//cfg file updated by Greg D. Swagler, SpectroGrafx Productions, Inc.
//www.sgpi.net - July 10, 2004
//Repaint by John Elliott Young (J.E.Young@bluestreamair.com)
//
[fltsim.0]
title=de Havilland C-7 Caribou - BSA Patriot
sim=caribou
model=
panel=
sound=
texture=
panel_alias =
sound_alias =
kb_checklists=
kb_reference=
tc_id_enable=1
atc_id=N949BS
ui_manufacturer=de Havilland
ui_type=C-7 Caribou
ui_variation="Bluestream Airlines - Patriot - N949BS"
description="This is the special patriotic painted version of the BSA airlines Caribou. This plane runs normal operations for BSA as well as attending airshows and other special events.\n \nThe DeHavilland-built Caribou transport aircraft was designed with Short Take-Off and Landing (STOL) characteristics. It featured a conventional stressed skin construction and had a cantilever wing with full-span double-slotted flaps with the outer portions acting as ailerons. It was the first DeHavilland Canada aircraft to feature a retractable undercarriage.\n \nThe RCAF initially selected the Caribou to fulfill UN support duties for the Congo purchasing four aircraft along with a range of support equipment. The aircraft were never deployed to the Congo but did see action in an extensive range of UN missions. The Caribou also proved popular with other armed forces such as the United States Army and the Royal Australian and Malaysian Air Forces."
atc_heavy=0
atc_airline=BLUESTREAM AIR
atc_flight_number=602
visual_damage=1
atc_parking_codes=BSC
atc_parking_types=RAMP
[fltsim.1]
title=de Havilland C-7 Caribou - BSA
sim=caribou
model=
panel=
sound=
texture=1
panel_alias =
sound_alias =
kb_checklists=
kb_reference=
tc_id_enable=1
atc_id=N950BS
ui_manufacturer=de Havilland
ui_type=C-7 Caribou
ui_variation="Bluestream Airlines - N950BS"
description= "Repainted by John Elliott Young for Bluestream Airlines livery. (www.bluestreamair.com)\n \nThe DeHavilland-built Caribou transport aircraft was designed with Short Take-Off and Landing (STOL) characteristics. It featured a conventional stressed skin construction and had a cantilever -wing with full-span double-slotted flaps with the outer portions acting as ailerons. It was the first DeHavilland Canada aircraft to feature a retractable undercarriage.\n \nThe RCAF initially selected the Caribou to fulfill UN support duties for the Congo purchasing four aircraft along with a range of support equipment. The aircraft were never deployed to the Congo but did see action in an extensive range of UN missions. The Caribou also proved popular with other armed forces such as the United States Army and the Royal Australian and Malaysian Air Forces. The Caribou has seen extensive use as a light tactical transport in a variety of military and now civilian uses."
atc_heavy=0
atc_airline=BLUESTREAM AIR
atc_flight_number=601
visual_damage=1
atc_parking_codes=BSC
atc_parking_types=RAMP
[General]
atc_type=Dehavilland
atc_model=c7
editable=1
performance="Crew/Passengers: 2 pilots, 1 flt engineer & 30 passengers or 32 troops\n \nWing Span: 95 feet 7.5 inches\n\nLength: 72 feet 7 inches\n\nHeight:31 feet 9 inches\n\nMaximum Gross Weight: 28,500 pounds\n\nPowerplants: 2 Pratt & Whitney R2000-7M2\n\nNormal operations - 33,000 pounds for ferry operations\n\nMaximum Speed: 214 mph (344 km/h)\nCruising Speed: 180 mph (290 km/h)\nService Ceiling: 27,500 ft (8,381 m)"
[WEIGHT_AND_BALANCE]
max_gross_weight = 28500.000
empty_weight = 18250.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations =50
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 = 400000.000
empty_weight_roll_MOI = 200000.000
empty_weight_yaw_MOI = 400000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0=0.000000,0.000000,0.000000,0.000000
[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
[GeneralEngineData]
engine_type = 0
Engine.0 = -7.000, -11.800, 1.600
Engine.1 = -7.000, 11.800, 1.600
fuel_flow_scalar = 1.000
min_throttle_limit=-0.250000
[piston_engine]
power_scalar =1.000
cylinder_displacement= 170.000
compression_ratio= 8.700
number_of_cylinders= 14
max_rated_rpm= 2700.000
max_rated_hp= 1450.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 1
max_design_mp= 51.000
min_design_mp= 10.000
critical_altitude= 25000.000
emergency_boost_type= 1
emergency_boost_mp_offset= 51.000
emergency_boost_gain_offset= 2.800
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
[propeller]
thrust_scalar =1.000
propeller_type= 0
propeller_diameter= 14.000
propeller_blades= 3
propeller_moi= 72.000
beta_max= 45.000
beta_min= 8.000
min_gov_rpm= 1100.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.000
beta_feather= 70.000
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[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 = 1.000, 17.700, 0.000, -8.300, 1600.000, 0.000, 1.100, 40.000, 0.500, 0.500, 1.000, 4.000, 4.000, 0.000, 0.000, 0.000
point.1 = 1.000, -5.000, -11.700, -8.300, 1600.000, 1.000, 1.400, 0.000, 0.500, 2.500, 0.850, 4.000, 4.000, 2.000, 0.000, 0.000
point.2 = 1.000, -5.000, 11.700, -8.300, 1600.000, 2.000, 1.400, 0.000, 0.500, 2.500, 0.850, 4.000, 4.000, 3.000, 0.000, 0.000
//SCRAPES
point.3= 2.000, 0.760, -18.910, 0.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, 0.760, 18.910, 0.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -17.080, 0.000, -0.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 7.360, 0.000, -1.240, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 0.000
static_cg_height = 8.000
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 = -8.213, -0.8612, 2.220 //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -0.17, -39.50, 2.14, fx_navred ,
light.1 = 3, -0.17, 39.50, 2.14, fx_navgre ,
light.2 = 3, -38.36, 0.00, 1.99, fx_navwhi ,
light.3 = 2, -0.34, -39.50, 2.14, fx_strobe ,
light.4 = 2, -0.34, 39.50, 2.14, fx_strobe ,
light.5 = 1, -11.81, 0.00, -5.48, fx_beacon ,
light.6 = 2, -35.39, 0.00, 17.05, fx_beacon ,
light.7 = 4, 12.62, 0.00, 2.15, 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 = -2.000, -12.000, 0.000, 300.000, 0.000
RightMain = -2.000, 12.000, 0.000, 300.000, 0.000
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[airplane_geometry]
wing_area = 950.000
wing_span = 95.000
wing_root_chord = 11.500
wing_dihedral = 2.000
wing_incidence = 0.000
wing_twist = -1.000
oswald_efficiency_factor= 0.800
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 0.000
wing_pos_apex_vert = 0.000
htail_area = 200.000
htail_span = 38.000
htail_pos_lon = -38.000
htail_pos_vert = 8.500
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 170.000
vtail_span = 11.500
vtail_sweep = 5.000
vtail_pos_lon = -36.000
vtail_pos_vert = 5.000
elevator_area = 30.000
aileron_area = 64.000
rudder_area = 71.000
elevator_up_limit = 17.000
elevator_down_limit = 15.500
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 30.000
elevator_trim_limit = 5.000
spoiler_limit = 0.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 100.000
full_flaps_stall_speed = 70.000
cruise_speed = 158.000
max_indicated_speed = 200.000000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
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
[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
[brakes]
toe_brakes_scale=1.000000
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=0.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 4.000
system_type= 0
damaging-speed= 150.000
blowout-speed= 250.000
lift_scalar= 0.600
drag_scalar= 0.500
pitch_scalar= 0.600
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 40.000, 0.000
flaps-position.3= 80.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.400
extending-time= 4.000
system_type= 0
damaging-speed= 150.000
blowout-speed= 250.000
lift_scalar= 0.400
drag_scalar= 0.300
pitch_scalar= 0.400
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 40.000, 0.000
