[fltsim.0]
title=ATR42-300 Pan Am
sim=ATR42-300 Pan Am
model=
panel=
sound=
texture=
checklists=
kb_checklists=checklist
ATR42-300Pan Am Express\nModel Design & Textures:Terry Gaff\nRepaint: Alf Werner \/ FS BERLIN \/ 07.2002\nPan AM Express used 4  ATR 42-300 to Berlin. Registration N4203G was used to Tegel and Tempelhof from 1988. In the year 1991 Pan Am Express ended the service in Berlin\n\n\n\n\n\n\n\n
ui_manufacturer=ATR
ui_type=42-300
ui_variation=Pan Am Express
atc_heavy=0
atc_id=N4203G
atc_airline=PAN AM
atc_flight_number=420
description=ATR42-300Pan Am Express\nModel Design & Textures:Terry Gaff\nRepaint: Alf Werner \/ FS BERLIN \/ 07.2002\nPan AM Express used 4  ATR 42-300 to Berlin. Registration N4203G was used to Tegel and Tempelhof from 1988. In the year 1991 Pan Am Express ended the service in Berlin. \n\n\n\n\n\n\n\n

[WEIGHT_AND_BALANCE]
empty_weight= 37655.000
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.0=0.000, 0.000, 0.000, 0.000
empty_weight_roll_MOI= 718955.000
empty_weight_pitch_MOI= 778504.000
empty_weight_yaw_MOI= 721882.000
empty_weight_coupled_MOI= 2000.000
max_gross_weight= 48857.400
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[turboprop_engine]
power_scalar=1.0
maximum_torque= 8275.000

[propeller]
thrust_scalar=1.2
propeller_type= 0
propeller_diameter= 8.950
propeller_blades= 4
propeller_moi= 60.000
beta_max= 86.500
beta_min= 0.000
min_gov_rpm= 26150.000
prop_tc= 0.001
gear_reduction_ratio= 16.000
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= 1
min_rpm_for_feather= 700.000
beta_feather= 86.500
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 1
minimum_on_ground_beta= 0.000
minimum_reverse_beta= -15.000

[pitot_static]
vertical_speed_time_constant=1.1

[flight_tuning]
cruise_lift_scalar=1.1
parasite_drag_scalar=1.0
induced_drag_scalar=1.0

[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

[electrical]
max_battery_voltage=28.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=40.0
avionics_bus=0, 0, 1
avionics=1, 0, 1
starter1=0, 0, 1
starter2=0, 0, 1
fuel_transfer_pump=0, 0, 1
flap_motor=0, 0, 1
gear_motor=0, 0, 1
autopilot=0, 0, 1
pitot_heat=0, 0, 1
additional_system=0, 0, 1
marker_beacon=1, 0, 1
fuel_pump=0, 0, 1=0, 0, 1
gear_warning=0, 0, 1
light_nav=0, 0, 1
light_beacon=0, 0, 1
light_landing=0, 0, 1
light_taxi=0, 0, 1
light_strobe=0, 0, 1
light_panel=0, 0, 1
auto_brake=0, 0, 1
standby_vacuum=0, 0, 1
hydraulic_pump=0, 0, 1
light_recognition=0, 0, 1
light_wing=0, 0, 1
light_logo=0, 0, 1

[General]
performance=ATR42-300\nWing span:\n27.05 m \/ 88.9 ft\nLength:\n26.30 m \/ 86.3 ft\nHeight:\n7.58 m \/ 24.9 ft\nWing area:\n90.1 m2 \/ 970 sqft\nMax. Fuel Weight:\n4,508 kg \/ 1506 gal\nMax. Take Off Weight:\n15,750 kg \/ 34,725 lb\nEngine: PW120\nPropeller HS 247F, 4 blade\n\nPassengers: 42 max. 50\nMax. speed Vmo:\n250 KIAS\nCruise speed:\n280 KTAS at FL170
atc_type=
atc_model=

[fuel]
LeftMain= -1.540, -14.900, 5.100, 836.000, 5.000
RightMain= -1.540, 14.900, 5.100, 836.000, 5.000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 970.000
wing_span= 88.833
wing_root_chord= 8.833
wing_dihedral= 2.000
wing_incidence= 1.851
wing_twist= 0.000
oswald_efficiency_factor= 0.818
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 126.000
htail_span= 24.583
htail_pos_lon= -24.833
htail_pos_vert= 0.000
htail_incidence= 0.500
htail_sweep= 0.000
vtail_area= 160.000
vtail_span= 14.422
vtail_sweep= 0.000
vtail_pos_lon= -46.083
vtail_pos_vert= 14.333
elevator_area= 40.500
aileron_area= 50.500
rudder_area= 44.500
elevator_up_limit= 22.918
elevator_down_limit= 22.918
aileron_up_limit= 22.918
aileron_down_limit= 22.918
rudder_limit= 22.918
elevator_trim_limit= 14.324
spoiler_limit= 45.837
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.000, 28.167, 0.000, -5.083, 1574.803, 0.000, 0.839, 50.280, 0.416, 2.500, 3.078, 12.000, 12.000, 0.000, 0.000, 0.000
point.1= 1.000, -4.333, -6.583, -5.267, 1574.803, 1.000, 0.839, 0.000, 0.736, 2.500, 0.661, 12.000, 12.000, 2.000, 0.000, 0.000
point.2= 1.000, -4.333, 6.583, -5.267, 1574.803, 2.000, 0.839, 0.000, 0.736, 2.500, 0.661, 12.000, 12.000, 3.000, 0.000, 0.000
point.3= 2.000, -7.667, -44.583, 5.083, 787.402, 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, -7.667, 44.583, 5.083, 787.402, 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, -53.250, 0.000, 3.583, 787.402, 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, 35.833, 0.000, -1.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= -0.500
static_cg_height= 4.168

[GeneralEngineData]
engine_type= 5
Engine.0= 5.167, -6.667, 3.083
Engine.1= 5.167, 6.667, 3.083
fuel_flow_scalar= 0.856

[TurbineEngineData]
fuel_flow_gain= 0.056
inlet_area= 1.100
rated_N2_rpm= 29995.000
static_thrust= 200.000
afterburner_available= 0

[Reference Speeds]
flaps_up_stall_speed= 97.000
full_flaps_stall_speed= 75.600
cruise_speed= 260.512

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=27.669271,-1.935183,2.588788

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1700.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=99.000000
use_no_default_pitch=1use_no_default_bank=1
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=3,0

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1
Transponder.1=1
Marker.1=1

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 8.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 9.931, 0.000
flaps-position.2= 19.863, 0.000
flaps-position.3= 29.794, 0.000