├── C152X ├── ModelBehaviorDefs │ └── C152X │ │ └── Asobo │ │ ├── Common.xml │ │ ├── Common │ │ ├── Index.xml │ │ ├── Instrument.xml │ │ └── Subtemplates │ │ │ └── Instrument_Subtemplates.xml │ │ └── NAVCOM │ │ ├── ADF.xml │ │ └── NavComSystem.xml ├── SimObjects │ └── Airplanes │ │ └── Asobo_C152 │ │ ├── Approach.flt │ │ ├── Climb.flt │ │ ├── Cruise.flt │ │ ├── Final.flt │ │ ├── aircraft.cfg │ │ ├── apron.flt │ │ ├── cockpit.cfg │ │ ├── engines.cfg │ │ ├── flight_model.cfg │ │ ├── hangar.flt │ │ ├── model │ │ └── Cessna152_interior.XML │ │ ├── panel │ │ ├── PANEL.CFG │ │ └── panel.xml │ │ ├── runway.FLT │ │ ├── systems.cfg │ │ ├── target_performance.cfg │ │ └── taxi.flt ├── de-DE.locPak ├── en-US.locPak ├── es-ES.locPak ├── fr-FR.locPak ├── it-IT.locPak ├── layout.json ├── manifest.json ├── pl-PL.locPak ├── pt-BR.locPak └── ru-RU.locPak └── README.md /C152X/ModelBehaviorDefs/C152X/Asobo/Common.xml: -------------------------------------------------------------------------------- 1 | 2 | -------------------------------------------------------------------------------- /C152X/ModelBehaviorDefs/C152X/Asobo/Common/Index.xml: -------------------------------------------------------------------------------- 1 | 2 | 3 | 4 | -------------------------------------------------------------------------------- /C152X/ModelBehaviorDefs/C152X/Asobo/Common/Instrument.xml: -------------------------------------------------------------------------------- 1 | 2 | 3 | 12 | 13 | 22 | 23 | -------------------------------------------------------------------------------- /C152X/ModelBehaviorDefs/C152X/Asobo/Common/Subtemplates/Instrument_Subtemplates.xml: -------------------------------------------------------------------------------- 1 | 111 | 112 | 113 | 472 | 473 | 474 | 598 | -------------------------------------------------------------------------------- /C152X/ModelBehaviorDefs/C152X/Asobo/NAVCOM/ADF.xml: -------------------------------------------------------------------------------- 1 | 2 | 3 | 12 | 13 | 78 | 79 | 80 | 89 | 90 | -------------------------------------------------------------------------------- /C152X/ModelBehaviorDefs/C152X/Asobo/NAVCOM/NavComSystem.xml: -------------------------------------------------------------------------------- 1 | 2 | 3 | 25 | 26 | 27 | 28 | 37 | 38 | 192 | 193 | 203 | 204 | 214 | 215 | 226 | 227 | 238 | 239 | 250 | 251 | 262 | 263 | 274 | 275 | 286 | 287 | 288 | 299 | 300 | 301 | 310 | 311 | -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/Approach.flt: -------------------------------------------------------------------------------- 1 | 2 | [SimVarForSpawningInTheAir.0] 3 | IAS=177 4 | FlapsDegree=0000.00 5 | 6 | [Avionics.0] 7 | Comm1Active=127.850 8 | Comm1Standby=124.850 9 | Comm2Active=124.850 10 | Comm2Standby=124.850 11 | Comm3Active=124.850 12 | Comm3Standby=124.850 13 | Nav1Active=110.50 14 | Nav1Standby=113.90 15 | OBS1=360 16 | Nav2Active=110.50 17 | Nav2Standby=113.90 18 | OBS2=360 19 | TransponderState=4 20 | ADFActive=890 21 | ADF2Active=890 22 | DMESelected=1 23 | ComTransmit=1 24 | ComReceiveBoth=False 25 | Com1Receive=True 26 | Com2Receive=False 27 | Com3Receive=False 28 | AudioNav1Listen=False 29 | AudioNav2Listen=False 30 | AudioMarkerListen=False 31 | AudioDmeListen=False 32 | AudioAdfListen=False 33 | AudioAdf2Listen=False 34 | AvionicsSwitch=True 35 | 36 | [Engine Parameters.1.0] 37 | ThrottleLeverPct=1 38 | PropellerLeverPct=0.99993896484375 39 | Pct Engine RPM=0.99956832930920125335 40 | MaxReachedEngineRPM=3903.5488821170947631 41 | LeftMagneto=True 42 | RightMagneto=True 43 | GeneratorSwitch=True 44 | FuelValveOpen=True 45 | CowlFlapPct=0 46 | FuelPumpSwitch=False 47 | FuelPumpSwitch_EX1=0 48 | FuelValveOpen=True 49 | CarbHeat/DeiceSwitch=False 50 | EngineMasterSwitch=True 51 | GlowPlugTemperaturePct=1 52 | IgnitionSwitch=0 53 | 54 | [Propeller.1.0] 55 | prop_beta=0.34139458438119674177 56 | prop_max_rpm_percent=0.99956832930920125335 57 | 58 | [Systems.0] 59 | BatterySwitch=True 60 | StructuralDeiceSwitch=False 61 | PropDeiceSwitch=False 62 | Autobrakes=0 63 | StandbyVacuum=False 64 | PropSync=False 65 | AutoFeatherSwitch=False 66 | FlightDirector=False 67 | PanelLights=False 68 | LaunchBarSwitch=False 69 | LaunchBarState=0 70 | TailhookHandle=False 71 | TailhookState=0 72 | FoldingWingsHandle=False 73 | FoldingWingsState=0, 0 74 | 75 | [LocalVars.0] 76 | ;Note these settings may override standard config settings 77 | ;-------------------------------------------- 78 | ;C152X Cessna 300 ADF 79 | XMLVAR_ADF_MODE_SEL=2 ;2='ADF' Mode 80 | XMLVAR_ADF_VOLUME=100 ;0=OFF, 100=FULL 81 | ;-------------------------------------------- 82 | ;C152X KX155 DUAL NAVCOM 83 | XMLVAR_NAVCOM_COM_1_VOLUME=100 ;0=OFF, 100=FULL 84 | XMLVAR_NAVCOM_COM_2_VOLUME=100 ;0=OFF, 100=FULL 85 | XMLVAR_NAVCOM_COM_1_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 86 | XMLVAR_NAVCOM_COM_2_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 87 | 88 | XMLVAR_NAVCOM_NAV_1_VOLUME=100 ;0=0,100=FULL 89 | XMLVAR_NAVCOM_NAV_2_VOLUME=100 ;0=0,100=FULL 90 | XMLVAR_NAVCOM_NAV_1_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 91 | XMLVAR_NAVCOM_NAV_2_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 92 | ;-------------------------------------------- 93 | ;C152X KA134 AUDIO SELECTOR 94 | XMLVAR_AUDIO_COM_1_MIC_SEL=1 ;1=SEL, (COM 1 TX SEL), MIC 1 and 2 mutually exclusive 95 | XMLVAR_AUDIO_COM_2_MIC_SEL=0 ;1=SEL, (COM 2 TX SEL), MIC 1 and 2 mutually exclusive 96 | 97 | XMLVAR_AUDIO_BOTH_SEL=0 ;0=OFF, 1=SEL 98 | XMLVAR_AUDIO_NAV_1_SEL=0 ; 99 | XMLVAR_AUDIO_NAV_2_SEL=0 ; 100 | XMLVAR_AUDIO_ADF_SEL=0 ; 101 | XMLVAR_AUDIO_DME_SEL=0 ; 102 | XMLVAR_AUDIO_MKR_SEL=1 ; 103 | XMLVAR_AUDIO_SPKR_SEL=0 ; 104 | ;-------------------------------------------- 105 | 106 | [Gauges.0] 107 | KollsmanSetting=30.079952239990234375 108 | 109 | [BleedAir.0] 110 | BleedAirSource=0 111 | 112 | [Switches.0] 113 | PitotHeat=False 114 | BeaconLights=True 115 | LandingLights=False 116 | LogoLights=True 117 | NavLights=True 118 | PanelLights=True 119 | RecognitionLights=True 120 | StrobeLights=True 121 | TaxiLights=False 122 | WingLights=True 123 | CabinLights=False 124 | GlareshieldLights=False 125 | PedestalLights=False 126 | 127 | [AutoPilot.0] 128 | MasterSwitch=True 129 | WingLeveler=False 130 | Nav1Lock=False 131 | HeadingLock=False 132 | HeadingValue=0 133 | AltitudeLock=False 134 | AltitudeValue=0 135 | AttitudeHold=False 136 | AirspeedHold=False 137 | AirspeedValue=0 138 | MachHold=False 139 | MachValue=0 140 | VerticalSpeedHold=False 141 | VerticalSpeedValue=0 142 | RPMHold=False 143 | RPMValue=0 144 | GlideslopeHold=False 145 | ApproachHold=False 146 | BackCourseHold=False 147 | YawDamper=False 148 | ToGa=False 149 | AutoThrottleArm=False 150 | GPSdrivesNAV1=False 151 | IsUsedForLesson=False 152 | ForceDisplayUI=False 153 | 154 | [Controls.0] 155 | SpoilersHandle=000.00 156 | FlapsHandle=000.00 157 | LeftFlap=000.00 158 | RightFlap=000.00 159 | GearsHandle=000.00 160 | Gear1=100.00 161 | Gear2=100.00 162 | Gear3=100.00 163 | YokeY=050.00 164 | YokeX=050.00 165 | Rudder=050.00 166 | LeftBrake=000.00 167 | RightBrake=000.00 168 | ParkingBrake=000.00 169 | 170 | RudderTrimPct=0 171 | AileronTrimPct=0 172 | AileronTrimDisabled=False 173 | ElevatorTrimDisabled=False 174 | RudderTrimDisabled=False -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/Climb.flt: -------------------------------------------------------------------------------- 1 | 2 | [SimVarForSpawningInTheAir.0] 3 | IAS=113 4 | FlapsDegree=0000.00 5 | 6 | [Avionics.0] 7 | Comm1Active=127.850 8 | Comm1Standby=124.850 9 | Comm2Active=124.850 10 | Comm2Standby=124.850 11 | Comm3Active=124.850 12 | Comm3Standby=124.850 13 | Nav1Active=110.50 14 | Nav1Standby=113.90 15 | OBS1=360 16 | Nav2Active=110.50 17 | Nav2Standby=113.90 18 | OBS2=360 19 | 20 | TransponderState=4 21 | ADFActive=890 22 | ADF2Active=890 23 | DMESelected=1 24 | ComTransmit=1 25 | ComReceiveBoth=False 26 | Com1Receive=True 27 | Com2Receive=False 28 | Com3Receive=False 29 | AudioNav1Listen=False 30 | AudioNav2Listen=False 31 | AudioMarkerListen=False 32 | AudioDmeListen=False 33 | AudioAdfListen=False 34 | AudioAdf2Listen=False 35 | AvionicsSwitch=True 36 | 37 | [Engine Parameters.1.0] 38 | ThrottleLeverPct=1 39 | PropellerLeverPct=0.99993896484375 40 | Pct Engine RPM=0.99956832930920125335 41 | MaxReachedEngineRPM=3903.5488821170947631 42 | LeftMagneto=True 43 | RightMagneto=True 44 | GeneratorSwitch=True 45 | FuelValveOpen=True 46 | CowlFlapPct=0 47 | FuelPumpSwitch=False 48 | FuelPumpSwitch_EX1=0 49 | FuelValveOpen=True 50 | CarbHeat/DeiceSwitch=False 51 | EngineMasterSwitch=True 52 | GlowPlugTemperaturePct=1 53 | IgnitionSwitch=0 54 | 55 | [Propeller.1.0] 56 | prop_beta=0.34139458438119674177 57 | prop_max_rpm_percent=0.99956832930920125335 58 | 59 | [Systems.0] 60 | BatterySwitch=True 61 | StructuralDeiceSwitch=False 62 | PropDeiceSwitch=False 63 | Autobrakes=0 64 | StandbyVacuum=False 65 | PropSync=False 66 | AutoFeatherSwitch=False 67 | FlightDirector=False 68 | PanelLights=False 69 | LaunchBarSwitch=False 70 | LaunchBarState=0 71 | TailhookHandle=False 72 | TailhookState=0 73 | FoldingWingsHandle=False 74 | FoldingWingsState=0, 0 75 | 76 | [LocalVars.0] 77 | ;Note these settings may override standard config settings 78 | ;-------------------------------------------- 79 | ;C152X Cessna 300 ADF 80 | XMLVAR_ADF_MODE_SEL=2 ;2='ADF' Mode 81 | XMLVAR_ADF_VOLUME=100 ;0=OFF, 100=FULL 82 | ;-------------------------------------------- 83 | ;C152X KX155 DUAL NAVCOM 84 | XMLVAR_NAVCOM_COM_1_VOLUME=100 ;0=OFF, 100=FULL 85 | XMLVAR_NAVCOM_COM_2_VOLUME=100 ;0=OFF, 100=FULL 86 | XMLVAR_NAVCOM_COM_1_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 87 | XMLVAR_NAVCOM_COM_2_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 88 | 89 | XMLVAR_NAVCOM_NAV_1_VOLUME=100 ;0=0,100=FULL 90 | XMLVAR_NAVCOM_NAV_2_VOLUME=100 ;0=0,100=FULL 91 | XMLVAR_NAVCOM_NAV_1_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 92 | XMLVAR_NAVCOM_NAV_2_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 93 | ;-------------------------------------------- 94 | ;C152X KA134 AUDIO SELECTOR 95 | XMLVAR_AUDIO_COM_1_MIC_SEL=1 ;1=SEL, (COM 1 TX SEL), MIC 1 and 2 mutually exclusive 96 | XMLVAR_AUDIO_COM_2_MIC_SEL=0 ;1=SEL, (COM 2 TX SEL), MIC 1 and 2 mutually exclusive 97 | 98 | XMLVAR_AUDIO_BOTH_SEL=0 ;0=OFF, 1=SEL 99 | XMLVAR_AUDIO_NAV_1_SEL=0 ; 100 | XMLVAR_AUDIO_NAV_2_SEL=0 ; 101 | XMLVAR_AUDIO_ADF_SEL=0 ; 102 | XMLVAR_AUDIO_DME_SEL=0 ; 103 | XMLVAR_AUDIO_MKR_SEL=1 ; 104 | XMLVAR_AUDIO_SPKR_SEL=0 ; 105 | ;-------------------------------------------- 106 | 107 | [Gauges.0] 108 | KollsmanSetting=30.079952239990234375 109 | 110 | [BleedAir.0] 111 | BleedAirSource=0 112 | 113 | [Switches.0] 114 | PitotHeat=False 115 | BeaconLights=True 116 | LandingLights=False 117 | LogoLights=True 118 | NavLights=True 119 | PanelLights=True 120 | RecognitionLights=True 121 | StrobeLights=True 122 | TaxiLights=False 123 | WingLights=True 124 | CabinLights=False 125 | GlareshieldLights=False 126 | PedestalLights=False 127 | 128 | [AutoPilot.0] 129 | MasterSwitch=False 130 | WingLeveler=False 131 | Nav1Lock=False 132 | HeadingLock=False 133 | HeadingValue=0 134 | AltitudeLock=False 135 | AltitudeValue=0 136 | AttitudeHold=False 137 | AirspeedHold=False 138 | AirspeedValue=0 139 | MachHold=False 140 | MachValue=0 141 | VerticalSpeedHold=False 142 | VerticalSpeedValue=0 143 | RPMHold=False 144 | RPMValue=0 145 | GlideslopeHold=False 146 | ApproachHold=False 147 | BackCourseHold=False 148 | YawDamper=False 149 | ToGa=False 150 | AutoThrottleArm=False 151 | GPSdrivesNAV1=False 152 | IsUsedForLesson=False 153 | ForceDisplayUI=False 154 | 155 | [Controls.0] 156 | SpoilersHandle=000.00 157 | FlapsHandle=000.00 158 | LeftFlap=000.00 159 | RightFlap=000.00 160 | GearsHandle=000.00 161 | Gear1=100.00 162 | Gear2=100.00 163 | Gear3=100.00 164 | YokeY=050.00 165 | YokeX=050.00 166 | Rudder=050.00 167 | LeftBrake=000.00 168 | RightBrake=000.00 169 | ParkingBrake=000.00 170 | 171 | RudderTrimPct=0 172 | AileronTrimPct=0 173 | AileronTrimDisabled=False 174 | ElevatorTrimDisabled=False 175 | RudderTrimDisabled=False -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/Cruise.flt: -------------------------------------------------------------------------------- 1 | 2 | [SimVarForSpawningInTheAir.0] 3 | IAS=177 4 | FlapsDegree=0000.00 5 | 6 | [Avionics.0] 7 | Comm1Active=127.850 8 | Comm1Standby=124.850 9 | Comm2Active=124.850 10 | Comm2Standby=124.850 11 | Comm3Active=124.850 12 | Comm3Standby=124.850 13 | Nav1Active=110.50 14 | Nav1Standby=113.90 15 | OBS1=360 16 | Nav2Active=110.50 17 | Nav2Standby=113.90 18 | OBS2=360 19 | TransponderState=4 20 | ADFActive=890 21 | ADF2Active=890 22 | DMESelected=1 23 | ComTransmit=1 24 | ComReceiveBoth=False 25 | Com1Receive=True 26 | Com2Receive=False 27 | Com3Receive=False 28 | AudioNav1Listen=False 29 | AudioNav2Listen=False 30 | AudioMarkerListen=False 31 | AudioDmeListen=False 32 | AudioAdfListen=False 33 | AudioAdf2Listen=False 34 | AvionicsSwitch=True 35 | 36 | [Engine Parameters.1.0] 37 | ThrottleLeverPct=1 38 | PropellerLeverPct=0.99993896484375 39 | Pct Engine RPM=0.99956832930920125335 40 | MaxReachedEngineRPM=3903.5488821170947631 41 | LeftMagneto=True 42 | RightMagneto=True 43 | GeneratorSwitch=True 44 | FuelValveOpen=True 45 | CowlFlapPct=0 46 | FuelPumpSwitch=False 47 | FuelPumpSwitch_EX1=0 48 | FuelValveOpen=True 49 | CarbHeat/DeiceSwitch=False 50 | EngineMasterSwitch=True 51 | GlowPlugTemperaturePct=1 52 | IgnitionSwitch=0 53 | 54 | [Propeller.1.0] 55 | prop_beta=0.34139458438119674177 56 | prop_max_rpm_percent=0.99956832930920125335 57 | 58 | [Systems.0] 59 | BatterySwitch=True 60 | StructuralDeiceSwitch=False 61 | PropDeiceSwitch=False 62 | Autobrakes=0 63 | StandbyVacuum=False 64 | PropSync=False 65 | AutoFeatherSwitch=False 66 | FlightDirector=False 67 | PanelLights=False 68 | LaunchBarSwitch=False 69 | LaunchBarState=0 70 | TailhookHandle=False 71 | TailhookState=0 72 | FoldingWingsHandle=False 73 | FoldingWingsState=0, 0 74 | 75 | [LocalVars.0] 76 | ;Note these settings may override standard config settings 77 | ;-------------------------------------------- 78 | ;C152X Cessna 300 ADF 79 | XMLVAR_ADF_MODE_SEL=2 ;2='ADF' Mode 80 | XMLVAR_ADF_VOLUME=100 ;0=OFF, 100=FULL 81 | ;-------------------------------------------- 82 | ;C152X KX155 DUAL NAVCOM 83 | XMLVAR_NAVCOM_COM_1_VOLUME=100 ;0=OFF, 100=FULL 84 | XMLVAR_NAVCOM_COM_2_VOLUME=100 ;0=OFF, 100=FULL 85 | XMLVAR_NAVCOM_COM_1_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 86 | XMLVAR_NAVCOM_COM_2_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 87 | 88 | XMLVAR_NAVCOM_NAV_1_VOLUME=100 ;0=0,100=FULL 89 | XMLVAR_NAVCOM_NAV_2_VOLUME=100 ;0=0,100=FULL 90 | XMLVAR_NAVCOM_NAV_1_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 91 | XMLVAR_NAVCOM_NAV_2_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 92 | ;-------------------------------------------- 93 | ;C152X KA134 AUDIO SELECTOR 94 | XMLVAR_AUDIO_COM_1_MIC_SEL=1 ;1=SEL, (COM 1 TX SEL), MIC 1 and 2 mutually exclusive 95 | XMLVAR_AUDIO_COM_2_MIC_SEL=0 ;1=SEL, (COM 2 TX SEL), MIC 1 and 2 mutually exclusive 96 | 97 | XMLVAR_AUDIO_BOTH_SEL=0 ;0=OFF, 1=SEL 98 | XMLVAR_AUDIO_NAV_1_SEL=0 ; 99 | XMLVAR_AUDIO_NAV_2_SEL=0 ; 100 | XMLVAR_AUDIO_ADF_SEL=0 ; 101 | XMLVAR_AUDIO_DME_SEL=0 ; 102 | XMLVAR_AUDIO_MKR_SEL=1 ; 103 | XMLVAR_AUDIO_SPKR_SEL=0 ; 104 | ;-------------------------------------------- 105 | 106 | [Gauges.0] 107 | KollsmanSetting=29.921342849731445313 108 | 109 | [BleedAir.0] 110 | BleedAirSource=0 111 | 112 | [Switches.0] 113 | PitotHeat=False 114 | BeaconLights=True 115 | LandingLights=False 116 | LogoLights=True 117 | NavLights=True 118 | PanelLights=True 119 | RecognitionLights=True 120 | StrobeLights=True 121 | TaxiLights=False 122 | WingLights=True 123 | CabinLights=False 124 | GlareshieldLights=False 125 | PedestalLights=False 126 | 127 | [AutoPilot.0] 128 | MasterSwitch=True 129 | WingLeveler=False 130 | Nav1Lock=False 131 | HeadingLock=False 132 | HeadingValue=0 133 | AltitudeLock=False 134 | AltitudeValue=0 135 | AttitudeHold=False 136 | AirspeedHold=False 137 | AirspeedValue=0 138 | MachHold=False 139 | MachValue=0 140 | VerticalSpeedHold=False 141 | VerticalSpeedValue=0 142 | RPMHold=False 143 | RPMValue=0 144 | GlideslopeHold=False 145 | ApproachHold=False 146 | BackCourseHold=False 147 | YawDamper=False 148 | ToGa=False 149 | AutoThrottleArm=False 150 | GPSdrivesNAV1=False 151 | IsUsedForLesson=False 152 | ForceDisplayUI=False 153 | 154 | [Controls.0] 155 | SpoilersHandle=000.00 156 | FlapsHandle=000.00 157 | LeftFlap=000.00 158 | RightFlap=000.00 159 | GearsHandle=000.00 160 | Gear1=100.00 161 | Gear2=100.00 162 | Gear3=100.00 163 | YokeY=050.00 164 | YokeX=050.00 165 | Rudder=050.00 166 | LeftBrake=000.00 167 | RightBrake=000.00 168 | ParkingBrake=000.00 169 | 170 | RudderTrimPct=0 171 | AileronTrimPct=0 172 | AileronTrimDisabled=False 173 | ElevatorTrimDisabled=False 174 | RudderTrimDisabled=False -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/Final.flt: -------------------------------------------------------------------------------- 1 | [SimVarForSpawningInTheAir.0] 2 | IAS=110 3 | FlapsDegree=0042.00 4 | 5 | [Avionics.0] 6 | Comm1Active=127.850 7 | Comm1Standby=124.850 8 | Comm2Active=124.850 9 | Comm2Standby=124.850 10 | Comm3Active=124.850 11 | Comm3Standby=124.850 12 | Nav1Active=110.50 13 | Nav1Standby=113.90 14 | OBS1=360 15 | Nav2Active=110.50 16 | Nav2Standby=113.90 17 | OBS2=360 18 | 19 | TransponderState=4 20 | ADFActive=890 21 | ADF2Active=890 22 | DMESelected=1 23 | ComTransmit=1 24 | ComReceiveBoth=False 25 | Com1Receive=True 26 | Com2Receive=False 27 | Com3Receive=False 28 | AudioNav1Listen=False 29 | AudioNav2Listen=False 30 | AudioMarkerListen=False 31 | AudioDmeListen=False 32 | AudioAdfListen=False 33 | AudioAdf2Listen=False 34 | AvionicsSwitch=True 35 | 36 | [Engine Parameters.1.0] 37 | ThrottleLeverPct=1 38 | PropellerLeverPct=0.99993896484375 39 | Pct Engine RPM=0.99996485171647575552 40 | MaxReachedEngineRPM=3903.5488821170947631 41 | LeftMagneto=True 42 | RightMagneto=True 43 | GeneratorSwitch=True 44 | FuelValveOpen=True 45 | CowlFlapPct=0 46 | FuelPumpSwitch=False 47 | FuelPumpSwitch_EX1=0 48 | FuelValveOpen=True 49 | CarbHeat/DeiceSwitch=False 50 | EngineMasterSwitch=True 51 | GlowPlugTemperaturePct=1 52 | IgnitionSwitch=1 53 | 54 | [Propeller.1.0] 55 | prop_beta=0.32654542996935487231 56 | prop_max_rpm_percent=0.99996485171647575552 57 | 58 | [Systems.0] 59 | BatterySwitch=True 60 | StructuralDeiceSwitch=False 61 | PropDeiceSwitch=False 62 | Autobrakes=0 63 | StandbyVacuum=False 64 | PropSync=False 65 | AutoFeatherSwitch=False 66 | FlightDirector=False 67 | PanelLights=False 68 | LaunchBarSwitch=False 69 | LaunchBarState=0 70 | TailhookHandle=False 71 | TailhookState=0 72 | FoldingWingsHandle=False 73 | FoldingWingsState=0, 0 74 | 75 | [LocalVars.0] 76 | ;Note these settings may override standard config settings 77 | ;-------------------------------------------- 78 | ;C152X Cessna 300 ADF 79 | XMLVAR_ADF_MODE_SEL=2 ;2='ADF' Mode 80 | XMLVAR_ADF_VOLUME=100 ;0=OFF, 100=FULL 81 | ;-------------------------------------------- 82 | ;C152X KX155 DUAL NAVCOM 83 | XMLVAR_NAVCOM_COM_1_VOLUME=100 ;0=OFF, 100=FULL 84 | XMLVAR_NAVCOM_COM_2_VOLUME=100 ;0=OFF, 100=FULL 85 | XMLVAR_NAVCOM_COM_1_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 86 | XMLVAR_NAVCOM_COM_2_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 87 | 88 | XMLVAR_NAVCOM_NAV_1_VOLUME=100 ;0=0,100=FULL 89 | XMLVAR_NAVCOM_NAV_2_VOLUME=100 ;0=0,100=FULL 90 | XMLVAR_NAVCOM_NAV_1_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 91 | XMLVAR_NAVCOM_NAV_2_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 92 | ;-------------------------------------------- 93 | ;C152X KA134 AUDIO SELECTOR 94 | XMLVAR_AUDIO_COM_1_MIC_SEL=1 ;1=SEL, (COM 1 TX SEL), MIC 1 and 2 mutually exclusive 95 | XMLVAR_AUDIO_COM_2_MIC_SEL=0 ;1=SEL, (COM 2 TX SEL), MIC 1 and 2 mutually exclusive 96 | 97 | XMLVAR_AUDIO_BOTH_SEL=0 ;0=OFF, 1=SEL 98 | XMLVAR_AUDIO_NAV_1_SEL=0 ; 99 | XMLVAR_AUDIO_NAV_2_SEL=0 ; 100 | XMLVAR_AUDIO_ADF_SEL=0 ; 101 | XMLVAR_AUDIO_DME_SEL=0 ; 102 | XMLVAR_AUDIO_MKR_SEL=1 ; 103 | XMLVAR_AUDIO_SPKR_SEL=0 ; 104 | ;-------------------------------------------- 105 | 106 | [Gauges.0] 107 | KollsmanSetting=29.921342849731445313 108 | 109 | [BleedAir.0] 110 | BleedAirSource=0 111 | 112 | [Switches.0] 113 | PitotHeat=False 114 | BeaconLights=True 115 | LandingLights=True 116 | LogoLights=True 117 | NavLights=True 118 | PanelLights=True 119 | RecognitionLights=True 120 | StrobeLights=True 121 | TaxiLights=False 122 | WingLights=True 123 | CabinLights=False 124 | GlareshieldLights=False 125 | PedestalLights=False 126 | 127 | [AutoPilot.0] 128 | MasterSwitch=False 129 | WingLeveler=False 130 | Nav1Lock=False 131 | HeadingLock=False 132 | HeadingValue=0 133 | AltitudeLock=False 134 | AltitudeValue=0 135 | AttitudeHold=False 136 | AirspeedHold=False 137 | AirspeedValue=0 138 | MachHold=False 139 | MachValue=0 140 | VerticalSpeedHold=False 141 | VerticalSpeedValue=0 142 | RPMHold=False 143 | RPMValue=0 144 | GlideslopeHold=False 145 | ApproachHold=False 146 | BackCourseHold=False 147 | YawDamper=False 148 | ToGa=False 149 | AutoThrottleArm=False 150 | GPSdrivesNAV1=False 151 | IsUsedForLesson=False 152 | ForceDisplayUI=False 153 | 154 | [Controls.0] 155 | SpoilersHandle=000.00 156 | FlapsHandle=100.00 157 | LeftFlap=100.00 158 | RightFlap=100.00 159 | GearsHandle=100.00 160 | Gear1=100.00 161 | Gear2=100.00 162 | Gear3=100.00 163 | YokeY=050.00 164 | YokeX=050.00 165 | Rudder=050.00 166 | LeftBrake=000.00 167 | RightBrake=000.00 168 | ParkingBrake=000.00 169 | RudderTrimPct=0 170 | AileronTrimPct=0 171 | AileronTrimDisabled=False 172 | ElevatorTrimDisabled=False 173 | RudderTrimDisabled=False -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/aircraft.cfg: -------------------------------------------------------------------------------- 1 | [VERSION] 2 | major = 1 3 | minor = 0 4 | 5 | [GENERAL] 6 | atc_type = "TT:ATCCOM.ATC_NAME CESSNA.0.text" 7 | atc_model = "TT:ATCCOM.AC_MODEL C152.0.text" 8 | Category = "airplane" 9 | pilot = "Pilot_Female_Casual" 10 | copilot = "Pilot_Male_Casual" 11 | instructor = "Pilot_Male_Casual" 12 | performance = "Todo" 13 | icao_type_designator = "C152" 14 | icao_manufacturer = "CESSNA" 15 | icao_model = "152" 16 | icao_engine_type = "Piston" 17 | icao_engine_count = 1 18 | icao_WTC = "L" 19 | 20 | [PILOT] 21 | pilot = "Pilot_Female_Casual" 22 | copilot = "Pilot_Male_Casual" 23 | instructor = "Pilot_Male_Casual" 24 | pilot_default_animation = "Idle1_PosePropeller" 25 | copilot_default_animation = "Idle2_PosePropeller" 26 | pilot_attach_node = "PILOT_0" 27 | copilot_attach_node = "PILOT_1" 28 | 29 | [SERVICES] 30 | FUELTRUCK = 1 31 | BAGGAGE_LOADER = 0 32 | CATERING_TRUCK = 0 33 | BOARDING_RAMP = 0 34 | GROUND_POWER_UNIT = 0 35 | PUSHBACK = 0 36 | SMALL_PUSHBACK = 1 37 | MARSHALLER = 1 38 | JETWAY = 0 39 | 40 | [EFFECTS] 41 | wake = fx_wake 42 | water = fx_spray ; (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) 43 | dirt = fx_tchdrt 44 | concrete = fx_sparks 45 | touchdown = fx_tchdwn_s, 1 46 | 47 | ;===================== FLTSIM ===================== 48 | 49 | [FLTSIM.0] 50 | title = "Cessna 152 Asobo" ; Variation name 51 | model = "" ; model folder 52 | panel = "" ; panel folder 53 | sound = "" ; sound folder 54 | texture = "" ; texture folder 55 | kb_checklists = "" ; Procedures/Checklist sibling file name 56 | kb_reference = "" ; Reference information sibling file name 57 | description = "TT:AIRCRAFT.DESCRIPTION" ; Variation description. 58 | wip_indicator = 0 ; know if the variation is good to go or still WIP : -1=Disabled, 0=Rough, 1=1st Pass, 2=Finished 59 | ui_manufacturer = "TT:AIRCRAFT.UI_MANUFACTURER" ; e.g. Boeing, Cessna 60 | ui_type = "TT:AIRCRAFT.UI_MODEL" ; e.g. 747-400, 172 61 | ui_variation = "TT:AIRCRAFT.LIVERY.DEFAULT" ; e.g. World Air, IFR Panel 62 | ui_typerole = "Single Engine Prop" ; e.g. Single Engine Prop, Twin Engine Prop, Rotorcraft, etc 63 | ui_createdby = "Asobo/C152X" ; e.g. Asobo Studio, Microsoft, FSAddonCompany, etc 64 | ui_thumbnailfile = "" ; app relative path to ThumbNail image file 65 | ui_certified_ceiling = 14700 ; service ceiling / max certified operating altitude (ft) 66 | ui_max_range = 690 ; max distance the aircraft can fly between take-off and landing in (NM) ;long range tanks 67 | ui_autonomy = 8.7 ; max duration the aircraft can fly between take-off and landing in (Hrs) ;long range tanks 68 | ui_fuel_burn_rate = 40 ; average fuel consumption per hour (lbs/hr) - reminder: fuel density is ~6.7lbs per US gallon 69 | atc_id = "VH-XSR" ; tail number 70 | atc_id_enable = 1 ; enable tail number 71 | atc_airline = "" ; airline name 72 | atc_flight_number = "" ; flight number 73 | atc_heavy = 0 ; heavy? 74 | atc_parking_types = "RAMP" ; "ANY" / "RAMP" / "CARGO" / "MIL_CARGO" / "MIL_COMBAT" / "GATE" / "DOCK" 75 | atc_parking_codes = "" ; Comma separated and may be as small as one character each 76 | atc_id_color = "" ; color for the tail number : i.e. "#ffff00ff" 77 | atc_id_font = "" ; font for the tail number 78 | isAirTraffic = 0 ; Is the plane usable for air traffic 79 | isUserSelectable = 1 ; Is the plane selectable by the user 80 | 81 | -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/apron.flt: -------------------------------------------------------------------------------- 1 | [SimVars.0] 2 | PVelBodyAxis=0 3 | BVelBodyAxis=0 4 | HVelBodyAxis=0 5 | XVelBodyAxis=0 6 | YVelBodyAxis=0 7 | ZVelBodyAxis=0 8 | SimOnGround=True 9 | 10 | [Avionics.0] 11 | Comm1Active=118.300 12 | Comm1Standby=124.850 13 | Comm2Active=124.850 14 | Comm2Standby=124.850 15 | Comm3Active=124.850 16 | Comm3Standby=124.850 17 | Nav1Active=112.00 18 | Nav1Standby=113.90 19 | OBS1=360 20 | Nav2Active=110.50 21 | Nav2Standby=113.90 22 | OBS2=360 23 | 24 | TransponderState=0 25 | ADFActive=890 26 | ADF2Active=890 27 | DMESelected=1 28 | ComTransmit=1 29 | ComReceiveBoth=False 30 | Com1Receive=True 31 | Com2Receive=False 32 | Com3Receive=False 33 | AudioNav1Listen=False 34 | AudioNav2Listen=False 35 | AudioMarkerListen=False 36 | AudioDmeListen=False 37 | AudioAdfListen=False 38 | AudioAdf2Listen=False 39 | AvionicsSwitch=True 40 | 41 | [Engine Parameters.1.0] 42 | ThrottleLeverPct=0 43 | PropellerLeverPct=0 44 | MixtureLeverPct=0 45 | Pct Engine RPM=0 46 | MaxReachedEngineRPM=2454.7394303494743326 47 | LeftMagneto=False 48 | RightMagneto=False 49 | GeneratorSwitch=False 50 | FuelValveOpen=False 51 | CowlFlapPct=0 52 | FuelPumpSwitch=False 53 | FuelPumpSwitch_EX1=0 54 | CarbHeat/DeiceSwitch=False 55 | EngineMasterSwitch=False 56 | GlowPlugTemperaturePct=1 57 | IgnitionSwitch=0 58 | 59 | [Propeller.1.0] 60 | prop_beta=0.20943951023931955957 61 | prop_max_rpm_percent=0 62 | 63 | [Systems.0] 64 | BatterySwitch=False 65 | StructuralDeiceSwitch=False 66 | PropDeiceSwitch=False 67 | Autobrakes=0 68 | StandbyVacuum=False 69 | PropSync=False 70 | AutoFeatherSwitch=False 71 | FlightDirector=False 72 | PanelLights=False 73 | LaunchBarSwitch=False 74 | LaunchBarState=0 75 | TailhookHandle=False 76 | TailhookState=0 77 | FoldingWingsHandle=False 78 | FoldingWingsState=0, 0 79 | 80 | [LocalVars.0] 81 | ;Note these settings may override standard config settings 82 | ;-------------------------------------------- 83 | ;C152X Cessna 300 ADF 84 | XMLVAR_ADF_MODE_SEL=2 ;2='ADF' Mode 85 | XMLVAR_ADF_VOLUME=0 ;0=OFF, 100=FULL 86 | ;-------------------------------------------- 87 | ;C152X KX155 DUAL NAVCOM 88 | XMLVAR_NAVCOM_COM_1_VOLUME=0 ;0=OFF, 100=FULL 89 | XMLVAR_NAVCOM_COM_2_VOLUME=0 ;0=OFF, 100=FULL 90 | XMLVAR_NAVCOM_COM_1_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 91 | XMLVAR_NAVCOM_COM_2_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 92 | 93 | XMLVAR_NAVCOM_NAV_1_VOLUME=100 ;0=0,100=FULL 94 | XMLVAR_NAVCOM_NAV_2_VOLUME=100 ;0=0,100=FULL 95 | XMLVAR_NAVCOM_NAV_1_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 96 | XMLVAR_NAVCOM_NAV_2_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 97 | ;-------------------------------------------- 98 | ;C152X KA134 AUDIO SELECTOR 99 | XMLVAR_AUDIO_COM_1_MIC_SEL=1 ;1=SEL, (COM 1 TX SEL), MIC 1 and 2 mutually exclusive 100 | XMLVAR_AUDIO_COM_2_MIC_SEL=0 ;1=SEL, (COM 2 TX SEL), MIC 1 and 2 mutually exclusive 101 | 102 | XMLVAR_AUDIO_BOTH_SEL=1 ;0=OFF, 1=SEL 103 | XMLVAR_AUDIO_NAV_1_SEL=0 ; 104 | XMLVAR_AUDIO_NAV_2_SEL=0 ; 105 | XMLVAR_AUDIO_ADF_SEL=0 ; 106 | XMLVAR_AUDIO_DME_SEL=0 ; 107 | XMLVAR_AUDIO_MKR_SEL=1 ; 108 | XMLVAR_AUDIO_SPKR_SEL=0 ; 109 | ;-------------------------------------------- 110 | 111 | [Gauges.0] 112 | KollsmanSetting=29.921342849731445313 113 | 114 | [BleedAir.0] 115 | BleedAirSource=0 116 | 117 | [Switches.0] 118 | PitotHeat=False 119 | BeaconLights=False 120 | LandingLights=False 121 | LogoLights=False 122 | NavLights=False 123 | PanelLights=False 124 | RecognitionLights=False 125 | StrobeLights=False 126 | TaxiLights=False 127 | WingLights=False 128 | CabinLights=False 129 | GlareshieldLights=False 130 | PedestalLights=False 131 | Potentiometer.4=0.8 132 | Potentiometer.5=0.5 133 | 134 | 135 | 136 | [AutoPilot.0] 137 | MasterSwitch=False 138 | WingLeveler=False 139 | Nav1Lock=False 140 | HeadingLock=False 141 | HeadingValue=0 142 | AltitudeLock=False 143 | AltitudeValue=0 144 | AttitudeHold=False 145 | AirspeedHold=False 146 | AirspeedValue=0 147 | MachHold=False 148 | MachValue=0 149 | VerticalSpeedHold=False 150 | VerticalSpeedValue=0 151 | RPMHold=False 152 | RPMValue=0 153 | GlideslopeHold=False 154 | ApproachHold=False 155 | BackCourseHold=False 156 | YawDamper=False 157 | ToGa=False 158 | AutoThrottleArm=False 159 | GPSdrivesNAV1=False 160 | IsUsedForLesson=False 161 | ForceDisplayUI=False 162 | 163 | [Controls.0] 164 | SpoilersHandle=000.00 165 | FlapsHandle=000.00 166 | LeftFlap=000.00 167 | RightFlap=000.00 168 | GearsHandle=000.00 169 | Gear1=100.00 170 | Gear2=100.00 171 | Gear3=100.00 172 | YokeY=050.00 173 | YokeX=050.00 174 | Rudder=050.00 175 | LeftBrake=000.00 176 | RightBrake=000.00 177 | ParkingBrake=100.00 178 | 179 | RudderTrimPct=0 180 | AileronTrimPct=0 181 | AileronTrimDisabled=False 182 | ElevatorTrimDisabled=False 183 | RudderTrimDisabled=False -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/cockpit.cfg: -------------------------------------------------------------------------------- 1 | [VERSION] 2 | major = 1 3 | minor = 0 4 | 5 | [FUEL_FLOW] 6 | min = 0 7 | lowLimit = 0 8 | green_start = 0 9 | green_end = 0 10 | highLimit = 0 11 | max = 0 12 | 13 | [FUEL_QUANTITY] 14 | min = 0 15 | lowLimit = 0 16 | green_start = 5 17 | green_end = 26 18 | yellow_start = 0 19 | yellow_end = 0 20 | red_start = 1 21 | red_end = 5 22 | highLimit = 0 23 | max = 26 24 | 25 | [FUEL_TEMPERATURE] 26 | min = 0 27 | lowLimit = 0 28 | low_red_start = 0 29 | low_red_end = 0 30 | low_yellow_start = 0 31 | low_yellow_end = 0 32 | green_start = 0 33 | green_end = 0 34 | yellow_start = 0 35 | yellow_end = 0 36 | red_start = 0 37 | red_end = 0 38 | highLimit = 0 39 | max = 0 40 | 41 | [FUEL_PRESSURE] 42 | min = 0 43 | lowLimit = 0 44 | low_red_start = 0 45 | low_red_end = 0 46 | low_yellow_start = 0 47 | low_yellow_end = 0 48 | green_start = 0 49 | green_end = 0 50 | yellow_start = 0 51 | yellow_end = 0 52 | red_start = 0 53 | red_end = 0 54 | highLimit = 0 55 | max = 0 56 | 57 | [OIL_PRESSURE] 58 | min = 0 59 | lowLimit = 25 60 | low_red_start = 0 61 | low_red_end = 0 62 | low_yellow_start = 0 63 | low_yellow_end = 0 64 | green_start = 60 65 | green_end = 90 66 | yellow_start = 0 67 | yellow_end = 0 68 | red_start = 0 69 | red_end = 0 70 | highLimit = 100 71 | max = 100 72 | 73 | [OIL_TEMPERATURE] 74 | min = 0 75 | lowLimit = 0 76 | low_red_start = 0 77 | low_red_end = 0 78 | low_yellow_start = 0 79 | low_yellow_end = 0 80 | green_start = 110 81 | green_end = 245 82 | yellow_start = 0 83 | yellow_end = 0 84 | red_start = 0 85 | red_end = 0 86 | highLimit = 245 87 | max = 245 88 | 89 | [EGT_TEMPERATURE] 90 | min = 0 91 | max = 0 92 | lowLimit = 0 93 | highLimit = 0 94 | 95 | [VACUUM] 96 | min = 0 97 | lowLimit = 0 98 | green_start = 0 99 | green_end = 0 100 | highLimit = 0 101 | max = 0 102 | 103 | [MANIFOLD_PRESSURE] 104 | min = 0 105 | lowLimit = 0 106 | green_start = 0 107 | green_end = 0 108 | highLimit = 0 109 | max = 0 110 | 111 | [AIRSPEED] 112 | min = 0 113 | lowLimit = 0 114 | white_start = 35 115 | white_end = 85 116 | green_start = 40 117 | green_end = 111 118 | yellow_start = 111 119 | yellow_end = 148 120 | red_start = 149 121 | red_end = 152 122 | highLimit = 0 123 | max = 155 124 | 125 | [TORQUE] 126 | min = 0 127 | lowLimit = 0 128 | green_start = 0 129 | green_end = 0 130 | yellow_start = 0 131 | yellow_end = 0 132 | red_start = 0 133 | red_end = 0 134 | highLimit = 0 135 | max = 0 136 | 137 | [RPM] 138 | min = 0 139 | lowLimit = 0 140 | green_start = 1900 141 | green_end = 2550 142 | yellow_start = 0 143 | yellow_end = 0 144 | red_start = 0 145 | red_end = 0 146 | highLimit = 2550 147 | max = 2550 148 | 149 | [TURBINE_NG] 150 | min = 0 151 | lowLimit = 0 152 | green_start = 0 153 | green_end = 0 154 | yellow_start = 0 155 | yellow_end = 0 156 | red_start = 0 157 | red_end = 0 158 | highLimit = 0 159 | max = 0 160 | 161 | [ITTENGINEOFF] 162 | min = 0 163 | lowLimit = 0 164 | low_red_start = 0 165 | low_red_end = 0 166 | low_yellow_start = 0 167 | low_yellow_end = 0 168 | green_start = 0 169 | green_end = 0 170 | yellow_start = 0 171 | yellow_end = 0 172 | red_start = 0 173 | red_end = 0 174 | highLimit = 0 175 | max = 0 176 | 177 | [ITTENGINEON] 178 | min = 0 179 | lowLimit = 0 180 | low_red_start = 0 181 | low_red_end = 0 182 | low_yellow_start = 0 183 | low_yellow_end = 0 184 | green_start = 0 185 | green_end = 0 186 | yellow_start = 0 187 | yellow_end = 0 188 | red_start = 0 189 | red_end = 0 190 | highLimit = 0 191 | max = 0 192 | 193 | [MAIN_BUS_VOLTAGE] 194 | min = 0 195 | lowLimit = 0 196 | low_red_start = 0 197 | low_red_end = 0 198 | low_yellow_start = 0 199 | low_yellow_end = 0 200 | green_start = 0 201 | green_end = 0 202 | yellow_start = 0 203 | yellow_end = 0 204 | red_start = 0 205 | red_end = 0 206 | highLimit = 0 207 | max = 0 208 | 209 | [HOT_BATTERY_BUS_VOLTAGE] 210 | min = 0 211 | lowLimit = 0 212 | low_red_start = 0 213 | low_red_end = 0 214 | low_yellow_start = 0 215 | low_yellow_end = 0 216 | green_start = 0 217 | green_end = 0 218 | yellow_start = 0 219 | yellow_end = 0 220 | red_start = 0 221 | red_end = 0 222 | highLimit = 0 223 | max = 0 224 | 225 | [BATTERY_BUS_AMPS] 226 | min = 0 227 | lowLimit = 0 228 | green_start = 0 229 | green_end = 0 230 | yellow_start = 0 231 | yellow_end = 0 232 | red_start = 0 233 | red_end = 0 234 | highLimit = 0 235 | max = 0 236 | 237 | [GENALT_BUS_AMPS] 238 | min = 0 239 | lowLimit = 0 240 | green_start = 0 241 | green_end = 0 242 | yellow_start = 0 243 | yellow_end = 0 244 | red_start = 0 245 | red_end = 0 246 | highLimit = 0 247 | max = 0 248 | 249 | [COOLANT_LEVEL] 250 | min = 0 251 | max = 0 252 | lowLimit = 0 253 | highLimit = 0 254 | 255 | [COOLANT_TEMPERATURE] 256 | min = 0 257 | lowLimit = 0 258 | low_red_start = 0 259 | low_red_end = 0 260 | low_yellow_start = 0 261 | low_yellow_end = 0 262 | green_start = 0 263 | green_end = 0 264 | yellow_start = 0 265 | yellow_end = 0 266 | red_start = 0 267 | red_end = 0 268 | highLimit = 0 269 | max = 0 270 | 271 | [GEAR_OIL_TEMPERATURE] 272 | min = 0 273 | lowLimit = 0 274 | green_start = 0 275 | green_end = 0 276 | yellow_start = 0 277 | yellow_end = 0 278 | red_start = 0 279 | red_end = 0 280 | highLimit = 0 281 | max = 0 282 | 283 | [CABIN_ALTITUDE] 284 | min = 0 285 | lowLimit = 0 286 | green_start = 0 287 | green_end = 0 288 | highLimit = 0 289 | max = 0 290 | 291 | [CABIN_ALTITUDE_CHANGE_RATE] 292 | min = 0 293 | max = 0 294 | lowLimit = 0 295 | highLimit = 0 296 | 297 | [CABIN_PRESSURE_DIFF] 298 | min = 0 299 | lowLimit = 0 300 | green_start = 0 301 | green_end = 0 302 | highLimit = 0 303 | max = 0 304 | 305 | [ATTITUDE_INDICATORS] 306 | attitude_indicator.0 = 1 307 | attitude_indicator.1 = 2 308 | 309 | [TURN_INDICATORS] 310 | turn_indicator.0 = 1,1 ; Turn AND Bank 311 | 312 | [DIRECTION_INDICATORS] 313 | direction_indicator.0 = 1,0 314 | 315 | ;Level flight Flap Up 316 | ;KIAS 40 50 60 70 80 90 100 110 120 130 140 317 | ;KCAS 46 53 60 69 78 88 97 107 117 127 136 318 | ; 319 | ;From earlier SDK. 320 | ;This section is used to define the characteristics of the airspeed indicators on the instrument panels. 321 | ;The list of indicators should be listed in order: 0,1,2,..n. 322 | ;These characteristics define the calibration between calibrated airspeed and indicated airspeed. 323 | ;The first parameter is a scalar on the calibrated airspeed, and the second is an offset in knots. 324 | ;The offset is applied first, then the scalar. The default value for the scalar is 1.0 and the default for the 325 | ;offset is 0.0, thus by default, indicated airspeed is equal to calibrated airspeed. example. Maule M7 1.3, -24.0 326 | ; 327 | [AIRSPEED_INDICATORS] 328 | airspeed_indicator.0 = 1.21, -14.91 329 | airspeed_indicator.1 = 1.21, -14.91 330 | 331 | [ALTIMETERS] 332 | altimeter.0 = 1 333 | altimeter.1 = 1 334 | 335 | [GPWS] 336 | max_warning_height = 0 337 | sink_rate_fpm = -1500 338 | excessive_sink_rate_fpm = -2000 339 | climbout_sink_rate_fpm = -100 340 | flap_and_gear_sink_rate_fpm = -100 341 | 342 | [THROTTLE_LEVELS] 343 | level_1_min = 0 344 | level_1_name = "" 345 | level_2_min = 0 346 | level_2_name = "" 347 | level_3_min = 0 348 | level_3_name = "" 349 | level_4_min = 0 350 | level_4_name = "" 351 | level_5_min = 0 352 | level_5_name = "" 353 | level_6_min = 0 354 | level_6_name = "" 355 | 356 | [FLAPS_LEVELS] 357 | slats_level_1 = 0 358 | flaps_level_1 = 0 359 | slats_level_2 = 0 360 | flaps_level_2 = 0 361 | slats_level_3 = 0 362 | flaps_level_3 = 0 363 | slats_level_full = 0 364 | flaps_level_full = 0 365 | 366 | -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/engines.cfg: -------------------------------------------------------------------------------- 1 | [VERSION] 2 | major = 1 3 | minor = 0 4 | 5 | [GENERALENGINEDATA] 6 | engine_type = 0 ; 0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop 7 | fuel_flow_scalar = 0.79 ; Fuel flow scalar **SG updated was 0.88 8 | min_throttle_limit = 0 ; Minimum percent throttle. Generally negative for turbine reverser 9 | master_ignition_switch = 0 10 | starter_type = 0 ; 0=Electric, 1=Manual, 2=Bleed Air 11 | max_contrail_temperature = -1 12 | Engine.0 = -0.5, 0, 0.5 13 | ThrustAnglesPitchHeading.0 = 0, 0 14 | 15 | [PISTON_ENGINE] 16 | power_scalar = 1 ; Piston power scalar **SG updated was 1 17 | cylinder_displacement = 58.325 ; Cubic inches per cylinder **SG updated was 56.5 18 | compression_ratio = 8.5 ; Compression ratio **SG updated was 8.5 19 | number_of_cylinders = 4 ; Number of cylinders 20 | max_rated_rpm = 2700 ; Max rated RPM **SG updated 21 | max_rated_hp = 115 ; Max rated HP **SG updated 22 | min_cruise_rpm = 2000 23 | max_cruise_rpm = 2500 24 | max_indicated_rpm = 3500 25 | fuel_metering_type = 1 ; 0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor 26 | cooling_type = 0 ; 0=Cooling type Air, 1=Cooling type Liquid 27 | normalized_starter_torque = 0.2 ; Starter torque factor **SG updated was 0.3 28 | starter_time = 0.55 ; Time the Starter stays active when pressed **SG updated was 1.5 29 | turbocharged = 0 ; Is it turbocharged? 0=FALSE, 1=TRUE 30 | max_design_mp = 0 ; Max design manifold pressure, (inHg) 31 | min_design_mp = 0 ; Min design manifold pressure, (inHg) 32 | critical_altitude = 0 ; Altitude to which the turbocharger will provide max design manifold pressure (feet) 33 | emergency_boost_type = 0 ; 0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power 34 | emergency_boost_mp_offset = 0 ; Additional manifold pressure supplied by emergency boost 35 | emergency_boost_gain_offset = 0 ; Multiplier on manifold pressure due to emergency boost 36 | fuel_air_auto_mixture = 0 ; Automixture available? 0=FALSE, 1=TRUE 37 | auto_ignition = 0 ; Auto-Ignition available? 0=FALSE, 1=TRUE 38 | max_rpm_mechanical_efficiency_scalar = 0.83 ; Scalar on maximum RPM mechanical efficiency **SG updated was 0.83 39 | idle_rpm_mechanical_efficiency_scalar = 1 40 | max_rpm_friction_scalar = 0.50 ; Scalar on maximum RPM friction ;**SG updated was 0.55 41 | idle_rpm_friction_scalar = 0.30 ; Scalar on idle RPM friction ;**SG updated was 0.35 42 | BestPowerSpecificFuelConsumption = 0.51 ; SFC at Best Power mixture ratio **SG updated was 0.62 Lycoming 100% 9.5USG/HR SFC=9.5*60/110 43 | egt_tuning_constant = 1 44 | egt_peak_temperature = 2100 ; typical peak EGT: 1200 degF + 460 45 | egt_tc = 0.05 46 | cht_tuning_constant = 1 47 | cht_cooling_constant = 0.65 48 | cht_heating_constant = 960 ; max temp degrees Rankine 49 | cht_tc = 0.015 50 | oil_press_tuning_constant = 1 51 | oil_press_max = 12000 ; max oil pressure (psf) **SG updated originally 10080 now 12000=83psi 52 | oil_press_tc = 0.8 53 | oil_temp_tuning_constant = 1 54 | oil_temp_cooling_constant = 0.2 ;**SG updated originally 0.21 Note this is cooling effect of airspeed/airflow 55 | oil_temp_heating_constant = 710 ; max oil temperature degrees Rankine *SG updated originally 700 710=250dgF=121dgC 56 | oil_temp_tc = 0.01 ;**SG updated originally 0.03 Note tc is 1/sec! 0.01 = 100sec 57 | radiator_temp_tuning_constant = 1 58 | radiator_temp_cooling_constant = 0.015 59 | radiator_temp_max = 670 ; max radiator temperature degrees Rankine 60 | radiator_temp_tc = 0.02 61 | fuel_press_tuning_constant = 1 62 | fuel_press_max = 2376 ; max fuel pressure (psf) 63 | fuel_press_tc = 2 64 | number_of_magnetos = 2 65 | two_stroke_cycle = 0 66 | supercharged = 0 67 | radiator_cooling_constant = 0.015 68 | radiator_heating_constant = 670 69 | radiator_tc = 0.02 70 | radiator_tuning_constant = 1 71 | magneto_order_left_right_both = 0 72 | engine_mechanical_efficiency_table = 0:0.17, 700:0.77, 2300:0.77, 2553:0.67, 2700:0.6 ;**SG updated 73 | engine_friction_table = -300:-50, 300:50, 500:25, 2553:31 ;**SG updated 74 | manifold_efficiency_table = 0:0.2, 1:0.97 75 | rpm_to_oil_pressure_table = 0:0, 0.1:0.2, 0.2:0.5, 0.7:1 ;**SG updated 76 | rpm_to_fuel_pressure_table = 0:0, 500:0.3, 1400:1, 2000:1 77 | ; SG updated 78 | ; Lowest temp likely to be encountered = -50dgC = ~400R = 0.57 (700) 79 | ; Idle RPM = ~ 120dgF = 49dgC = 580R = 0.82 (700) 80 | ; 1000 RPM = ~150dgF = 65dgC = 609R = 0.87 (700) 81 | ; 2100 RPM = ~ 185dgF = 85dgC = 645R = 0.92 (700) 82 | ; 2400 RPM = ~ 210dgF = 98dgC = 668R = 0.95 (700) 83 | ; 2500 RPM = ~ 240dgF = 115dgC = 698R = 1.0 (700) 84 | oil_temp_factor_from_rpm = 0:0.57, 800:0.82, 2550:1 ; Gives the Oil temperature factor (to oil_temp_heating_constant) from rpm. **SG updated 85 | prop_lever_pos_to_oil_pressure_delta_table = 0:2160, 1:0 ; Delta in oil pressure when governor is taking over 86 | diesel = 0 ; Is it diesel engine? 87 | induction_air_temp_tc = 4 ; Induction Air Temp time constant 88 | carb_heat_delta_temp = 55 ; Delta of temperature when the Carburator Heater is activated (In Rankine) 89 | single_magneto_efficiency = 0.95 ; Efficiency ratio of the engine if it is designed for 2 magnetos but only 1 is currently active. **SG updated was 0.97 now gives ~ 100rpm drop at 1700rpm (max 125) 90 | oil_temp_to_oil_pressure_table = 0:0, 500:-1, 700:-600 ; Pressure differential (in psf) of the oil depending on its temperature (in K). 91 | shaft_torque_tc = 2.5 ; Gives the speed at which the shaft torque reaches its target value. 92 | recip_stop_arc_degrees = 90 ; Gives the amplitude of the motion made by a reciprocating engine while it is having a spring compression behaviour after it stops producing work. 93 | recip_stop_arc_restitution = 0.8 ; Gives the amount of torque in % restituted when reaching its max arc by a reciprocating engine while it is having a spring compression behaviour after it stops producing work. 94 | recip_stop_arc_max_pct_rpm = 0.04 ; Gives the % max rpm at which a reciprocating engine that stopped producing work will start having a spring compression behaviour. 95 | recip_stop_arc_friction_factor = 2 ; Factor on how much friction affects the reciprocating engine while having a spring compression behaviour. 96 | egt_factor_from_pct_power = 0:0.5, 0.5:0.894, 0.64:0.956, 0.75:0.98, 1:1 ; Gives the EGT temperature factor (to egt_peak_temperature) from the pct of power (HP/maxHP) 97 | egt_delta_from_mixture_ratio = 0.043:-100, 0.05:-89.7, 0.067:-50, 0.07:0, 0.075:-4.9, 0.083:-80, 0.108:-120.5 ; Gives the EGT temperature delta (to current egt value after factor is applied) from the mixture ratio 98 | carb_icing_sensiblity = 0.25 ; from 0 for no icing to 1 for full sebsibility 99 | 100 | [PROPELLER] 101 | thrust_scalar = 1.2 ; Propeller thrust scalar **SG updated was 1.2 102 | propeller_type = 1 ; 0=Constant Speed, 1=Fixed Pitch 103 | propeller_diameter = 5.75 ; Propeller Diameter, (feet) **SG updated originally 5.9 104 | propeller_blades = 2 ; Number of propeller blades 105 | propeller_moi = 4 ; Propeller moment of inertia **SG updated originally 5 106 | beta_max = 0 ; Maximum blade pitch angle for constant speed prop, (degrees) 107 | beta_min = 0 ; Minimum blade pitch angle for constant speed prop, (degrees) 108 | min_gov_rpm = 0 ; Miminum governed RPM 109 | prop_tc = 0 ; Prop time-constant 110 | gear_reduction_ratio = 1 ; Propeller gear reduction ratio 111 | fixed_pitch_beta = 20 ; Fixed pitch angle of fixed pitch prop, (degrees) 112 | low_speed_theory_limit = 67 ; Speed at which low speed theory becomes blended in (feet/second) **SG updated 67=40kts originally 0 113 | prop_sync_available = 0 ; Prop synchronization available? 0=FALSE, 1=TRUE 114 | prop_deice_available = 0 ; Prop de-icing available? 0=FALSE, 1=TRUE 115 | prop_feathering_available = 0 ; Prop feathering available? 0=FALSE, 1=TRUE 116 | prop_auto_feathering_available = 0 ; Prop auto-feathering available? 0=FALSE, 1=TRUE 117 | min_rpm_for_feather = 0 ; Minimum RPM for prop feathering 118 | beta_feather = 0 ; Feathering pitch angle (degrees) 119 | power_absorbed_cf = 0 ; Coefficient of friction for power absorbed by propeller 120 | defeathering_accumulators_available = 0 ; Defeathering accumulators available? 0=FALSE, 1=TRUE 121 | prop_reverse_available = 0 ; Prop reverse available? 0=FALSE, 1=TRUE 122 | minimum_on_ground_beta = 0 ; Miminum pitch angle on ground, (degrees) 123 | minimum_reverse_beta = 0 ; Minimum pitch angle in reverse, (degrees) 124 | prop_reverse_max_vel = 2 ; Max uvel when reversing 125 | prop_governor_p = 0 ; Propeller governor controller P 126 | prop_governor_i = 0 ; Propeller governor controller I 127 | prop_governor_d = 0 ; Propeller governor controller D 128 | prop_governor_iboundary = 0 ; Propeller governor controller I Boundary 129 | prop_governor_dboundary = 0 ; Propeller governor controller D Boundary 130 | prop_efficiency_table = 0.0:0.00:0.20:0.40:0.60:0.80:1.00:1.20:1.40:1.60:1.80:2.00:2.20, 15.0:0.15:0.40:0.71:0.86:0.72:0.50:0.34:0.23:0.15:0.11:0.08:0.06, 20.0:0.10:0.30:0.67:0.81:0.80:0.74:0.55:0.42:0.30:0.19:0.12:0.09, 25.0:0.08:0.23:0.49:0.72:0.82:0.87:0.82:0.60:0.41:0.28:0.18:0.13 131 | prop_power_cf = 0.0:0.000:0.200:0.400:0.600:0.800:1.000:1.200:1.400:1.600:1.800:2.000:2.200:2.400, 15.0:0.032:0.029:0.025:0.022:0.009:-0.057:-0.188:-0.338:-0.522:-0.705:-0.915:-1.092:-1.220, 20.0:0.084:0.075:0.066:0.058:0.045:0.010:-0.074:-0.188:-0.338:-0.525:-0.726:-0.942:-1.120, 25.0:0.098:0.094:0.088:0.080:0.070:0.050:0.020:-0.040:-0.134:-0.272:-0.468:-0.717:-0.933, 30.0:0.138:0.132:0.128:0.120:0.110:0.099:0.078:0.040:-0.017:-0.110:-0.248:-0.468:-0.741, 35.0:0.206:0.198:0.188:0.178:0.163:0.150:0.130:0.105:0.070:0.023:-0.074:-0.254:-0.510, 40.0:0.250:0.242:0.233:0.223:0.214:0.204:0.190:0.175:0.150:0.118:0.072:0.019:-0.059 132 | use_propeller_rpm = 0 133 | 134 | [DISABLED_CONTROLS] 135 | DisableFuelValveControls = 0 ; Disable fuel valve controls 136 | DisableMixtureControls = 0 ; Disable mixture controls 137 | DisableParkingBrakeControls = 0 ; Disable parking brake controls 138 | DisablePropellerControls = 0 ; Disable propeller controls 139 | 140 | -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/flight_model.cfg: -------------------------------------------------------------------------------- 1 | [VERSION] 2 | major = 1 3 | minor = 0 4 | 5 | [WEIGHT_AND_BALANCE] 6 | max_gross_weight = 1670 ; Empty weight, (LBS) 7 | empty_weight = 1081 ; Empty weight, (LBS) 8 | reference_datum_position = 7.2, 0, 0 ; Position of reference datum relative to FS(0,0,0) (FEET), z, x, y 9 | empty_weight_CG_position = -5.5, 0, 0 ; Position of airplane empty weight CG relative to reference datum (FEET), z, x, y 10 | CG_forward_limit = 0.12 ; Gravity center forward limit in %MAX (divided by 100: 0.12 = 12%MAC) 11 | CG_aft_limit = 0.34 ; Gravity center aft limit in %MAX (divided by 100: 0.34 = 34%MAC) 12 | empty_weight_pitch_MOI = 1717 ; Empty pitch moment of inertia, Jxx (SLUG SQ FEET) 13 | empty_weight_roll_MOI = 1388 ; Empty roll moment of inertia, Jzz (SLUG SQ FEET) 14 | empty_weight_yaw_MOI = 2770 ; Empty yaw moment of inertia, Jyy (SLUG SQ FEET) 15 | empty_weight_coupled_MOI = 10 ; Empty transverse moment of inertia, Jyz (SLUG SQ FEET) 16 | activate_mach_limit_based_on_cg = 0 ; Activate mach limitation depending on CG position (true if > 0 /false othewise). Mostly for Concorde). 17 | activate_cg_limit_based_on_mach = 0 ; Activate cg limitation depending on mach value (true if > 0 /false othewise). Mostly for Concorde). 18 | max_number_of_stations = 2 ; Number of payload stations 19 | station_load.0 = 170, -7.5, -0.86, 0, TT:MENU.PAYLOAD.PILOT, 1 20 | station_load.1 = 170, -7.5, 0.86, 0, TT:MENU.PAYLOAD.FRONT_PAX, 2 21 | 22 | [CONTACT_POINTS] 23 | static_pitch = 0.6 ; degrees, pitch when at rest on the ground (+=Up, -=Dn) 24 | static_cg_height = 3.15 ; feet, altitude of CG when at rest on the ground 25 | gear_system_type = 0 ; gear system type (betweeen 0 and 4) 0 = electrical, 1 = hydraulic, 2 = pneumatic, 3 = manual, 4 = none, 5 = undefined 26 | tailwheel_lock = 0 ; Is tailwheel lock available TRUE/FALSE 27 | max_number_of_points = 11 ; Number of contact points 28 | gear_locked_on_ground = 0 ; Defines whether or not the landing gear handle is locked to down when the plane is on the ground. 29 | gear_locked_above_speed = -1 ; Defines the speed at which the landing gear handle becomes locked in the up position. (-1 = Disabled) 30 | max_speed_full_steering = 10 ; Defines the speed under which the full angle of steering is available (in feet/second). 31 | max_speed_decreasing_steering = 20 ; Defines the speed above which the angle of steering stops decreasing (in feet/second). 32 | min_available_steering_angle_pct = 0.2 ; Defines the percentage of steering which will always be available even above max_speed_decreasing_steering (in percent over 100). 33 | max_speed_full_steering_castering = 20 ; Defines the speed under which the full angle of steering is available for free castering wheels (in feet/second). 34 | max_speed_decreasing_steering_castering = 40 ; Defines the speed above which the angle of steering stops decreasing for free castering wheels (in feet/second). 35 | min_castering_angle = 0.05236 ; Defines the minimum angle a free castering wheel can take (in radians). 36 | max_castering_angle = 3.14159265358979 ; Defines the maximum angle a free castering wheel can take (in radians). 37 | point.0 = 1, -2.7, 0, -3.45, 750, 0, 0.523, 15, 0.245, 1.33, 0.8, 0, 0, 0, 165, 165, 4 38 | point.1 = 1, -7.9, -4, -3.30, 1500, 1, 0.523, 0, 0.162, 2, 0.8, 0, 0, 2, 165, 165, 4 39 | point.2 = 1, -7.9, 4, -3.30, 1500, 2, 0.523, 0, 0.162, 2, 0.8, 0, 0, 3, 165, 165, 4 40 | point.3 = 17, -0.2, 0, 0.6, 1, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 41 | point.4 = 2, -6, 0, 2.7, 350, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0 42 | point.5 = 2, -6.8, -16.5, 2.7, 350, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 43 | point.6 = 2, -6.8, 16.5, 2.7, 350, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 44 | point.7 = 2, -20, 0, 0, 750, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 45 | point.8 = 2, -20, -5, 0.8, 350, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0, 0 46 | point.9 = 2, -20, 5, 0.8, 350, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 47 | point.10 = 2, -23.1, 0, 5.4, 350, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 48 | 49 | [FUEL] 50 | ; 51 | ;Short range tanks 52 | ;LeftMain = -6.5, -4, 2.6, 13, 0.75 ; For each tank: Tank position (z longitudinal, x lateral, y vertical) (FEET), total fuel capacity (GALLONS), unusable fuel capacity (GALLONS) **SG updated 53 | ;RightMain = -6.5, 4, 2.6, 13, 0.75 ; **SG updated 54 | ;Panel currently has long range tanks... 55 | LeftMain = -6.5, -4, 2.6, 19.5, 0.75 ; For each tank: Tank position (z longitudinal, x lateral, y vertical) (FEET), total fuel capacity (GALLONS), unusable fuel capacity (GALLONS) **SG updated 56 | RightMain = -6.5, 4, 2.6, 19.5, 0.75 ; **SG updated 57 | Center1 = -3.6, 0, 0, 0, 0 58 | Center2 = -3.6, 0, 0, 0, 0 59 | Center3 = -3.6, 0, 0, 0, 0 60 | LeftAux = -3.6, 0, 0, 0, 0 61 | LeftTip = -3.6, 0, 0, 0, 0 62 | RightAux = -3.6, 0, 0, 0, 0 63 | RightTip = -3.6, 0, 0, 0, 0 64 | External1 = -3.6, 0, 0, 0, 0 65 | External2 = -3.6, 0, 0, 0, 0 66 | fuel_type = 1 ; 1 = OCTANE 100, 2 = JET_A, 3 = OCTANE 80, 4 = AUTO GAS, 5 = JET B 67 | number_of_tank_selectors = 1 ; Max 4 68 | electric_pump = 0 69 | engine_driven_pump = 1 70 | manual_transfer_pump = 0 71 | manual_pump = 0 72 | anemometer_pump = 0 73 | fuel_dump_rate = 0.02 74 | default_fuel_tank_selector.1 = 1 ; Default fuel selector used in case of autostart for engine 1, default is ALL. 75 | default_fuel_tank_selector.2 = 1 ; Default fuel selector used in case of autostart for engine 2, default is ALL. 76 | default_fuel_tank_selector.3 = 1 ; Default fuel selector used in case of autostart for engine 3, default is ALL. 77 | default_fuel_tank_selector.4 = 1 ; Default fuel selector used in case of autostart for engine 4, default is ALL. 78 | 79 | [AIRPLANE_GEOMETRY] 80 | wing_area = 159.5 ; Wing area S (SQUARE FEET) **SG updated 81 | wing_span = 33.33 ; Wing span b (FEET) **SG updated 82 | wing_root_chord = 5.5 ; Wing root chord croot (FEET) 83 | wing_camber = 1 ; (DEGREES) 84 | wing_thickness_ratio = 0.033 ; Local thickness is local_chord(x)*wing_thickness_ratio, x = lateral coord 85 | wing_dihedral = 1.5 ; Dihedral angle Lambda (DEGREES) 86 | wing_incidence = 0 ; Wing incidence (DEGREES) 87 | wing_twist = 0 ; Wing twist epsilon (DEGREES) **SG updated originally -2 88 | oswald_efficiency_factor = 0.75 ; Wing Oswald efficiency factor e (non dimensional) 89 | wing_winglets_flag = 0 ; Has winglets true/false 90 | wing_sweep = 0 ; Wing sweep (DEGREES) **SG updated originally 2 91 | wing_pos_apex_lon = -7.41723 ; Longitudinal (z) position of wing apex w.r.t reference datum (FEET) 92 | wing_pos_apex_vert = 2.25 ; Vertical (y) position of wing apex w.r.t reference datum (FEET) 93 | htail_area = 15 ; Horizontal tail area (SQUARE FEET) 94 | htail_span = 8.5 ; Horizontal tail span (FEET) 95 | htail_pos_lon = -20 ; Longitudinal (z) position of horizontal tail w.r.t reference datum (FEET) 96 | htail_pos_vert = 0.9 ; Vertical (y) position of horizontal tail w.r.t reference datum (FEET) 97 | htail_incidence = 1 ; Horizontal tail incidence (DEGREES) 98 | htail_sweep = 10 ; Horizontal tail sweep angle (DEGREES) 99 | htail_thickness_ratio = 0.04 ; Local thickness is local_chord(x)*htail_thickness_ratio, x = lateral coord 100 | vtail_area = 14.22 ; Vertical tail area (SQUARE FEET) 101 | vtail_span = 5 ; Vertical tail span (FEET) 102 | vtail_sweep = 40 ; Vertical tail sweep angle (DEGREES) 103 | vtail_pos_lon = -19.5 ; Longitudinal (z) position of vertical tail w.r.t reference datum (FEET) 104 | vtail_pos_vert = 2.75 ; Vertical (y) position of vertical tail w.r.t reference datum (FEET) 105 | vtail_thickness_ratio = 0.04 ; Local thickness is local_chord(x)*vtail_thickness_ratio, x = lateral coord 106 | fuselage_length = 22 ; Nose to tail (FEET) 107 | fuselage_diameter = 3.5 108 | fuselage_center_pos = -9, 0, 0.25 109 | elevator_area = 15 ; Elevator area (SQUARE FEET) 110 | aileron_area = 20 ; Elevator area (SQUARE FEET) 111 | rudder_area = 14 ; Elevator area (SQUARE FEET) 112 | elevator_up_limit = 25 ; Elevator max deflection up angle (DEGREES) 113 | elevator_down_limit = 18 ; Elevator max deflection down angle (absolute value) (DEGREES) 114 | aileron_up_limit = 20 ; Aileron max deflection angle (DEGREES) 115 | aileron_down_limit = 15 ; Aileron max deflection down angle (absolute value) (DEGREES) 116 | rudder_limit = 23 ; Rudder max deflection angle (absolute value) (DEGREES) 117 | rudder_trim_limit = 0 ; Rudder trim max deflection angle (absolute value) (DEGREES) 118 | elevator_trim_limit = 19.5 ; Elevator trim max angle (absolute value) (DEGREES) 119 | spoiler_limit = 0 ; Spoiler max deflection angle (absolute value) (DEGREES) 120 | spoilerons_available = 0 ; Aircraft has spoilerons true/false 121 | aileron_to_spoileron_gain = 0 ; Aileron influence on spoileron angle (non-dimensional) 122 | min_ailerons_for_spoilerons = 0 ; Minimum aileron deflection (absolute value) in which spoilerons are active (DEGREES) 123 | min_flaps_for_spoilerons = 0 ; Minimum flaps deflection (absolute value) in which spoilerons are active (DEGREES) 124 | spoiler_extension_time = 0 ; Spoilers extension time (SECONDS) 125 | spoiler_handle_available = 0 ; Spoiler handles available true/false 126 | auto_spoiler_available = 0 ; Auto spoilers available true/false 127 | auto_spoiler_min_speed = 0 ; Auto spoilers minimum trigger speed 128 | positive_g_limit_flaps_up = 4.4 ; Flap positive load limit when up. Same dimension as gravity vector FEET/SECONDS^2 **SG updated originally 4 129 | positive_g_limit_flaps_down = 3.5 ; Flap positive load limit when down. Same dimension as gravity vector FEET/SECONDS^2 **SG updated originally 3.8 130 | negative_g_limit_flaps_up = -1.76 ; Flap negative load limit when up. Same dimension as gravity vector FEET/SECONDS^2 **SG updated originally -3.2 131 | negative_g_limit_flaps_down = -1.76 ; Flap negative load limit when down. Same dimension as gravity vector FEET/SECONDS^2 **SG updated originally -2.4 132 | load_safety_factor = 1.5 ; Flap negative load limit when down. Same dimension as gravity vector FEET/SECONDS^2 133 | elevator_trim_neutral = 1 ; Elevator trim max angle (absolute value) (DEGREES), for indicators only (no influence on flight model) 134 | aileron_to_rudder_scale = 0 ; non-dimensional 135 | flap_to_aileron_scale = 0 ; non-dimensional 136 | fly_by_wire = 0 ; Fly-by-wire available true/false 137 | elevator_elasticity_table = 0:1, 10:1, 50:0.5, 100:0.333333, 200:0.1 138 | aileron_elasticity_table = 0:1, 10:1, 50:0.5, 100:0.333333, 200:0.1 139 | rudder_elasticity_table = 0:1, 10:1, 50:0.5, 100:0.333333, 200:0.1 140 | elevator_trim_elasticity_table = 0:1, 10:1, 50:0.5, 100:0.333333, 200:0.1 141 | 142 | [AERODYNAMICS] 143 | lift_coef_pitch_rate = -12.277 ; The change in lift per change in pitch rate 144 | lift_coef_daoa = 0 ; lift per change in angle of attack rate 145 | lift_coef_delta_elevator = -1.032 ; The change in lift per change in elevator deflection 146 | lift_coef_horizontal_incidence = 0 ; The change in lift per change in horizontal incidence angle 147 | lift_coef_flaps = 0.3522 ; Change in lift due to flaps 148 | lift_coef_spoilers = 0 ; Change in lift due to spoilers 149 | drag_coef_zero_lift = 0.0350 ; The zero lift drag polar 150 | drag_coef_flaps = 0.0602 151 | drag_coef_gear = 0.01 152 | drag_coef_spoilers = 0 153 | side_force_slip_angle = -2.229 ; (yaw angle) The change in side force per change in side slip angle 154 | side_force_roll_rate = 0.279 ; (roll velocity) The change in side force per change in roll rate 155 | side_force_yaw_rate = 2.689 ; (yaw velocity) The change in side force per change in yaw rate 156 | side_force_delta_rudder = -2.186 ; The change in side force per change in rudder deflection 157 | pitch_moment_horizontal_incidence = 0 ; The change in pitch moment per change in horizontal incidence angle 158 | pitch_moment_delta_elevator = -3.237 ; The change in pitch moment per change in elevator deflection 159 | pitch_moment_delta_trim = -3.237 ; The change in pitch moment per change in trim 160 | pitch_moment_pitch_damping = -108.961 ; The change in pitch moment per change in pitch rate(PRIMARY PITCH STABILITY FACTOR). deg/s 161 | pitch_moment_aoa_0 = -0.031 ; Pitch moment at zero angle - of - attack 162 | pitch_moment_daoa = 0 ; The change in pitch moment per change in angle of attack 163 | pitch_moment_flaps = 0.0 ; The pitch moment due to flaps 164 | pitch_moment_gear = 0 ; The pitch moment due to gear 165 | pitch_moment_spoilers = 0 ; The pitch moment due to spoilers 166 | pitch_moment_delta_elevator_propwash = 0 167 | pitch_moment_pitch_propwash = 0 ;**SG updated was 0 effect??? 168 | roll_moment_slip_angle = 0.293 ; The change in roll moment per sideslip angle(DIHEDRAL EFFECT) 169 | roll_moment_roll_damping = -1.988 170 | roll_moment_yaw_rate = -0.231 171 | roll_moment_spoilers = 0 ; The change in roll moment due to spoilers 172 | roll_moment_delta_aileron = -0.313 ; (control)The change in roll moment per change in aileron deflection 173 | roll_moment_delta_rudder = 0.192 ; (control)The change in roll moment per change rudder deflection 174 | roll_moment_delta_aileron_trim_scalar = -0.313 ; Change in roll moment due to aileron trim 175 | yaw_moment_slip_angle = 0.929 ; The change in yaw moment per change sideslip angle(WEATHER VANING EFFECT) 176 | yaw_moment_roll = 0.065 ; (adverse yaw) The change in yaw moment per change in roll rate deg/s 177 | yaw_moment_yaw_damping = -4.825 ; (damping)The change in yaw moment per change in yaw rate(PRIMARY YAW STABILITY FACTOR deg/s) 178 | yaw_moment_yaw_propwash = 0 ; (damping) 179 | yaw_moment_delta_aileron = 0.002 ; (adverse yaw) The change in yaw moment per change aileron deflection 180 | yaw_moment_delta_rudder = 0.974 ; (control)The change in yaw moment per change in rudder deflection PRIMARY YAW POWER FACTOR 181 | yaw_moment_delta_rudder_propwash = 0 ; (control) 182 | yaw_moment_delta_rudder_trim_scalar = 0.974 ; Change in yaw moment due to rudder trim 183 | compute_aero_center = 0 184 | aero_center_lift = 1 ; Init to center 185 | lift_coef_aoa_table = -3.15:0, -0.8:-0.989, -0.4:-0.71, -0.2:-0.474, -0.1:-0.281, 0:0.2, 0.2:1.105, 0.23:1.201, 0.26:1.3961, 0.29:1.27, 0.31:1.233, 0.4:0.772, 0.8:0.979, 3.15:0 186 | lift_coef_ground_effect_mach_table = 0:1.2 187 | lift_coef_mach_table = 0:1 188 | lift_coef_delta_elevator_mach_table = 0:0 189 | lift_coef_daoa_mach_table = 0:0 190 | lift_coef_pitch_rate_mach_table = 0:0 191 | lift_coef_horizontal_incidence_mach_table = 0:0 192 | drag_coef_zero_lift_mach_tab = 0:0, 0.57:0, 0.58:0.05, 0.6:0.1, 0.65:0.2, 1:0.2, 1.2:0.027846, 1.4:0.02638, 1.6:0.024426, 1.8:0.02296, 2:0.021495, 2.2:0.020518, 2.4:0.020029, 2.6:0.019541, 2.8:0.019541, 3:0.019541, 3.2:0.019541 193 | side_force_slip_angle_mach_table = 0:0 194 | side_force_delta_rudder_mach_table = 0:0 195 | side_force_yaw_rate_mach_table = 0:0 196 | side_force_roll_rate_mach_table = 0:0 197 | pitch_moment_aoa_table = -3.15:0, -0.8:-0.947, -0.4:-0.522, -0.2:-0.167, -0.1:-0.062, 0:0, 0.2:0.216, 0.23:0.26, 0.26:0.308, 0.29:0.363, 0.31:0.4, 0.4:0.473, 0.8:0.923, 3.15:0 198 | pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.612, -20:0.837, -10:0.93, -5:0.968, 0:1, 5:0.974, 10:0.93, 20:0.824, 40:0.577, 180:-1 ; AoA(alpha) is given in DEGREES 199 | pitch_moment_horizontal_incidence_aoa_table = 0:1 ; AoA(alpha) is given in DEGREES 200 | pitch_moment_daoa_aoa_table = 0:1 ; AoA(alpha) is given in DEGREES 201 | pitch_moment_pitch_alpha_table = 0:1 ; AoA(alpha) is given in DEGREES 202 | pitch_moment_delta_elevator_mach_table = 0:0 203 | pitch_moment_daoa_mach_table = 0:0 204 | pitch_moment_pitch_rate_mach_table = 0:0 205 | pitch_moment_horizontal_incidence_mach_table = 0:0 206 | pitch_moment_aoa_0_mach_table = 0:0 207 | roll_moment_aoa_table = 0:0 ; Cl (roll moment coef) versus AoA 208 | roll_moment_slip_angle_aoa_table = 0:1 209 | roll_moment_roll_rate_aoa_table = 0:1 210 | roll_moment_delta_aileron_aoa_table = 0:1 211 | roll_moment_slip_angle_mach_table = 0:0 212 | roll_moment_delta_rudder_mach_table = 0:0 213 | roll_moment_delta_aileron_mach_table = 0:0 214 | roll_moment_yaw_rate_mach_table = 0:0 215 | roll_moment_roll_rate_mach_table = 0:0 216 | yaw_moment_aoa_table = 0:0 ; Cn (yaw moment coef) versus AoA 217 | yaw_moment_slip_angle_aoa_table = 0:1 218 | yaw_moment_yaw_rate_aoa_table = 0:1 219 | yaw_moment_delta_rudder_aoa_table = 0:1 220 | yaw_moment_slip_angle_mach_table = 0:0 221 | yaw_moment_delta_rudder_mach_table = 0:0 222 | yaw_moment_delta_aileron_mach_table = 0:0 223 | yaw_moment_yaw_rate_mach_table = 0:0 224 | yaw_moment_roll_rate_mach_table = 0:0 225 | elevator_scaling_table = -0.366519:1, -0.244346:1, -0.122173:1, 0:1, 0.162897:1, 0.325795:1, 0.488692:1 ; scales control based on its deflection 226 | aileron_scaling_table = -0.261799:1, -0.174533:1, -0.087266:1, 0:1, 0.116355:1, 0.232711:1, 0.349066:1 ; scales control based on its deflection 227 | rudder_scaling_table = -0.418879:1, -0.279253:1, -0.139626:1, 0:1, 0.139626:1, 0.279253:1, 0.418879:1 ; scales control based on its deflection 228 | aileron_load_factor_effectiveness_table = 0:1, 2:1, 4:1, 8:1, 10:1 ; scaling of roll_moment_delta_aileron versus gravity forces, G effects on aileron effectiveness, acts on roll_moment_delta_aileron 229 | lift_coef_at_drag_zero = 0.1 230 | lift_coef_at_drag_zero_flaps = 0.1 231 | 232 | [FLIGHT_TUNING] 233 | cruise_lift_scalar = 1 234 | parasite_drag_scalar = 1 235 | induced_drag_scalar = 1.5 236 | flap_induced_drag_scalar = 1.5 237 | elevator_effectiveness = 1 238 | elevator_maxangle_scalar = 0.9 239 | aileron_effectiveness = 1.25 240 | rudder_effectiveness = 1 241 | rudder_maxangle_scalar = 0.66 242 | pitch_stability = 0.33 243 | roll_stability = 0.25 244 | yaw_stability = 0.25 245 | elevator_trim_effectiveness = 1 246 | aileron_trim_effectiveness = 1 247 | rudder_trim_effectiveness = 1 248 | hi_alpha_on_roll = 0 ; **SG updated 1 no effect? originally 0 249 | hi_alpha_on_yaw = 0 ; **SG updated 1 no effect? originally 0 250 | p_factor_on_yaw = 1 251 | torque_on_roll = 1 252 | gyro_precession_on_roll = 1 253 | gyro_precession_on_yaw = 1 254 | engine_wash_on_roll = 1 ; Torque effect 255 | 256 | [REFERENCE SPEEDS] 257 | full_flaps_stall_speed = 42 ; Knots True (KTAS) **SG updated KCAS = 42 @ average cg/S.L. (originally 33) 258 | flaps_up_stall_speed = 47 ; Knots True (KTAS) **SG updated KCAS = 42 @ average cg/S.L. (originally 40) 259 | cruise_speed = 107 ; Knots True (KTAS) **SG 75% at 8000ft 260 | max_mach = 0.3 261 | max_indicated_speed = 149 ; Red line (KIAS) 262 | max_flaps_extended = 85 ; **SG updated originally 91 263 | normal_operating_speed = 111 ; **SG updated originally 129 264 | airspeed_indicator_max = 170 ; **SG updated originally 200 265 | rotation_speed_min = 50 ; Min speed required (Kts) 266 | climb_speed = 65 ; Climb speed (Kts) 267 | cruise_alt = 1500 ; (ft) 268 | takeoff_speed = 50 ; Takeoff Speed (Kts) 269 | spawn_cruise_altitude = 1500 ; Spawn Cruise Altitude (ft) 270 | spawn_descent_altitude = 500 ; Spawn Descent Altitude (ft) 271 | best_angle_climb_speed = 55 ; Best angle climb speed (Kts) **SG updated originally 0 272 | approach_speed = 65 ; Approach speed (Kts) **SG updated originally 0 273 | best_glide = 60 ; Best Glide (Kts) **SG updated originally 0 274 | 275 | [INTERACTIVE POINTS] 276 | number_of_interactive_points = 0 277 | 278 | ;===================== FLAPS ===================== 279 | 280 | [FLAPS.0] 281 | type = 1 ; Flap type 0 = None, 1 = trailing edge, 2 = leading edge 282 | system_type = 0 ; Flap system type 0 = electrical, 1 = hydraulic, 2 = pneumatic, 3 = manual, 4 = none 283 | span-outboard = 0.4 ; Outboard span area (added area) (percentage, non dimensional) 284 | extending-time = 5 ; Flap extension time (SECONDS) 285 | damaging-speed = 120 ; Speed above which flap is damaged (Kts) 286 | blowout-speed = 170 ; Speed above which flap is blown out (Kts) 287 | maneuvering_flaps = 0 288 | lift_scalar = 1.9 ; Scalar coefficient to ponderate global flap lift coef (non dimensioned) 289 | drag_scalar = 1.9 ; Scalar coefficient to ponderate global flap drag coef (non dimensioned) 290 | pitch_scalar = 1 ; Scalar coefficient to ponderate global flap pitch coef (non dimensioned) 291 | max_on_ground_position = 3 ; Dynamically set in-tool to last flap-position index by defaut when -1 is found. 292 | flaps-position.0 = 0, -1, 0 293 | flaps-position.1 = 10, -1, 0.25 294 | flaps-position.2 = 20, -1, 0.75 295 | flaps-position.3 = 30, -1, 1 296 | 297 | -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/hangar.flt: -------------------------------------------------------------------------------- 1 | 2 | [Avionics.0] 3 | Comm1Active=118.300 4 | Comm1Standby=124.850 5 | Comm2Active=124.850 6 | Comm2Standby=124.850 7 | Comm3Active=124.850 8 | Comm3Standby=124.850 9 | Nav1Active=110.50 10 | Nav1Standby=113.90 11 | OBS1=360 12 | Nav2Active=110.50 13 | Nav2Standby=113.90 14 | OBS2=360 15 | 16 | TransponderState=0 17 | ADFActive=890 18 | ADF2Active=890 19 | DMESelected=1 20 | ComTransmit=1 21 | ComReceiveBoth=False 22 | Com1Receive=True 23 | Com2Receive=False 24 | Com3Receive=False 25 | AudioNav1Listen=False 26 | AudioNav2Listen=False 27 | AudioMarkerListen=True 28 | AudioDmeListen=False 29 | AudioAdfListen=False 30 | AudioAdf2Listen=False 31 | AvionicsSwitch=False 32 | 33 | [Engine Parameters.1.0] 34 | ThrottleLeverPct=0 35 | PropellerLeverPct=0 36 | MixtureLeverPct=0.9998779296875 37 | Pct Engine RPM=0 38 | MaxReachedEngineRPM=2454.7394303494743326 39 | LeftMagneto=False 40 | RightMagneto=False 41 | GeneratorSwitch=False 42 | FuelValveOpen=False 43 | CowlFlapPct=0 44 | FuelPumpSwitch=False 45 | FuelPumpSwitch_EX1=0 46 | CarbHeat/DeiceSwitch=False 47 | EngineMasterSwitch=False 48 | GlowPlugTemperaturePct=1 49 | IgnitionSwitch=0 50 | 51 | [Propeller.1.0] 52 | prop_beta=0.20943951023931955957 53 | prop_max_rpm_percent=0 54 | 55 | [Systems.0] 56 | BatterySwitch=False 57 | StructuralDeiceSwitch=False 58 | PropDeiceSwitch=False 59 | Autobrakes=0 60 | StandbyVacuum=False 61 | PropSync=False 62 | AutoFeatherSwitch=False 63 | FlightDirector=False 64 | PanelLights=False 65 | LaunchBarSwitch=False 66 | LaunchBarState=0 67 | TailhookHandle=False 68 | TailhookState=0 69 | FoldingWingsHandle=False 70 | FoldingWingsState=0, 0 71 | 72 | [LocalVars.0] 73 | ;Note these settings may override standard config settings 74 | ;-------------------------------------------- 75 | ;C152X Cessna 300 ADF 76 | XMLVAR_ADF_MODE_SEL=2 ;2='ADF' Mode 77 | XMLVAR_ADF_VOLUME=0 ;0=OFF, 100=FULL 78 | ;-------------------------------------------- 79 | ;C152X KX155 DUAL NAVCOM 80 | XMLVAR_NAVCOM_COM_1_VOLUME=0 ;0=OFF, 100=FULL 81 | XMLVAR_NAVCOM_COM_2_VOLUME=0 ;0=OFF, 100=FULL 82 | XMLVAR_NAVCOM_COM_1_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 83 | XMLVAR_NAVCOM_COM_2_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 84 | 85 | XMLVAR_NAVCOM_NAV_1_VOLUME=100 ;0=0,100=FULL 86 | XMLVAR_NAVCOM_NAV_2_VOLUME=100 ;0=0,100=FULL 87 | XMLVAR_NAVCOM_NAV_1_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 88 | XMLVAR_NAVCOM_NAV_2_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 89 | ;-------------------------------------------- 90 | ;C152X KA134 AUDIO SELECTOR 91 | XMLVAR_AUDIO_COM_1_MIC_SEL=0 ;1=SEL, (COM 1 TX SEL), MIC 1 and 2 mutually exclusive 92 | XMLVAR_AUDIO_COM_2_MIC_SEL=1 ;1=SEL, (COM 2 TX SEL), MIC 1 and 2 mutually exclusive 93 | 94 | XMLVAR_AUDIO_BOTH_SEL=1 ;0=OFF, 1=SEL 95 | XMLVAR_AUDIO_NAV_1_SEL=0 ; 96 | XMLVAR_AUDIO_NAV_2_SEL=0 ; 97 | XMLVAR_AUDIO_ADF_SEL=0 ; 98 | XMLVAR_AUDIO_DME_SEL=0 ; 99 | XMLVAR_AUDIO_MKR_SEL=1 ; 100 | XMLVAR_AUDIO_SPKR_SEL=0 ; 101 | ;-------------------------------------------- 102 | 103 | [Gauges.0] 104 | KollsmanSetting=29.921342849731445313 105 | 106 | [BleedAir.0] 107 | BleedAirSource=0 108 | 109 | [Switches.0] 110 | PitotHeat=False 111 | BeaconLights=False 112 | LandingLights=False 113 | LogoLights=False 114 | NavLights=False 115 | PanelLights=False 116 | RecognitionLights=False 117 | StrobeLights=False 118 | TaxiLights=False 119 | WingLights=False 120 | CabinLights=False 121 | GlareshieldLights=False 122 | PedestalLights=False 123 | 124 | [AutoPilot.0] 125 | MasterSwitch=False 126 | WingLeveler=False 127 | Nav1Lock=False 128 | HeadingLock=False 129 | HeadingValue=0 130 | AltitudeLock=False 131 | AltitudeValue=0 132 | AttitudeHold=False 133 | AirspeedHold=False 134 | AirspeedValue=0 135 | MachHold=False 136 | MachValue=0 137 | VerticalSpeedHold=False 138 | VerticalSpeedValue=0 139 | RPMHold=False 140 | RPMValue=0 141 | GlideslopeHold=False 142 | ApproachHold=False 143 | BackCourseHold=False 144 | YawDamper=False 145 | ToGa=False 146 | AutoThrottleArm=False 147 | GPSdrivesNAV1=False 148 | IsUsedForLesson=False 149 | ForceDisplayUI=False 150 | 151 | [Controls.0] 152 | SpoilersHandle=000.00 153 | FlapsHandle=000.00 154 | LeftFlap=000.00 155 | RightFlap=000.00 156 | GearsHandle=000.00 157 | Gear1=100.00 158 | Gear2=100.00 159 | Gear3=100.00 160 | YokeY=050.00 161 | YokeX=050.00 162 | Rudder=050.00 163 | LeftBrake=000.00 164 | RightBrake=000.00 165 | ParkingBrake=000.00 166 | 167 | RudderTrimPct=0 168 | AileronTrimPct=0 169 | AileronTrimDisabled=False 170 | ElevatorTrimDisabled=False 171 | RudderTrimDisabled=False -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/model/Cessna152_interior.XML: -------------------------------------------------------------------------------- 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | 9 | 10 | 11 | 12 | 13 | 14 | 15 | 16 | 17 | 18 | 19 | 20 | 21 | 22 | 23 | 24 | 25 | 26 | 27 | 28 | 29 | 30 | 1 (A:FUEL LEFT QUANTITY, gallon) (A:FUEL TANK LEFT MAIN CAPACITY, gallon) / - 20 * (A:TURN COORDINATOR BALL, scaler) * - 31 | 32 | 33 | 34 | 1 (A:FUEL RIGHT QUANTITY, gallon) (A:FUEL TANK RIGHT MAIN CAPACITY, gallon) / - 20 * (A:TURN COORDINATOR BALL, scaler) * + 35 | 36 | 37 | 38 | 39 | 40 | 400 41 | True 42 | 43 | 44 | 45 | 46 | 47 | 48 | 49 | 50 | ELECTRICAL_Switch_Magneto 51 | ELECTRICAL_Switch_Magneto 52 | Horizontal 53 | 0.75 54 | Forward 55 | 0 56 | 1 57 | 2 58 | 3 59 | Curved 60 | 61 | 62 | 3 63 | 0 64 | 1 65 | TT:COCKPIT.TOOLTIPS.MAGNETO_START_SWITCH_OFF 66 | TT:COCKPIT.TOOLTIPS.MAGNETO_START_SWITCH_R 67 | TT:COCKPIT.TOOLTIPS.MAGNETO_START_SWITCH_L 68 | TT:COCKPIT.TOOLTIPS.MAGNETO_START_SWITCH_BOTH 69 | TT:COCKPIT.TOOLTIPS.MAGNETO_START_SWITCH_START 70 | 71 | 72 | 73 | 74 | 75 | 76 | (A:ELECTRICAL MASTER BATTERY:1, Bool) (A:AVIONICS MASTER SWITCH, Bool) != if{ 77 | (>K:TOGGLE_AVIONICS_MASTER) 78 | } 79 | 80 | 81 | 82 | 5 83 | 84 | (A:ELECTRICAL MASTER BATTERY:1, Bool) (A:AVIONICS MASTER SWITCH, Bool) != if{ 85 | (>K:TOGGLE_AVIONICS_MASTER) 86 | } 87 | 88 | 89 | 90 | 91 | 92 | 93 | 94 | 95 | 96 | -400 97 | FUEL_Lever_Mixture_1_Push 98 | 99 | 100 | ENGINE_LEVER_PRIMER 101 | ENGINE_LEVER_PRIMER 102 | 103 | 104 | 105 | 106 | 107 | 108 | 109 | Checklist_FuelValve 110 | 111 | 112 | 113 | 114 | 115 | TT:COCKPIT.TOOLTIPS.YOKE_VISIBILITY 116 | 117 | 118 | 1 119 | HANDLING_Yoke_Hider_1_Add 120 | 121 | 122 | 2 123 | 124 | 125 | 126 | 2 127 | HANDLING_Yoke_Hider_2_Add 128 | 129 | 130 | HANDLING_Yoke_1_Cable 131 | 1 132 | 133 | 134 | 135 | HANDLING_Yoke_2_Cable 136 | 2 137 | 138 | 139 | 140 | 141 | 142 | 143 | SPLITTED 144 | True 145 | HANDLING_RudderPedals_1_1 146 | HANDLING_RudderPedals_ 147 | _1_Brake 148 | HANDLING_RudderPedals_ 149 | _2_Brake 150 | True 151 | True 152 | 153 | 154 | 155 | True 156 | True 157 | 158 | 159 | 160 | 161 | 162 | 163 | 164 | 165 | 166 | 167 | 168 | 169 | 0.2 170 | 171 | 172 | 173 | 174 | 175 | 176 | 177 | 100 178 | 179 | 180 | 181 | 0 182 | True 183 | 184 | 185 | 186 | 0 187 | 170 188 | INSTRUMENT_AirspeedIndicator_Highlight 189 | True 190 | 191 | 192 | 193 | 194 | INSTRUMENT_AttitudeIndicator_Highlight_1 195 | True 196 | 197 | 198 | 199 | 200 | 201 | 202 | 203 | 27.9 204 | 31.6 205 | 28.2 206 | 31.3 207 | INSTRUMENT_Altimeter_Highlight_1 208 | 209 | 210 | 211 | 212 | 213 | 214 | 215 | INSTRUMENT_Heading_Highlight_1 216 | 217 | 218 | 219 | 220 | 221 | 222 | 0 223 | 3500 224 | 225 | 226 | 227 | 244 | 245 | 246 | 247 | 248 | 265 | 266 | 2 267 | 268 | 269 | 270 | 271 | 272 | 273 | (A:ELECTRICAL MAIN BUS VOLTAGE, Volts) 14 > 274 | 100 275 | 276 | 277 | 278 | LEFT MAIN 279 | 0 280 | True 281 | 282 | 283 | 284 | liter 285 | 286 | 287 | 288 | 0 289 | 11.5 @FuelTankSensorAdjustmentLeftTank 290 | 22.7 @FuelTankSensorAdjustmentLeftTank 291 | 30.3 @FuelTankSensorAdjustmentLeftTank 292 | 37.9 @FuelTankSensorAdjustmentLeftTank 293 | 45.4 @FuelTankSensorAdjustmentLeftTank 294 | 52.9 @FuelTankSensorAdjustmentLeftTank 295 | 60.6 @FuelTankSensorAdjustmentLeftTank 296 | 68.1 @FuelTankSensorAdjustmentLeftTank 297 | 73.8 @FuelTankSensorAdjustmentLeftTank 298 | 0 299 | 15 300 | 35 301 | 47 302 | 57 303 | 68 304 | 80 305 | 92 306 | 99 307 | 100 308 | 9 309 | 100 310 | 100 311 | 0 312 | 313 | 314 | RIGHT MAIN 315 | 0 316 | 2 317 | True 318 | 319 | 320 | 321 | liter 322 | 323 | 324 | 325 | 0 326 | 11.5 @FuelTankSensorAdjustmentRightTank 327 | 22.7 @FuelTankSensorAdjustmentRightTank 328 | 30.3 @FuelTankSensorAdjustmentRightTank 329 | 37.9 @FuelTankSensorAdjustmentRightTank 330 | 45.4 @FuelTankSensorAdjustmentRightTank 331 | 52.9 @FuelTankSensorAdjustmentRightTank 332 | 60.6 @FuelTankSensorAdjustmentRightTank 333 | 68.1 @FuelTankSensorAdjustmentRightTank 334 | 73.8 @FuelTankSensorAdjustmentRightTank 335 | 0 336 | 13 337 | 37 338 | 45 339 | 59 340 | 67 341 | 82 342 | 91 343 | 97 344 | 100 345 | 9 346 | 100 347 | 100 348 | 0 349 | 350 | 351 | 352 | 75 353 | -75 354 | 50 355 | True 356 | 357 | 358 | 26 359 | 360 | 361 | fahrenheit 362 | 70 363 | 270 364 | 0 365 | True 366 | 367 | 368 | psi 369 | -20 370 | 120 371 | 0 372 | True 373 | 374 | 375 | -60 376 | 80 377 | 378 | 379 | 380 | 381 | 382 | 383 | 384 | 385 | 386 | 387 | 388 | 389 | 390 | 391 | 392 | 393 | 394 | 395 | 396 | 397 | 398 | 399 | 400 | 401 | LIGHTING_Knob_Panel 402 | LIGHTING_Knob_Panel 403 | 1.5 404 | 405 | 406 | 407 | 408 | 409 | 410 | 411 | 5 412 | 413 | 414 | 415 | LIGHTING_Panel_Emisive 416 | 417 | 418 | 419 | 420 | 421 | 422 | 0 423 | TT:COCKPIT.TOOLTIPS.CABIN_AIR_2STATES_PUSHED 424 | TT:COCKPIT.TOOLTIPS.CABIN_AIR_2STATES_PULLED 425 | 426 | 427 | 428 | DOD 429 | TT:COCKPIT.TOOLTIPS.CABIN_HEAT_2STATES_PUSHED 430 | TT:COCKPIT.TOOLTIPS.CABIN_HEAT_2STATES_PULLED 431 | 432 | 433 | 434 | 435 | 436 | 437 | 438 | 439 | 440 | 441 | 442 | 443 | 500 444 | 445 | 4 446 | True 447 | 448 | 449 | 1 450 | 0.2 451 | True 452 | (A:COM VOLUME:1,Percent) 0 > (A:CIRCUIT GENERAL PANEL ON, Bool) and 453 | 454 | 455 | 456 | 2 457 | 0.2 458 | True 459 | (A:COM VOLUME:2,Percent) 0 > (A:CIRCUIT GENERAL PANEL ON, Bool) and 460 | 461 | 462 | 463 | 1 464 | NavCom1_Screen 465 | 466 | 467 | 1 468 | 469 | 470 | 2 471 | NavCom2_Screen 472 | 473 | 474 | 1 475 | 476 | 477 | 478 | 479 | 480 | 481 | 482 | 483 | 484 | 485 | 486 | 1 487 | true 488 | 2 489 | AUDIO_Push_MIC_1 490 | AUDIO_Push_MIC_1 491 | 492 | 493 | 494 | 2 495 | true 496 | 1 497 | AUDIO_Push_MIC_2 498 | AUDIO_Push_MIC_2 499 | 500 | 501 | 502 | AUDIO_Push_NAV_Both 503 | AUDIO_Push_NAV_Both 504 | 505 | 506 | 507 | 1 508 | AUDIO_Push_NAV_1 509 | AUDIO_Push_NAV_1 510 | 511 | 512 | 513 | 2 514 | AUDIO_Push_NAV_2 515 | AUDIO_Push_NAV_2 516 | 517 | 518 | 519 | 520 | 1 521 | AUDIO_Push_AOE 522 | AUDIO_Push_AOE 523 | 524 | 525 | 526 | 527 | AUDIO_Push_DME 528 | AUDIO_Push_DME 529 | 530 | 531 | 532 | 533 | AUDIO_Push_MKR 534 | AUDIO_Push_MKR 535 | 536 | 537 | 538 | 539 | AUDIO_Push_SPKR 540 | AUDIO_Push_SPKR 541 | 542 | 543 | 544 | 545 | 546 | 547 | True 548 | 4 549 | 550 | 551 | 552 | 553 | 554 | 555 | 556 | 557 | 600 558 | 559 | 560 | ADF_Screen 561 | 1 562 | (A:ADF VOLUME:1, Percent) 0 > (A:CIRCUIT GENERAL PANEL ON, Bool) and 563 | 564 | 565 | 566 | 567 | 568 | True 569 | 500 570 | 571 | 572 | 573 | 574 | True 575 | 576 | 577 | 578 | 579 | 580 | 581 | (A:CIRCUIT GENERAL PANEL ON, Bool) 582 | 583 | 584 | 585 | 586 | 587 | 588 | 589 | 590 | 591 | 592 | 593 | 594 | 595 | 596 | AUDIO_Switch_Intercom 597 | 598 | 599 | AUDIO_Switch_Test 600 | 601 | 602 | 603 | 604 | 605 | 606 | -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/panel/PANEL.CFG: -------------------------------------------------------------------------------- 1 | [Vcockpit01] 2 | size_mm = 230,45 3 | pixel_size = 230,45 4 | texture = $Hourmeter 5 | emissive = 0 6 | htmlgauge00=Generic/Misc/HourMeter/HourMeter.html, 0,0,230,45 7 | 8 | [VCockpit02] 9 | size_mm = 512,70 10 | pixel_size = 512,70 11 | texture = $NavCom1_Screens 12 | htmlgauge00=Generic/Radios/KX155A/KX155A.html?Index=1, 0, 0, 512, 70 13 | 14 | [VCockpit03] 15 | size_mm = 512,70 16 | pixel_size = 512,70 17 | texture = $NavCom2_Screens 18 | htmlgauge00=Generic/Radios/KX155A/KX155A.html?Index=2, 0, 0, 512, 70 19 | 20 | [VCockpit04] 21 | size_mm = 512,79 22 | pixel_size = 512,79 23 | texture = $ADF_Screen 24 | htmlgauge00=Generic/Radios/C300ADF/C300ADF.html, 0,0,512,79 25 | 26 | [VPainting01] 27 | size_mm = 256, 64 28 | texture = $RegistrationNumber 29 | location = interior 30 | painting00=Registration/Registration.html?font_color=white, 0, 0, 256, 64 31 | 32 | [VPainting02] 33 | size_mm = 1024, 256 34 | texture = $RegistrationNumber 35 | location = exterior 36 | painting00=Registration/Registration.html?font_color=000000, 0, 0, 1024, 256 -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/panel/panel.xml: -------------------------------------------------------------------------------- 1 | 2 | 3 | 4 | C300ADF 5 | 6 | 7 | 8 | 9 | 0 10 | 11 | 12 | 13 | 14 | 15 | 16 | 17 | -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/runway.FLT: -------------------------------------------------------------------------------- 1 | [SimVars.0] 2 | PVelBodyAxis=0 3 | BVelBodyAxis=0 4 | HVelBodyAxis=0 5 | XVelBodyAxis=0 6 | YVelBodyAxis=0 7 | ZVelBodyAxis=0 8 | SimOnGround=True 9 | 10 | [Avionics.0] 11 | Comm1Active=127.850 12 | Comm1Standby=124.850 13 | Comm2Active=124.850 14 | Comm2Standby=124.850 15 | Comm3Active=124.850 16 | Comm3Standby=124.850 17 | Nav1Active=110.50 18 | Nav1Standby=113.90 19 | OBS1=360 20 | Nav2Active=110.50 21 | Nav2Standby=113.90 22 | OBS2=360 23 | 24 | TransponderState=4 25 | ADFActive=890 26 | ADF2Active=890 27 | DMESelected=1 28 | ComTransmit=1 29 | ComReceiveBoth=False 30 | Com1Receive=True 31 | Com2Receive=False 32 | Com3Receive=False 33 | AudioNav1Listen=False 34 | AudioNav2Listen=False 35 | AudioMarkerListen=False 36 | AudioDmeListen=False 37 | AudioAdfListen=False 38 | AudioAdf2Listen=False 39 | AvionicsSwitch=True 40 | 41 | [Engine Parameters.1.0] 42 | ThrottleLeverPct=0 43 | PropellerLeverPct=1 44 | Pct Engine RPM=0.32811646340229250196 45 | MaxReachedEngineRPM=3903.5488821170947631 46 | LeftMagneto=True 47 | RightMagneto=True 48 | GeneratorSwitch=True 49 | FuelValveOpen=True 50 | CowlFlapPct=0 51 | FuelPumpSwitch=False 52 | CarbHeat/DeiceSwitch=False 53 | EngineMasterSwitch=True 54 | GlowPlugTemperaturePct=1 55 | 56 | [Propeller.1.0] 57 | prop_beta=0.20943951023931955957 58 | 59 | [Systems.0] 60 | BatterySwitch=True 61 | StructuralDeiceSwitch=False 62 | PropDeiceSwitch=False 63 | Autobrakes=0 64 | StandbyVacuum=False 65 | PropSync=False 66 | AutoFeatherSwitch=False 67 | FlightDirector=False 68 | PanelLights=False 69 | LaunchBarSwitch=False 70 | LaunchBarState=0 71 | TailhookHandle=False 72 | TailhookState=0 73 | FoldingWingsHandle=False 74 | FoldingWingsState=0, 0 75 | 76 | [LocalVars.0] 77 | ;Note these settings may override standard config settings 78 | ;-------------------------------------------- 79 | ;C152X Cessna 300 ADF 80 | XMLVAR_ADF_MODE_SEL=2 ;2='ADF' Mode 81 | XMLVAR_ADF_VOLUME=100 ;0=OFF, 100=FULL 82 | ;-------------------------------------------- 83 | ;C152X KX155 DUAL NAVCOM 84 | XMLVAR_NAVCOM_COM_1_VOLUME=100 ;0=OFF, 100=FULL 85 | XMLVAR_NAVCOM_COM_2_VOLUME=100 ;0=OFF, 100=FULL 86 | XMLVAR_NAVCOM_COM_1_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 87 | XMLVAR_NAVCOM_COM_2_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 88 | 89 | XMLVAR_NAVCOM_NAV_1_VOLUME=100 ;0=0,100=FULL 90 | XMLVAR_NAVCOM_NAV_2_VOLUME=100 ;0=0,100=FULL 91 | XMLVAR_NAVCOM_NAV_1_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 92 | XMLVAR_NAVCOM_NAV_2_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 93 | ;-------------------------------------------- 94 | ;C152X KA134 AUDIO SELECTOR 95 | XMLVAR_AUDIO_COM_1_MIC_SEL=1 ;1=SEL, (COM 1 TX SEL), MIC 1 and 2 mutually exclusive 96 | XMLVAR_AUDIO_COM_2_MIC_SEL=0 ;1=SEL, (COM 2 TX SEL), MIC 1 and 2 mutually exclusive 97 | 98 | XMLVAR_AUDIO_BOTH_SEL=0 ;0=OFF, 1=SEL 99 | XMLVAR_AUDIO_NAV_1_SEL=0 ; 100 | XMLVAR_AUDIO_NAV_2_SEL=0 ; 101 | XMLVAR_AUDIO_ADF_SEL=0 ; 102 | XMLVAR_AUDIO_DME_SEL=0 ; 103 | XMLVAR_AUDIO_MKR_SEL=1 ; 104 | XMLVAR_AUDIO_SPKR_SEL=0 ; 105 | ;-------------------------------------------- 106 | 107 | [Gauges.0] 108 | KollsmanSetting=29.921342849731445313 109 | 110 | [BleedAir.0] 111 | BleedAirSource=0 112 | 113 | [Switches.0] 114 | PitotHeat=False 115 | BeaconLights=True 116 | LandingLights=True 117 | LogoLights=True 118 | NavLights=True 119 | PanelLights=False 120 | PanelLightsNight=True 121 | RecognitionLights=True 122 | StrobeLights=True 123 | TaxiLights=False 124 | WingLights=True 125 | CabinLights=False 126 | GlareshieldLights=True 127 | PedestalLights=False 128 | 129 | [AutoPilot.0] 130 | MasterSwitch=False 131 | WingLeveler=False 132 | Nav1Lock=False 133 | HeadingLock=False 134 | HeadingValue=0 135 | AltitudeLock=False 136 | AltitudeValue=0 137 | AttitudeHold=False 138 | AirspeedHold=False 139 | AirspeedValue=0 140 | MachHold=False 141 | MachValue=0 142 | VerticalSpeedHold=False 143 | VerticalSpeedValue=0 144 | RPMHold=False 145 | RPMValue=0 146 | GlideslopeHold=False 147 | ApproachHold=False 148 | BackCourseHold=False 149 | YawDamper=False 150 | ToGa=False 151 | AutoThrottleArm=False 152 | GPSdrivesNAV1=False 153 | IsUsedForLesson=False 154 | ForceDisplayUI=False 155 | 156 | [Controls.0] 157 | SpoilersHandle=000.00 158 | FlapsHandle=000.00 159 | LeftFlap=000.0 160 | RightFlap=000.0 161 | GearsHandle=000.00 162 | Gear1=100.00 163 | Gear2=100.00 164 | Gear3=100.00 165 | YokeY=050.00 166 | YokeX=050.00 167 | Rudder=050.00 168 | LeftBrake=000.11 169 | RightBrake=000.11 170 | ParkingBrake=100.00 171 | 172 | RudderTrimPct=0 173 | AileronTrimPct=0 174 | AileronTrimDisabled=False 175 | ElevatorTrimDisabled=False 176 | RudderTrimDisabled=False -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/systems.cfg: -------------------------------------------------------------------------------- 1 | [VERSION] 2 | major = 1 3 | minor = 0 4 | 5 | [LIGHTS] 6 | lightdef.0 = Type:3#Index:0#LocalPosition:-6.00000000000001,16.62,2.56#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_NavigationGreen#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_NavigationGreen 7 | lightdef.1 = Type:3#Index:0#LocalPosition:-6.00000000000001,-16.62,2.56#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_NavigationRed#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_NavigationRed 8 | lightdef.2 = Type:3#Index:0#LocalPosition:-9.55,-30,0#LocalRotation:0,0,180#EffectFile:LIGHT_ASOBO_NavigationWhite#Node:LIGHT_ASOBO_NavigationTail#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_NavigationTail 9 | lightdef.3 = Type:1#Index:0#LocalPosition:-21.65,0,5.58#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_BeaconTop#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_BeaconTop 10 | lightdef.4 = Type:5#Index:0#LocalPosition:-1.1,0,-0.45#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_Landing#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_Landing 11 | lightdef.5 = Type:6#Index:0#LocalPosition:-1.1,0,-0.43#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_Taxi#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_Taxi 12 | lightdef.6 = Type:2#Index:1#LocalPosition:-6.00000000000001,16.75,2.56#LocalRotation:0,0,-90#EffectFile:LIGHT_ASOBO_StrobeSimple#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_StrobeWing 13 | lightdef.7 = Type:2#Index:2#LocalPosition:-6.00000000000001,-16.75,2.56#LocalRotation:0,0,90#EffectFile:LIGHT_ASOBO_StrobeSimple#Node:#PotentiometerIndex:1#EmMesh:LIGHT_ASOBO_StrobeWing 14 | lightdef.8 = Type:10#Index:0#LocalPosition:-7.6,0,2.34#LocalRotation:65,0,0#EffectFile:LIGHT_ASOBO_CockpitSpot#PotentiometerIndex:5 15 | lightdef.9 = Type:10#Index:0#LocalPosition:-6.1,0,1#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_CabinBounceSmall#PotentiometerIndex:5 16 | lightdef.10 = Type:13#Index:0#LocalPosition:-6.5,0,0.5#LocalRotation:0,0,0#EffectFile:LIGHT_ASOBO_CockpitMinimalAmbiantLow#PotentiometerIndex:5 17 | lightdef.11 = Type:4#Index:0#LocalPosition:-5.1,0.23,1.12#LocalRotation:0,0,180#EffectFile:LIGHT_ASOBO_ScreenOrange#PotentiometerIndex:4 18 | lightdef.12 = Type:10#Index:0#LocalPosition:-7.3,0,2.4#LocalRotation:45,0,0#EffectFile:LIGHT_ASOBO_CockpitSpotRed#PotentiometerIndex:5 19 | 20 | [BRAKES] 21 | parking_brake = 1 ; BrakeTypes enum 22 | auto_brakes = 0 ; This value is the number of "positive" settings, not including OFF. '0' means NO AutoBrake 23 | toe_brakes_scale = 0.5 ; Brake scalar 24 | differential_braking_scale = 0 ; Delta on the amount of brake when the rudder pedals deflected 25 | hydraulic_system_scalar = 0 ; On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure 26 | 27 | [ELECTRICAL] 28 | ;SG updated 29 | bus.1 = Name:MAIN_BUS 30 | bus.2 = Connections:bus.1#Name:AVIONICS_BUS 31 | battery.1 = Connections:bus.1#Capacity:15.5#Voltage:curve.1#Name:MAIN_BATTERY ; Main Battery RW options - 17Ah, 15.5Ah or 12.75Ah 32 | alternator.1 = Connections:bus.1#iEng:0#Voltage:curve.3#Load:curve.2#Name:Main_Alternator 33 | ; 0:24.2, 0.1:24.3, 0.3:24.7, 0.5:25.3, 0.9:26.2, 1:26.3 - NO LOAD battery voltage 34 | curve.1 = 0:15.0, 0.1:18.5, 0.3:21.0, 0.5:22.5, 0.9:23.2, 1:24 ; Battery voltage for capacity % (UNDER ASSUMED LOAD) 35 | ;curve.1 = 0:5.0, 0.1:6, 0.3:7.0, 0.5:10.0, 0.9:15.0, 1:24 ; Battery voltage for capacity % (UNDER ASSUMED LOAD) test curve -fast discharge 36 | curve.2 = 500:8, 1000:30, 1400:55, 2000:60 ; Load from RPM table 30A at idle speed & 60 at max rpm 37 | ;curve.2 = 0.08:0, 0.09:8, 0.15:52, 0.22:70 ; Load from RPM table (asobo post patch) 38 | curve.3 = 500:10, 1000:26.0, 1400:27.4, 2000:28.0 ; Alternator Voltage from RPM 39 | circuit.1 = Type:CIRCUIT_STARTER #Connections:bus.1 #Power:2035, 3135, 21.5 #Name:Starter_1 ; Starter 40 | circuit.2 = Type:CIRCUIT_GENERAL_PANEL #Connections:bus.1 #Power:16.9, 20, 18.9 #Name:General_Panel ; General panel 41 | ; Encoding Altimeter 2.4W 42 | ; Fuel Gauges 2.4W 43 | ; Battery Contactor 12W 44 | circuit.3 = Type:CIRCUIT_FUEL_PUMP #Connections:bus.1 #Power:0, 0, 10.0 #Name:Fuel_Pump ; not used 45 | circuit.4 = Type:CIRCUIT_FLAP_MOTOR #Connections:bus.1 #Power:204, 300, 20.5 #Name:Flaps_Motor ; Flap motor 46 | circuit.5 = Type:CIRCUIT_GEAR_MOTOR #Connections:bus.1 #Power:0, 0, 10.0 #Name:Inop ; not used 47 | circuit.6 = Type:CIRCUIT_DIRECTIONAL_GYRO #Connections:bus.1 #Power:0, 0, 10.0 #Name:Directional_Gyro ; not used 48 | circuit.7 = Type:CIRCUIT_STANDBY_VACUUM #Connections:bus.1 #Power:0, 0, 10.0 #Name:STBY_Vacuum ; not used 49 | circuit.8 = Type:CIRCUIT_AUTOPILOT #Connections:bus.1 #Power:0, 0, 10.0 #Name:Autopilot ; not used 50 | circuit.9 = Type:CIRCUIT_XPNDR #Connections:bus.1 #Power:32, 32, 20.7 #Name:Transponder ; Transponder 51 | circuit.10 = Type:CIRCUIT_ADF_DME #Connections:bus.1 #Power:12, 12, 20.3 #Name:ADF_DME ; ADF 52 | circuit.11 = Type:CIRCUIT_MARKER_BEACON #Connections:bus.1 #Power:2.4, 3, 19.1 #Name:Marker_Position ; marker beacon 53 | circuit.12 = Type:CIRCUIT_TURN_COORDINATOR #Connections:bus.1 #Power:7.2, 8, 16.9 #Name:Turn_Coordinator ; turn coordinator 54 | circuit.13 = Type:CIRCUIT_GPS #Connections:bus.1 #Power:0, 0, 10.0 #Name:GPS ; not used 55 | circuit.14 = Type:CIRCUIT_AVIONICS #Connections:bus.1 #Power:0, 0, 15.0 #Name:Avionics_1 ; not used 56 | circuit.15 = Type:CIRCUIT_AUDIO #Connections:bus.1 #Power:1, 1, 19.0 #Name:Audio ; 57 | circuit.16 = Type:CIRCUIT_PITOT_HEAT #Connections:bus.1 #Power:69.6, 80, 17.5 #Name:Pitot_Heat ; pitot_heat 58 | circuit.17 = Type:CIRCUIT_NAV:1 #Connections:bus.1 #Power:6, 8, 20.3 #Name:NAV1 ; NAV 1 59 | circuit.18 = Type:CIRCUIT_COM:1 #Connections:bus.1 #Power:6, 8, 20.3 #Name:COM1 ; COM 1 60 | circuit.19 = Type:CIRCUIT_NAV:2 #Connections:bus.1 #Power:6, 8, 19.9 #Name:NAV2 ; NAV 2 61 | circuit.20 = Type:CIRCUIT_COM:2 #Connections:bus.1 #Power:6, 8, 19.9 #Name:COM2 ; COM 2 62 | circuit.21 = Type:CIRCUIT_NAV:3 #Connections:bus.1 #Power:0, 0, 19.1 #Name:NAV3 ; not used 63 | circuit.22 = Type:CIRCUIT_COM:3 #Connections:bus.1 #Power:0, 0, 19.1 #Name:COM3 ; not used 64 | circuit.23 = Type:CIRCUIT_LIGHT_LANDING #Connections:bus.1 #Power:213, 240, 21.5 #Name:Landing_Light ; Landing light 65 | circuit.24 = Type:CIRCUIT_LIGHT_BEACON #Connections:bus.1 #Power:144, 150, 19.5 #Name:Beacon_Light ; Beacon light 66 | circuit.25 = Type:CIRCUIT_LIGHT_PANEL #Connections:bus.1 #Power:0, 0, 10.0 #Name:Instruments_Lights ; not used 67 | circuit.26 = Type:CIRCUIT_LIGHT_CABIN #Connections:bus.1 #Power:4.8, 5, 18.8 #Name:Cabin_Light_pilot ; Cabin light 68 | circuit.27 = Type:CIRCUIT_LIGHT_PEDESTAL #Connections:bus.1 #Power:0, 0, 10.0 #Name:Pedestal_Light ; not used 69 | circuit.28 = Type:CIRCUIT_LIGHT_GLARESHIELD #Connections:bus.1 #Power:14.4, 15, 19.3 #Name:Glareshield_Light ; glareshield light 70 | circuit.29 = Type:CIRCUIT_LIGHT_NAV #Connections:bus.1 #Power:60, 60, 20.1 #Name:Nav_Light_1 ; nav light 71 | circuit.30 = Type:CIRCUIT_LIGHT_STROBE #Connections:bus.1 #Power:72, 72, 20.7 #Name:Strobe_Light_1 ; strobe light 72 | circuit.31 = Type:CIRCUIT_LIGHT_RECOGNITION #Connections:bus.1 #Power:0, 0, 10.0 #Name:Recognition_Light ; 73 | circuit.32 = Type:CIRCUIT_LIGHT_WING #Connections:bus.1 #Power:0, 0, 10.0 #Name:Wing_Light ; not used 74 | circuit.33 = Type:CIRCUIT_LIGHT_LOGO #Connections:bus.1 #Power:0, 0, 10.0 #Name:Logo_Light ; not used 75 | circuit.34 = Type:CIRCUIT_LIGHT_TAXI #Connections:bus.1 #Power:172, 190, 21.6 #Name:Taxi_Light ; taxi light 76 | ;circuit.35 = Type:CIRCUIT_XML:1 #Connections:bus.1 #Power:5000, 500, 27.9 #Name:Dummy1 77 | 78 | 79 | [HYDRAULIC_SYSTEM] 80 | normal_pressure = 0.00000 ; PSI 81 | 82 | [PNEUMATIC_SYSTEM] 83 | max_pressure = 0 ; PSI 84 | bleed_air_scalar = 0.15 85 | 86 | [PITOT_STATIC] 87 | vertical_speed_time_constant = 1 ; Increasing this value will cause a more instantaneous reaction in the VSI 88 | pitot_heat = 1 ; Scalar on heat effectiveness, 0 = not available 89 | 90 | [VACUUM_SYSTEM] 91 | max_pressure = 5.15 ; PSI 92 | vacuum_type = 1 ; Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi 93 | electric_backup_pressure = 4.9 ; PSI 94 | engine_map = 1, 0, 0, 1 95 | 96 | [STALL_WARNING] 97 | type = 2 ; 0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop 98 | stick_shaker = 0 99 | 100 | [DEICE_SYSTEM] 101 | structural_deice_type = 0 ; 0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots 102 | 103 | [RADIOS] 104 | Audio.1 = 1 105 | Com.1 = 1, 1 106 | Com.2 = 1, 1 107 | Nav.1 = 1, 1, 1 108 | Nav.2 = 1, 1, 0 109 | Adf.1 = 1 110 | Transponder.1 = 1 111 | Marker.1 = 1 112 | 113 | [GEAR_WARNING_SYSTEM] 114 | gear_warning_available = 0 115 | pct_throttle_limit = 0.00000 116 | flap_limit_idle = 24.75000 117 | flap_limit_power = 12.37500 118 | 119 | [AUTOPILOT] 120 | autopilot_available = 0 121 | flight_director_available = 0 122 | default_vertical_speed = 700 123 | autothrottle_available = 0 124 | pitch_takeoff_ga = 8 125 | max_pitch = 25 126 | max_pitch_acceleration = 1 127 | max_pitch_velocity_lo_alt = 2 128 | max_pitch_velocity_hi_alt = 1.5 129 | max_pitch_velocity_lo_alt_breakpoint = 20000 130 | max_pitch_velocity_hi_alt_breakpoint = 28000 131 | max_bank = 25 132 | max_bank_acceleration = 5 133 | max_bank_velocity = 10 134 | max_throttle_rate = 0.1 135 | yaw_damper_gain = 0 136 | default_pitch_mode = 0 137 | default_bank_mode = 1 138 | autothrottle_arming_required = 0 139 | autothrottle_takeoff_ga = 1 140 | autothrottle_max_rpm = 90 141 | use_no_default_bank = 1 142 | use_no_default_pitch = 1 143 | pitch_use_elevator_only = 1 144 | -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/target_performance.cfg: -------------------------------------------------------------------------------- 1 | [TARGET_PERFORMANCE] 2 | 3 | // stall 4 | full_flap_full_weight_poweron_stall_speed = 49,0.1; 5 | no_flap_full_weight_poweron_stall_speed = 52,0.1; 6 | stall_aoa = 16.8,0.5; 7 | 8 | // lift 9 | no_flap_zero_lift_aoa = -3.63,0.1; 10 | full_flap_zero_lift_aoa = -6.20,0.1; 11 | no_flap_max_lift_coef = 1.9,0.01; 12 | full_flap_max_lift_coef = 2.14,0.01; 13 | 14 | // drags 15 | no_flap_zero_aoa_drag_coef = 0.0306,0.001; 16 | full_flap_zero_aoa_drag_coef = 0.1061,0.01; 17 | no_flap_flap_parasit_drag_coef = 0.0306,0.001; 18 | full_flap_parasit_drag_coef = 0.1061,0.01; 19 | no_flap_induced_drag_coef = 0.0414,0.1; 20 | full_flap_induced_drag_coef = 0.0414,0.1; 21 | 22 | // glide 23 | no_flap_full_weight_glide_speed = 77,1.0; 24 | no_flap_full_weight_vert_glide_speed = 555,1.0; 25 | no_flap_full_weight_best_glide_finesse = 14.04,0.1; 26 | 27 | // climb rate 28 | best_max_weight_climb_angle_speed = 56,1.0; 29 | best_max_weight_angle_of_climb_rate = 0,1.0; 30 | best_max_weight_angle_of_climb = 6.55,0.1; 31 | best_max_weight_climb_rate_speed = 77,0.1; 32 | best_max_weight_climb_rate = 764.5,1.0; 33 | 34 | 35 | max_endurance_speed = 65.8,0.1; 36 | max_range_speed = 75,0.1; 37 | cruise_speed_level_flight_75pctpower = 115.0,0.1; 38 | max_speed_level_flight_max_power = 133.0,0.1; 39 | 40 | no_flap_max_vert_dive_speed_0pctpower = 381,5.0; 41 | full_flap_max_vert_dive_speed_0pctpower = 207.3,1.0; 42 | no_flap_max_flat_fall_speed_0pctpower = 53.0,0.1; 43 | 44 | [DOUBLE_CHECKS] 45 | wing_area=145.75,0.1; 46 | wing_span = 39.17,0.1; 47 | htail_area = 22.35,0.1; 48 | htail_span = 10.82,0.1; 49 | vtail_area = 22.28,0.1; 50 | vtail_span = 3.6,0.1; 51 | max_gross_weight = 2535,1.0; 52 | empty_weight = 2200,1.0; 53 | max_hp = 135,0.1; 54 | 55 | [PERFORMANCE_REPORT] 56 | //file_path="C:\Users\golivier\Desktop\JUNK_MESH\perf_report.csv" 57 | -------------------------------------------------------------------------------- /C152X/SimObjects/Airplanes/Asobo_C152/taxi.flt: -------------------------------------------------------------------------------- 1 | [SimVars.0] 2 | PVelBodyAxis=0 3 | BVelBodyAxis=0 4 | HVelBodyAxis=0 5 | XVelBodyAxis=0 6 | YVelBodyAxis=0 7 | ZVelBodyAxis=0 8 | SimOnGround=True 9 | 10 | [Avionics.0] 11 | Comm1Active=127.850 12 | Comm1Standby=124.850 13 | Comm2Active=124.850 14 | Comm2Standby=124.850 15 | Comm3Active=124.850 16 | Comm3Standby=124.850 17 | Nav1Active=110.50 18 | Nav1Standby=113.90 19 | OBS1=360 20 | Nav2Active=110.50 21 | Nav2Standby=113.90 22 | OBS2=360 23 | 24 | TransponderState=4 25 | ADFActive=890 26 | ADF2Active=890 27 | DMESelected=1 28 | ComTransmit=1 29 | ComReceiveBoth=False 30 | Com1Receive=True 31 | Com2Receive=False 32 | Com3Receive=False 33 | AudioNav1Listen=False 34 | AudioNav2Listen=False 35 | AudioMarkerListen=False 36 | AudioDmeListen=False 37 | AudioAdfListen=False 38 | AudioAdf2Listen=False 39 | AvionicsSwitch=True 40 | 41 | [Engine Parameters.1.0] 42 | ThrottleLeverPct=0 43 | PropellerLeverPct=1 44 | Pct Engine RPM=0.32811646340229250196 45 | MaxReachedEngineRPM=3903.5488821170947631 46 | LeftMagneto=True 47 | RightMagneto=True 48 | FuelValveOpen=True 49 | GeneratorSwitch=True 50 | FuelValveOpen=True 51 | CowlFlapPct=0 52 | FuelPumpSwitch=False 53 | CarbHeat/DeiceSwitch=False 54 | EngineMasterSwitch=True 55 | GlowPlugTemperaturePct=1 56 | 57 | [Propeller.1.0] 58 | prop_beta=0.20943951023931955957 59 | 60 | [Systems.0] 61 | BatterySwitch=True 62 | StructuralDeiceSwitch=False 63 | PropDeiceSwitch=False 64 | Autobrakes=0 65 | StandbyVacuum=False 66 | PropSync=False 67 | AutoFeatherSwitch=False 68 | FlightDirector=False 69 | PanelLights=False 70 | LaunchBarSwitch=False 71 | LaunchBarState=0 72 | TailhookHandle=False 73 | TailhookState=0 74 | FoldingWingsHandle=False 75 | FoldingWingsState=0, 0 76 | 77 | [LocalVars.0] 78 | ;Note these settings may override standard config settings 79 | ;-------------------------------------------- 80 | ;C152X Cessna 300 ADF 81 | XMLVAR_ADF_MODE_SEL=2 ;2='ADF' Mode 82 | XMLVAR_ADF_VOLUME=100 ;0=OFF, 100=FULL 83 | ;-------------------------------------------- 84 | ;C152X KX155 DUAL NAVCOM 85 | XMLVAR_NAVCOM_COM_1_VOLUME=100 ;0=OFF, 100=FULL 86 | XMLVAR_NAVCOM_COM_2_VOLUME=100 ;0=OFF, 100=FULL 87 | XMLVAR_NAVCOM_COM_1_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 88 | XMLVAR_NAVCOM_COM_2_TEST=0 ;0=SQ ENABLED, 1=TEST (PULLED) 89 | 90 | XMLVAR_NAVCOM_NAV_1_VOLUME=100 ;0=0,100=FULL 91 | XMLVAR_NAVCOM_NAV_2_VOLUME=100 ;0=0,100=FULL 92 | XMLVAR_NAVCOM_NAV_1_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 93 | XMLVAR_NAVCOM_NAV_2_IDENT=0 ;0=OFF, 1=IDENT (PULLED) 94 | ;-------------------------------------------- 95 | ;C152X KA134 AUDIO SELECTOR 96 | XMLVAR_AUDIO_COM_1_MIC_SEL=1 ;1=SEL, (COM 1 TX SEL), MIC 1 and 2 mutually exclusive 97 | XMLVAR_AUDIO_COM_2_MIC_SEL=0 ;1=SEL, (COM 2 TX SEL), MIC 1 and 2 mutually exclusive 98 | 99 | XMLVAR_AUDIO_BOTH_SEL=0 ;0=OFF, 1=SEL 100 | XMLVAR_AUDIO_NAV_1_SEL=0 ; 101 | XMLVAR_AUDIO_NAV_2_SEL=0 ; 102 | XMLVAR_AUDIO_ADF_SEL=0 ; 103 | XMLVAR_AUDIO_DME_SEL=0 ; 104 | XMLVAR_AUDIO_MKR_SEL=1 ; 105 | XMLVAR_AUDIO_SPKR_SEL=0 ; 106 | ;-------------------------------------------- 107 | 108 | [Gauges.0] 109 | KollsmanSetting=29.921342849731445313 110 | 111 | [BleedAir.0] 112 | BleedAirSource=0 113 | 114 | [Switches.0] 115 | PitotHeat=False 116 | BeaconLights=True 117 | LandingLights=False 118 | LogoLights=True 119 | NavLights=True 120 | PanelLights=True 121 | RecognitionLights=True 122 | StrobeLights=False 123 | TaxiLights=True 124 | WingLights=True 125 | CabinLights=False 126 | GlareshieldLights=False 127 | PedestalLights=False 128 | 129 | [AutoPilot.0] 130 | MasterSwitch=False 131 | WingLeveler=False 132 | Nav1Lock=False 133 | HeadingLock=False 134 | HeadingValue=0 135 | AltitudeLock=False 136 | AltitudeValue=0 137 | AttitudeHold=False 138 | AirspeedHold=False 139 | AirspeedValue=0 140 | MachHold=False 141 | MachValue=0 142 | VerticalSpeedHold=False 143 | VerticalSpeedValue=0 144 | RPMHold=False 145 | RPMValue=0 146 | GlideslopeHold=False 147 | ApproachHold=False 148 | BackCourseHold=False 149 | YawDamper=False 150 | ToGa=False 151 | AutoThrottleArm=False 152 | GPSdrivesNAV1=False 153 | IsUsedForLesson=False 154 | ForceDisplayUI=False 155 | 156 | [Controls.0] 157 | SpoilersHandle=000.00 158 | FlapsHandle=000.00 159 | LeftFlap=000.00 160 | RightFlap=000.00 161 | GearsHandle=000.00 162 | Gear1=100.00 163 | Gear2=100.00 164 | Gear3=100.00 165 | YokeY=050.00 166 | YokeX=050.00 167 | Rudder=050.00 168 | LeftBrake=000.11 169 | RightBrake=000.11 170 | ParkingBrake=000.00 171 | 172 | RudderTrimPct=0 173 | AileronTrimPct=0 174 | AileronTrimDisabled=False 175 | ElevatorTrimDisabled=False 176 | RudderTrimDisabled=False -------------------------------------------------------------------------------- /C152X/de-DE.locPak: -------------------------------------------------------------------------------- 1 | { 2 | "LocalisationPackage": { 3 | "Language": "de-DE", 4 | "Strings": { 5 | "AIRCRAFT.DESCRIPTION": "1977 setze Cessna es sich zum Ziel, das über alle Maßen beliebte Kleinflugzeug Model 150 zu modernisieren – was letztendlich zur Entwicklung der 152 führte: eines Eindeckers mit zwei Sitzen, der sich nach kurzer Zeit nicht nur zu einem wahren Klassiker der allgemeinen Luftfahrt, sondern auch zu einem der beliebtesten Schulflugzeuge der Ära nach dem Zweiten Weltkrieg mauserte.

Wenn man die Produktion der primären Cessna-Fabrik in Kansas, Wichita, und die Produktion von Reims Aviation (Frankreich) zusammenaddiert, wurden während des gesamten Produktionsprozesses der 152 (1977–85) mehr als 7500 Flugzeuge gefertigt.

Weithin als Zugpferd betrachtet, wartete die 152 mit einem leistungsfähigeren Kolbenmotor als ihre Vorgängerin auf. Darüber hinaus verfügt sie über einen Knickflügelpropeller und profitiert von Veränderungen bezüglich ihres Motors und ihrer Motorhaube, wodurch Motorenlärm und -vibrationen geringer ausfallen.

Während die 152 Fehler schnell vergibt und leicht zu fliegen ist – wobei sie über eine Hochdecker-Konfiguration verfügt, die eine exzellente Cockpitsicht gewährt –, ist diese Maschine die Inkarnation des Kleinflugzeugs schlechthin, wobei das geringe Gewicht die Herausforderung des Fliegens bei starken Seitenwinden nur noch erhöht. Allerdings überzeugt sie gleichzeitig durch ein sanftes Handling und verspricht eine angenehme Reise, egal, ob Sie ein erfahrener Pilot sind oder gerade erst das Fliegen lernen.", 6 | "AIRCRAFT.UI_MANUFACTURER": "Textron Aviation", 7 | "AIRCRAFT.UI_MODEL": "Cessna 152", 8 | "GAME.CHECKLIST_ADJUST_1000_RPM_OR_LESS": "1000 RPM oder weniger EINSTELLEN" 9 | } 10 | } 11 | } 12 | -------------------------------------------------------------------------------- /C152X/en-US.locPak: -------------------------------------------------------------------------------- 1 | { 2 | "LocalisationPackage": { 3 | "Language": "en-US", 4 | "Strings": { 5 | "AIRCRAFT.DESCRIPTION": "In 1977, Cessna set out to modernize their exceedingly-popular light aircraft Model 150, and the result was the 152 -- a new two-seat monoplane that quickly became a general aviation classic and one of the most popular trainer aircraft of the post-World War II era.

During the 152's full production run (1977-1985), Cessna manufactured over 7,500 aircraft, between its primary factory in Wichita, Kansas and affiliated Reims Aviation of France.

Widely recognized as a workhorse aircraft, the 152 came stock with a more powerful piston-engine than its predecessor, an improved 'gull wing' propeller, and changes to its powerplant and cowling for reduced noise and vibration.

While the 152 is forgiving of mistakes and easy to fly -- with a high-wing configuration that translates to excellent cockpit visibility -- it does put the 'light' in light aircraft, a trait that may add to the challenge of breezy crosswind flight, but also makes for generally docile handling and an overall enjoyable journey, whether you're a seasoned pilot of just learning to fly.", 6 | "AIRCRAFT.UI_MANUFACTURER": "Textron Aviation", 7 | "AIRCRAFT.UI_MODEL": "Cessna 152", 8 | "GAME.CHECKLIST_ADJUST_1000_RPM_OR_LESS": "ADJUST for 1000 RPM or less" 9 | } 10 | } 11 | } 12 | -------------------------------------------------------------------------------- /C152X/es-ES.locPak: -------------------------------------------------------------------------------- 1 | { 2 | "LocalisationPackage": { 3 | "Language": "es-ES", 4 | "Strings": { 5 | "AIRCRAFT.DESCRIPTION": "En 1977, Cessna se propuso modernizar su modelo 150 de aeronaves ligeras, las cuales tuvieron gran popularidad, y el resultado fue el 152, un nuevo monoplano biplaza que rápidamente se convirtió en un clásico de la aviación general y uno de los aviones de instrucción más populares tras la Segunda Guerra Mundial.

Durante la producción completa del 152 (1977-1985), Cessna fabricó más de 7500 aeronaves, tanto en su fábrica principal de Wichita (Kansas) como en la filial francesa Reims Aviation.

Reconocida como una aeronave de gran eficacia, el 152 venía con un motor de pistón más potente que su predecesor, una mejor hélice de \"alas de gaviota\" y otros cambios en su unidad de potencia y capó para Disminuir el ruido y la vibración.

Si bien el 152 es indulgente con los errores y fácil de volar, con una configuración de ala alta que se traduce en una excelente visibilidad de la cabina del piloto, es una aeronave ligera, lo que puede ser un desafío a la hora de afrontar un vuelo con viento de costado, pero también es suave de pilotar haciendo los viajes agradables en general, ya seas un piloto experimentado o estés aprendiendo a volar.", 6 | "AIRCRAFT.UI_MANUFACTURER": "Textron Aviation", 7 | "AIRCRAFT.UI_MODEL": "Cessna 152", 8 | "GAME.CHECKLIST_ADJUST_1000_RPM_OR_LESS": "PONER 1000 RPM o menos" 9 | } 10 | } 11 | } 12 | -------------------------------------------------------------------------------- /C152X/fr-FR.locPak: -------------------------------------------------------------------------------- 1 | { 2 | "LocalisationPackage": { 3 | "Language": "fr-FR", 4 | "Strings": { 5 | "AIRCRAFT.DESCRIPTION": "En 1977, Cessna se met en tête de moderniser son avion léger extrêmement populaire, le Modèle 150. Le résultat fut le 152, un nouveau monoplan biplace qui est rapidement devenu un classique de l'aviation générale et l'un des avions d'entraînement les plus populaires de l'après-guerre.

Pendant la phase de production du 152 (1977-1985), Cessna a fabriqué plus de 7 500 avions, répartis entre son usine principale de Wichita, au Kansas, et sa filiale Reims Aviation en France.

Réputé pour être un avion utilitaire, le 152 était équipé d'un moteur à piston plus puissant que celui de son prédécesseur et d'une hélice de type « aile en mouette » améliorée. Des modifications ont été apportées au groupe motopropulseur et au capot afin de réduire le bruit et les vibrations.

Bien que le 152 pardonne les erreurs et soit facile à piloter, avec une configuration d'ailes hautes qui se traduit par une excellente visibilité depuis le cockpit, sa légèreté peut mettre le pilote au défi lors de vol par vent latéral violent. Toutefois, le Cessna 152 est aussi connu pour sa souple maniabilité et ses trajets particulièrement agréables, que vous soyez un pilote chevronné ou débutant.", 6 | "AIRCRAFT.UI_MANUFACTURER": "Textron Aviation", 7 | "AIRCRAFT.UI_MODEL": "Cessna 152", 8 | "GAME.CHECKLIST_ADJUST_1000_RPM_OR_LESS": "AJUSTER à 1 000 tr\/min ou moins" 9 | } 10 | } 11 | } 12 | -------------------------------------------------------------------------------- /C152X/it-IT.locPak: -------------------------------------------------------------------------------- 1 | { 2 | "LocalisationPackage": { 3 | "Language": "it-IT", 4 | "Strings": { 5 | "AIRCRAFT.DESCRIPTION": "Nel 1977, la Cessna decise di modernizzare il suo popolarissimo aeromobile leggero, il Model 150, e il risultato fu il 152, un nuovo monoplano biposto che diventò in fretta un classico dell'aviazione generale e uno dei più famosi aeromobili d'addestramento del dopoguerra.

Durante il periodo di piena produzione del 152 (1977-1985), la Cessna produsse oltre 7.500 aeromobili tra la sua sede principale a Wichita, in Kansas, e la società affiliata Reims Aviation francese.

Ampiamente riconosciuto come un aeromobile da lavoro pesante, il 152 venne provvisto di un motore a pistoni ancor più potente del suo predecessore, un'elica ad ala di gabbiano migliorata e vennero effettuate modifiche al suo propulsore e alla cappottatura per ridurre il rumore e le vibrazioni.

Anche se il 152 ammette un certo margine di errore ed è facile da manovrare, grazie alla sua configurazione ad ali alte, che si traduce in eccellente visibilità dalla cabina di pilotaggio, il nome di \"aeromobile leggero\" non gli è stato certo assegnato a caso, ed è una caratteristica che può complicare ulteriormente le sfide delle tratte con vento trasversale, ma si lascia manovrare facilmente e consente viaggi piacevoli, che tu sia un pilota esperto o alle prime armi.", 6 | "AIRCRAFT.UI_MANUFACTURER": "Textron Aviation", 7 | "AIRCRAFT.UI_MODEL": "Cessna 152", 8 | "GAME.CHECKLIST_ADJUST_1000_RPM_OR_LESS": "REGOLATI per 1000 giri al minuto o meno" 9 | } 10 | } 11 | } 12 | -------------------------------------------------------------------------------- /C152X/layout.json: -------------------------------------------------------------------------------- 1 | { 2 | "content": [ 3 | { 4 | "path": "de-DE.locPak", 5 | "size": 1791, 6 | "date": "132402817714110148" 7 | }, 8 | { 9 | "path": "en-US.locPak", 10 | "size": 1369, 11 | "date": "132402817714110148" 12 | }, 13 | { 14 | "path": "es-ES.locPak", 15 | "size": 1474, 16 | "date": "132402817714110148" 17 | }, 18 | { 19 | "path": "fr-FR.locPak", 20 | "size": 1542, 21 | "date": "132402817714110148" 22 | }, 23 | { 24 | "path": "it-IT.locPak", 25 | "size": 1574, 26 | "date": "132402817714110148" 27 | }, 28 | { 29 | "path": "pl-PL.locPak", 30 | "size": 1480, 31 | "date": "132402817714110148" 32 | }, 33 | { 34 | "path": "pt-BR.locPak", 35 | "size": 1522, 36 | "date": "132402817714110148" 37 | }, 38 | { 39 | "path": "ru-RU.locPak", 40 | "size": 2510, 41 | "date": "132402817714110148" 42 | }, 43 | { 44 | "path": "ModelBehaviorDefs/C152X/Asobo/Common.xml", 45 | "size": 36, 46 | "date": "132402817714110148" 47 | }, 48 | { 49 | "path": "ModelBehaviorDefs/C152X/Asobo/Common/Index.xml", 50 | "size": 63, 51 | "date": "132402817714110148" 52 | }, 53 | { 54 | "path": "ModelBehaviorDefs/C152X/Asobo/Common/Instrument.xml", 55 | "size": 1077, 56 | "date": "132402817714110148" 57 | }, 58 | { 59 | "path": "ModelBehaviorDefs/C152X/Asobo/Common/Subtemplates/Instrument_Subtemplates.xml", 60 | "size": 22988, 61 | "date": "132402817714110148" 62 | }, 63 | { 64 | "path": "ModelBehaviorDefs/C152X/Asobo/NAVCOM/ADF.xml", 65 | "size": 5044, 66 | "date": "132402817714110148" 67 | }, 68 | { 69 | "path": "ModelBehaviorDefs/C152X/Asobo/NAVCOM/NavComSystem.xml", 70 | "size": 18423, 71 | "date": "132402817714110148" 72 | }, 73 | { 74 | "path": "SimObjects/Airplanes/Asobo_C152/aircraft.cfg", 75 | "size": 3065, 76 | "date": "132402817714110148" 77 | }, 78 | { 79 | "path": "SimObjects/Airplanes/Asobo_C152/Approach.flt", 80 | "size": 3930, 81 | "date": "132402817714110148" 82 | }, 83 | { 84 | "path": "SimObjects/Airplanes/Asobo_C152/apron.flt", 85 | "size": 3991, 86 | "date": "132402817714110148" 87 | }, 88 | { 89 | "path": "SimObjects/Airplanes/Asobo_C152/Climb.flt", 90 | "size": 3933, 91 | "date": "132402817714110148" 92 | }, 93 | { 94 | "path": "SimObjects/Airplanes/Asobo_C152/cockpit.cfg", 95 | "size": 5891, 96 | "date": "132402817714110148" 97 | }, 98 | { 99 | "path": "SimObjects/Airplanes/Asobo_C152/Cruise.flt", 100 | "size": 3930, 101 | "date": "132402817714110148" 102 | }, 103 | { 104 | "path": "SimObjects/Airplanes/Asobo_C152/engines.cfg", 105 | "size": 9545, 106 | "date": "132402817714110148" 107 | }, 108 | { 109 | "path": "SimObjects/Airplanes/Asobo_C152/Final.flt", 110 | "size": 3928, 111 | "date": "132402817714110148" 112 | }, 113 | { 114 | "path": "SimObjects/Airplanes/Asobo_C152/flight_model.cfg", 115 | "size": 19050, 116 | "date": "132402817714110148" 117 | }, 118 | { 119 | "path": "SimObjects/Airplanes/Asobo_C152/hangar.flt", 120 | "size": 3832, 121 | "date": "132402817714110148" 122 | }, 123 | { 124 | "path": "SimObjects/Airplanes/Asobo_C152/runway.FLT", 125 | "size": 3897, 126 | "date": "132402817714110148" 127 | }, 128 | { 129 | "path": "SimObjects/Airplanes/Asobo_C152/systems.cfg", 130 | "size": 9252, 131 | "date": "132402817714110148" 132 | }, 133 | { 134 | "path": "SimObjects/Airplanes/Asobo_C152/target_performance.cfg", 135 | "size": 1639, 136 | "date": "132402817714110148" 137 | }, 138 | { 139 | "path": "SimObjects/Airplanes/Asobo_C152/taxi.flt", 140 | "size": 3897, 141 | "date": "132402817714110148" 142 | }, 143 | { 144 | "path": "SimObjects/Airplanes/Asobo_C152/model/Cessna152_interior.XML", 145 | "size": 24176, 146 | "date": "132402817714110148" 147 | }, 148 | { 149 | "path": "SimObjects/Airplanes/Asobo_C152/panel/PANEL.CFG", 150 | "size": 979, 151 | "date": "132402817714110148" 152 | }, 153 | { 154 | "path": "SimObjects/Airplanes/Asobo_C152/panel/panel.xml", 155 | "size": 318, 156 | "date": "132402817714110148" 157 | } 158 | ] 159 | } -------------------------------------------------------------------------------- /C152X/manifest.json: -------------------------------------------------------------------------------- 1 | { 2 | "dependencies": [ 3 | { 4 | "name": "asobo-aircraft-c152", 5 | "package_version": "0.1.46" 6 | }, 7 | { 8 | "name": "fs-base-aircraft-common", 9 | "package_version": "0.1.61" 10 | } 11 | ], 12 | "content_type": "AIRCRAFT", 13 | "title": "Cessna 152X", 14 | "manufacturer": "Textron Aviation", 15 | "creator": "DRF30q", 16 | "package_version": "0.0.11", 17 | "minimum_game_version": "1.7.12", 18 | "release_notes": { 19 | "neutral": { 20 | "LastUpdate": "", 21 | "OlderHistory": "" 22 | } 23 | }, 24 | "total_package_size": "00000000000533490847" 25 | } -------------------------------------------------------------------------------- /C152X/pl-PL.locPak: -------------------------------------------------------------------------------- 1 | { 2 | "LocalisationPackage": { 3 | "Language": "pl-PL", 4 | "Strings": { 5 | "AIRCRAFT.DESCRIPTION": "W 1977 r. firma Cessna zaczęła modernizować swój niezwykle popularny samolot lekki Model 150, w wyniku czego powstała Cessna 152 – nowy dwuosobowy górnopłat, który szybko stał się klasykiem lotnictwa ogólnego i jednym z najpopularniejszych samolotów szkolnych okresu po II wojnie światowej.

W całym okresie produkcji modelu 152 (1977–1985 r.) w fabryce Cessny w Wichita w stanie Kansas oraz stowarzyszonej firmie Reims Aviation we Francji wyprodukowano ponad 7500 egzemplarzy.

Model 152, służący wiernie jak niezawodny wół roboczy, ma silnik o większej mocy niż poprzedni model oraz udoskonalone śmigło. Zmiany wprowadzone w jednostce napędowej i omaskowaniu silnika pozwoliły też zmniejszyć hałas i drgania.

Cessna 152 wybacza wiele błędów i łatwo nią latać, a dzięki konfiguracja górnopłata przekłada się na doskonałą widoczność z kabiny. Niewielka masa może stanowić dodatkowe wyzwanie podczas lotu z bocznym wiatrem, jednak sprawia też, że sterowanie jest łatwe i daje dużo przyjemności z lotu, niezależnie od tego, czy za sterami siedzi doświadczony pilot, czy ktoś, kto dopiero uczy się latać.", 6 | "AIRCRAFT.UI_MANUFACTURER": "Textron Aviation", 7 | "AIRCRAFT.UI_MODELX": "Cessna 152", 8 | "GAME.CHECKLIST_ADJUST_1000_RPM_OR_LESS": "WYREGULUJ na 1000 obr.\/min lub mniej" 9 | } 10 | } 11 | } 12 | -------------------------------------------------------------------------------- /C152X/pt-BR.locPak: -------------------------------------------------------------------------------- 1 | { 2 | "LocalisationPackage": { 3 | "Language": "pt-BR", 4 | "Strings": { 5 | "AIRCRAFT.DESCRIPTION": "Em 1977, a Cessna decidiu modernizar sua pequena e extremamente popular aeronave Modelo 150, e o resultado foi o 152 – um novo monoplano de dois assentos que rapidamente se tornou um clássico da aviação geral e uma das aeronaves de treinamento mais populares da era pós-Segunda Guerra Mundial.

Durante a produção total do 152 (1977-1985), a Cessna fabricou mais de 7.500 aeronaves, entre sua principal fábrica em Wichita, no Kansas, e sua afiliada, Reims Aviation da França.

Bastante reconhecido como uma aeronave muito confiável, o 152 entrou em cena com um motor de pistão mais poderoso que o seu antecessor, uma hélice de \"asa de gaivota\" aprimorada e alterações no motor e na carenagem para redução de ruído e vibração.

Embora o 152 ignore alguns erros e seja fácil de pilotar – com uma configuração de asas altas que resulta em excelente visibilidade no cockpit – ele adiciona ainda mais leveza ao seu modelo já pequeno, uma característica que pode aumentar o desafio do voo em vento de través, mas que também contribui para manobras geralmente dóceis e uma viagem agradável no geral, não importa se você é um piloto experiente ou se está apenas aprendendo a voar.", 6 | "AIRCRAFT.UI_MANUFACTURER": "Textron Aviation", 7 | "AIRCRAFT.UI_MODEL": "Cessna 152", 8 | "GAME.CHECKLIST_ADJUST_1000_RPM_OR_LESS": "AJUSTE para 1.000 RPM ou menos" 9 | } 10 | } 11 | } 12 | -------------------------------------------------------------------------------- /C152X/ru-RU.locPak: -------------------------------------------------------------------------------- 1 | { 2 | "LocalisationPackage": { 3 | "Language": "ru-RU", 4 | "Strings": { 5 | "AIRCRAFT.DESCRIPTION": "В 1977 году компания Cessna взялась за модернизацию своего невероятно популярного лёгкого самолёта Model 150. Новая модель получила номер 152 — это двухместный моноплан, который быстро завоевал популярность в сегменте лёгких частных воздушных судов и стал самым популярным учебным самолётом послевоенного периода.

За всё время, сколько производилась модель Cessna 152 (1977–1985), компания Cessna успела выпустить более 7500 самолётов на своей главной фабрике в канзасском городе Уичито, а также с помощью мощностей французской компании Reims Aviation.

Cessna 152 — это идеальная рабочая лошадка. Самолёт был оснащён поршневым двигателем, превосходившим своего предшественника по мощности, а также улучшенным воздушным винтом с изменённым сечением лопастей. Благодаря форме капота двигателя удалось добиться снижения шума и вибраций.

Cessna 152 прощает пилотам различные ошибки и отличается отличной управляемостью, а высокое расположение крыла гарантирует отличную видимость из кабины, однако эта модель, как и всё лёгкие самолёты, обладает своими ограничениями и не очень любит боковой ветер. Тем не менее, это по-прежнему отличный самолёт для путешественников, опытных пилотов и курсантов лётных училищ.", 6 | "AIRCRAFT.UI_MANUFACTURER": "Textron Aviation", 7 | "AIRCRAFT.UI_MODEL": "Cessna 152", 8 | "GAME.CHECKLIST_ADJUST_1000_RPM_OR_LESS": "УСТАНОВИТЬ мощность не более 1000 об\/мин" 9 | } 10 | } 11 | } 12 | -------------------------------------------------------------------------------- /README.md: -------------------------------------------------------------------------------- 1 | # MSFS C152X Realism Mod 2 | V0.17 3 | 4 | 5 | ## Installation 6 | Place the "C152X" folder in your community package folder. 7 | 8 | The installation does not create a new aircraft selection in the simulator. The modifications are applied to the Textron Aviation Cessna 152. Once the package is installed in the community folder, selecting this aircraft in the sim should load the C152X Mod aircraft. 9 | 10 | Note that none of the base files for the default aircraft are directly modified in any way. Removing the "C152X" folder from the community package folder should remove and deactivate the C152X Realism Mod. 11 | 12 | ### 0.17 13 | Some of the current improvements (not exhaustive): 14 | - Modified stall speeds flap up/flap down in accordance with published information. Aircraft will now stall at a significantly higher speed. 15 | - Numerous changes to engine performance, now in accordance with Lycoming O-235L2C (115HP, 2700RPM) See note below. 16 | - Fuel consumption adjusted. 17 | - Long Range Fuel Tanks 37.5USG total useable. See note below. 18 | - Fuel Gauges correctly calibrated. 19 | - Fuel Gauge indications will vary realistically in out of balance flight (depending on quantity of fuel in tank) and also on the ground when the aircraft is not wings level. 20 | - Flight tested to verify climb, cruise, service ceiling, fuel consumption etc in accordance with published information. 21 | - Oil Temperature Gauge - gauge calibration and oil temperature modelling adjusted. 22 | - Oil Pressure Gauge - gauge calibration and oil pressure modelling adjusted. 23 | - Electrical system - completely remodelled, using documented electrical loads etc. 24 | - Now models realistic battery discharge/charge and subsequent electrical system behaviour. 25 | - If battery goes flat, various systems will fail at various voltage levels as the battery discharges. 26 | - Ammeter - gauge calibration and behaviour. 27 | - Low voltage light now comes on below ~ 1000 RPM as in real life. 28 | - OAT thermometer now operates regardless of the position of the master switch. 29 | - The overhead (Dome) light can now be dimmed by the dimmer knob below the pilot control yoke. 30 | - The NAV CDI gauges completely revised: 31 | - CDI gauges now respond correctly to: User selected On/Off state of corresponding NAV/COM Radio. 32 | - CDI gauges now respond correctly to: Power state of corresponding NAV/COM Radio. 33 | - CDI gauges now power off when Avionics Power (Battery Master Switch) switched off. 34 | - CDI gauges now power off when the applicable NAV/COM Radio is turned off using the Volume/Off knob. 35 | - CDI gauges now power off if the battery discharges and the voltage level supplied to the applicable 36 | NAV/COM radio drops below the minimum required for operation. 37 | - CDI gauges, Glideslope/Localiser Needle behaviour adjusted. 38 | - CDI gauges, Glideslope/Localiser Flag behaviour adjusted. 39 | - CDI gauges, NAV Flag behaviour adjusted. 40 | - ADF Radio completely revised Knob behaviour. ADF Modes: BFO/REC/ADF and spring return TEST position. 41 | - ADF Rotatable Card gauge behaviour completely revised: 42 | - ADF Needle is driven to point to the selected NDB station only in ADF Mode. (Note that currently the ADF Mode Knob defaults to BFO Mode and must be manually rotated to ADF Mode.) 43 | - ADF Needle remains in current position in ADF Mode when no signal received from an NDB on the currently selected frequency. 44 | - ADF Needle remains in current position in BFO and REC Modes. 45 | - ADF Needle is slewed in a clockwise direction while ADF Mode Knob held in TEST position. When released, the ADF Mode Knob spring returns to ADF Mode. 46 | - ADF Needle remains in current position when ADF Radio is turned off using the Volume/Off knob. 47 | - ADF Needle remains in current position if battery discharges and voltage level to the radio drops below the minimum required for operation. 48 | - ADF Volume and ADF Mode Knob position state now loaded from .flt files. ADF Mode knob defaults to 'ADF' position. 49 | - NAVCOM (KX155) reworked. Various states including volume/Off state etc now loaded from .flt files. 50 | - NAV Ident / COM Test remain out when pulled. 51 | - Audio Selector (KA134) completely revised. Various states now loaded from .flt files. 52 | - Buttons now remain depressed when selected. 53 | - MIC1/MIC2 selects either COM1 or COM2 as active transmitter. 54 | - BOTH allows selection of reception on both COM1 and COM2. 55 | - NAV1, NAV2, ADF (AOE wtf?) etc select ident audio. 56 | - MKR selects Marker ident audio. Note: My testing so far indicates audio received (and light flashes) from Middle Marker, however Outer Marker light flashes but no audio heard. Not sure if this is a sim issue. 57 | - DME, SPKR buttons now operate but are currently non functional. 58 | 59 | ### Notes: 60 | - The default aircraft panel has a Tachometer with a 2700RPM redline. As a result I have taken the decision to model the C152 with the corresponding and slightly uprated 115HP engine. (It is essentially the same engine as the 'standard' C152 Lycoming engine with 110HP/2550RPM redline, with a few extra horsepower gained from the additional RPM. The standard performance charts eg cruise power settings etc will still be valid. The extra horsepower means slightly better takeoff and go-around performance and a slightly higher service ceiling. The current version tested in the sim has a service ceiling around 15,500ft.) 61 | - The default aircraft panel depicted fuel gauges for Long Range Tanks (37.5USG) but the sim data was for Short Range Tanks (24.5USG useable). Again I have taken the decision to model the Long Range Tanks. This now gives the aircraft a nearly 9 hour endurance and a range of up to 670 nm. This makes the aircraft much more capable of long range flights in the sim, and I think much more useful. (Round the world type flight capability. :)) 62 | - I have not tested this Mod in any of the activities, lessons etc that may utilise the default aircraft. I can't guarantee that it will not cause issues in some of these situations. Use at your own risk. :) 63 | 64 | ## Changelog 65 | [0.11] - 2020-09-04 66 | Initial release. 67 | 68 | [0.12] - 2020-09-05 69 | Corrected situation with no avionics power in certain startup situations. 70 | 71 | [0.14] - 2020-09-10 72 | Navigation CDI gauges completely revised. 73 | 74 | [0.15] - 2020-09-14 75 | Aircraft name reverted to default. Flight Training lessons now selectable. 76 | Navigation ADF Radio and associated gauge completely revised. 77 | 78 | [0.16] - 2020-09-19 79 | ADF/NAVCOM/Audio Selection Panel completely revised. Various states now loaded with .flt files. 80 | 81 | [0.17] - 2020-10-14 82 | Corrected manifest.json 83 | 84 | ## Donation 85 | 86 | If you enjoy the mod and would like to show your appreciation, a donation would great :). 87 | 88 | [![paypal](https://www.paypalobjects.com/en_US/i/btn/btn_donateCC_LG.gif)](https://www.paypal.com/cgi-bin/webscr?cmd=_donations&business=WLG9J2FFWNH7Y¤cy_code=USD) 89 | --------------------------------------------------------------------------------