SmartCycle+ Addendum B Installation Instructions …

1 Pratt & Whitney Engine Services, Vanderbilt , MA 02062-i-EMU-G-010-1/BPratt & Whitney Engine Services, + Addendum B Installation InstructionsEMU-G-010-1/BBell Helicopter Textron Model Series 212,412,412EP,and412 CFAgusta BellModel SeriesAB412and AB412 EPManual Number:EMU-G-010-1/BPreparation Date:November 1, 2002 Prepared By:David DesaulnierRelease Date:April25, 2003 DFetherston, Manager of EngineeringRevision Date:July 24, 2008S Sackos, Manager of Manufacturing & QualityRevision Ltr:GTotal Pages:41 Approvals:P&W ENGINE SERVICES, +EMU-G-010-1/BBell Helicopter Textron / Agusta BellModel Series 212, 412, 412EP, 412CF, AB412, and AB412EP-ii-EMU-G-010-1/BPratt & Whitney Engine Services, HISTORYRevGGGGGGGGGGGGGGGGRev Statusof SheetsSheetiiiiii12345678910111213 RevGGGGGGGGGGGGGGGGS heet14151617181920212223242526272829 RevGGGGGGGGGGGGS heet303132333435363738394041 RevSheetLOG OF REVISIONSREV.

2 NOECO #DESCRIPTIONPAGES REVISEDAI nitial ReleaseB726 Reformat all pictures, Change Tq T Fitting P/N, Replacefigure B-13 with better picture, and correct Tq harnessdescriptionAllC755 Add Mast Torque and Revision Section. ReviseWiringSchematicand Connection Chart(Synchro Option).i, 2, 13, 19, 21, 26, 28,29, 30, 31D830 Add inserts to the misc. Pitot/Static Meter,N2, and Nrconnection any reference toSynchro iv and 2 30E861865 Revised Connection ChartRevised Part Numbers in Parts KitsRevised Torque Transducer InstallationCorrected Section to remove un-needed drawingsi-iii, 2-3,9-30F960 Corrected spelling and grammar. Updated company name,address and schematics and connectioncharts. Updated formatting. Added wire numbers toconnection chart and Skid Switch option. Changed parts list, installationprocedures, electrical connections, schematics andconnection chart.

3 Added Appendix A consisting of theEMU-A-078-1 :If the smartcycle + Installation Manuals are revised, all operators will be provided with a copy ofthe applicable revision. If you have a subscription with TurbineTracker , you willbe informedvia email of new revisions to this manual. In addition to this,Pratt & Whitney Engine Services, the latest versions of all manuals in the 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 ENGINE SERVICES, +EMU-G-010-1/BBell Helicopter Textron / Agusta BellModel Series 212, 412, 412EP, 412CF, AB412, and AB412EP-iii-EMU-G-010-1/BPratt & Whitney Engine Services, OF CONTENTS1 BELL / AGUSTA BELL HELICOPTER MODEL SERIES 212 / 412 AND MAINTENANCE + by Parts by Processor TREND Switch / Fault Lamp and Download / Static Pressure Transducer Mounting (306-4 Hose).

4 / Static Pressure Transducer Mounting (44-NSR Tubing).. Air Temperature (OAT) (WEIGHT-ON-WHEELS) Installation (OPTIONAL) .. Transducer Harness Harness Harness TREND Switch / Fault Lamp Port Connector / Static Pressure Transducer Air Temperature (OAT) (WEIGHT-ON-WHEELS)WIRING(OPTIONAL).. Temp(ITT) Signal N1 (Ng) Signal N2 (Nf) Signal Tq Wiring Option 1 P&E Engine Services Supplied Tq Tq Wiring Option 2-Aircraft Equipped with OEM DC Voltage Tq Transmitters and Mast Nr (Rotor) Speed Signal Collective Power Power Power Breaker Switch / Fault Lamp Breaker ENGINE SERVICES, +EMU-G-010-1/BBell Helicopter Textron / Agusta BellModel Series 212, 412, 412EP, 412CF, AB412, and AB412EP-iv-EMU-G-010-1/BPratt & Whitney Engine Services, CONNECTOR SIGNAL , , ,J3, OPTION1 P& OPTION2 AIRCRAFTEQUIPPED OPTION3 P&WENGINESERVICESSUPPLIEDTORQUETRANSDUCE RS OPTION4 AIRCRAFTEQUIPPED WITHOEMDCVOLTAGETORQUETRANSMITTERS ANDP& + (OPTIONAL).

5 36 LIST OF FIGURESFIGUREB-1: smartcycle + : smartcycle + :COCKPITFAULTLAMP : :PITOT/STATICPRESSURETRANSDUCERMOUNTING( 306-4 HOSE)..9 FIGUREB-7:PITOT/STATICPRESSURETRANSDUCER MOUNTING(44-NSRTUBING)..10 FIGUREB-8:OUTSIDEAIRTEMPERATURE(OAT) : : :OUTSIDEAIRTEMPERATURE(OAT) :SKIDSWITCH(WOW) : :FAULTLAMP :WIRINGSCHEMATIC OPTION1 P& :WIRINGSCHEMATIC OPTION2 AIRCRAFTEQUIPPED :WIRINGSCHEMATIC OPTION3 P&WENGINESERVICESSUPPLIEDTORQUETRANSDUCE RS :WIRINGSCHEMATIC OPTION4 AIRCRAFTEQUIPPED WITHOEMDCVOLTAGETORQUETRANSMITTERSANDP& OF TABLESTABLEB-1: smartcycle + ENGINE SERVICES, +EMU-G-010-1/BBell Helicopter Textron / Agusta BellModel Series 212, 412, 412EP, 412CF, AB412, and AB412EP-v-EMU-G-010-1/BPratt & Whitney Engine Services, AFIGUREA-1:WEIGHT-ON-WHEELSINSTALLATION INSTALLATIONINSTRUCTIONS :WEIGHT-ON-WHEELSINSTALLATION MOUNTINGLOCATION :WEIGHT-ON-WHEELSINSTALLATION ASSEMBLYINSTRUCTIONS :WEIGHT-ON-WHEELSINSTALLATION ASSEMBLYINSTRUCTIONS :WEIGHT-ON-WHEELSINSTALLATION ASSEMBLYINSTRUCTIONS.

6 WEIGHT-ON-WHEELSINSTALLATION PARTSLIST ENGINE SERVICES, +EMU-G-010-1/BBell Helicopter Textron / Agusta BellModel Series 212, 412, 412EP, 412CF, AB412, and AB412EP-1-EMU-G-010-1/BPratt & Whitney Engine Services, Agusta BellHelicopter Model Series212 / 412 purpose of this document is to provide users of this product withP&W Engine Servicesapprovedinstallation Instructions for theSmartCycle+system. Any deviation from theprocedures described within thisdocument could result in a failure of the product to perform properly and could possibly result in damage toother systems of the Instructions are for aircraft associated with the FAAType Certificate Data Sheet ENGINE SERVICES, +EMU-G-010-1/BBell Helicopter Textron / Agusta BellModel Series 212, 412, 412EP, 412CF, AB412, and AB412EP-2-EMU-G-010-1/BPratt & Whitney Engine Services, AND MAINTENANCE ListFor BellHelicopter Textron Model Series212 & 412:The parts listed below consist of the Installation kits for theSmartCycle+system for the Bell Helicopter Textronhelicopters 212 & kit numbers are listed in individual components are detailedby kit numbers in +by Parts KitsBell Helicopter Model Series212 & 412.

7 QtyEMU-K-010-6 WeightProcessor Harness Torque Kit (Optional) OAT Pitot / Static Pressure Pitot / Static Fault Lamp Assembly Switch Kit (Optional,Purchased Separately) Installation Materials by KitFor Bell HelicopterTextron Model Series 212 & 412:PROCESSORASSEMBLYKITEMU-K-018-2 ProcessorEMU-A-010-1 Qty 1 Mounting BracketDPU-D-030-1 Qty 1 Shock Mounts, Lord990-00020 Qty 4 Washer, Processor Mount920-00006 Qty 4 Nut, Locking, Processor MountMS21042-06 Qty 4 Screw, MountMS35207-267 Qty 4 Nut, Locking, MountMS21044N10 Qty 4 AlternativeP/NAN365-1032 AWasher, MountAN970-3 Qty 4 Strap, GroundDPU-C-050-1 Qty 1 ENGINEHARNESSKITEMU-K-019-6 Cable Assembly, J1 EMU-C-025-1 Qty 1 Cable Assembly, J2 EMU-C-033-1 Qty 1 Cable Assembly, J3 (Comm)EMU-C-060-1 Qty 1P&W ENGINE SERVICES, +EMU-G-010-1/BBell Helicopter Textron / Agusta BellModel Series 212, 412, 412EP, 412CF, AB412, and AB412EP-3-EMU-G-010-1/BPratt & Whitney Engine Services, (OPTIONAL)

8 EMU-K-024-7 Transducer, 0 150 PSIG750-00003 Qty 2 Double Swivel Nut Union960-00050 Qty 2 Swivel Nut Union960-00051 Qty 2 Tee, Flared TubeAN824-4 JQty 2 ClampMS21919 WCJ16 Qty 2 BoltAN3-15 AQty 2 NutAN365-1032 AQty 2 WasherAN960-10 Qty6 Spacer 3/8 OD x 1/2 L940-00004 Qty 2 AIRCRAFTOATPROBEKITDPU-K-032-1 Probe, TemperatureTWIN-A-050-2 Qty 1 Nut, JamTWIN-D-061-1 Qty 1 WasherAN960-816 LQty 2 Seal, O RingAN6227B-10 Qty 1 Bolt, DrilledAN3H-4 AQty 1 Doubler, OAT ProbeDPU-D-047-1 Qty 1 WasherAN960-10 Qty 1 Nut, Fiber LockAN365-1032 AQty 1 AIRCRAFTPITOT/STATICKITTWIN-K-033-3 Hose, Inlet Pressure990-00028 Qty 4 , Inlet Pressure Hose960-00027 Qty 4 Adapter, Pipe to 37 flare960-00002 Qty 1 Tee, PipeAN917-2 DQty 1 Nipple, FlareAN816-4-4 DQty 1 BushingAN912-1 DQty 1 Fitting, Male Nylo-Seal960-00024 Qty 1 Tubing, Tygon990-00030 Qty 1 1 Transducer, 0 3 PSID750-00001 Qty 1 Transducer, 0 15 PSIA750-00002 Qty 1 Clamp, Inlet Pressure HoseMS21919 WDG17 Qty 1 Clamp, Inlet Pressure TransducerMS21919 WDG26 Qty 1 Bolt, 10-32MS35207-263 Qty 2 Nut, Locking, 10-32AN365-1032 AQty 2 Washer, #10AN960-10 Qty 2 Fitting, T Swivel960-00003 Qty 2P&W ENGINE SERVICES, +EMU-G-010-1/BBell Helicopter Textron / Agusta BellModel Series 212, 412, 412EP, 412CF, AB412, and AB412EP-4-EMU-G-010-1/BPratt & Whitney Engine Services, , Tube, Nylo-Seal960-00033 Qty 3 Tubing, OD990-00023 Qty 6 Tube, Tygon, Clear, 1/8 990-00030 Qty , Tube to male960-00025 Qty 2 Insert, Nylon Tube OD 920-00024 Qty 4 COCKPITFAULTLAMPASSEMBLYDPU-K-046-3 Assy.

9 , Cockpit Fault LampDPU-A-043-1 orQty 1 Alternative P/NDPU-A-043-2 LensTREND-D-041-1 Qty 1 Connector, 6 Pin Female400-00026 Qty 1 Alternative P/N8282-6SG-3 XXAssy., Download PortDPU-A-044-1 Qty 1 Alternative P/NDPU-A-044-2 Cover990-00031 Qty 1 Alternative , 6 Pin, Male400-00027 Qty 1 Alternative P/N6282-6PG-3 XXScrew, Pan Head, 4-40900-00009 Qty 1 WasherAN960-4 Qty 1 Nut, Fiber Lock910-00001 Qty 1 SKIDSWITCHKIT(OPTIONAL PURCHASEDSEPARATELY)EMU-K-077-1 Bracket, Bell 412 Skid Switch, L/SEMU-D-074-1 Qty 1 Bracket, Bell 412 Skid Switch, R/SEMU-D-075-1 Qty 1 Bracket, Bell 412 Skid Tube Switch, BottomEMU-D-076-1 Qty 1 Switch Enclosed700-00013 Qty 1 Bolt, 10-32 X 17/32AN3-4 AQty 8 Nut, Elastic Stop, 10-32AN365-1032 AQty 4 Washer, Flat 3/16 AN960-10 Qty 12 ADDITIONALMATERIALINSTALLATIONKITEMU-K-0 23-3 Crimp Lug, Alumel400-00031 Qty 2 Crimp Lug, Chromel400-00032 Qty 2 Breaker, 1 Amp990-00032 Qty 1 Fuse, Amp990-00033 Qty 1 Holder, FuseDPU-C-057-1 Qty 1P&W ENGINE SERVICES, +EMU-G-010-1/BBell Helicopter Textron / Agusta BellModel Series 212, 412, 412EP, 412CF, AB412, and AB412EP-5-EMU-G-010-1/BPratt & Whitney Engine Services, system processor may be mounted(Figure B-1andFigure B-2)in various positions using mountingbracket, DPU-D-030-1.

10 The processor will not require access during normal / 412 FuselageNOTTO SCALEF igure B-1: SmartCycle+ Processor Location View 1212 / 412 FuselageNOT TO SCALEF igure B-2: SmartCycle+ Processor Location View 2P&W ENGINE SERVICES, +EMU-G-010-1/BBell Helicopter Textron / Agusta BellModel Series 212, 412, 412EP, 412CF, AB412, and AB412EP-6-EMU-G-010-1/BPratt & Whitney Engine Services, ProcessorMountingThe system processor shall be mounted in accordance with the following procedure: 010 Assemble the smartcycle + processor to the mounting bracket (FigureB-3) and test fit the assemblyin a suitable location within the aircraft that does not interfere with wiring or CAUTION: Excessive torque on the processor-mounting studs can deform shock mounts. The lockingnut should be tightened to the point of contact with the shock mount. 020 When a location has been determined for the smartcycle +, mark the location of the 4 mounting holes,then drill to accommodate a #10 screw.