P&W ENGINE SERVICES, INC. - TurbineTracker

1 P&W ENGINE SERVICES, Transmission UnitDTU-G-260-7 Dassault Aviation Model Falcon 2000 EXRevision EThis Document is Subject to the Restrictions Contained on Cover PageThe export control classification with respect to this document is contained on the first pageDTU-G-260-7, December 4, 2012i of ivREVISION HISTORYRev Status ofSheetsRevEEEEBBBBBBBBES heetiiiiiiiv123456789 RevBEBBBBBBBBBBBS heet10111213141516171819202122 RevBDDDDS heet2324252627 LOG OF REVISIONSREV. NOECO #DESCRIPTIONDATEPAGES REVISEDAN/AInitial Release09/06/2007N/AB954 Updated company name, address and wire numbers to connection chartand schematic. Updated spelling and DTU bus power Parts List. Updated wiringschematic. Correct typographical , ii, 24 26D1020 Update Comm Port wiring in , ii, 26E1142 Change DTU Inspection Interval fromPhase 4A to B 12/04/2012 Cover, i, ii, iii, iv, 9,11, 24, 25, 26, 27 Note: Revisions to this document shall be coordinated through the Boston Aircraft Certification Office,the Aircraft Evaluation Group, and the STC holder.

2 If the DTU Instructions for ContinuedAirworthiness are revised, all operators will be provided with a copy of the applicable revision. Ifyou have a subscription with TurbineTracker , you will be informed via email of new revisionsto this manual. In addition to this, P&W ENGINE Services maintains the latest versions of allmanuals in the Support Section of TurbineTracker .If you are not a subscriber to TurbineTracker , you may call P&W ENGINE Services CustomerSupport at 781-762-8600 for the latest ENGINE SERVICES, Transmission UnitDTU-G-260-7 Dassault Aviation Model Falcon 2000 EXRevision EThis Document is Subject to the Restrictions Contained on Cover PageThe export control classification with respect to this document is contained on the first pageDTU-G-260-7, December 4, 2012ii of ivTABLE OF CONTENTS1 INTRODUCTION .. 22 DESCRIPTION .. / GPRS Antenna .. 73 CONTROL AND OPERATION 84 SERVICING 85 MAINTENANCE .. RF Switch.

3 Port .. Shorting Plug .. Antenna .. Test .. Switch .. Shorting Plug .. 126 SYSTEM Test .. Switch Port Test .. 16P&W ENGINE SERVICES, Transmission UnitDTU-G-260-7 Dassault Aviation Model Falcon 2000 EXRevision EThis Document is Subject to the Restrictions Contained on Cover PageThe export control classification with respect to this document is contained on the first pageDTU-G-260-7, December 4, 2012iii of iv7 REMOVAL AND REPLACEMENT Removal .. Configuration .. Test .. (s) Off: .. (s) Running: .. Switch Switch Replacement .. Antenna Removal .. Antenna Shorting Plug Shorting Plug Replacement .. 228 SPECIAL INSPECTION REQUIREMENTS .. 239 APPLICATION OF PROTECTIVE TREATMENTS .. 2310 DATA .. by Parts Kits .. by 2311 LIST OF SPECIAL TOOLS .. 2412 FOR COMMUTER CATEGORY AIRCRAFT .. 2413 RECOMMENDED OVERHAUL PERIODS .. 2414 AIRWORTHINESS .. Cable J1, 37 Pin A Keyed Connector .. 27P&W ENGINE SERVICES, Transmission UnitDTU-G-260-7 Dassault Aviation Model Falcon 2000 EXRevision EThis Document is Subject to the Restrictions Contained on Cover PageThe export control classification with respect to this document is contained on the first pageDTU-G-260-7, December 4, 2012iv of ivFIGURESFIGURE1 3 FIGURE2 4 FIGURE3:BAGGAGECOMPARTMENT(VIEW LOOKING FORWARD).

4 5 FIGURE5:DTURFSWITCH 6 FIGURE7: 7 FIGURE8 7 FIGURE9 9 FIGURE10 9 FIGURE11 10 FIGURE12 11 FIGURE13 12 FIGURE14 12 FIGURE15 14 FIGURE16 15 FIGURE17 16 FIGURE18:COMMUNICATIONPORTSOCKET 16 FIGURE20 27 LIST OF TABLESTABLE1:SUMMARY 4 TABLE2 19 TABLE3 20P&W ENGINE SERVICES, Transmission UnitDTU-G-260-7 Dassault Aviation Model Falcon 2000 EXRevision EThis Document is Subject to the Restrictions Contained on Cover PageThe export control classification with respect to this document is contained on the first pageDTU-G-260-7, December 4, 20121 of 271 ScopeThe purpose of this document is to provide users of this product with the P&W ENGINE Services approvedinstructions for continued airworthiness. Any deviation from the procedures described within this documentcould result in a failure of the product to perform properly and could possibly result in damage to other systemsof the instructions are for aircraft associated with the FAA Type Certificate Data Sheet No.

5 ApplicabilityThis document applies to aircraft that have been altered by P&W ENGINE Services Data Transmission Unit(DTU), Definitions and AbbreviationsConfiguration File:An MLP data file that contains cellular carrier information, aircraft subsystem (ACS)information for a specific aircraft. This information is transmitted to the processor during Version:A number stored with a particular configuration file. The MLP and TurbineTracker both maintain version numbers of the current configuration file in use. These must match each other andcorrespond with the data collected and stored by the system processor. If the configuration file is changed, theversion number is automatically (Monitor Link Program):The P&W ENGINE Services communication program is used to transfer data toand from the Approved Model ListDTU Data Transmission UnitEDU ENGINE Diagnostic UnitGPRS General Packet Radio ServiceGSM Global System for Mobile CommunicationsICA Instructions for Continued AirworthinessLAN Local Area NetworkRF Radio FrequencySTC Supplemental Type PrecautionsSection and CAUTION:Excessive torque on the processor-mounting studs can deform the shock mounts.

6 The locking nutshould be tightened to the point of contact with the shock making any wiring connections, verify all connection locations with the aircraftmanufacturer s wiring diagram a continuity check on all wires before final all harnesses along existing harnesses wherever may be marked with shrink-on labels near the terminal end. When you shorten a cablebehind a label, be sure to re-label wire in accordance with Dassault Model Falcon 2000EX Wiring Diagram Manual(Wiring Maintenance Practices)P&W ENGINE SERVICES, Transmission UnitDTU-G-260-7 Dassault Aviation Model Falcon 2000 EXRevision EThis Document is Subject to the Restrictions Contained on Cover PageThe export control classification with respect to this document is contained on the first pageDTU-G-260-7, December 4, 20122 of Units of MeasureThis section not Referenced PublicationsGSS-T-301-1 Monitor Link Program (MLP)DTU-G-010-7 DTU Installation Manual for the Dassault Falcon 2000 EXPub. 680/689 Falcon 2000EX Maintenance Manual, Maintenance Connector ENGINE 1, 2 Section DistributionThese Instructions for Continued Airworthiness are to be furnished with new production Data TransmissionUnits (DTU) for Dassault Falcon 2000EX aircraft and are to become part of the permanent aircraft record Weight and BalanceCalculating weight and balance of the DTU after installation is the responsibility of the installer.

7 Theinformation needed is shown below:DTU KitWeight 21 (11161)NOTE: Arm location is for typical installations only and should be verified at time of install. Refer toaircraft equipment list for actual measurements for weight and balance ENGINE SERVICES, Transmission UnitDTU-G-260-7 Dassault Aviation Model Falcon 2000 EXRevision EThis Document is Subject to the Restrictions Contained on Cover PageThe export control classification with respect to this document is contained on the first pageDTU-G-260-7, December 4, 20123 of 272 DTU General DescriptionThe DTU will connect to the existing left and right maintenance connectors (located in the baggagecompartment) of the PW308C engines to provide the communications system through which aircraft and engineperformance data can stream to the Internet without operator intervention. The source of this data will be fromthe PW308C ENGINE Diagnostic Unit (EDU). The destination will be the P&W ENGINE ServicesTurbineTracker DTU passively monitors real-time ENGINE data from the EDU while the aircraft is airborne by reading theEDU Status Message.

8 Once the EDU Status Message is received, the DTU actively commands the EDU to goto the Maintenance Page of the EDU. The Maintenance Page will display the ENGINE criteria to the DTU and theDTU will determine whether or not both engines are off. When the DTU ascertains that aircraft has landed andpowered down the DTU downloads the following ENGINE data from the EDU and stores this data in non-volatilememory. EDU Log Files Fault Codes Exceedances Events TrendsThe DTU utilizes GSM Cellular Network off the shelf quad-band modem for transmission over 850 MHz,900 MHz, 1800 MHz and 1900 MHz for the automatic data transfer. The cellular telephone circuitry of the DTUis disabled during the time that the aircraft is airborne. The system will initiate a data transfer based on theengine parameters detailed in Section DTU supports multiple communication modes to achieve data transfer. These will include hardwire,Cellular and Wireless LAN. The capabilities of the certified system are illustrated in Figure TrackerTMInternetCelluarWirelessLANC ustomerCustomerCustomerISPA irport HubCellTowerHand HeldControllerFigure 1.

9 DTU Simplified Block DiagramP&W ENGINE SERVICES, Transmission UnitDTU-G-260-7 Dassault Aviation Model Falcon 2000 EXRevision EThis Document is Subject to the Restrictions Contained on Cover PageThe export control classification with respect to this document is contained on the first pageDTU-G-260-7, December 4, 20124 of 27 The capabilities of the DTU are detailed below in Table serial interface withP&W ENGINE Servicesengine monitors and OEM enginemonitorsMulti-mode GSM Cellular and Wireless LAN RF communications for data retrieval andsystem configuration downloadBi-directional serial interface for hardwire data retrieval and system configuration downloadIndividual discrete digital outputs for system diagnosis and for control ofP&W ENGINE Servicesengine monitorHardware and software for power control for the RF sections of the DTUS oftware for Internet protocol addressing and packet data transmissionBuilt-in test of interface and communication functionsTable 1: Summary of DTU System ProcessorThe processor (Figure 2) facilitates wireless connectivity between the PW308C EDU and P&W ENGINE ServicesTurbineTracker Server.

10 This connectivity is bi-directional with the ability of the DTU to request ENGINE statusfrom the EDU in near real time, and then retrieve data from the EDU when both engines have shut down. TheDTU processor then sends the ENGINE data to the TurbineTracker website via the cellular network. The DTUsystem interfaces with only the aircraft power and the PW308C EDU and does not connect to any other aircraftsystems. The processor does not require access during processor measures high by long by deep and weighs lbs. An aluminum bracket withLord Aerospace shock mounts is used to mount the processor to the 2: ProcessorThe system processor is mounted in the baggage compartment behind the lavatory panel (F2MB800838A2)where the maintenance connectors are located (Frame 21, Station 11161), as shown in Figure 3. The processorwill be mounted onto the ADHY-D-026-1 bracket, shown in Figure 4. Although the processor will not requireaccess during normal operation, care should be taken to install the processor in an area that complies with theenvironmental requirements of the : For mounting instructions, refer to the DTU Installation Manual (DTU-G-010-7) for the DassaultAviation Falcon 2000EX ENGINE SERVICES, Transmission UnitDTU-G-260-7 Dassault Aviation Model Falcon 2000 EXRevision EThis Document is Subject to the Restrictions Contained on Cover PageThe export control classification with respect to this document is contained on the first pageDTU-G-260-7, December 4, 20125 of 27 Figure 3: Baggage Compartment (view looking forward)Figure4: DTU Mounting Control ComponentsFollowing are the descriptions and functions of the control components.