Pratt & Whitney Engine Services, Inc. Norwood, …

1 Pratt & Whitney Engine services , Vanderbilt AveNorwood, MA 02062249 Vanderbilt Avenue, norwood , MA 02062, Phone 781-762-8600, Fax 781-762-2287 ADAS+InstructionsforContinuedAirworthine ssADAS-G-260-1/AForCessnaCaravanModel208 SeriesManual Number:ADAS-G-260-1/APreparation Date:December 2, 2002 Prepared By:D ElsemillerRelease Date:December 16, 2002S Sackos, Manager of Manufacturing ServicesRevision Date:November 15, 2011J Miller, Manager of EngineeringRevision Ltr:ITotal Pages:37 Approvals:P&WENGINE services , +ADAS-G-260-1/ACessna Aircraft CompanyModel 208 Series-i-ADAS-G-260-1/APratt & Whitney EngineServices, all instrumentation, the Pratt & Whitney Engine services , Inc. ADAS+systemrequires knowledgeable interpretation bythe recommendations and operating procedures contained in this manual shall not supersede the Aircraft orEngine manufacturer recommendations, operating procedures, or limits.

2 The Pratt & Whitney Engine services , Inc. ADAS+systemshould not be used as a primaryguide monitoring the Aircraft and Engine manufacturersoperating limits. Pratt & Whitney Engine services , Inc. is not liable for any damages resulting fromthe use of this Information NoticeThis manual contains proprietary information that is protected by copyright, and all rights are reserved. No portion of thisdocument may be copied, photocopied, reproduced by any means, or translated into another language without the priorwritten permission ofP&W Engine services , +ADAS-G-260-1/ACessna Aircraft CompanyModel 208 Series-ii-ADAS-G-260-1/APratt & Whitney Engine services , Statusof SheetsSheetiiiiiiivv1234567891011 RevHHGGHHHHHHGGGGGGS heet12131415161718192021222324252627 RevHHHHHHIIIIS heet28293031323334353637 LOGOFREVISIONSREV. NOECO#DESCRIPTIONDATEPAGES REVISEDAI nitial Release12/16/0 2B735 Change Processor Assembly Kit contents byadding Ground Strap DPU-C-050-305/27/04I and1C812 Reformat manual andaddSplit LampOption.

3 Correct Typos05/24/05 AllD839 Revise ConnectionChart to showthe correctpin-outfortheJ2 ,I iv, and 27E860 Correct dimensions for OAT Probeconnections07/06/064, 29-32F957 Update Split Lamp. ChangeUTC logo toP& address. VaneSwitch Kit to Parts List. AddContinued Airworthiness Instructions for IceVane , ii-iv, 7-33H994 Revise Parts List. Update OAT, Torque, Circuit Breaker, andDownload Port Instructions. CorrectTypographical , ii iv, 4, 5, 8, 10,12-14, 17-22, 29-33I1103 Addoptional Garmin G620 Interface CableP/N ADAS-C-072-1 to Parts List. AddSchematics to support theinterface cable11/15/11 Cover, ii, iv, v, 19, 22,34- 37 NOTE:Revisions to this document shall be coordinated through the Boston Aircraft Certification Office,the Kansas City AEG, and the STC holder. If the ADAS+ Instructions for ContinuedAirworthiness are revised, all operators will be provided with a copy of the applicablerevision.

4 Ifyou have a subscription with TurbineTracker , you will be informed viaemail of new revisionsto this to this, P&WEngine services maintains the latest versions of allmanuals inthe Support Section of TurbineTracker .If you are not a subscriber to TurbineTracker , you may callP&W Engine ServicesCustomerSupport at 781-762-8600 for the latest services , +ADAS-G-260-1/ACessna Aircraft CompanyModel 208 Series-iii-ADAS-G-260-1/APratt & Whitney Engine services , OFCONTENTS1 INTRODUCTION ..23 CONTROL AND OPERATION ..25 MAINTENANCE INSTRUCTIONS .. TREND Lamp orOptionalSplit Lamp / Static Transducers .. Temperature SeparatorSwitch .. ,J2,andJ3 Harnesses .. Test .. TREND Lamp orOptionalSplit Lamp / Static Transducers .. Temperature SeparatorSwitch .. AND REPLACEMENT INFORMATION .. SWITCHORENGINE/TREND 178 SPECIAL INSPECTION REQUIREMENTS.

5 199 APPLICATION OF PROTECTIVE services , +ADAS-G-260-1/ACessna Aircraft CompanyModel 208 Series-iv-ADAS-G-260-1/APratt & Whitney Engine services , .. +byParts Kits .. byKit ..1911 LIST OF SPECIAL COMMUTER CATEGORY AIRCRAFT ..2313 RECOMMENDED OVERHAUL PERIODS ..2314 AIRWORTHINESS LIMITATIONS ..2315 DIAGRAMS .. SENSORCABLEJ1, 15 PINS , 15 PINSA SENSORCABLE, J3, 37 PINS + CONNECTIONCHART + INTERCONNECTSCHEMATIC + INTERCONNECTSCHEMATIC + INTERCONNECTSCHEMATIC(SPLITLAMPOPTION) + INTERCONNECTSCHEMATIC(SPLITLAMPOPTION) + SCHEMATIC(GARMING620 OPTION) + SCHEMATIC(GARMING620 OPTION) + SCHEMATIC(GARMING620/ SPLITLAMPOPTION) + SCHEMATIC(GARMING620/ SPLITLAMPOPTION) 1: ADAS+ 2: STANDARDTRENDSWITCH 3: TYPICALMOUNTINGLOCATION 4: 5: 6: 7: PITOT/ 8: 9: 10 11 12:STANDARDTRENDSWITCH 13:TYPICALMOUNTINGLOCATION 14:PITOT/STATICINSTALLATION(SIDEVIEW).

6 11 FIGUREA- 15 16 17 18:PARTICLESEPARATORSWITCH(EXPLODEDVIEW) ..18 FIGUREA- 19:WIRINGSCHEMATIC 20:WIRINGSCHEMATIC 21:WIRINGSCHEMATIC(SPLITLAMPOPTION) services , +ADAS-G-260-1/ACessna Aircraft CompanyModel 208 Series-v-ADAS-G-260-1/APratt & Whitney Engine services , 22: WIRINGSCHEMATIC(SPLITLAMPOPTION) 33 FIGUREA- 23: WIRINGSCHEMATIC(GARMING620 OPTION) 34 FIGUREA- 24: WIRINGSCHEMATIC(GARMING620 OPTION) 35 FIGUREA- 25: WIRINGSCHEMATIC(GARMING620 / SPLITLAMPOPTION) 36 FIGUREA- 26: WIRINGSCHEMATIC(GARMING620 / SPLITLAMPOPTION) 37 LISTOFTABLESTABLEA- 1: ADAS+ services , +ADAS-G-260-1/ACessna Aircraft CompanyModel 208 Series1 ADAS-G-260-1/APratt & Whitney Engine services , ofthis documentis to provideusers of this product with P&WEngineServices approvedInstructionforContinued Airworthiness for theADAS +. Anydeviation fromtheprocedures described withinthis documentcould result in a failure oftheproduct to performproperly andcould possibly result in damage toother systems documentapplies to aircraft that are altered bythe installationofa P&WEngineServices ADAS+, and AbbreviationsADAS+ Aircraft Data AcquisitionSystemPlusAML Approved model ListICA Instructions for Continued AirworthinessMLP MonitorLinkProgramSTC Supplemental of MeasureThis PublicationsADAS-G-260-1 generic InstructionsforContinued Instructions for Continued Airworthinessareto be furnished with ADAS+ Engine trend monitors fo rCessna Aircraft model 208 Series aircraftand is to become part of the permanent aircraft record services , +ADAS-G-260-1/ACessna Aircraft CompanyModel 208 Series2 ADAS-G-260-1/APratt & Whitney Engine services .

7 Detailed descriptionofthe systemcan befoundinADAS-G-260-1, ADAS+Instructions for ContinuedAirworthiness, OPERATIONINFORMATIONA detailed descriptionofthe control andoperationofthesystemcan befound inADAS-G-260-1,ADAS+InstructionsforConti nued Airworthiness, INFORMATIONThis section is not applicableP&WENGINE services , +ADAS-G-260-1/ACessna Aircraft CompanyModel 208 Series3 ADAS-G-260-1/APratt & Whitney Engine services , INSTRUCTIONSS cheduled Maintenance Programtasks are to beadded to theaircraft operator s appropriate maintenanceprogramas Periodic Scheduled Servicing TasksTheP&WEngineServices ADAS+ has been designed with thelatest solid-state technology. The onlycomponentthat has a limited life span is theinternal battery. This battery, under normal operatingconditions, isexpected to last 10years. If the battery is discharged, theprocessormust be returned to P&WEngineServicesforbattery Periodic Scheduled Preventive Maintenance Periodic Scheduled InspectionsThefollowinginformationshould beused to insure thecontinuous andtrouble free operationof theADAS +.

8 These inspectionstepsshould befollowed duringevery instructionsdescribegeneral inspection methods. All inspections should lookforgeneral deterioration ofhoses, brackets, andanyother componentoftheADAS+ system. Other than the specific periodic inspections,maintenance is on-condition,andthere is noother scheduled + processoris located at approximately FS 70in theenginecompartmentonthelower enginemountingtube. For the SystemProcessorinstallation(Figure A- 1), performthefollowinginspections: 010 Inspect processor for security to the mounting bracket. 020 Inspect electrical ground strap for proper connection. 030 Inspect electrical connectors for proper connection toADAS+ A- 1: ADAS+MountingP&WENGINE services , +ADAS-G-260-1/ACessna Aircraft CompanyModel 208 Series4 ADAS-G-260-1/APratt & Whitney Engine services , Lampor Optional Split Lampand Download PortThe ADAS+ has a standard TREND switch / fault lamp or an optional Engine /Trend Split Lamp that is installedin the cockpit (Figure A- 5) and consist of a 75" x.

9 75" square Push-to-test lamp for standard TREND switch /fault lamp or .68" x .68" for the optional Engine /Trend Split Lamp. The ADAS+ also has a download portinstalled in the cockpit (Figure A- 6) and consist of a 19/32" serial download TREND switch / fault lamp orthe optional Engine /TREND Split Lamp anddownload portinstallations(Figure A- 2 andFigure A- 3), performthe followinginspections: 010 Verify that the proper connectors are in place. Refer toFigure A- 4,Figure A- 5, andFigure A- 6. 020 Inspect electrical connectors for loose connections. 030 Inspect wiring for proper routing and security. 040 Inspect wiringfor signs of interference and wire A- 2: Standard Trend Switch orOptionalENGINE/TRENDS plit LampFigure A- 3: Typical Mounting Location forDownload PortP&WENGINE services , +ADAS-G-260-1/ACessna Aircraft CompanyModel 208 Series5 ADAS-G-260-1/APratt & Whitney Engine services , A- 4: StandardTREND Switch/Fault Lamp ConnectorWiringFigure A- 5: OptionalENGINE/TRENDS plit Lamp Connector WiringFigure A- 6: Download Port Connector / Static TransducersADAS + has the capability of measuring airspeed and altitude for event monitoring or trend monitoring.

10 Bothpitot and static transducers are plumbed (Figure A- 7) into the aircraft s existing pitot and static are mounted in tandem under the instrument panel on the co-pilots side. They are accessed from thecockpit by removing the control column cover assembly and glove compartment services , +ADAS-G-260-1/ACessna Aircraft CompanyModel 208 Series6 ADAS-G-260-1/APratt & Whitney Engine services , A- 7: Pitot / Static Transducer InstallationTo insure theintegrity ofthe system, performthefollowinginspection: 010 Verify that the proper connectors are in place. Refer toFigure A- 8. 020 Inspect electrical connectors for loose connections. 030 Inspect wiring for proper routing and security. 040 Inspect wiringfor signs of interference and wire A- 8: Pitot/Static WiringP&WENGINE services , +ADAS-G-260-1/ACessna Aircraft CompanyModel 208 Series7 ADAS-G-260-1/APratt & Whitney Engine services , Air TemperatureProbeThetemperature probeis mounted ontheunderside oftheaircraft s enginecowling to providetheprocessorwith OAT OAT probe installation(Figure A- 9) performthefollowinginspection: 010 Inspect wiring for proper routing and security.