[fltsim.0] JABIndex=1 title=DH82a Tiger Moth 1937 sim=dh82 model=1 panel=1 sound= texture=1 checklists= kb_checklists=DH82_check kb_reference=DH82_ref kb_notes=DH82_notes ui_manufacturer=De Havilland ui_type=DH82 Tiger Moth ui_variation=1937 RAF Trainer K4242 description=De Havilland's basic trainer. The Tiger Moth was a derivative of the DH60T Moth trainer adapted to the requirements of the RAF.\n K4242 is shown in pre WW2 RAF trainer yellow.\n atc_heavy=0 atc_id=K4242 atc_airline= atc_flight_number= [fltsim.1] JABIndex=2 title=DH82a Tiger Moth 1940 sim=dh82 model=2 panel= sound= texture=2 checklists= kb_checklists=DH82_check kb_reference=DH82_ref kb_notes=DH82_notes ui_manufacturer=De Havilland ui_type=DH82 Tiger Moth ui_variation=1940 RAF Trainer R5130 description=De Havilland's basic trainer. The Tiger Moth was a derivative of the DH60T Moth trainer adapted to the requirements of the RAF.\n R5130 survived the war and was converted to a four seat Jackaroo.\n atc_heavy=0 atc_id=R5130 atc_airline= atc_flight_number= [fltsim.2] JABIndex=3 title=DH82a Tiger Moth 1942 sim=dh82 model= panel= sound= texture= checklists= kb_checklists=DH82_check kb_reference=DH82_ref kb_notes=DH82_notes ui_manufacturer=De Havilland ui_type=DH82 Tiger Moth ui_variation=1942 RAF Trainer DE208 description=De Havilland's basic trainer. The Tiger Moth was a derivative of the DH60T Moth trainer adapted to the requirements of the RAF.\n DE-208 is still flying and is based at Jurby in the Isle of Man.\n atc_heavy=0 atc_id=DE208 atc_airline= atc_flight_number= [General] performance=Span\t29ft4ins\nLength\t23ft11ins\nWeight (empty)\t1,115lb.\nPower:\tDH.Gypsy Major 4 cyl. 130 hp\nDesigner:\tJohn Woodside 2002 atc_type=dehavilland atc_model=AA5 [propeller] thrust_scalar=0.82 // evolved propeller_type= 1 propeller_diameter= 6.300 // checked propeller_blades= 2 // checked propeller_moi= 5.000 beta_max= 0.000 beta_min= 0.000 min_gov_rpm= 500.000 prop_tc= 0.100 gear_reduction_ratio= 1.000 fixed_pitch_beta= 21.200 // evolved low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 [piston_engine] power_scalar=1.0 max_rpm_mechanical_efficiency_scalar=1.0 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 cylinder_displacement= 90.3 // evolved compression_ratio= 5.25 // checked number_of_cylinders= 4 max_rated_rpm= 2350.000 // checked max_rated_hp= 130.000 // checked fuel_metering_type= 1 // checked cooling_type= 0 // checked normalized_starter_torque= 0.300 turbocharged= 0 max_design_mp= 0.000 min_design_mp= 0.000 critical_altitude= 0.000 // n/a emergency_boost_type= 0 // n/a emergency_boost_mp_offset= 0.000 // n/a emergency_boost_gain_offset= 0.000 // n/a fuel_air_auto_mixture= 0 auto_ignition= 0 [flight_tuning] cruise_lift_scalar=0.503 pitch_stability=1.000 roll_stability=1.00 yaw_stability=1.101 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.00 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.200, 0.000, 0.000 max_number_of_stations=50 station_load.0= 135.000, 0.500, 0.000, 0.000 empty_weight= 1115.000 // checked empty_weight_roll_MOI= 1500.000 empty_weight_pitch_MOI= 1596.000 empty_weight_yaw_MOI= 3000.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 1825.000 // checked CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1=0.500, 0.000, 3.000, 22.800, 1.000 fuel_type=1.000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 239.000 // checked wing_span= 41.00 // should be 29.33 but adjusted for biplane wing_root_chord= 4.383 // checked wing_dihedral= 2.750 // checked wing_incidence= 2.000 // checked but reduced from 4 to 2 wing_twist= 0.000 // checked oswald_efficiency_factor= 0.800 // no idea wing_winglets_flag= 0 wing_sweep= 5.8156 // checked - top wing wing_pos_apex_lon= 2.000 wing_pos_apex_vert= 3.000 htail_area= 27.200 // checked htail_span= 9.8300 // checked htail_pos_lon= -12.500 htail_pos_vert= 2.600 htail_incidence= 0.000 // checked htail_sweep= 0.000 // checked vtail_area= 12.200 // checked vtail_span= 3.950 // checked vtail_sweep= 0.000 // checked vtail_pos_lon= -12.500 vtail_pos_vert= 2.600 elevator_area= 13.800 // checked aileron_area= 22.400 // checked rudder_area= 9.400 // checked elevator_up_limit= 27.500 // checked elevator_down_limit= 20.000 // checked aileron_up_limit= 19.481 aileron_down_limit= 10.00 rudder_limit= 31.5 // checked elevator_trim_limit= 19.481 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 [contact_points] // FORE LEFT UP ROD BRAKE WH RA STANG SCOM C/R DR EXT RET ST AL D/AS point.0= 3, -16.0, 0.0, -1.7, 1180.0, 0, 0.115, 31.0, 0.388, 2.5, 0.835, 0.0, 0.0, 0.0, 0.0, 0.0 //TAIL point.1= 1, 1.5, -2.5, -5.2, 1574.0, 0, 0.765, 0.0, 0.428, 2.5, 0.750, 0.0, 0.0, 2.0, 0.0, 0.0 //LEFT point.2= 1, 1.5, 2.5, -5.2, 1574.0, 0, 0.765, 0.0, 0.428, 2.5, 0.750, 0.0, 0.0, 3.0, 0.0, 0.0 //RIGHT point.3= 2, -1.5, -14.4, -1.0, 787.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 //LWS point.4= 2, -1.5, 14.4, -1.0, 787.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0 //RWS point.5= 2, 6.0, 0.0, -2.5, 787.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0 //TS static_pitch= 11.5000 static_cg_height=4.4827 [GeneralEngineData] engine_type= 0 Engine.0= 7.180, 0.000, 1.100 fuel_flow_scalar= 1.000 [Reference Speeds] flaps_up_stall_speed= 39.000 // checked full_flaps_stall_speed= 37.000 // checked - all values not run through FSEdit cruise_speed= 74.000 // checked - so they may not produce any effect. [keyboard_response] elevator=150.000, 250.000 aileron=150.000, 250.000 rudder=150.000, 250.000 [Views] eyepoint=-2.958, 0.000, 1.5416 [electrical] max_battery_voltage = 0 generator_alternator_voltage = 0 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=1,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 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
