[fltsim.0] title=Classic USAir 737-201 sim=USAir732 model= panel= sound= texture= kb_checklists=Boeing737-400_check kb_reference=Boeing737-400_ref atc_id=N322US atc_airline=US AIR atc_flight_number=427 ui_manufacturer=Boeing ui_type=737-200 ui_variation=USAir description=There were 64 of these JT8D-7 + JT8D-9 powered 737-200's in USAir's fleet. Many of them now are being moved across to the MetroJet operation. These aircraft are the oldest 737's in the current fleet with an average age of 15.7 years. Those 737-200's still in the mainline fleet are configured with 110 seats\s eight business and 102 coach.\n [forcefeedback] 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=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 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 [ground_reaction] main_gear_static_compression=1.0 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.8 // (feet), The distance the center gear strut is compressed when at rest on the ground main_gear_damping_ratio=0.9 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=0.9 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [General] performance=Engine's type: P & W JT8D-9A \nWing span: 93 ft\nTake-off thrust (lb): 15,500\nCruise speed: .74 mach \nLength: 100ft 2in\nMax. T\/O weight: 117,000 lb. \nWingspan: 93ft 0in\nFuselage width: 12ft 4in\nMax range (nm): 1,350\nMax payload (lb): 29,250\nNo of seats: 110\n\n [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=85000.000000 empty_weight_roll_MOI=1062809.000000 empty_weight_pitch_MOI=1411739.000000 empty_weight_yaw_MOI=1779732.000000 empty_weight_coupled_MOI=1300.000000 [fuel] LeftMain=-3.000000,-19.000000,0.000000,1400.000000,0.000000 RightMain=-3.000000,19.000000,0.000000,1400.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=980.000000 wing_span=93.000000 wing_root_chord=10.500000 wing_dihedral=5.998535 wing_incidence=0.000000 wing_twist=-0.994263 oswald_efficiency_factor=4.997227 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=408.000000 htail_span=41.666667 htail_pos_lon=-37.166667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=305.000000 vtail_span=19.912308 vtail_sweep=0.000000 vtail_pos_lon=-37.166667 vtail_pos_vert=5.833333 elevator_area=102.000000 aileron_area=39.200000 rudder_area=51.850000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=1 aileron_to_spoileron_gain=3.000000 min_ailerons_for_spoilerons=9.969466 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1.000000,32.916667,0.000000,-8.083333,1181.102362,0.000000,1.219307,53.700000,0.800000,2.500000,0.900000,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-4.250000,-8.583333,-9.333333,1574.803150,1.000000,1.219307,0.000000,1.000000,2.500000,0.900000,6.900000,6.900000,2.000000,0.000000,0.000000 point.2=1.000000,-4.250000,8.583333,-9.333333,1574.803150,2.000000,1.219307,0.000000,1.000000,2.500000,0.900000,7.100000,7.100000,3.000000,0.000000,0.000000 point.3=2.000000,-15.000000,-46.500000,2.250000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-15.000000,46.500000,2.250000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-48.000000,0.000000,1.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,34.833333,0.000000,1.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=0.000000 static_cg_height=7.790762 [Flaps.0] type=1 span-outboard=0.500000 extending-time=7.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=4.999057,0.000000 flaps-position.2=9.998114,0.000000 flaps-position.3=14.997170,0.000000 flaps-position.4=19.996227,0.000000 flaps-position.5=24.995284,0.000000 flaps-position.6=29.994341,0.000000 flaps-position.7=34.993397,0.000000 flaps-position.8=39.992454,0.000000 [GeneralEngineData] engine_type=1 Engine.0=5.416667,-15.833333,-2.583333 Engine.1=5.416667,15.833333,-2.583333 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.002000 inlet_area=19.600000 rated_N2_rpm=29920.000000 static_thrust=15900.000000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=142.000000 full_flaps_stall_speed=113.600000 cruise_speed=395.374600 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=35.832923,0.000000,4.588050 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=3,0