28-11-2005, 11:31 PM
Wow, what can I say, thank you!
Ok, here comes, first the passenger version:
<--- aircraft.cfg
//Ron Freimuth 2/21/05; 6/17/05
//Search for "!" for test only settings (SPD hold)
[fltsim.0]
title=Cessna Grand Caravan! Deluxe
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=N208KT
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Passenger
description=Cessna C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[General]
atc_type=CESSNA
atc_model=C208
editable=1
performance=Maximum Speed\n175 kts 324 km\/hr\nCruise Speed\n164 kts \t 305 km\/hr at 20,000 ft\nEngine\nPratt & Whitney Canada,
Inc., PT6A-114A Free Turbine Flat Rated at 675 Shaft hp \nPropeller\nThree-Bladed, Constant Speed, Full Feathering, Reversible McCauley, 106-inch
diameter\nMaximum Range\n5.1 hours maximum cruise at 10,000 ft\n6.6 hours maximum cruise at 18,000 ft\n6.4 hours maximum range at 10,000 ft\n7.2 hours
maximum range at 18,000 ft\nService Ceiling\n22,800 ft 6,949 m\nFuel Capacity\n335 gal 1,268 L\nEmpty Weight\n4,040 lb
1,830 kg\nMaximum Gross Weight\n8,785 lb\t 3,980 kg\nUseful Load\n4,745 lb\t 2,150 kg\nLength\n41 ft, 7 in
12.7 m\nWingspan\n52 ft, 1 in\t 15.8 m\nHeight\n15 ft, 5-1\/2 in 4.8 m\nSeating\nUp to 14
//Maximum Speed 175 (180) kts
//Cruise Speed 164 kts at 20,000 ft
//Engine Pratt & Whitney Canada, Inc., PT6A-114A Free Turbine Flat Rated at 675 Shaft hp
//Propeller Three-Blade, Constant Speed, Full Feathering, Reversible McCauley, 106-inch diameter
//Maximum Range
//5.1 hours maximum cruise at 10,000 ft
//6.6 hours maximum cruise at 18,000 ft
//6.4 hours maximum range at 10,000 ft
//7.2 hours maximum range at 18,000 ft
//Service Ceiling 22,800 ft
//Fuel Capacity 335 gal
//Empty Weight 4,040 lb
//Maximum Gross Weight 8,785 lb
//Useful Load 4,745 lb
//Cruise: 184 kts at 10,000 ft
//Range: 907 nm " " 45 min reserve
//Stall: 61 kts (8500 lb?)
[weight_and_balance]
max_gross_weight = 8785 //Ramp TCDS 8750 lb TO, 8500 landing
empty_weight = 4575 //4250 lb for 4500 lb useful load
reference_datum_position = 16.5, 0, 0 //-15.6 8.33 ft fwd NG jack (Amphib: firewall)
empty_weight_CG_position = -15.4, 0, 0 //-15.4 Col -15.84 ;-16.2
empty_weight_pitch_MOI = 9529 //8874.87
empty_weight_roll_MOI = 5554 //6026.96
empty_weight_yaw_MOI = 11844 //11858.54
empty_weight_coupled_MOI = 0
CG_forward_limit=0.150
CG_aft_limit=0.310
//B: 16.6 to 17.04 ft at 8750 lb; 16.11 at 8000 lb, 14.97 at 5500 lb
// 14.51 to 15.36 ft at 8000 lb; 15.9%; 14.94 ft mean.
//CoL: -15.84 ;was -16.2 MAC: 5.36 ft [-15.84 org]
max_number_of_stations = 20
station_load.0 =" 170, -11.3, -1.4, 0, Pilot" ;133.5" to 146.5" -11.13 to -12.21 ft TCDS
station_load.1 =" 170, -11.3, 1.4, 0, CoPilot"
station_load.2 =" 001, -13.9, -1.4, 0, -13.9 "
station_load.3 =" 001, -13.9, 1.4, 0, -13.9 "
station_load.4 =" 160, -17.2, -1.4, 0, -17.2 "
station_load.5 =" 160, -17.2, 1.4, 0, -17.2 "
station_load.6 =" 001, -20.2, -1.4, 0, -20.2 "
station_load.7 =" 001, -20.2, 1.4, 0, -20.2 "
station_load.8 =" 001, -23.2, -1.4, 0, -23.2 "
station_load.9 =" 001, -23.2, 1.4, 0, -23.2 " ;-19.5 max aft TCDS
station_load.10 ="400, -15.8, 0, -2.8, Cargo Pod"
//720 lb pass & cargo + 2 170 lb pilots: 1060 lb
//4575 + 2225 = 6800 + 1060 = 7860 lb
[Views]
eyepoint=-12.5, -1.4, 2.32 //was -12.5, -1.4, 2.12
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -16.30, -26.41, 3.60, fx_navred
light.1 = 3, -16.30, 26.41, 3.60, fx_navgre
light.2 = 3, -42.90, 0.00, 1.09, fx_navwhi
light.3 = 2, -16.56, -26.51, 3.60, fx_strobe
light.4 = 2, -16.56, 26.51, 3.60, fx_strobe
light.5 = 1, -41.25, 0.00, 9.40, fx_beacon
light.6 = 4, -10.90, 0.00, 0.90, fx_vclight_ftc
light.7 = 4, -12.00, 0.00, 2.90, fx_vclight_ftc
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.05 //1.00 350 pph at 1650 ft-lb,1750 rpm
engine.0 = -1.5, -0.15, 0.0, //Reduced lateral offset
min_throttle_limit=-0.45 //-0.50 //Too high?
[TurbineEngineData]
fuel_flow_gain=0.030 //0.021
inlet_area=0.30 //1.00
rated_N2_rpm=33000
static_thrust= 120 //158
afterburner_available=0
[turboprop_engine] //PT6A-114A
power_scalar=1.00
maximum_torque=1965 //1865
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
//Max Power: 675 all conditions, inc reverse
//Max NG: 101.6%
//Max Torque: 1865/1970 don't exceed Pmax
//ITT: 805, 765, 740 TO, Climb, Cruise
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
LeftMain = -16.98,-8.0, 2.6, 167.5, 3.6 //B, 167.5 gal TCDS -203.8 in = -16.98 ft
RightMain = -16.98, 8.0, 2.6, 167.5 3.6
electric_pump=1
[propeller] //McCauley 3GFR34C703/106GA-0; Hartzel HC-B3MN3/M10083 100"]
thrust_scalar=1.00
propeller_type = 0 //3
propeller_diameter= 8.833 // 106", 102" min
propeller_blades=3
propeller_moi = 15.0 //19.0
beta_max = 40.0
beta_min = 15.6 //15.6 deg at 30" 56.6%, Beta Pickup
min_gov_rpm = 25520
prop_tc = 0.0002 //0.014
gear_reduction_ratio= 17.37 //17.40
fixed_pitch_beta = 20.0
low_speed_theory_limit= 80
prop_sync_available= 0
prop_deice_available= 1
prop_feathering_available = 1
prop_auto_feathering_available= 1 //?
min_rpm_for_feather = 700
beta_feather = 88.0
power_absorbed_cf = 1.30 //0.90 //Prop Cp at feather angle
defeathering_accumulators_available= 0
prop_reverse_available= 1
minimum_on_ground_beta= 1.0 //?
minimum_reverse_beta =-14.0
//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]
static_pitch = 0.00
static_cg_height = 5.9 //6.0
max_number_of_points = 8
// -6.1 40
point.0 = 1, -4.50, 0.0 -6.0, 1200, 0, 0.8, 35, 0.3, 2.5, 0.85, 0, 0, 0, ;nose gear
point.1 = 1,-17.00, -5.8, -6.0, 1500, 1, 1.1, 0, 0.3, 2.5, 0.90, 0, 0, 2, ;left gear
point.2 = 1,-17.00, 5.8, -6.0, 1500, 2, 1.1, 0, 0.3, 2.5, 0.90, 0, 0, 3, ;right gear was +- 5.6
point.3 = 2,-15.90,-26.0, 3.6, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, ;left wing
point.4 = 2,-15.90, 26.0, 3.6, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, ;right wing
point.5 = 2,-41.60, 0.0, 0.0, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, ;tail
point.6 = 2, -1.60, 0.0 -4.2, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, ;prop tip
point.7 = 2,-41.25, 0.0 9.5, 800, 0, 0, 0, 0, 0, 0, 0, 0, 7, ;vert tail
[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[airplane_geometry]
//reference_datum_position = 16.5, 0, 0 //-16.2 8.33 ft fwd NG jack pt (Amphib: firewall)
//empty_weight_CG_position = -15.4, 0, 0 //-15.4
//Length 41 ft, 7 in, Wingspan 52 ft, 1 in, Height 15 ft, 5-1/2 in
wing_area = 279.5
wing_span = 52.09
wing_root_chord = 5.36 //MAC
wing_dihedral = 2.0
wing_incidence = 0.85 // dCL/dAoA = 5.611; CL=0 at -3.86 deg
wing_twist =-1.70
oswald_efficiency_factor = 0.80
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon =-14.5 //CoL: -15.84 (org) ;-14.5 -1.34 = -15.84
wing_pos_apex_vert= 2.40
htail_area = 49.0 //Sh/Sw ~ 0.23
htail_span = 21.0
htail_pos_lon =-35.7 //-1.1 + 15.6 = -21.2 ft dh/cbar ~ 4.0
htail_pos_vert = 0.0
htail_incidence = 2.0
htail_sweep = 10 //5
vtail_area = 28.0
vtail_span = 7.50
vtail_sweep = 30
vtail_pos_lon =-35.0 //-1.8 + 15.6 = -21.2 ft 52.1/21.2 ~ 2.5
vtail_pos_vert = 2.43 //hbar~2.4+3.0 = 5.4 ft 5.4/21.5 ~ 0.25
elevator_area = 16.0
aileron_area = 18.3
rudder_area = 6.7
elevator_up_limit = 25.0 //28.00
elevator_down_limit = 20.0 //21.00
aileron_up_limit = 26.0 //20.00
aileron_down_limit = 16.0 //15.00
rudder_limit = 25.0 //24.00
elevator_trim_limit = 15.0
spoiler_limit = 40.0
aileron_to_spoileron_gain = 1.60
min_ailerons_for_spoilerons= 5.0 //0.0 new
min_flaps_for_spoilerons = 0.0
spoilerons_available = 1
[electrical]
max_battery_voltage = 25.2
generator_alternator_voltage = 28.5
max_generator_alternator_amps = 60
electric_always_available = 0
[pitot_static]
vertical_speed_time_constant= 1 //20 //4.0 //Increasing this value will cause a more instantaneous reaction in the VSI
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
[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
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second
[Reference Speeds]
flaps_up_stall_speed = 78.0 //66.0 ? //CAS lower ?
full_flaps_stall_speed = 60.0 //52.8 ? //CAS higher ?
cruise_speed = 165.0 //TAS
max_indicated_speed = 175 //IAS
max_mach = 0.60
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed= 800 //1000.0
autothrottle_available= 0 //1 for test !
autoland_available=1
pitch_takeoff_ga= 10.0 //8.0
autothrottle_arming_required=0
autothrottle_takeoff_ga= 1 //0 !temp
autothrottle_max_rpm= 100.0
max_pitch=10.0
max_pitch_acceleration= 2.0 //1.0 //more?
max_pitch_velocity_lo_alt=4.0 //2.0 // ?
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank= 25.0
max_bank_acceleration = 1.8
max_bank_velocity = 3.0
max_throttle_rate = 0.2 //0.1
nav_proportional_control=9.0
nav_integrator_control= 0.25
nav_derivative_control= 0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=14.0 //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
[Flaps.0] //Lift
type=1
span-outboard=0.500
extending-time=5.700
system_type=0
damaging-speed = 175
blowout-speed = 175
lift_scalar=1.00
drag_scalar=0.00 //1.00
pitch_scalar=1.00
flaps-position.0= 0.0,
flaps-position.1=12.0, 175 //10.0
flaps-position.2=22.0, 150 //20.0
flaps-position.3=30.0, 125 //0.5236 rad
[Flaps.1] //Drag
type=1
span-outboard=0.500
extending-time=5.700
system_type=0
damaging-speed = 175
blowout-speed = 175
lift_scalar=0.00 //1.00
drag_scalar=1.00
pitch_scalar=0.00 //1.00
flaps-position.0= 0.0,
flaps-position.1= 3.5, 175 //8.0
flaps-position.2=14.0, 150 //18.0
flaps-position.3=30.0, 125 //0.5236 rad
[brakes]
toe_brakes_scale=0.68
parking_brake=1
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=3000
[stall_warning]
type=2
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0 // 0=None, 1=Electric Gyro, 2=Vacuum Gyro
[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
[airspeed_indicators]
airspeed_indicator.0 = 1.067, -10.0 //Reads 161 kts at CAS = 160 kts
[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[fltsim.1]
title=Cessna Grand Caravan! Deluxe - Air Caraibes
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=CARAIBES
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=F-OHQN
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Air Caraibes
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[fltsim.2]
title=Cessna Grand Caravan! Deluxe- Kato Air
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=KATO
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=LN-KAT
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Kato Air
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[fltsim.3]
title=Cessna Grand Caravan! Deluxe - Linear Air
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=LINEAR
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=N610LA
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Linear Air
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[fltsim.4]
title=Cessna Grand Caravan! Deluxe - Macair
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=MACAIR
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=VH-TFS
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Macair
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[fltsim.5]
title=Cessna Grand Caravan! Deluxe - Pacific Wings N303PW
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=PACIFIC1
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=N303PW
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Pacific Wings
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[fltsim.6]
title=Cessna Grand Caravan! Deluxe - San Juan Airlines N1030N
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=SANJUAN1
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=N1030N
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=San Juan Airlines
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[fltsim.7]
title=Cessna Grand Caravan! Deluxe - Sansa HP-1402APP
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=SANSA1
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=HP-1402APP
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Sansa
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
Regards
/Martin Jacobsson
Post Edited ( 11-28-05 23:32 )
Ok, here comes, first the passenger version:
<--- aircraft.cfg
//Ron Freimuth 2/21/05; 6/17/05
//Search for "!" for test only settings (SPD hold)
[fltsim.0]
title=Cessna Grand Caravan! Deluxe
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=N208KT
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Passenger
description=Cessna C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[General]
atc_type=CESSNA
atc_model=C208
editable=1
performance=Maximum Speed\n175 kts 324 km\/hr\nCruise Speed\n164 kts \t 305 km\/hr at 20,000 ft\nEngine\nPratt & Whitney Canada,
Inc., PT6A-114A Free Turbine Flat Rated at 675 Shaft hp \nPropeller\nThree-Bladed, Constant Speed, Full Feathering, Reversible McCauley, 106-inch
diameter\nMaximum Range\n5.1 hours maximum cruise at 10,000 ft\n6.6 hours maximum cruise at 18,000 ft\n6.4 hours maximum range at 10,000 ft\n7.2 hours
maximum range at 18,000 ft\nService Ceiling\n22,800 ft 6,949 m\nFuel Capacity\n335 gal 1,268 L\nEmpty Weight\n4,040 lb
1,830 kg\nMaximum Gross Weight\n8,785 lb\t 3,980 kg\nUseful Load\n4,745 lb\t 2,150 kg\nLength\n41 ft, 7 in
12.7 m\nWingspan\n52 ft, 1 in\t 15.8 m\nHeight\n15 ft, 5-1\/2 in 4.8 m\nSeating\nUp to 14
//Maximum Speed 175 (180) kts
//Cruise Speed 164 kts at 20,000 ft
//Engine Pratt & Whitney Canada, Inc., PT6A-114A Free Turbine Flat Rated at 675 Shaft hp
//Propeller Three-Blade, Constant Speed, Full Feathering, Reversible McCauley, 106-inch diameter
//Maximum Range
//5.1 hours maximum cruise at 10,000 ft
//6.6 hours maximum cruise at 18,000 ft
//6.4 hours maximum range at 10,000 ft
//7.2 hours maximum range at 18,000 ft
//Service Ceiling 22,800 ft
//Fuel Capacity 335 gal
//Empty Weight 4,040 lb
//Maximum Gross Weight 8,785 lb
//Useful Load 4,745 lb
//Cruise: 184 kts at 10,000 ft
//Range: 907 nm " " 45 min reserve
//Stall: 61 kts (8500 lb?)
[weight_and_balance]
max_gross_weight = 8785 //Ramp TCDS 8750 lb TO, 8500 landing
empty_weight = 4575 //4250 lb for 4500 lb useful load
reference_datum_position = 16.5, 0, 0 //-15.6 8.33 ft fwd NG jack (Amphib: firewall)
empty_weight_CG_position = -15.4, 0, 0 //-15.4 Col -15.84 ;-16.2
empty_weight_pitch_MOI = 9529 //8874.87
empty_weight_roll_MOI = 5554 //6026.96
empty_weight_yaw_MOI = 11844 //11858.54
empty_weight_coupled_MOI = 0
CG_forward_limit=0.150
CG_aft_limit=0.310
//B: 16.6 to 17.04 ft at 8750 lb; 16.11 at 8000 lb, 14.97 at 5500 lb
// 14.51 to 15.36 ft at 8000 lb; 15.9%; 14.94 ft mean.
//CoL: -15.84 ;was -16.2 MAC: 5.36 ft [-15.84 org]
max_number_of_stations = 20
station_load.0 =" 170, -11.3, -1.4, 0, Pilot" ;133.5" to 146.5" -11.13 to -12.21 ft TCDS
station_load.1 =" 170, -11.3, 1.4, 0, CoPilot"
station_load.2 =" 001, -13.9, -1.4, 0, -13.9 "
station_load.3 =" 001, -13.9, 1.4, 0, -13.9 "
station_load.4 =" 160, -17.2, -1.4, 0, -17.2 "
station_load.5 =" 160, -17.2, 1.4, 0, -17.2 "
station_load.6 =" 001, -20.2, -1.4, 0, -20.2 "
station_load.7 =" 001, -20.2, 1.4, 0, -20.2 "
station_load.8 =" 001, -23.2, -1.4, 0, -23.2 "
station_load.9 =" 001, -23.2, 1.4, 0, -23.2 " ;-19.5 max aft TCDS
station_load.10 ="400, -15.8, 0, -2.8, Cargo Pod"
//720 lb pass & cargo + 2 170 lb pilots: 1060 lb
//4575 + 2225 = 6800 + 1060 = 7860 lb
[Views]
eyepoint=-12.5, -1.4, 2.32 //was -12.5, -1.4, 2.12
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -16.30, -26.41, 3.60, fx_navred
light.1 = 3, -16.30, 26.41, 3.60, fx_navgre
light.2 = 3, -42.90, 0.00, 1.09, fx_navwhi
light.3 = 2, -16.56, -26.51, 3.60, fx_strobe
light.4 = 2, -16.56, 26.51, 3.60, fx_strobe
light.5 = 1, -41.25, 0.00, 9.40, fx_beacon
light.6 = 4, -10.90, 0.00, 0.90, fx_vclight_ftc
light.7 = 4, -12.00, 0.00, 2.90, fx_vclight_ftc
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.05 //1.00 350 pph at 1650 ft-lb,1750 rpm
engine.0 = -1.5, -0.15, 0.0, //Reduced lateral offset
min_throttle_limit=-0.45 //-0.50 //Too high?
[TurbineEngineData]
fuel_flow_gain=0.030 //0.021
inlet_area=0.30 //1.00
rated_N2_rpm=33000
static_thrust= 120 //158
afterburner_available=0
[turboprop_engine] //PT6A-114A
power_scalar=1.00
maximum_torque=1965 //1865
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
//Max Power: 675 all conditions, inc reverse
//Max NG: 101.6%
//Max Torque: 1865/1970 don't exceed Pmax
//ITT: 805, 765, 740 TO, Climb, Cruise
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
LeftMain = -16.98,-8.0, 2.6, 167.5, 3.6 //B, 167.5 gal TCDS -203.8 in = -16.98 ft
RightMain = -16.98, 8.0, 2.6, 167.5 3.6
electric_pump=1
[propeller] //McCauley 3GFR34C703/106GA-0; Hartzel HC-B3MN3/M10083 100"]
thrust_scalar=1.00
propeller_type = 0 //3
propeller_diameter= 8.833 // 106", 102" min
propeller_blades=3
propeller_moi = 15.0 //19.0
beta_max = 40.0
beta_min = 15.6 //15.6 deg at 30" 56.6%, Beta Pickup
min_gov_rpm = 25520
prop_tc = 0.0002 //0.014
gear_reduction_ratio= 17.37 //17.40
fixed_pitch_beta = 20.0
low_speed_theory_limit= 80
prop_sync_available= 0
prop_deice_available= 1
prop_feathering_available = 1
prop_auto_feathering_available= 1 //?
min_rpm_for_feather = 700
beta_feather = 88.0
power_absorbed_cf = 1.30 //0.90 //Prop Cp at feather angle
defeathering_accumulators_available= 0
prop_reverse_available= 1
minimum_on_ground_beta= 1.0 //?
minimum_reverse_beta =-14.0
//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]
static_pitch = 0.00
static_cg_height = 5.9 //6.0
max_number_of_points = 8
// -6.1 40
point.0 = 1, -4.50, 0.0 -6.0, 1200, 0, 0.8, 35, 0.3, 2.5, 0.85, 0, 0, 0, ;nose gear
point.1 = 1,-17.00, -5.8, -6.0, 1500, 1, 1.1, 0, 0.3, 2.5, 0.90, 0, 0, 2, ;left gear
point.2 = 1,-17.00, 5.8, -6.0, 1500, 2, 1.1, 0, 0.3, 2.5, 0.90, 0, 0, 3, ;right gear was +- 5.6
point.3 = 2,-15.90,-26.0, 3.6, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, ;left wing
point.4 = 2,-15.90, 26.0, 3.6, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, ;right wing
point.5 = 2,-41.60, 0.0, 0.0, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 9, ;tail
point.6 = 2, -1.60, 0.0 -4.2, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, ;prop tip
point.7 = 2,-41.25, 0.0 9.5, 800, 0, 0, 0, 0, 0, 0, 0, 0, 7, ;vert tail
[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[airplane_geometry]
//reference_datum_position = 16.5, 0, 0 //-16.2 8.33 ft fwd NG jack pt (Amphib: firewall)
//empty_weight_CG_position = -15.4, 0, 0 //-15.4
//Length 41 ft, 7 in, Wingspan 52 ft, 1 in, Height 15 ft, 5-1/2 in
wing_area = 279.5
wing_span = 52.09
wing_root_chord = 5.36 //MAC
wing_dihedral = 2.0
wing_incidence = 0.85 // dCL/dAoA = 5.611; CL=0 at -3.86 deg
wing_twist =-1.70
oswald_efficiency_factor = 0.80
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon =-14.5 //CoL: -15.84 (org) ;-14.5 -1.34 = -15.84
wing_pos_apex_vert= 2.40
htail_area = 49.0 //Sh/Sw ~ 0.23
htail_span = 21.0
htail_pos_lon =-35.7 //-1.1 + 15.6 = -21.2 ft dh/cbar ~ 4.0
htail_pos_vert = 0.0
htail_incidence = 2.0
htail_sweep = 10 //5
vtail_area = 28.0
vtail_span = 7.50
vtail_sweep = 30
vtail_pos_lon =-35.0 //-1.8 + 15.6 = -21.2 ft 52.1/21.2 ~ 2.5
vtail_pos_vert = 2.43 //hbar~2.4+3.0 = 5.4 ft 5.4/21.5 ~ 0.25
elevator_area = 16.0
aileron_area = 18.3
rudder_area = 6.7
elevator_up_limit = 25.0 //28.00
elevator_down_limit = 20.0 //21.00
aileron_up_limit = 26.0 //20.00
aileron_down_limit = 16.0 //15.00
rudder_limit = 25.0 //24.00
elevator_trim_limit = 15.0
spoiler_limit = 40.0
aileron_to_spoileron_gain = 1.60
min_ailerons_for_spoilerons= 5.0 //0.0 new
min_flaps_for_spoilerons = 0.0
spoilerons_available = 1
[electrical]
max_battery_voltage = 25.2
generator_alternator_voltage = 28.5
max_generator_alternator_amps = 60
electric_always_available = 0
[pitot_static]
vertical_speed_time_constant= 1 //20 //4.0 //Increasing this value will cause a more instantaneous reaction in the VSI
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
[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
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second
[Reference Speeds]
flaps_up_stall_speed = 78.0 //66.0 ? //CAS lower ?
full_flaps_stall_speed = 60.0 //52.8 ? //CAS higher ?
cruise_speed = 165.0 //TAS
max_indicated_speed = 175 //IAS
max_mach = 0.60
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed= 800 //1000.0
autothrottle_available= 0 //1 for test !
autoland_available=1
pitch_takeoff_ga= 10.0 //8.0
autothrottle_arming_required=0
autothrottle_takeoff_ga= 1 //0 !temp
autothrottle_max_rpm= 100.0
max_pitch=10.0
max_pitch_acceleration= 2.0 //1.0 //more?
max_pitch_velocity_lo_alt=4.0 //2.0 // ?
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank= 25.0
max_bank_acceleration = 1.8
max_bank_velocity = 3.0
max_throttle_rate = 0.2 //0.1
nav_proportional_control=9.0
nav_integrator_control= 0.25
nav_derivative_control= 0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=14.0 //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
[Flaps.0] //Lift
type=1
span-outboard=0.500
extending-time=5.700
system_type=0
damaging-speed = 175
blowout-speed = 175
lift_scalar=1.00
drag_scalar=0.00 //1.00
pitch_scalar=1.00
flaps-position.0= 0.0,
flaps-position.1=12.0, 175 //10.0
flaps-position.2=22.0, 150 //20.0
flaps-position.3=30.0, 125 //0.5236 rad
[Flaps.1] //Drag
type=1
span-outboard=0.500
extending-time=5.700
system_type=0
damaging-speed = 175
blowout-speed = 175
lift_scalar=0.00 //1.00
drag_scalar=1.00
pitch_scalar=0.00 //1.00
flaps-position.0= 0.0,
flaps-position.1= 3.5, 175 //8.0
flaps-position.2=14.0, 150 //18.0
flaps-position.3=30.0, 125 //0.5236 rad
[brakes]
toe_brakes_scale=0.68
parking_brake=1
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=3000
[stall_warning]
type=2
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0 // 0=None, 1=Electric Gyro, 2=Vacuum Gyro
[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
[airspeed_indicators]
airspeed_indicator.0 = 1.067, -10.0 //Reads 161 kts at CAS = 160 kts
[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[fltsim.1]
title=Cessna Grand Caravan! Deluxe - Air Caraibes
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=CARAIBES
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=F-OHQN
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Air Caraibes
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[fltsim.2]
title=Cessna Grand Caravan! Deluxe- Kato Air
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=KATO
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=LN-KAT
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Kato Air
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[fltsim.3]
title=Cessna Grand Caravan! Deluxe - Linear Air
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=LINEAR
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=N610LA
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Linear Air
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[fltsim.4]
title=Cessna Grand Caravan! Deluxe - Macair
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=MACAIR
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=VH-TFS
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Macair
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[fltsim.5]
title=Cessna Grand Caravan! Deluxe - Pacific Wings N303PW
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=PACIFIC1
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=N303PW
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Pacific Wings
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[fltsim.6]
title=Cessna Grand Caravan! Deluxe - San Juan Airlines N1030N
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=SANJUAN1
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=N1030N
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=San Juan Airlines
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
[fltsim.7]
title=Cessna Grand Caravan! Deluxe - Sansa HP-1402APP
sim=Cessna208B-FT
model=
panel=vfr
sound=
texture=SANSA1
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=HP-1402APP
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type=feelThere Caravan! Deluxe
ui_variation=Sansa
description=C208B Passenger
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0
Regards
/Martin Jacobsson
Post Edited ( 11-28-05 23:32 )