//Mods (air & cfg) by C. Backus (napamule). 06Jan27
//Orig Model, Panel, Sound, and Textures by Dave ('Big D')
//Dave at 'daveanjackie@netzero.com'. filename:'Pickupcb.zip'
[fltsim.0]
title=Pickup
sim=PickupCb
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=Robbins Motorworks //o=Shipworks
ui_type=100ft Jackie
ui_variation=Yacht
atc_heavy=0
atc_airline=
[General]
atc_type=
atc_model=
editable=1
performance=Maximum Speed\t60 mph (err...how's 250 kts?)
[WEIGHT_AND_BALANCE]
max_gross_weight = 7500.000
empty_weight = 3500.000
reference_datum_position = 0.0000, 0.0000, 0.0000 // (ft) dist from FSim Ref pos: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -3.000,0.000, 0.500 //ZXY dist from specified datum
max_number_of_stations = 30
station_load.0= 190.000, 0.000, -1.000, 0.000 //Driver
station_load.1= 200.000, 0.000, 1.000, 0.000 // Passengers
station_load.3= 1000.000, -4.000, 0.000, 0.000 // Luggage, misc.
;Moments of Inertia
empty_weight_pitch_MOI = 74110.000
empty_weight_roll_MOI = 42310.000
empty_weight_yaw_MOI = 29000.000
empty_weight_coupled_MOI = 0.000
// 0 Class (0=floats)
// 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) [N/A]
// 6 Wheel Radius (feet)
// 7 Steer Angle (degrees)
// 8 Static Compression (feet) (0=rigid)
// 9 Max/Static Compression Ratio
//10 Damping Ratio/Water Rudder Effectiveness (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)
[contact_points]
point.0=1, 3.500, -3.000, -1.660, 9999.000, 1, 2.500, 25.000, 0.400, 2.5, 0.950, 1.000, 1.000, 0, 60.00, 100.00
point.1=1, 3.500, 3.000, -1.660, 9999.000, 2, 2.500, 25.000, 0.400, 2.5, 0.950, 1.000, 1.000, 0, 60.00, 100.00
point.2=1, -10.300, -3.600, -1.680, 9999.000, 1, 2.500, 0.000, 0.250, 2.5, 0.950, 1.000, 1.000, 0, 60.00, 100.00
point.3=1, -10.300, 3.600, -1.680, 9999.000, 2, 2.500, 0.000, 0.250, 2.5, 0.950, 1.000, 1.000, 0, 60.00, 100.00
static_pitch = 0.1000 //degrees (pitch when loaded on ground)
static_cg_height=1.525 //feet, altitude of CG when at rest on the ground
gear_system_type = 0
[GeneralEngineData]
engine_type = 1 // 1=Jet
Engine.0 = -4.000, 0.000, 0.000 //ZXY distance from ref datum
fuel_flow_scalar = 0.050000 //Scalar for fuel flow efficiency
min_throttle_limit = -0.490000 //neg for turbine reverser
[TurbineEngineData]
fuel_flow_gain =0.002000 //Gain on fuel flow
inlet_area = 1.0 // Square Feet, engine nacelle inlet area
rated_N2_rpm = 5920.000000 //RPM, 2nd stage compressor rated value
static_thrust = 1800.000000 // Lbs, max rated static thrust at SL
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
[jet_engine]
thrust_scalar =1.0
[brakes]
parking_brake = 1 // Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
differential_braking_scale =1.0
[Reference Speeds]
flaps_up_stall_speed = 40.000
full_flaps_stall_speed = 0.000
cruise_speed = 70.000
max_indicated_speed = 210.000
max_mach = 0.26
[Views]
;ZXY distance from reference datum (feet)
eyepoint= -4.99, -1.12, 4.36 //(feet) longitudinal, lateral, vertical distance from reference datum
[flight_tuning]
cruise_lift_scalar = .000
parasite_drag_scalar = 1.000
induced_drag_scalar = 2.000
elevator_effectiveness = .000
aileron_effectiveness = 000
rudder_effectiveness = 1
pitch_stability = 1.000
roll_stability = 1.000
yaw_stability =1.000
elevator_trim_effectiveness = .000
aileron_trim_effectiveness = .000
rudder_trim_effectiveness = 1.000
[airplane_geometry]
wing_area =12.500000 //Square feet
wing_span =4.600000 //o= 111.4
wing_root_chord= 8.8
wing_dihedral =0.000000 //Degrees
wing_incidence =0.000000 //Degrees
wing_twist= -1.0 //Degrees
oswald_efficiency_factor= 0.000100 //Measure of lift effeciency of wing
wing_winglets_flag= 0 //Are winglets available?
wing_sweep=0.000000 //Degrees, wing leading edge
wing_pos_apex_lon = -1.000000 //Z distance from ref point
wing_pos_apex_vert =0.000000 //Y distance from ref point
htail_area =144.000000 //Square feet
htail_span =4.000000
htail_pos_lon=-9.000000 //Z distance from ref point
htail_pos_vert=1.000000 //Y distance from ref point
htail_incidence =0.000000 //Degrees
htail_sweep=0.000000 // horizontal tail leading edge
vtail_area= 144.000000 //Square feet
vtail_span= 3.000000 //tip to body
vtail_sweep =0.000000 //Degrees, vertical tail leading edge
vtail_pos_lon=-10.000000 //Z distance from ref point
vtail_pos_vert =4.000000 //Y from ref point
elevator_area = 0 //Square feet
aileron_area = 0 //Square feet
rudder_area=70.000000 //Square feet
elevator_up_limit=5.000000 //Degrees
elevator_down_limit=5.000000 //Degrees
aileron_up_limit=5.000000 //Degrees
aileron_down_limit=5.000000 //Degrees
rudder_limit= 25.5 //Degrees
elevator_trim_limit=15.000000 //Degrees
spoiler_limit = 0 //Degrees
spoilerons_available= 0 //Spoilerons Available?
aileron_to_spoileron_gain= 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons= 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Flaps.0]
type=0
span-outboard=0.500000
extending-time=0.000000
system_type=0
[fuel]
Center1 = -6.000, 0.000, -2.000,18.000, 0.000 //ZXY GAL MIN
fuel_type = 1 // ;2 = JetA
number_of_tank_selectors = 1
electric_pump = 1
[electrical]
electric_always_available = 0
[Radios]
// Radio Type = available, 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
[gear_warning_system]
gear_warning_available = 0
[hydraulic_system]
normal_pressure = 3000 //PSI
electric_pumps = 1 //electric pumps
engine_map = 1,0,0,0 // pumps
[pitot_static]
vertical_speed_time_constant = 1
//Increasing this value will cause a more instantaneous reaction in the VSI
[direction_indicators]
direction_indicator.0 = 3,0 //3=Electro-Mag Slaved Compass, 0=NA
[attitude_indicators]
attitude_indicator.0 = 0 //0=None
[turn_indicators]
turn_indicator.0 = 1,0 //1=Electric Gyro
[stall_warning]
type = 0
[exits]
number_of_exits=1
exit_rate.0=0.4 //Percent per second
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8.0
max_pitch=12.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=2.8
max_bank_velocity=4.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0
[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 = 50.000, 150.000
aileron = 50.000, 150.000
rudder = 50.000, 150.000
;[forcefeedback] //Note: FF does NOT work well in FS9
;gear_bump_nose_magnitude = 3000.000 // 0 - 10000
;gear_bump_nose_direction = 18000.000 //0 - 35999 degrees
;gear_bump_nose_duration = 250000.000 //in microseconds
;gear_bump_left_magnitude = 2700.000 // 0 - 10000
;gear_bump_left_direction = 35500.000 // 0 - 35999 degrees
;gear_bump_left_duration = 250000.000 //in microseconds
;gear_bump_right_magnitude = 2700.000 // 0 - 10000
;gear_bump_right_direction = 500.000 //0 - 35999 degrees
;gear_bump_right_duration = 250000.000 //in microseconds
;ground_bumps_magnitude1 = 1300.000 //0 - 10000
;ground_bumps_angle1 = 8900.000 //0 - 35999 degrees
;ground_bumps_intercept1 = 3.000
;ground_bumps_slope1 = 0.200
;ground_bumps_magnitude2 = 200.000 //0 - 10000
;ground_bumps_angle2 = 9100.000 //0 - 35999 degrees
;ground_bumps_intercept2 = 1.075
;ground_bumps_slope2 = 0.035
;crash_magnitude1 = 10000.000 //0 - 10000
;crash_direction1 = 1000.000 // 0 - 35999 degrees
;crash_magnitude2 = 10000.000 //0 - 10000
;crash_direction2 = 9000.000 //0 - 35999 degrees
;crash_period2 = 75000.000 //in microseconds
;crash_duration2 = 2500000.000 //in microseconds