*************************************************************** Flight Dynamics for the Fiat G.12CR with Fiat A.74 RC42 engines *************************************************************** [fltsim.0] title=G12CR sim=G12CR model= panel= sound= texture= kb_checklists= kb_reference=G12CR_ref atc_id=605-5 ui_manufacturer=Fiat ui_type=1941 G.12-CR ui_variation=605th Squad. Regia Areonautica atc_heavy=0 atc_airline= atc_flight_number= description=The original 12 seat G.12C was rejected by all potential buyers. The 14 seat G.12CR for ultra short routes added a bench seat facing the door and was certificated for take off at no more than 12,800Kg (28,219lbs). However with full fuel the CR could lift only four passengers plus bags. During the summer of 1941 the first CR became the VIP transport of the Chief of the General Staff based at Rome (LIRU) flying to everywhere Italian troops were serving. Four more later flew scheduled VIP / diplomatic services with Nucleo Comunicazioni A.L.I. as part of the wartime 'Special Air Service' based at Rome (LIRA). One later served with 605 Sq flying CASEVAC missions from the Ukraine. See G.12 History.rtf in common folder. Skin by Manuele Villa, May 2009. [General] atc_type=Fiat atc_model=G12 performance=Press F10 and then lowest icon for step by step on screen handling notes. Read 'How to fly the Fiat G.12' in the G.12 'common folder' before flight. [Views] eyepoint = 5.7, -1.325, 4.85 [WEIGHT_AND_BALANCE] empty_weight = 22495 ;including lubricating oil, equipment, avionics etc max_gross_weight = 28219 ;Fiat G.12CR reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 station_load.0 = 800, 0, 0, 0 ;4 crew with bags station_load.1 = 800, 0, 0, 0 ;4 pax with bags With full fuel the Fiat G.12CR could carry only four passengers plus bags. Full fuel and restricted payload is loaded by default in FS9 to allow the longest routes flown in real life to also be flown in FS9. Moments of Inertia empty_weight_pitch_MOI = 170000 empty_weight_roll_MOI = 500000 empty_weight_yaw_MOI = 600000 empty_weight_coupled_MOI = 0.000 [fuel] Max fuel 4,123lbs and is loaded by default. LeftMain = 0, 0, 0, 229, 0 RightMain = 0, 0, 0, 229, 0 Center1 = 0, 0, 0, 229, 0 fuel_type = 1 number_of_tank_selectors=1 electric_pump=0 [GeneralEngineData] engine_type = 0 engine.0 = 10.30, -9.14, -0.16 engine.1 = 23.65, 0, 1.67 engine.2 = 10.30, 9.14, -0.16 min_throttle_limit = 0 master_ignition_switch = 1 fuel_flow_scalar = 1.014 [piston_engine] Fiat A.74 RC42 cylinder_displacement = 136.2 compression_ratio = 6.7 number_of_cylinders = 14 critical_altitude = 7600 //adjusted to rated RPM max_design_mp = 37.5 //1.26C max_rated_rpm = 2520 //TOGA and emergency max_rated_hp = 820 //TOGA and emergency fuel_metering_type = 1 turbocharged = 1 min_design_mp = 0 emergency_boost_type = 0 emergency_boost_mp_offset = 0 emergency_boost_gain_offset = 0 fuel_air_auto_mixture = 1 auto_ignition = 0 emergency_boost_duration = 0 cooling_type = 1 normalized_starter_torque = 0.25 max_rpm_mechanical_efficiency_scalar = 1 idle_rpm_mechanical_efficiency_scalar = 1 max_rpm_friction_scalar = 1 idle_rpm_friction_scalar = 1 [propeller] //Hamilton Standard constant speed screw built under licence by Fiat. propeller_type = 0 propeller_diameter = 7.5 propeller_blades = 3 gear_reduction_ratio = 1 propeller_moi = 6 beta_max = 65 beta_min = 15 min_gov_rpm = 600 prop_tc = 0.01 fixed_pitch_beta = 0 low_speed_theory_limit = 80 prop_sync_available = 0 prop_deice_available = 0 prop_feathering_available = 1 feathering_switches = 1 prop_auto_feathering_available=0 min_rpm_for_feather=700 beta_feather=88 defeathering_accumulators_available =0 prop_reverse_available =0.000000 minimum_on_ground_beta =0.000000 minimum_reverse_beta=0.000000 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 [airplane_geometry] oswald_efficiency_factor= 0.74 wing_area = 1222 ;113.5 square metres wing_span = 94.2 ;28.72 metres wing_root_chord = 13 wing_pos_apex_lon = 3.25 wing_pos_apex_vert = -3 htail_area = 175 htail_span = 20 htail_pos_lon = -30 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 81 vtail_span = 10 vtail_sweep = 0 vtail_pos_lon = -30 vtail_pos_vert = 3 elevator_area = 75 aileron_area = 37 rudder_area = 37 elevator_up_limit = 18 elevator_down_limit = 15 aileron_up_limit = 18 aileron_down_limit = 18 rudder_limit = 25 elevator_trim_limit = 15 spoiler_limit = 60 ;used for cowl varied engine drag spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 wing_dihedral = 0 wing_incidence = 0 wing_twist = 0 wing_winglets_flag = 0 wing_sweep = 0 [Flaps.0] Max flap was 48 degrees. The crew could select any angle. The angles below are the recommended angles for max gross departure and typical landing weight. I suspect the crew selected 20 then 45 during approach without using 15, but we must select flap stage by stage in MSFS. See on screen handling notes and 'How to fly the Fiat G.12'. type= 1 span-outboard= 0.5 extending-time= 22 system_type = 1 flaps-position.0= 0,0 flaps-position.1= 15, 95 flaps-position.2= 20, 95 flaps-position.3= 45, 95 [Reference Speeds] full_flaps_stall_speed = 57 flaps_up_stall_speed = 74 cruise_speed = 171 max_indicated_speed = 189 //estimated [brakes] parking_brake = 1 toe_brakes_scale = 0.35 [contact_points] static_pitch = 13 static_cg_height = 9 tailwheel_lock = 1 gear_system_type=1 point.0 = 1, -41.27, 0, 0.1, 800, 0, 0.94, 40, 0.19, 2, 0.8, 8, 8, 0, 95, 95 point.1 = 1, 1, -9.1, -9, 1200, 1, 2.06, 0, 0.22, 2, 0.8, 8, 8, 2, 95, 95 point.2 = 1, 1, 9.1, -9, 1200, 2, 2.06, 0, 0.22, 2, 0.8, 9, 9, 3, 95, 95 point.3 = 2, -2.2609, 47.0354, 2.36, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.4 = 2, -2.2609, -47.0354, 2.36, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.5 = 2, 17.1406, 0, -3.8369, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.6 = 2, -43.3417, 0, 16.3464, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.7 = 2, -49.9017, 0, 6.2648, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.8 = 2, 1.8, -26, 0, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.9 = 2, 1.8, 26, 0, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.1 flap_limit_power=16.0 flap_limit_idle=0.0 [hydraulic_system] normal_pressure = 732.0 electric_pumps = 0 engine_map = 1,1,0 [Radios] Com.1 = 1 Nav.1 = 1 Adf.1 = 1 Audio.1 = 1 Marker.1 = 1 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -3.07, -47.35, 2.1, fx_navred light.1 = 3, -3.07, 47.35, 2.1, fx_navgre light.2 = 3, -51.0, 0, 5.95, fx_navwhi light.3 = 4, 7, 0, 3.7, fx_vclight light.4 = 4, -22.7, 0, 4.4, fx_vclight light.5 = 5, 0.03, -25.54, -0.34, fx_SM74_landing light.6 = 5, 0.03, 25.54, -0.34, fx_SM74_landing light.7 = 5, 1.03, -25.54, -0.34, Newll light.8 = 5, 1.03, 25.54, -0.34, Newll [keyboard_response] elevator =200, 1000 aileron =200, 1000 rudder =200, 1000 [direction_indicators] direction_indicator.0=1,0 direction_indicator.1=2,0 [attitude_indicators] attitude_indicator.0 = 1 attitude_indicator.1 = 2 [turn_indicators] turn_indicator.0=2,0 [stall_warning] type=1 [exits] number_of_exits = 1 exit_rate.0 = 0.27 ;Percent per second [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 25 max_generator_alternator_amps = 100 [autopilot] autopilot_available= 0 [forcefeedback] //not tested ground_bumps_magnitude1 = 2600 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5.0 ground_bumps_slope1 = 0.6 ground_bumps_magnitude2 = 1200 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.085 ground_bumps_slope2 = 0.65 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 3500000