[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