CAS-67A TRAFFIC ALERT AND COLLISION AVOIDANCESYSTEM(TCASII) ICASupplement

Transcription

1 AIRCRAFTDIVISION WICHITA,KANSAS67277 CAS-67A TRAFFIC ALERT AND COLLISION AVOIDANCESYSTEM(TCASII) ICASupplement MODELNO:S550 SUPPLEMENTNO: SUPPLEMENTDATE:6/15/2015 CessnaAircraftCompany

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3 AIRCRAFTDIVISION WICHITA,KANSAS67277 REVISIONS ICA-S Rev: - Date: 6/15/2015 ICA Summary Pages 1-6 Manuals Affected Description Title Introduction SUPPLIER PUBLICATION LIST Updates this section to include the Honeywell System Installation Manual for the CAS 67A/67B TCAS II System Pages 1-2 AddsthispageblockfortheTCASIIsystem Page 101 AddsthispageblockfortheTCASIIsystem Pages AddsthispageblockfortheTCASIIsystem Pages AddsthispageblockfortheTCASIIsystem. Appendix A: Parts List Page 1 PARTS LIST Appendix B: Wiring Diagram Manual 1. ExportCompliance NOT USED CAS-67A/67B TRAFFIC ALERT AND COLLISION AVOIDANCESYSTEM(TCASII)-DESCRIPTION AND OPERATION(For Airplanes-0001 thru-0160 Incorporating SBS ) CAS-67A/67B TRAFFIC ALERT AND COLLISION AVOIDANCESYSTEM(TCASII)-TROUBLESHOOTING (For Airplanes thru Incorporating SBS ) CAS-67A/67B TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM(TCAS II)- MAINTENANCE PRACTICES (For Airplanes thru Incorporating SBS ) CAS-67A/67B TRAFFIC ALERT AND COLLISION AVOIDANCESYSTEM(TCASII)-ADJUSTMENT/TEST (For Airplanes thru Incorporating SBS ) Information on the wiring for this system is located in the Avionics Wiring Diagramsforthespecific serial number of the airplane. A. ThispublicationcontainstechnicaldataandissubjecttoU.S.exportregulations.Thisinformationhas been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E Revision Bars A. RevisionbarsinthisICAsupplementidentifynewICAsand/orchangestothecurrentICAsinthe released maintenance manual. CessnaAircraftCompany Page1of6 Jun 15/2015

4 AIRCRAFTDIVISION WICHITA,KANSAS67277 NewICAsthatarenotinthecurrentmaintenancemanualwillhavearevisionbarfromtopto bottom along the left margin. ICAs that are in the current maintenance manual and have information added, deleted or revised will have a revision bar(s) in the left margin adjacent to the added, deleted or revised information. Neworchangedillustrationswillhaveachangebarfortheentirelengthofthepage. 3. PageNumbering A. The page number system for ICA included in this supplement have three-element numbers that are separated by dashes. The three-element number is found at the bottom right corner of the page, left ofthepagenumber. Thedateisfoundbelowthepagenumber. B. When the chapter/system element number is followed with zeros in the section/subsystem and subject/unit element number( ), the information is applicable to the entire system. C. When the section/subsystem element number is followed with zeros in the subject/unit element number( ), the information is applicable to the subsystems in the system. D. The subject/unit element number is used to identify information applicable to units in the subsystems. The subject/unit element number continues in sequence from the number-01- with the number of subsystem units in which maintenance information is necessary. E. All system/subsystem/unit (chapter/section/subject) maintenance data is separated into specified types of information: Description and Operation, Troubleshooting, Maintenance Practices, etc. Blocksofpagenumbersthatareinsequenceareusedtoidentifythetypeofinformation: (1) Description and Operation or Troubleshooting information may not be included if the procedure is easy. When subtopics are short, they may be put together into the Maintenance Practices section. Maintenance Practices can have a mix of subtopics that includes information to service, remove, install, adjust, test, clean, paint or do approved repairs. (2) Longerproceduresthatarenotaseasytodomaybeincludedinaspecifiedsection. Page 1 through 99- Description and Operation Page 101 through 199- Troubleshooting Page 201 through 299- Maintenance Practices Page301through399-Servicing Page 401 through 499- Removal/Installation Page 501 through 599- Adjustment/Test Page 601 through 699- Inspection/Check Page 701 through 799- Cleaning/Painting Page801through899-ApprovedRepairs F. A typical page number: CessnaAircraftCompany Page2of6 Jun 15/2015

5 AIRCRAFTDIVISION WICHITA,KANSAS67277 G. Illustrations use the same figure numbers as the page block in which they appear. For example, Figure 202 would be the second figure in a Maintenance Practices section. 4. SupplementRevisions A. Revisions to this supplement may be accomplished if changes to this supplement are required after release of the original issue and prior to incorporation into the manuals listed in the REVISIONS table. B. All revisions to this supplement willhave changes identified in detail in the revision block(s) above. C. AllpagesinthisICAsupplementwillhavethesamedateandarevalidasofthedateshown. 5. ICAIncorporationintoApplicableManuals NOTE: Most ICA supplements will be incorporated in the next available revision to the manuals listed above and should be used in conjunction with those manuals until the next available revision is released. A. The ICA Supplement List located in the Introduction section of each manual listed in the REVISIONS table will indicate the incorporation status as of the release date of the published revision. B. The manual revision level of the supplement incorporation will be listed in the"manual Incorporation Status" column in the ICA Supplement List, when those ICAs associated with that manual have been incorporated. After ICAs are incorporated, the manual that they are incorporated in must now be used for those ICAs instead of the supplement. Based on revision cycle times for the affected manuals, MM ICAs, WDM ICAs, etc. in this supplement may be incorporated in the manuals at different times. There will not be a revision to this supplement to indicate incorporation in the manuals. Users are required to check the ICA Supplement List for each manual affected to determine incorporation status. C. This supplement will be completely superseded by the manuals listed in the REVISIONS table when ithasbeenincorporatedinallofthemanuals. CessnaAircraftCompany Page3of6 Jun 15/2015

6 AIRCRAFTDIVISION WICHITA,KANSAS Purpose INTRODUCTION A. The purpose of this Supplement is to provide the maintenance technician with the information necessary to ensure the correct functionality and performance of the CAS-67A/67B TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM(TCAS II)on the Cessna Model S550 until this information gets incorporated into the next revision to the manuals listed in the "REVISIONS" section of this supplement. B. This ICA supplement is designed to satisfy the requirements of 14 CFR "Instructions for Continued Airworthiness" associated with this installation. This document is a supplement to the Model S550 and will be incorporated in the next revision to the manual. C. When this information is incorporated in the next revision to the manuals listed in the"revisions" section,those manuals shall take precedence over this supplemental document. Refer to the"ica Supplement List" in the"introduction" section of the respective manual for the status of all applicable ICA Supplements. D. RevisionstothissupplementmayoccurifthereisachangetoanyoftheICAsinthissupplement prior to incorporation into all of the affected manuals. 2. Effectivity NOTE: This document must be placed with the aircraft operator's Technical Library CD-ROM or Model S550 and incorporated into the operator's scheduled maintenance program. A. These Instructions for Continued Airworthiness(ICA) are effective for the following aircraft model and serialization. Model BeginningEffectivity EndingEffectivity S CompleteICADocuments A. The following document(s), in conjunction with this supplement, constitute the Instructions for Continued Airworthiness for the CAS-67A/67B TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM(TCASII)ontheCessnaModelS550. Allitemsmustbeavailabletotheoperatoratinitial delivery. (1) Model S Systems A. Refer to Appendix A: Illustrated Parts Catalog CessnaAircraftCompany Page4of6 Jun 15/2015

7 AIRCRAFTDIVISION WICHITA,KANSAS Model S550 LIST OF INSTRUCTIONS FOR CONTINUED AIRWORTHINESS A. Introduction (1) Refer to Publication List B. Chapter 34- Navigation (1) Referto CAS-67A/67B Traffic Alert and Collision Avoidance System (TCAS II) - Description and Operation (2) Refer to CAS-67A/67B Traffic Alert and Collision Avoidance System (TCAS II) - Troubleshooting (3) Refer to CAS-67A/67B Traffic Alert and Collision Avoidance System (TCAS II) - Maintenance Practices (4) Referto CAS-67A/67B Traffic Alert and Collision Avoidance System (TCAS II) - Adjustment/Test CessnaAircraftCompany Page5of6 Jun 15/2015

8 AIRCRAFTDIVISION WICHITA,KANSAS ContinuousInspectionProgram INSPECTION PROGRAM AND AIRWORTHINESS LIMITATIONS A. ThisICASupplementdoesnotaffectthecurrentinspectionprogram. 2. Airworthiness Limitations A. Cessna Aircraft Company Model S550, Chapter 4, Airworthiness Limitations, contains the system and airframe limitations for the Model S550. NOTE: The Airworthiness Limitations section is FAA-approved and specifies maintenance required under Section and of Title 14 Code of Federal Regulations, unless an alternative program has been FAA approved. (1) There are no new(or additional) airworthiness limitations associated with this equipment and/or installation. CessnaAircraftCompany Page6of6 Jun 15/2015

9 1. General SUPPLIER PUBLICATION LIST A. ThissectiongivesyoualistofsomeofthesupplierpublicationsfortheModelS550Airplane. Use the supplier publication list to cross reference the component part number and the applicable supplier publication part number to find the correct supplier publication. It can be necessary to have special tools and equipment to complete some of the maintenance procedures in the supplier publications. Some supplier publications may also have certification requirements for the related components. Refer to Table 1 for the supplier publication list. Table 1. Publication List Air Conditioning System Cabin Pressure ControlSystem Compressor Compressor Condenser Module Assembly DC Generators and Starter Generators Environmental ControlSystem PartNumber SD-5 PublicationTitle Chapter 21 - Air Conditioning Freon Air Conditioning System Maintenance Data Cabin Pressure Control System Operation and Maintenance Instructions CompressorService Manual Publication Part Number TR-119 Parker-Hannifin Corp. JBSystemsDiv Center Rd. POBox158 Avon, OH Honeywell International, Inc N. Oracle Rd. Tucson, AZ SD Operating, R-12 Servicing, and FWA R-134a with Illustrated Parts List ModelR70 DC Generators and Starter Generators Field Support Manual Model R70 Environmental Control Systems Sanden International (USA),Inc Sanden Dr. Dallas, TX Enviro Systems Inc NHighway99 Seminole, OK Lucas Aerospace Power Equipment Corp Darrow Road Twinsburg, OH R4142 United Technologies Corp. Hamilton Standard Division Flight Systems Dept New Britain Avenue Farmington, CT SUPPLIERPUBLICATIONLIST Page1

10 Table 1. Publication List(continued) Evaporator Module Assembly CassetteDeckAuto Reverse CassetteDeckAuto Reverse Communications SystemKHF 950 HF Dukane Underwater LocatingBeacon FlitefoneVSystem FlitefoneVSystem PartNumber PublicationTitle Publication Part Number /-23 Operating, R-12 Servicing, and FWA R-134a 23/24 with Illustrated Parts List Chapter 23 - Communications 5114 Service Manual Auto ReverseCassette Deck 5114 Owners Manual Auto ReverseCassette Deck DK100, DK120 Flitefone VI System KHF 950 HF Communications SystemMaintenance and Overhaul Manual Enviro Systems Inc NHighway99 Seminole,OK P61804F02-0 Alpine Electronics of America Inc Gramercy Place Torrance, CA P60806F04-0 Alpine Electronics of America Inc Gramercy Place Torrance, CA Allied Signal W.105th St. Olathe, KS Technical Manual 03-TM-0037 Dukane Corp Dukane Drive Saint Charles, IL Flitefone V Installation/Operator Manual Flitefone V Addendum to Installation and Flitefone VI Installation Manual, Operators Manual Wulfsberg Electronics Division 6400WilkinsonDrive Prescott, AZ Wulfsberg Electronics Division 6400WilkinsonDrive Prescott, AZ , Wulfsberg Electronics Division 6400WilkinsonDrive Prescott, AZ SUPPLIERPUBLICATIONLIST Page2

11 Table 1. Publication List(continued) PartNumber Microphone Monitor Voice Recorder Battery and ChargerSystem Battery Battery DC Converter DC Generator Control Unit StaticInverter CBS LT55A PC-350 PublicationTitle Calibration and Test Procedure for Microphone Monitor Model AV-557C Cockpit Voice Recorder 052 Chapter 24 - Electrical Power with Illustrated Parts List Marathon Battery Instruction Manual Care and Maintenance of Nickel-Cadium Batteries Saft with Illustrated Parts List Nickel Cadmium Battery Model LT-55(A) DC-DC Converter Regulated,Variable DC Output With Illustrated Parts List Models B Thru H and-006mdcgen Control Unit 350VA Static Inverter Publication Part Number Honeywell International, Inc. Commercial Aviation Systems 15001NE36thSt Redmond, WA Honeywell International, Inc. Commercial Aviation Systems 15001NE36thSt Redmond, WA RadiantPowerCorp Parkland Dr. SuiteB Sarasota, FL BA-89 Marathon Norco Aerospace, Inc Imperial Drive Waco, TX SaftAmerica 711 Industrial Blvd. Valdosta, GA LT-55(A) KGSElectronics, Inc. 418A E. Live Oak Ave. Arcadia, CA Lucas Aerospace Power Equipment Corp Darrow Road Twinsburg, OH Flite-Tronics, Inc. 2525N.NaomiSt. Burbank, CA SUPPLIERPUBLICATIONLIST Page3

12 Table 1. Publication List(continued) Artex ELT Transmitter ELTTransmitter FlotationDevice Flotation Device HydrolokSeat Fire Extinguisher Fire Extinguisher Electric Trim Actuator PartNumber Model 3000 AV-8TypeA AV-8 LL , PublicationTitle Chapter 25 - Equipment/Furnishings Installation and OperationManual Model 3000 Series Overhaul Manual Flotation Device ServiceBulletinRev. 2 Dated Feb 29, 1984 Overhaul Manual with Illustrated Parts List Chapter 26 - Fire Protection Fire Extinguisher Container Overhaul Manual with Illustrated Parts Listing Kidde Fire Extinguisher with Illustrated Parts List Chapter 27 - Flight Controls Publication Part Number Artex Aircraft Supplies, Inc S Township Road Canby, Oregon Model 3000 Pointer Inc N. Stadem Drive Tempe, AZ Switlik Parachute Co. 1325E.StateSt. P.O. Box 1328 Trenton,NJ08607 SB Switlik Parachute Co. 1325E.StateSt. P.O. Box 1328 Trenton,NJ P.L. Porter Co DeSoto Ave. Woodland Hills, CA PacificScientific Advanced Technology Division, HTL.Div Walker Ave. Monrovia, CA Kidde Inc Airport Dr Wilson,NC /56CM09 Cessna Aircraft Co. Citation Marketing Dept. 569 Attn: Publications P.O. Box 7706 Wichita, KS SUPPLIERPUBLICATIONLIST Page4

13 Table 1. Publication List(continued) Speed Brake Actuator Speed Brake Actuator Speed Brake Actuator PartNumber Trim Tab Actuator Electrical Fuel Pumps Indicator Fuel Quantity C VSDLOC 403A Tube Connectors 900 Series Wig-O-Flex PublicationTitle for Speed Brake Actuator Overhaul Manual withiplforspeed BrakeActuator Speed Brake ActuatorAssembly Chapter 28 - Fuel Electrical Fuel Pumps Service Manual With Illustrated Parts Tube Connectors W900 Series Flexible "Wig-O- Flex" Swage Type Electrically Bonded Chapter 29 - Hydraulic Power Publication Part Number Schneebecks Industries,Inc Roberts Rd. ColoradoSprings, CO RM-01 Phoenix Controls Inc E. Broadway Dr. Tempe, AZ Nabtesco (formerly Teijin Seiki America,Inc.) GifuPlant Miyashiro, Tarui-Cho, Fuwa-Gun, Gifu-Ken, Japan 50/56CM09 CessnaAircraftCo. Citation Marketing Dept. 569 Attn: Publications P.O. Box 7706 Wichita, KS Parker Hannifin Corp. Airborne Division 711 Taylor St. P.O. Box 4032 Elyria, OH Ametek Inc. U.S. Gauge Div. 900 Clymer Ave. Sellersville, PA Catalog 126B Delaval Turbine Inc. Wiggins Connectors Div Triggs St. LosAngeles, CA SUPPLIERPUBLICATIONLIST Page5

14 Table 1. Publication List(continued) HydraulicShutoff Valve De-icing Panels NylonTubingand Couplings Proportioning Units Data Nav III System Digital Clock PartNumber B24A AirBottleAssembly PublicationTitle Tandem Hydraulic Shutoff Center Valve Assembly-Mean Time Between Overhaul Chapter 30 - Ice and Rain Protection De-icing Panels Fitted to Cessna Models S550 and 552 with IllustratedParts List GeneralPractices Manual- TKS Tubing And Couplings Proportioning Units Fitted to Cessna SII, with Illustrated Parts List Publication Part Number MTBO Chapter 31 - Indicating/Recording Systems Data Nav III System withskipandrecall SystemDescription and Installation Manual Digital Clock Chapter 32 - Landing Gear Air Bottle Assembly Overhaul Manual Eaton Aerospace LLC Fluid Control & Actuation Div. 4690ColoradoBlvd. Los Angeles, CA Aerospace System & Technologies Greencroft Ind. Park Stanley, County Durham, England DH97 YB CAV Aerospace, Inc Arnold Court Salina, Kansas CAV Aerospace, Inc Arnold Court Salina, Kansas B M811 Legacy- Brochure RCACorp. RCA Avionics Systems 7821 Orion Ave. VanNuys,CA91406 Davtron Inc. 427 Hillcrest Way RedwoodCity,CA Tavco Inc. Fluid Control Systems Prairie St. Chatsworth, CA SUPPLIERPUBLICATIONLIST Page6

15 Table 1. Publication List(continued) PartNumber Air Bottle Assembly Brake Assembly Brake Assembly Brake Assembly Brake Relay Valve Main Landing Gear Actuator Main Landing Gear Actuator , , PublicationTitle Air Bottle Assembly Overhaul Manual With Illustrated Parts ListForTheMain WheelAssy &BrakeAssy With Illustrated Parts List With Illustrated Parts List General Aviation BrakeRelayValve Hydro-AireMarkIII GA With Illustrated Parts List With Illustrated Parts List Publication Part Number PacificScientificCo. Advanced Technology Group HTLDivision 1800 Highland Ave. Duarte,CA Parker Aerospace Aircraft Wheel and BrakeDivision Parker Hannifin Corp Center Road Avon, OH AP-527. AP-527. Loral Corp. Aircraft Braking SystemsDiv Massillon Rd. Akron, OH Loral Corp. Aircraft Braking SystemsDiv Massillon Rd. Akron, OH Crane Co. Hydro-Aire Div Winona Ave. Burbank, CA Dowty Decoto AircraftCompany 2720 W. Washington Ave. P.O. Box 9907 Yakima, WA Nabtesco (formerly Teijin Seiki America,Inc.) GifuPlant Miyashiro, Tarui-Cho, Fuwa- Gun, Gifu-Ken, Japan SUPPLIERPUBLICATIONLIST Page7

16 Table 1. Publication List(continued) Main Landing Gear Actuator Main Landing Gear Assembly Main Wheel Assembly Main Wheel Assembly Main Wheel Assembly Nose Landing Gear Assembly Nose Landing Gear Retract Actuator PartNumber , , PublicationTitle With Illustrated Parts List Main Landing Gear Assembly - With Illustrated Parts List With Illustrated Parts ListForTheMain Wheel Assy & Brake Assy With Illustrated Parts List Nose Landing Gear Assembly - With Illustrated Parts List Publication Part Number Nabtesco (formerly Teijin Seiki America, Inc.) Gifu Plant Miyashiro, Tarui-Cho, Fuwa- Gun, Gifu-Ken, Japan 50/55/S55CMM05 Cessna Aircraft Co. Citation Marketing Dept. 569 Attn: Publications P.O. Box 7706 Wichita, KS Loral Corp. Aircraft Braking SystemsDiv Massillon Rd. Akron, OH Parker Aerospace Aircraft Wheel and Brake Division Parker Hannifin Corp. 1160CenterRoad Avon,OH44011 JN45927/175 BF Goodrich Aerospace Aircraft Wheels & Brakes P.O.Box340 Troy, OH /55/S55CMM05 Cessna Aircraft Co. Citation Marketing Dept. 569 Attn: Publications P.O. Box 7706 Wichita, KS Nabtesco (formerly Teijin Seiki America, Inc.) Gifu Plant Miyashiro, Tarui-Cho, Fuwa- Gun, Gifu-Ken, Japan SUPPLIERPUBLICATIONLIST Page8

17 Table 1. Publication List(continued) Nose Landing Gear Retract Actuator Nose Landing Gear Wheel Nose Landing Gear Wheel Uplock and Sequence Actuator Oscillating Light AA-300 Radio Altimeter System CAS 67A/67B TCAS II System ADF-462 Automatic Direction Finding System PartNumber AA PublicationTitle With Illustrated Parts List WithIllustrated Parts List With Illustrated Parts List Uplock and Sequence Actuator - Chapter 33 - Lights Tandem Oscillating Aircraft Navigational Light Overhaul Manual with Illustrated Parts List Chapter 34 - Navigation AA300 Series Radio Altimeter System Operation and Installation Manual SystemInstallation Manual ADF-462 Automatic DirectionFinding System Instruction Manual Publication Part Number Dowty Decoto AircraftCompany 2720 W. Washington Ave. P.O. Box 9907 Yakima, WA Loral Corp. Aircraft Braking SystemsDiv Massillon Rd. Akron, OH BF Goodrich Aerospace Aircraft Wheels & Brakes P.O.Box340 Troy,OH /55/S55CMM05 Cessna Aircraft Co. Citation Marketing Dept. 569 Attn: Publications P.O. Box 7706 Wichita,KS Midland-Ross Corp. MidtexDivision 1650 Tower Blvd. North Mankato, MN Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ , Revision9(orlater) A Honeywell International Inc W.105thSt. Olathe, KS Rockwell Collins, Inc. 400CollinsRDNE CedarRapids, IA SUPPLIERPUBLICATIONLIST Page9

18 Table 1. Publication List(continued) ADF-60 Automatic Direction Finding System PartNumber AltimeterALT-55B ANS-31C Area Navigation System CA-320 Digital Compass Directional Gyro CompassSystem DFS-43ADirection Finder System DF 206 Direction Finder System DME-42Distance Measuring Equipment System DMS-44A Distance Measuring System S DFS-43A DMS-44A PublicationTitle ADF-60Automatic Direction Finding SystemInstruction Manual ANS-31C Area Navigation System Instruction Manual CA-320 Digital Compass Operator Manual C-14 Compass SystemMaintenance Manual DFS-43A Direction Finder System DF206Direction Finder System DME-42 Distance Measuring Equipment System Instruction Manual DMS-44A Distance Measuring System Publication Part Number A Rockwell Collins, Inc. 400CollinsRDNE Cedar Rapids, IA Rockwell Collins, Inc. 400CollinsRDNE Cedar Rapids, IA A Rockwell Collins, Inc. 400 CollinsRD NE Cedar Rapids, IA Capital Avionics 3701 Hartsfield RD Tallahassee, FL C-14 Honeywell, Inc. Defense Avionics SystemsDiv. 9201SanMateoNE Albuquerque, NM IB2043A Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ Rockwell Collins, Inc. 400CollinsRDNE Cedar Rapids, IA Rockwell Collins, Inc. 400CollinsRDNE Cedar Rapids, IA IB2044A Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ SUPPLIER PUBLICATION LIST Page 10

19 Table 1. Publication List(continued) EFS-10 Electronic Flight Instrumentation System Emergency Power Supply GNS-500A NavigationSystem Primus 300SL ColoRadar System Primus 400SL ColoRadar System Primus 800 Antenna Pedestal Primus 800 ColoRadar System PartNumber EFS PublicationTitle EFS-10 Electronic Flight Instrumentation SystemInstruction and Maintenance Manual Emergency Power SupplyMaintenance Manual GNS-500A(Series 3) Navigation System Maintenance Manual with InstallationData Primus 300SL ColoRadarSystem Description and Installation Manual Primus 400SL ColoRadarSystem Description and Installation Manual Primus 800 ColoRadar Antenna Pedestal Primus 800 ColoRadarSystem Description and Installation Manual Publication Part Number IB2010A Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ L-3 Avionics Systems, Inc ndSt. S.E. Grand Rapids, MI Global-Wulfsberg System Division of Sundstrand Data ControlInc th Avenue NE Redmond, WA IB IB IB IB Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ SUPPLIERPUBLICATIONLIST Page11

20 Table 1. Publication List(continued) Primus 800 Digital Indicator Primus 800 Receiver- Transmitter PS-835Emergency PowerSupply PS-835Emergency PowerSupply TDR-90 Transponder TRS-42A ATC Transponder System RDR-1150 Weather Radar System RDS-86 Weather Radar System PartNumber , , TRS-42A RDS-86 PublicationTitle Primus 800 ColoRadar Digital Indicator WI-800 WR-800 Receiver Transmitter Volume I - Description And Operation and Maintenance Practices PS-835 Emergency Power Supply PS-835()-Battery Maintenance Service Letter SL-80 TDR-90 Transponder Instruction Manual TRS-42A ATC Transponder System RDR-1150 Weather Radar System RDS-86 Weather Radar System Publication Part Number IB IB Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ L-3 Avionics Systems,Inc ndSt. S.E. Grand Rapids, MI SL A IB2042A IB21150A IB2086 L-3 Avionics Systems,Inc ndSt. S.E. Grand Rapids, MI Rockwell Collins, Inc. 400CollinsRDNE Cedar Rapids, IA Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ HoneywellInc North 19th Avenue P.O. Box Phoenix, AZ Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ SUPPLIER PUBLICATION LIST Page 12

21 Table 1. Publication List(continued) RMI-30 Radio Magnetic Indicator RNS-3500 Area NavigationSystem VCS-40A VHF Communication System VIR-32Navigation System VNS-41A VHF NavigationSystem WXR-300Weather Radar System High Pressure Cylinders Oxygen Cylinder and Regulator PartNumber VCS-40A VNS-41A ZR807 PublicationTitle RMI-30 Radio Magnetic Indicator RNS-3500 VCS-40A Communications System Maintenance Manual VIR-30 Radio NavigationSystem Instruction Manual VNS-41A VHF NavigationSystem WXR-300 Weather Radar System Instruction Manual Chapter 35 - Oxygen Guidelines for Visual Inspection and Requalification of FiberReinforced High Pressure Cylinders Oxygen Cylinder and Regulator Overhaul Manual Publication Part Number Rockwell Collins, Inc. 400CollinsRDNE CedarRapids, IA IB23500A Part 1 Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ IB2040A A IB2041A A Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ Rockwell Collins, Inc. 400CollinsRDNE CedarRapids, IA Honeywell Inc North 19th Avenue P.O. Box Phoenix, AZ Rockwell Collins, Inc. 400CollinsRDNE CedarRapids, IA CGAC CompressedGas Association,Inc. Arlington, VA ZR807 Puritan-Bennett Aero Systems Pflumm Rd. Shawnee Mission, KS SUPPLIERPUBLICATIONLIST Page13

22 Table 1. Publication List(continued) PartNumber Oxygen Fill Valve Oxygen Mask Oxygen Outlet Regulating and ReliefValve Water Separator Toilet Toilet Z908, Z E E06-2A PublicationTitle Overhaul Manual ZV951 Oxygen Fill Valve Oxygen Mask Overhaul Manual Overhaul Manual OxygenOutlet Chapter 36 - Pneumatic Regulating and Relief Valve Overhaul Instructions with Illustrated Parts List Water Separator and Filter Overhaul Manual with Illustrated Parts List Chapter 38 - Water/Waste Executive Aircraft ToiletInstallation, Service and ExecutiveAircraft ToiletInstallation, Service and Chapter 71 - Powerplant Publication Part Number ZV951 Z908/Z909 38U BB Puritan-Bennett Aero Systems Pflumm Rd. Shawnee Mission, KS Puritan-BennettAero Systems Pflumm Rd. Shawnee Mission, KS Puritan-BennettAero Systems Pflumm Rd. Shawnee Mission, KS TheBendixCorp. Electric and Fluid Power Div. 211 Seward Ave. Utica, NY U A2-13 Lucas Western, Inc. Lucas Aerospace Power Transmission 211SewardAve. Utica, NY SM NO. 131 SM NO. 131 Monogram Industries, Inc. Monogram/ Sanitation Group SubofNortekInc Freeman Blvd. Redondo Beach, CA Monogram Industries, Inc. Monogram/ Sanitation Group SubofNortekInc Freeman Blvd. Redondo Beach, CA SUPPLIER PUBLICATION LIST Page 14

23 Table 1. Publication List(continued) EngineMounting System Turbofan Engine Turbofan Engine Turbofan Engine Turbofan Engine PartNumber LM-420 JT15D JT15D-4 JT15D-4 JT15D-4 Fuel Flow Indicator VSDLOC 208A Fuel Flow Indicator VSDLOC208E PublicationTitle Aircraft Engine Mounting System TurbofanEngine- Models JT15D-1, -1A,-1B,-4, -4B, 04DIllustratedParts Catalog Turbofan Engine Turbofan Engine- Parts Catalog Turbofan Engine Overhaul Manual Publication Part Number Chapter 73 - Engine Fuel And Control With Illustrated Parts List With Illustrated Parts List Chapter 76 - Engine Controls Lord Corp. Aerospace Products Div. 1635W.12thSt. P.O. Box Erie, PA Pratt & Whitney Canada 1000 Marie-Victorin, Longueuil Quebec, Canada J4G1A Pratt & Whitney Canada 1000 Marie-Victorin, Longueuil Quebec, Canada J4G1A Pratt & Whitney Canada 1000 Marie-Victorin, Longueuil Quebec, Canada J4G1A Pratt &Whitney Canada 1000 Marie-Victorin, Longueuil Quebec, Canada J4G1A Ametek Inc. U.S. Gauge Div. 900 Clymer Ave. Sellersville, PA Ametek Inc. U.S. Gauge Div. 900 Clymer Ave. Sellersville, PA SUPPLIERPUBLICATIONLIST Page15

24 Table 1. Publication List(continued) Synchronizer Fan Speed Indicator Fan Speed Indicator Interturbine Temperature Indicator Turbine Speed Indicator HydraulicSolenoid Operated Valve ThrustReverser Oil Pressure Indicator PartNumber VSDLOC410AD PN: VSDLOC410AD VSDLOC 419E DDLOC110A AV14K PublicationTitle Woodward Electronic Synchronizer Chapter 77 - Engine Indicating Fan Speed Indicator Fan Speed Indicator With Illustrated Parts List Turbine Speed Indicator Chapter 78 - Engine Exhaust With Illustrated Parts List Maintenance Citation Thrust Reverser Chapter 79 - Oil Oil Pressure Indicator Publication Part Number Bulletin Woodward Governor Co. AircraftControlsDiv. 5001N.SecondSt. P.O. Box 7001 Rockford,IL Ametek Inc. U.S.GaugeDiv. 900 Clymer Ave. Sellersville, PA Ametek Inc. U.S.GaugeDiv. 900 Clymer Ave. Sellersville, PA Ametek Inc. U.S.GaugeDiv. 900 Clymer Ave. Sellersville, PA Ametek Inc. U.S.GaugeDiv. 900 Clymer Ave. Sellersville, PA ITT General Controls Aerospace Products 1200 S. Flower Burbank,CA TheNordamGroup, Inc East Pine Street Tulsa, OK Ametek Inc. U.S.GaugeDiv. 900 Clymer Ave. Sellersville, PA SUPPLIER PUBLICATION LIST Page 16

25 Table 1. Publication List(continued) OilTemperature Indicator DC Starter Generator DC Starter Generator PartNumber VSDLOC 219C PublicationTitle Oil Temperature Indicator Chapter 80 - Starting DC Generators and Starter Generators With Illustrated Parts List DC Starter-Generator , -002, -004,-006 Publication Part Number Ametek Inc. U.S. Gauge Div. 900 Clymer Ave. Sellersville, PA Lucas Aerospace Power Equipment Corp Darrow Road Twinsburg,OH Lucas Aerospace Power Equipment Corp Darrow Road Twinsburg, OH SUPPLIERPUBLICATIONLIST Page17

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27 1. General CAS-67A/67B TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS II) - DESCRIPTION AND OPERATION (ForAirplanes-0001 thru-0160 Incorporating SBS ) A. The CAS-67A/67B Traffic Alert and Collision Avoidance System (TCAS II), Traffic Advisory (TA), Resolution Advisory(RA),and Vertical Speed Indicator(VSI)shows visual traffic advisories to the flight crew on the TCAS II display. An interrogation of every transponder-equipped airplane in range ofthetcasiisystemwillshowitsbearingandaltitudedata. Thisdatacalculatesaflightpathfor collision avoidance. Non-airborne reporting intruders will also be sensed and monitored by the TCAS IIsystem. 2. Description A. The CAS-67A/67B TCAS II system supplies traffic alert functions without support from Air Traffic Control(ATC) ground stations. The CAS-67A/67B TCAS II system uses dual MST-67A Transponders. B. The system supplies safe separation between the airplane in which it is installed and other aircraft equipped with Mode S, Mode C, or Mode A/C transponders. C. The TCAS II system monitors airspace that surrounds the airplane by interrogations and replies from transponders in other aircraft. Interrogation reply enables TCAS II to compute the information about the intruders that follows: (1) Range between the airplane and intruder (2) Relative bearing to the intruder (3) Altitudeandverticalspeedoftheintruder,ifaltitudeisreported (4) Closingratebetweentheintruderandtheairplane (5) SendaTAwhentrafficintheareaistooneartotheairplane (6) SendaRAtokeepsafeverticalseparationiftheintrudercontinuestoapproach (7) Monitor 45 aircraft, display up to 30, and coordinate a resolution advisory for up to three intruders atthesametime. D. System components include a TPU-67A/67B Processor, CM-67A Configuration Module, Top and Bottom TCAS II Antennas, MST-67A Transponder(Mode S) and antennas, PS-578A Transponder/ TCAS II Control Head, TCAS II, TA/RA/VSI display Transponder Programming Module(Mode-S Relay Box), and system annunciators, found on the center instrument panel. E. Before you perform TCAS system self-test, make sure that the following aircraft systems are powered and operating with no failure flags on the appropriate cockpit instruments: (1) Mode S transponder system (2) Encoding Altitude Sources(Air Data Systems) (3) Radio Altimeter systems (4) Attitude(VerticalGyro)systems (5) Heading(Compass)systems 3. Operation A. The TCAS II processor sets the directional antenna beams, makes and moves pulsed 1030 MHz surveillance interrogation data through the top and bottom TCAS antennas, and receives 1090 MHz reply data from transponders via the TCAS antennas. The TCAS processor examines reply data and calculates the threat potential of intruder aircraft. B. The information that follows about the airplane is regularly read and stored in the TCAS II processor. (1) Airplane heading(pitch, roll, and radio altimeter) inputs. This information, along with pressure altitude data, lets the TCAS II calculate the airplane s position and flight path,which is used during advisory and traffic display computations. (2) Pressure altitude is sent to the transponder from the airplane s pressure altitude source. (3) Pressure altitude is usedto find the airplane s flight level altitude in relation to the intruder s reported altitude Page1

28 (4) Airplane identification issentto the TCASIIprocessor,whichthentransmitsit toothertcas equipped aircraft in the area to decrease interference. (5) AirplanemaximumairspeedissenttotheTCASIIprocessorandusedinmaximumclosingrate projections. C. The TCAS II processor has functions that find range, bearing, and altitude of intruder aircraft from information calculated from or contained in reply messages. The altitude can only be found if the intruder reports altitude in its transponder s reply message. D. From the use of transponder reply data, the TCAS II processor makes an analysis of the threat potential of the intruder. This is done by a calculation of the position of the intruder and the rate the intruder nears a collision. From this evaluation, the TCAS II processor categorizes the intruder as a non-threat, proximity, or traffic advisory. E. For traffic advisory-category aircraft, the TCAS II processor supplies traffic advisory symbol position andalertdatatothetcasdisplay. TheTCASIIprocessoralsooutputstrafficadvisoryalertvoice messages through the cockpit audio system. F. For proximity and non-threat aircraft, TCAS II processor supplies proximity or non-threat traffic symbol position data to TCAS display. Voice alerts are not given for proximity or non-threat category aircraft. G. FormoreinformationabouttheoperationoftheCAS-67A/67BTCASIIsystemrefertotheCAS67A/ 67B TCAS II System Installation Manual(P/N ). Refer to the Introduction, Publication List Page2

29 CAS-67A/67BTRAFFICALERTANDCOLLISIONAVOIDANCESYSTEM(TCASII)-TROUBLESHOOTING (ForAirplanes-0001thru-0160IncorporatingSBS ) 1. General A. This section gives the troubleshooting procedures for the Honeywell CAS-67A/67B Traffic Alert And Collision Avoidance System(TCAS II). B. System components include a TPU-67A/67B Processor, CM-67A Configuration Module, Top and Bottom TCAS II Antennas, MST-67A Transponder(Mode S) and antennas, PS-578A Transponder/ TCAS II Control Head, TCAS II, TA/RA/VSI display Transponder Programming Module(Mode-S Relay Box), and system annunciators, found on the center instrument panel. 2. Troubleshooting A. For the troubleshooting procedures of the CAS 67A/67B Traffic Alert And Collision Avoidance System (TCAS II), refer to the CAS 67A/67B TCAS II System Installation Manual(P/N ). Refer to the Introduction, Publication List Page 101

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31 1. General CAS-67A/67B TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS II) - MAINTENANCE PRACTICES (ForAirplanes-0001 thru-0160 Incorporating SBS ) A. The maintenance of the CAS-67A/67B TCAS II system includes the removal and installation of the system components. Information on a system self-test is also included in this section. For detailed information on complete system functional tests refer to CAS-67A/67B TrafficAlert and Collision Avoidance System(TCAS II)- Adjustment/Test. B. For maintenance practices on components not covered in this section, refer to the CAS 67A/67B TCAS II System Installation Manual(P/N ) Refer to the Introduction, Publication List. C. The TCAS II system also includes transponder components that will be covered in this section. These components include dual MST-67A Transponders, CM-67A Configuration Module, dual Top and Bottom Transponder Antennas, and PS-578A Control Head. D. There are three location options for the TPU-67A/67B Processor. These location options are in the left front baggage compartment area at approximately FS and LBL 9.50(location option A), right front baggage compartment area at approximately FS and RBL 6.03(location option B), leftafttailconeareaatapproximatelyfs486.50andwl139.19(locationoptionc). E. There are three location options for the CM-67A Configuration Module. All locations will be near to the related TCAS II Processor. These location options are in the left front baggage compartment area at approximately FS and LBL 14.03(location option A), right front baggage compartment area at approximately FS and RBL 6.03(location option B), left aft tailcone area at approximately FS and WL (location option C). F. There is an Top and Bottom TCAS II Antenna used in thesystem. The top antenna is locatedat FS ThebottomantennaislocatedatFS258.50andRBL2.80. G. There is a PS-578A Control Head installed in the instrument panel assembly in the cockpit. 2. ToolsandEquipment A. For a list of the required tools and equipment, refer to Navigation- General. 3. TPU-67A/67BProcessorRemoval/Installation A. Remove the TPU-67A/67B Processor. (Refer to Figure 201). NOTE: The removal of the TPU-67A/67B processor is typical. Refer to the General section for the different locations of the TPU-67A/67B Processor. (1) Remove electrical power from the airplane. (2) Disengage the TCAS circuit breaker on the right circuit breaker panel. (3) Loosentheknurlednutsonthemountingtray. (4) Liftthehandleonthefrontoftheprocessorandcarefullypulltheprocessoroutofthemounting tray. NOTE: This action will disengage the coaxial cables and electrical connectors. (5) Remove the processor from the airplane. B. Install the TPU-67A/67B Processor. (Refer to Figure 201). NOTE: The installation of the TPU-67A/67B processor is typical. Refer to the General section for the different locations of the TPU-67A/67B Processor Page 201

32 TPU-67A/67BProcessorInstallation Figure 201(Sheet 1) Page 202

33 TPU-67A/67BProcessorInstallation Figure 201(Sheet 2) Page 203

34 TPU-67A/67BProcessorInstallation Figure 201(Sheet 3) Page 204

35 TPU-67A/67BProcessorInstallation Figure 201(Sheet 4) Page 205

36 CAUTION: Damagetotheelectricalconnectorswilloccuriftheconnectorsdo not align correctly. (1) Make sure that the connectors on the mounting tray and processor align correctly as the processor is put into the mounting tray. (2) After the connectors align correctly, push the processor firmly into the mounting tray. (3) Tighten the knurled nuts on the mounting tray. (4) Make sure the coaxial cables and connectors are tightly set in position when the processor is installedinthemountingtray. (5) Lowerthehandleonthefrontoftheprocessor. (6) Engage the TCAS circuit breaker on the right circuit breaker panel. (7) DoanoperationalcheckoftheTCASIIsystemasfollows: (a) Connect external electrical power to the airplane. (b) PuttheAVIONICMASTER(S509)switchtotheONposition. (c) Do the self-test with the MODE S/TCAS control unit. Refer to MST-67A Transponder Self- Testinthissection. (d) ForairplaneswithadualMODES,setthetransponder'sselectswitchtoNumber1position todoatestofthenumber1transponder. (e) AfteryouselectTESTMODE,youwillseetheFAILlightcomeon. (8) Thetestsequencemustbeasfollows: (a) For airplanes with Traffic Advisory (TA), Resolution Advisory (RA) and Vertical Speed Indicator(VSI), do the steps below: 1 TheTA/RA/VSIwillshowafixedresolutionadvisoryandatrafficsymboltestpattern. 2 ThewordTESTwillshowontheTCASprocessor. NOTE: After you do the self-test successfully, you will hear a synthesized voice with the words that follow: TCAS SYSTEM TEST OK. After a self-test failure,youwillhearasynthesizedvoicewiththewords,tcassystem TESTFAILandseeadisplaymessageforthefailedsystemcomponent. (9) Iferrorsarefound, doafunctionaltest. RefertoChapter34,CAS-67A/67BTrafficAlertand Collision Avoidance System(TCAS II)- Adjustment/Test. 4. CM-67AConfigurationModuleRemoval/Installation A. Remove the CM-67A Configuration Module. (Refer to Figure 202). NOTE: The removal of the CM-67A Configuration Module is typical. Refer to the General section for the different locations of the CM-67A Configuration Module. (1) Remove electrical power from the airplane. (2) Disengage the TCAS circuit breaker on the right circuit breaker panel. (3) Disconnect the electrical connector from the configuration module. (4) Removethescrewsthatattachtheconfigurationmoduletotheairplane. (5) Remove the configuration module from the airplane. B. Install the CM-67A Configuration Module. (Refer to Figure 202). NOTE: The installation of the CM-67A Configuration Module is typical. Refer to the General section for the different locations of the CM-67A Configuration Module. (1) Put the configuration module in position and attach with the screws. (2) Connecttheelectricalconnectortotheconfigurationmodule Page 206

37 CM-67A Configuration Module Installation Figure 202(Sheet 1) Page 207

38 (3) Connect electrical power to the airplane. NOTE: If a new TCAS II configuration module has been installed, before tests are done, you must program it with the model of the airplane and the avionics equipment installed. Diagnostic software and a laptop computer are necessary to diagnose and programthetcasiisystem. ThetestequipmentconnectstotheRS232testport connector(ji851), whichisfoundattheleftforwardendofthepedestalunderthe instrument panel. For information on programming, diagnostic software, self-test, and operational checks, refer to the CAS 67A/67B TCAS II System Installation Manual(P/N ). Refer to the Introduction, Publication List. (4) Engage the TCAS circuit breaker on the right circuit breaker panel. (5) Do an operational check of the CAS-67A/67B Traffic Alert and Collision Avoidance system. Refer to MST-67A Transponder Self-Test in this section. 5. TCASIITopandBottomAntennaRemoval/Installation A. RemovetheTopTCASIIAntenna. (RefertoFigure203). (1) Remove electricalpower from the airplane. (2) Disengage the TCAS circuit breaker on the right circuit breaker panel. (3) Remove the overhead console to get access to the antenna coaxial connectors at FS Refer to Chapter 25, Overhead Console- Maintenance Practices. (4) Identify and disconnect the coaxial connectors(pf1047, PF1048, PF1049, and PF1050) from the top antenna. (5) Carefully remove the fillet seal around the top antenna and the antenna adapter on the airplane exterior. Refer to Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing - Maintenance Practices. (6) Removethescrewsandwashersthatattachthetopantennatotheairplane. (7) Remove the top antenna from the airplane. B. InstalltheTopTCASIIAntenna. (RefertoFigure203). (1) Make sure all used sealant is removed from around the base of the antenna, the antenna adapter, the doubler hole where the antenna connector passes through the fuselage, and the fuselage skin. Refer to Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing -Maintenance Practices. (2) Apply electrically conductive chemical film treatment to the fuselage skin. Refer to Chapter 20, Electrical Bonding- Maintenance Practices. (3) Putthetopantennainitspositionontheairplane. (4) Install the screws and washers that attach the top antenna to the airplane. (a) ApplyalayerofTypeI,ClassA(or)Bsealantovertheantennascrews.RefertoChapter 20, Fuel, Weather, Pressure and High-Temperature Sealing- Maintenance Practices. (5) Makesurethereisagoodelectricalbondbetweenthesurfacesofthetopantenna,antenna adapter, and the fuselage skin. Refer to Chapter 20, Electrical Bonding- Maintenance Practices. (6) Identify and connect the coaxial connectors(pf1047, PF1048, PF1049 and PF1050) to the top antenna. (7) UseTypeI,ClassBsealanttomakeafilletsealaroundthebaseofthetopantenna(exterior surface of airplane) and the antenna adapter. Refer to Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing- Maintenance Practices. (8) FillinthetopofthescrewswithRTVClass"VC"sealanttopreventwaterentrance. Referto Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing- Maintenance Practices. (9) Install the overhead console. Refer to Chapter 25, Overhead Console- Maintenance Practices. (10) EngagetheTCAScircuitbreakerontherightcircuitbreakerpanel Page 208

39 TCAS II Antennas Figure 203(Sheet 1) Page 209

40 (11) DoanoperationalcheckoftheTCASIIsystemasfollows: NOTE: If antenna coaxial connectors were replaced, the self-test of the TCAS II system will be sufficient. If an antenna coaxial cable was changed for length, you must complete thetcastestsetupandtopantennatestorbottomantennatestasapplicable. Refer to Chapter 34, CAS-67A/67B Traffic Alert and Collision Avoidance System (TCAS II)- Adjustment/Test. (a) Connect external electrical power to the airplane. (b) PuttheAVIONICMASTER(S509)switchintheONposition. (c) Do the self-test with the MODE S/TCAS control unit. Refer to MST-67A Transponder Self- Testinthissection. (d) ForairplaneswithadualMODES,setthetransponder'sselectswitchtoNumber1position todoatestofthenumber1transponder. (e) AfteryouselectTESTMODE,youwillseetheFAILlightcomeon. (12) Thetestsequencemustbeasfollows: (a) ForairplaneswithTA/RA/VSI,dothestepsbelow: 1 TheTA/RA/VSIwillshowafixedresolutionadvisoryandatrafficsymboltestpattern. 2 ThewordTESTwillshowontheTCASprocessor. NOTE: Afteryoudotheself-testsuccessfully,youwillhearasynthesizedvoice with the words that follow: TCAS SYSTEM TEST OK. After a self-test failure,youwillhearasynthesizedvoicewiththewords,tcassystem TEST FAIL and see a display message for the failed system component. (13) Iftheselftestfails, refertothecas67a/67btcasiisysteminstallationmanual(p/n ) for additional information on failure messages and fault isolation procedures. Refer to the Introduction, Publication List. C. RemovetheBottomTCASIIAntenna. (RefertoFigure203). (1) Put the AVIONIC MASTER(S509) switch in the OFF position. (2) Remove electrical power from the airplane. (3) Disengage the TCAS circuit breaker on the right circuit breaker panel. (4) To get access to the bottom antenna coaxial connectors, do as follows: (a) Remove the carpet. Refer to Chapter 25, Carpet- Maintenance Practices. (b) Remove cabin floorboard panel. Refer to Chapter 53, Floor Panels - Description and Operation. (c) Remove cabin floorboard access panel 261BTC at FS Refer to Chapter 6, Access Plates and Panels Identification-Description and Operation. (5) Identify and disconnect the coaxial connectors(pf1051, PF1052, PF1053, and PF1054) from the bottom antenna. (6) Carefully remove the fillet seal around the bottom antenna and the antenna adapter on the airplane exterior. Refer to Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing - Maintenance Practices. (7) Remove the screws and washers that attach the bottom antenna and spacer to the airplane. (8) Remove the bottom antenna and spacer from the airplane. D. Install the Bottom TCAS II Antenna. (Refer to Figure 203). (1) Makesureallusedsealantisremovedfromaroundthebaseoftheantennaandantennaadapter, doubler hole where antenna connector passes through the fuselage, and the fuselage skin. Refer to Chapter 20, Fuel, Weather, Pressure and High-Temperature Sealing - Maintenance Practices. (2) Apply electrically conductive chemical film treatment to the fuselage skin. Refer to Chapter 20, Electrical Bonding- Maintenance Practices. (3) Putthebottomantennaandspacerinitspositionontheairplane. (4) Install the screws and washers that attach the bottom antenna and spacer to the airplane. (5) Makesurethereisagoodelectricalbondbetweenthesurfacesofthebottomantenna,antenna spacer, antenna adapter, and the fuselage skin. Refer to Chapter 20, Electrical Bonding - Maintenance Practices Page 210