passenger"
station_load.6 = "0, 0.0, 0.0, 0.0, Rear Passenger"
station_load.7 = "0, 0.0, 0.0, 0.0, Cargo"
station_load.8 = "30, 0.0, 0.0, 0.0, Baggage" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight=4856.000000
empty_weight_roll_MOI=13273.000000
empty_weight_pitch_MOI=13335.000000
empty_weight_yaw_MOI=11655.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=8000.00000
[fuel]
LeftMain=0.000, 0.000, 0.000, 70.000, 0.000
RightMain=0.000, 0.000, 0.000, 70.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=2
electric_pump=1
[airplane_geometry]
wing_area=375.000000
wing_span=49.500000
wing_root_chord=7.916667
wing_dihedral=0.998779
wing_incidence=2.499634
wing_twist=0.000000
oswald_efficiency_factor=1.070
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=-2.000000
wing_pos_apex_vert=0.000000
htail_area=32.000000
htail_span=12.250000
htail_pos_lon=-16.416667
htail_pos_vert=0.000000
htail_incidence=-0.697632
htail_sweep=0.000000
vtail_area=69.000000
vtail_span=6.140033
vtail_sweep=0.000000
vtail_pos_lon=-27.916667
vtail_pos_vert=1.500000
elevator_area=12.820000
aileron_area=18.070000
rudder_area=18.230000
elevator_up_limit=28.000447
elevator_down_limit=20.998903
aileron_up_limit=16.999658
aileron_down_limit=16.999658
rudder_limit=19.996227
elevator_trim_limit=19.996227
spoiler_limit=20.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
//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
[contact_points]
point.0 =1, -16.80, 0.00, -1.80, 3200, 0, 0.70,70.0, 0.30, 2.5, 0.90, 4.5, 4.5, 0, 0, 190
point.1 =1, 1.40, -3.91, -3.90, 2200, 1, 1.40, 0.0, 0.50, 2.5, 0.85, 0.0, 0.0, 2, 0, 0
point.2 =1, 1.40, 3.91, -3.90, 2200, 2, 1.40, 0.0, 0.50, 2.5, 0.85, 5.5, 5.5, 3, 0, 190
point.3 = 4, 4.00, -1.50, -1.410, 36000, 0, 0.00, 47.0, 0.85, 40.5, 1.25, 0.0, 0.0, 0, 0.0, 0.0
point.4 = 4, 4.00, 1.50, -1.410, 36000, 0, 0.00, 47.0, 0.85, 40.5, 1.25, 0.0, 0.0, 0, 0.0, 0.0
point.5 = 4, -4.35, -1.250, -1.310, 36000, 0, 0.00, 0.0, 0.85, 40.5, 3.25, 0.0, 0.0, 0, 0.0, 0.0
point.6 = 4, -4.35, 1.250, -1.310, 36000, 0, 0.00, 0.0, 0.85, 40.5, 3.25, 0.0, 0.0, 0, 0.0, 0.0
point.7 = 2, -3.35, -16.250, 0.200, 136000, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0, 0.0, 0.0
point.8 = 2, -3.35, 16.250, 0.200, 136000, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0, 0.0, 0.0
point.9 = 5, 0.90, 0.0, 7.300, 1600, 0, 0.00, 50.0, 2.0, 2.0, 2.00, 2.0, 2.0, 2.0,2.0, 2.0
point.10 = 4, -14.35, 0.0, 0.20, 136000,1, 1.40, 0.0, 0.50, 5.5, 0.85, 0.0, 0.0, 0, 0, 0
static_cg_height = 3.20 //(feet) altitude of CG when at rest (altitude when loaded on ground)
static_pitch = 6.50 //degrees (pitch when loaded on ground)
gear_system_type=0
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=7.000,0.000000
flaps-position.2=12.000,0.000000
flaps-position.3=17.000,0.000000
flaps-position.4=25.000,0.000000
lift_scalar = 1.0
drag_scalar = 1.0
//pitch_scalar= 0.0
[GeneralEngineData]
engine_type=0
Engine.0=0.500000,-6.000000,1.000000
Engine.1=0.500000, 6.000000,1.000000
fuel_flow_scalar=1.000000
min_throttle_limit=0.0000
master_ignition_switch = 1 //Master Ignition Switch
[piston_engine]
cylinder_displacement=83.000000
compression_ratio=7.000000
number_of_cylinders=9
max_rated_rpm=2300.000000
max_rated_hp=350.000000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.0775000
turbocharged=0
max_design_mp=40.999999
min_design_mp=1.000000
critical_altitude=17000.000000
emergency_boost_type=2
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=1
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=0.450000
power_scalar =1.00
[propeller]
propeller_type=0
propeller_diameter=7.0000
propeller_blades=3
propeller_moi=25.400000
beta_max=60.000000
beta_min=7.000000
min_gov_rpm=1800.000000
prop_tc=0.010000
gear_reduction_ratio=1.20000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 1100.0 //Minimum RPM for prop feathering
beta_feather= 89.5 //Feathering pitch angle (degrees)
power_absorbed_cf= 1.9 //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees)
feathering_switches = 1 //Switches which invoke feathering
thrust_scalar =1.40
[SMOKESYSTEM]
smoke.0=12.0, 0.0, -6.30, fx_goosefire
[EFFECTS]
wake=fx_wake
dirt=fx_dustrun
concrete=fx_sparksx
touchdown=fx_tchdwn_s, 1
startup=fx_engstrt_g21
water=fx_goose_spray
[keyboard_response]
elevator=300.000000,500.000000
aileron=150.000000,300.000000
rudder=200.000000,1000.000000
[Views]
eyepoint=-0.800000,-1.30000,4.100000
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3, -0.0, -21.4, 6.10, fx_navredc
light.1=3, -0.0, 21.4, 6.10, fx_navgrec
light.2=2, -21.0, 0.00, 10.70, fx_navredc //whi
light.3=1, -21.0, 0.00, 10.70, fx_beacon
light.4=4, -3.0, 0.00, 2.5, fx_vclight_goose
light.5=4, -10.0, 0.00, 4.0, fx_vclight_goose
light.6=4, 2.2, 0.00,3.2, fx_vclight_goosef
//[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
//light.0=2, -0.0, -21.4, 6.10, fx_navredc
//light.1=2, -0.0, 21.4, 6.10, fx_navgrec
//light.2=2, -21.0, 0.00, 10.70, fx_navredc
//light.3=4, -3.0, 0.00, 2.5, fx_vclight_goose
//light.4=4, -10.0, 0.00, 4.0, fx_vclight_goose
xxlight.5=4, 2.2, 0.00,3.2, fx_vclight_goosef
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1
Com.2 =1
Nav.1 = 1
Nav.2 = 1
Adf.1 = 1
Adf.2 =1
Transponder.1 = 1
Marker.1 =1
[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
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
starter2 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
[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
[direction_indicators]
direction_indicator.0=1,0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[Reference Speeds]
flaps_up_stall_speed=60.000000
full_flaps_stall_speed=47.600000
cruise_speed=167.0
max_indicated_speed=260.00000
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.7 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[hydraulic_system]
normal_pressure = 732.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[stall_warning]
type=0
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position = -17.5, 0.0, -0.5 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0