P8CTT-950TCAS II

Aviation Communication and Surveillance Systems 19810 North 7th Avenue Phoenix, Arizona 85027--4400 U.S.A. 15 FEBRUARY 2003 34-43-20 Page T--1 PRINTED IN U.S.A. PUB. NO. 8000451--001 T 2 CAS Traffic and Terrain Collision Avoidance System System Description and Installation Manual T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to therestrictions in the proprietary notice of this document. Page T--2 PROPRIETARY NOTICE This document and the information disclosed herein are proprietary data of ACSS. Neither this document nor the information contained herein shall be used, reproduced, or disclosed to others without the written authorization of ACSS, except to the extent required for installation or maintenance of the recipientís equipment. NOTICE -- FREEDOM OF INFORMATION ACT (5 USC 552) AND DISCLOSURE OF CONFIDENTIAL INFORMATION GENERALLY (18 USC 1905) This document is being furnished in confidence by ACSS. The information disclosed herein falls within exemption (b) (4) of 5 USC 552 and the prohibitions of 18 USC 1905. S2003 ACSS is a U.S. registered trademark. All other marks are owned by their respective companies. T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. Page RR--1 RECORD OF REVISIONS For each revision, put the revised pages in your manual and discard the superseded pages. Write the revision number and date, date put in manual, and the incorporatorís initials in the applicable columns on the Record of Revisions. The initial A shows ACSS is the incorporator. Revision Number Revision DateDate Put in ManualBy T 2 CAS / Part No. 9000000 SYSTEMDESCRIPTIONANDINSTALLATIONMANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. Page RR--2 Blank Page T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. Page RTR--1 RECORD OF TEMPORARY REVISIONS Read the location instructions on each temporary revision page to know where to put the pages in your manual. Remove temporary revision pages only when discard instructions are given. For each temporary revision, give the correct data in the applicable columns. Temporary Revision No. Temporary Revision Date Date Put in Manual By * Date Removed from Manual By * * The initial A in this column shows ACSS has done the task. T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. Page RTR--2 Blank Page T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. Page SBL--1 SERVICE BULLETIN LIST Service Bulletin Identified Mod Date Included in this Manual Description T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. Page SBL--2 Blank Page T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. LEP--1 LIST OF EFFECTIVE PAGES Original--15 Feb 2003 Subheading and Page RevisionSubheading and PageRevisionSubheading and PageRevision Title T--1 T--2-- -- Record of Revisions RR--1-- RR--2-- Record of Temporary Revisions RTR--1-- RTR--2-- Service Bulletin List SBL--1-- SBL--2-- List of Effective Pages LEP--1-- LEP--2-- LEP--3-- LEP--4-- LEP--5-- LEP--6-- Table of Contents TC--1-- TC--2-- TC--3-- TC--4-- TC--5-- TC--6-- TC--7-- TC--8-- TC--9-- T C -- 1 0-- T C -- 11-- T C -- 1 2-- T C -- 1 3-- T C -- 1 4-- Introduction INTRO--1-- INTRO--2-- INTRO--3-- INTRO--4-- INTRO--5-- INTRO--6-- System Description 1--1-- 1--2-- 1--3-- 1--4-- 1--5-- 1--6-- 1--7-- 1--8-- 1--9-- 1--10-- 1--11-- 1--12-- 1--13-- 1--14-- 1--15-- 1--16-- 1--17-- 1--18-- F 1--19/1--20-- 1--21-- 1--22-- 1--23-- Hindicates changed, added, or deleted page. F indicates right foldout page with blank back. T 2 CAS / Part No. 9000000 SYSTEMDESCRIPTIONANDINSTALLATIONMANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. LEP--2 1--24-- 1--25-- 1--26-- 1--27-- 1--28-- 1--29-- 1--30-- 1--31-- 1--32-- 1--33-- 1--34-- 1--35-- 1--36-- F 1--37/1--38-- 1--39-- 1--40-- 1--41-- 1--42-- 1--43-- 1--44-- 1--45-- 1--46-- 1--47-- 1--48-- 1--49-- 1--50-- 1--51-- 1--52-- 1--53-- 1--54-- 1--55-- 1--56-- 1--57-- 1--58-- 1--59-- 1--60-- 1--61-- 1--62-- 1--63-- 1--64-- 1--65-- 1--66-- 1--67-- 1--68-- 1--69-- 1--70-- 1--71-- 1--72-- 1--73-- 1--74-- 1--75-- 1--76-- 1--77-- 1--78-- 1--79-- 1--80-- 1--81-- 1--82-- 1--83-- 1--84-- 1--85-- 1--86-- Mechanical Installation 2--1-- 2--2-- 2--3-- 2--4-- 2--5-- 2--6-- 2--7-- 2--8-- 2--9-- 2--10-- F 2 -- 11 / 2 -- 1 2-- F 2--13/2--14-- F 2--15/2--16-- F 2--17/2--18-- F 2--19/2--20-- F 2--21/2--22-- F 2--23/2--24-- F 2--25/2--26-- F 2--27/2--28-- F 2--29/2--30-- Subheading and Page RevisionSubheading and PageRevisionSubheading and PageRevision T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. LEP--3 F 2--31/2--32-- F 2--33/2--34-- F 2--35/2--36-- F 2--37/2--38-- 2--39-- 2--40-- F 2--41/2--42-- F 2--43/2--44-- F 2--45/2--46--…

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T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION M ANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. 2--53/(2--54 blank) Figure 2--13 (Sheet 2). Directional Antenna Baseplate Outline and Installation Diagram T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION M ANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. 2--55/(2--56 blank) Figure 2--14. Gables G130--XX Control Panel Outline and Installation Diagram T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION M ANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. 2--57/(2--58 blank) Figure 2--15. VSI/TRA Outline and Installation Diagram T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. 3--1 ELECTRICAL INSTALLATION 1. General This section gives electrical installation procedures, power distribution, and interconnect information for each component on the T 2 CAS system. 2. Equipment and Materials For new T 2 CAS installations, refer to Table 1--1 for RCZ--852 Transponder Installation Kit information. For all other components, refer to the applicable Outline and Installation Diagram in the MECHANICAL INSTALLATION section for mating connector part numbers. 3. Electrical Installation Procedure The information necessary to provide the electrical interconnections is contained in the following paragraphs. Refer to Section 4, LOADING/GRADIENT SPECIFICATIONS, for a list of the signal names used in the interconnect diagrams and tables. NOTE:Unless otherwise specified, all wires shall be stranded #22 AWG. NOTE:All ARINC 429 Data Bus wires shall be stranded #22 AWG twisted shield wire. All outer shields shall be terminated to the airframe ground. Unshielded portions of the cable and shield ground wires should be kept to a minimum length to minimize RF susceptibility. NOTE:All electrical installations must be in compliance with SFAR--88. 4. Electrical Installation A. TT--950/951/952 T 2 CAS Computer Units Figure 3--1 shows some general types of T 2 CAS system installations, using various combinations of controllers (control panels) and transponders. The various installation options require different electrical connections as described in the paragraphs that follow. The T 2 CAS Computer Unit uses programming and configuration straps to select or deselect various TCAS functions. In addition, the T 2 CAS uses the APM and ASDB to select or deselect various TAWS/RWS functions. The T 2 CAS Computer Unit ARINC 600 connector layout is shown in Figure 3--2. The contact arrangement for the various connector plugs are shown in Figure 3--3 thru Figure 3--8. Figure 3--9 shows the connector pin layout for the DATA LOADER connector located on the front of the computer unit. B. APM Figure 2--6 shows a typical APM installation. An APM can be mounted to existing aircraft structure or can be mounted to the ACSSí APM mounting bracket that is secured to the aftsideoftheT 2 CAS computer tray connector, reference Figure 3--3. If the Customer specifies the ACSS APM mounting bracket, the Contractor shall manufacture and provide this APM bracket sub kit for this Customerís T 2 CAS installations T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. 3--2 C. TCAS Antennas The electrical installation for the TCAS antennas is specified in the LOADING AND GRADIENT section. Figure 3--3 shows the T 2 CAS computer contact arrangement for the top directional antenna and Figure 3--4 shows the T 2 CAS computer contact arrangement for the bottom antenna. T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. 3--3 Figure 3--1. Typical TCAS Installation Types T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. 3--4 D. GPS Antenna and Coax All T 2 CAS installations require a GPS position source (that includes GPS altitude). The installation design will consist of an A429 interface to the GPS sensor if the signal is available, or the T 2 CAS internal GPS modulewill be required. The installation then consists of the installation of a GPS antenna and the coax cable to the T 2 CAS unit, LBP pin 13. Figure 2--4 shows a typical T 2 CAS installation with an existing GPS source. Where the internal module is required, the T 2 CAS GPS Installation Data Package includes the GPS antenna mounting structures provisions and all of the coax details to secure the coax to the airframe and connect the T 2 CAS GPS antenna with the T 2 CAS computerís LBP pin 13. Figure 2--4 shows a typical T 2 CAS installation with an internal GPS module (installation includes GPS antenna and coax kit). T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. 3--5 Figure 3--2. T 2 CAS Computer Tray Mating Connector T 2 CAS / Part No. 9000000 SYSTEM DESCRIPTION AND INSTALLATION MANUAL 34-43-20 15 Feb 2003 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. 3--6 Figure 3--3. Contact Arrangement for CU Left Top Plug (LTP) Insert Figure 3--4. Contact Arrangement for CU Le…

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1 T 2 CAS BLOCK DIAGRAMS 1.1 T 2 CAS Typical Installation The figure below illustrates a typical aircraft installation of the T 2 CAS. The system is designed as an integrated safety solution, available as a replacement to the existing TCAS 2000 LRU. The developed LRU is intended for use without modification across the range from general aviation to commercial aircraft. TOP ANT GPS Function TCAS-2000 Function MODE S XPDRS A429 DADC RAD ALT A429 & Analog Traffic Display EFIS or VSI/TRA A429 Aural Alerts ICS or Speaker 8 / 600 Ohm TAWS / Windshear Function A429 & Analog GPS A429 FMS A429 IRS / AHRS A429 ILS / MLS A429 & Analog EFIS/Wx CP A429 AOA / FLAPS A429 & Analog DISCRETES APM Visual Alerts EFIS, EICAS, Lamps A429 & Discrete Terrain Display EFIS or Wx A453 Visual Alerts EFIS, EICAS, Lamps A429 & Discrete Laptop PC or Palm Pilot RS-232 Mode S CP A 4 2 9 & D i s c r e t e A615 PDL A429 A615A PDL Ethernet Compact Flash Card CMC/CFDS A429 8 / 600 Ohm BOT ANT GPS ANT A743A Output System Aircraft Interface 1.2 T 2 CAS Functional Overview The figure below indicates the functional block diagram for T 2 CAS functions. System inputs and outputs are described in terms of the information driving the functions and do not describe the LRUs themselves. Several key data transfer points are shown in this diagram, but some function-to-function data transfers are omitted. - Indicates T2CAS system unique functionality. - Indicates functions interfaced to, but not under ACSS design responsibility for T 2 CAS. GCAM Pre-Processing - Data Source Selection - Parameter Consolidation - Data Extrapol ati on GCAM - TAWS Algorithms - GPWS - FLTA - PDA - Windshear Algorithms - Caution or warning generation GCAM Post-Processing - Al er t Pri ori t i zati on - Display Buffer Formatti ng Power-up/Power-down Dat a Recor der : Faul t Log, Event Data Recording BI TE Aircraft Specific Database GPS System TCAS Syst em (no change from heritage TCAS 2000 design, including BITE and I/O characteristics) OMS T 2 CAS Functional Block Diagram A/C State - Speed (VS, CAS, TAS) - Air Temp - Fl ap Setting - Angle Of Attack - Gli desl ope Devi ati on - Localizer Deviation - Headi ng - Flight Path Angle - Altitude - Lat / Long - Airborne/On ground (Landing Gear) - Selected Altitude - Sel ected Al titude Rate - Sel ected Ai rspeed Ai rspace Surveillance -Transponder Input Data loading - TAWS Database - Terrain Database - Airport Database - Fl i ght Test Data - Aircraft Performance Dat a Data loading -BITE data - Event records - Fault records Aircraft Health Monitoring - Central Mainenance Computer - Centralized Fault DIsplay System Di spl ay Out put s - Caution and Warning Indicators to Symbol Generators - Terrain Map Display Aural Messages - Traffic Advisories - Resolution Advisories Aural Messages - TAWS and Windshear Caut i ons - Altitude Callouts - Bank Angle warnings GPS Ant enna - RF Input Perf DB # - Section where function i s descri bed 8 10 11 1111 4 7 4 6 9 System Inputs System Outputs Dataloader 4 LRU Configuration Data IO DB Di spl ay Out put s - Traffic Advisory - Resolution Advosory TAWS / RWS Functionality GPS Out put s - ARINC 743A GNSSU Data loading -BITE data - Event records - Fault records Aircraft Specific Database 8 LRU Confi guration Dat a IO DB GFM Out put Accepts Platform speciific output variables and allocates to specific Aircraft buses and labels; such as: Converting Caution and War ni ng message #1 and #2 To speci fic A429 or A453 bus words and labels GFM Input Accept s specific bus words and bits and allocates to pl atform specific input variables. Exampl e: Converting ARI NC 429 Label 310 and 311 To IRS Lat #1 and IRS Long #1 GFM Functionality External System Internal Function New T 2 CAS External Data Transfer Heritage TCAS External Data Transfer New T 2 CAS Internal Data Transfer - Indicates aircraft specific functionality loaded through a separate database. T 2 CAS LRU A7 TAWS / Windshear Processor A1 Interconnect ARINC 600 Conn. A8 GPS (optional) A2 TCAS Processor A3 TCAS Transmtter Transmitter Output A4 Power Supply A5 TCAS Receiver I/O Local Oscillator Output PDL Conn. BITE LEDS Test Switch PDL I/O Internal TCAS I/O P/S Voltages Aircraft Power TCAS RF Antenna BITE I/O Transmitter Modulation & P/S Voltages Internal GPS I/O External GPS I/O GPS Antenna External TAWS I/O P/S Voltages TCAS to TAWS I/O P/S Voltages External TCAS I/O Internal TCAS I/O P/S Voltages Internal TCAS I/O P/S Voltages PDL I/O BITE I/O APM Comp. Flash Conn. P1 MOT 8245 P2 MOT 8245 CAS SDP-185 SURV SDP-185 AMD K-6 - Indicates heritage TCAS 2000 design which will be unchanged on T 2 CAS program Note: A6 assembly is the cooling fan, present 4-MCU units only.

Internal and external photos are contained in FCC Compliance Report, ACC document No. 8000709-001, Rev -.

Engineering Drawing CAGE Code Initial Release Date Revision Date Document Number Revision 1WYD3 See PDM None 9000299 B PROPRIETARY NOTICE THIS DOCUMENT AND THE INFORMATION DISCLOSED HEREIN ARE PROPRIETARY DATA OF ACSS. NEITHER THIS DOCUMENT NOR THE INFORMATION CONTAINED HEREIN SHALL BE REPRODUCED, USED, OR DISCLOSED TO OTHERS WITHOUT THE WRITTEN AUTHORIZATION OF ACSS. NOTICE FREEDOM OF INFORMATION ACT (5 USC 552) AND DISCLOSURE OF CONFIDENCE INFORMATION GENERALLY (18 USC 1905) THIS DOCUMENT IS BEING FURNISHED IN CONFIDENCE BY ACSS. THE INFORMATION DISCLOSED HEREIN FALLS WITHIN EXEMPTION (b) (4) OF 5 USC 552 AND THE PROHIBITIONS OF 18 USC 1905. Copyright 2002 ACSS. All Rights Reserved ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 1 Labels for T2CAS/APM Engineering Drawing 9000299 ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 2 LABELS FOR T2CAS/APM................................................................................................. 1 REQUIREMENTS ................................................................................................................ 3 1.1. Material:................................................................................................................................................................3 1.2. Background...........................................................................................................................................................3 1.2.1. Metallized Polyester...................................................................................................... 3 1.3. Characters and Lines ...........................................................................................................................................3 1.3.1. Black, Thermal Printed ................................................................................................. 3 1.4. Label Construction: .............................................................................................................................................3 REFERENCE DOCUMENTS ............................................................................................... 3 FIGURES: ............................................................................................................................ 4 T2CAS 6MCU Label ....................................................................................................... 4 APM Label........................................................................................................................ 5 T2CAS 4 MCU (No GPS or 115VAC) Label ............................................................... 6 Nomenclature Plate Configuration Table ......................................................................... 7 REVISION HISTORY ........................................................................................................... 8 Revision Date of Revision Description of Change .............................................................. 8 Engineering Drawing 9000299 ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 3 Requirements 1.1. MATERIAL: BRADY MATERIAL: MATTE METALLIZED POLYESTER (B-428) ADHESIVE BACKED OR EQUIVALENT. 1.2. BACKGROUND 1.2.1. METALLIZED POLYESTER 1.3. CHARACTERS AND LINES 1.3.1. BLACK, THERMAL PRINTED 1.4. LABEL CONSTRUCTION: LABELS ARE CONSTRUCTED OF COMPUTER GENERATED/COMPUTER PRINTED ADHESIVE BACKED METALLIZED POLYESTER. Reference Documents None Engineering Drawing 9000299 ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 4 Figures: T2CAS 6MCU Label Notes: Background color (Metallized Polyester) 1.2.1, Character and Line (Black) 1.3.1 Weight, Date, Inspector #, serial number, and PNR dash number all added at time of printing. Bar codes will change appearance depending on the information coded. Figure 1 Part Number 9000299-001 Engineering Drawing 9000299 ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 5 APM Label Notes: Background color (Metallized Polyester) 1.2.1, Character and Line (Black) 1.3.1 Date and serial number added at time of printing. Figure 2 Part Number 9000299-002 Engineering Drawing 9000299 ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 6 T2CAS 4 MCU (No GPS or 115VAC) Label Note: Background color (Metallized Polyester) 1.2.1, Character and Line (Black) 1.3.1 Weight, Date, Inspector #, serial number, and PNR dash number all added at time of printing. Bar codes will change appearance depending on the information coded. Figure 3 Part Number 9000299-003 Engineering Drawing 9000299 ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 7 Nomenclature Plate Configuration Table ACSS S/W Label Uses Dash Number TSO Categories TAWS S/W MOD TCAS S/W MOD 9000299-030 Reserved for Future 9000299-031 Reserved for Future 9000299-032 Reserved for Future 9000299-033 Reserved for Future 9000299-034 Reserved for Future 9000299-035 Reserved for Future 9000299-036 Reserved for Future 9000299-037 Reserved for Future 9000299-038 Reserved for Future 9000299-039 Reserved for Future 9000299-040 Reserved for Future 9000299-041 Reserved for Future 9000299-042 Reserved for Future 9000299-043 Reserved for Future 9000299-044 Reserved for Future 9000229-045 Reserved for Future 9000229-046 Reserved for Future 9000229-047 Reserved for Future 9000229-048 Reserved for Future 9000229-049 Reserved for Future Table 1 Nomenclature Plates – The software labels for field updates Engineering Drawing 9000299 ACSS Proprietary Use or dis…

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Internal and external photos are contained in FCC Compliance Report, ACC document No. 8000709-001, Rev -.

Operational descriptions are contained in FCC Compliance Report, ACC document No. 8000709-001, Rev -.

Parts List/Tune Up Info are contained in FCC Compliance Report, ACC document No. 8000709-001, Rev -.

SECURITY NOTATION SPEC NO. 8000253-001 B CAGE CODE 1WYD3 REV LTR SEE THE TITLE PAGE FOR PROPRIETARY AND DATA RIGHTS NOTATIONS. DOCUMENT TYPE Acceptance Test Specification CLASS A INITIAL RELEASE DATE 20 Nov 02 AW/CRITICAL NOTATION TITLE PAGE CR-1 SECURITY NOTATIONPAGE ENGINEERING SPECIFICATION DIVISIONDEPARTMENT NO.PRODUCT LINE NO.CONTRACT NO. TITLE ACCEPTANCE TEST PROCEDURESPECIFICATION FOR THE T2CAS TT-950/951/952 COMPUTER UNIT, PART NO. 9000000-10001, 9000000-55001, and 9000000-20001 Proprietary Notice This document and the information disclosed herein are proprietary data of Aviation Communication & Surveillance Systems, LLC. Neither this document nor the information contained herein shall be reproduced, used, or disclosed to others without the written authorization of Aviation Communication & Surveillance Systems, LLC. Notice Freedom of Information Act (5 USC 552) and Disclosure of Confidential Information Generally (18 USC 1905) This document is being furnished in confidence by Aviation Communication & Surveillance Systems, LLC. The information disclosed herein falls within exemption (b) (4) of 5 USC 552 and the prohibitions of 18 USC 1905. Copyright 2002 Aviation Communication & Surveillance Systems, LLC. All Rights Reserved. SECURITY NOTATION SPEC NO. 8000253-001 B CAGE CODE 1WYD3 REV LTR SEE THE TITLE PAGE FOR PROPRIETARY AND DATA RIGHTS NOTATIONS. Rev Ltr Test No.Operator limitsTest DescriptionWork Steps AW/CRITICAL NOTATION SUPPLEMENTS 1 SECURITY NOTATIONPAGE ENGINEERING SPECIFICATION ACCEPTANCE TEST PROCEDURE SPECIFICATION FOR THE T2CAS TT-950/951/952 COMPUTER UNIT, PART NO. 9000000-10001, -20001, -55001 1. SCOPE This acceptance test procedure specification (ATP) establishes the manufacturing and operational requirements that the T2CAS TT-950. TT-951, TT-952 Computer Unit, Part No. 9000000-10001, 9000000- 55001, and 9000000-20001 must meet to ensure that the unit is in proper operating condition. 2. REFERENCE DOCUMENTS 2.1 These documents are not required for performance of the test procedure. The purpose of listing these documents is to provide an aid for troubleshooting should any discrepancies occur during the performance of the test procedure. 9000000-10001End Item Drawing – T2CAS 6MCU 9000000-20001End Item Drawing – T2CAS 6MCU (with GPS) 9000000-55001End Item Drawing – T2CAS 4MCU 9000001-10001End Item Drawing – Aircraft Personality Module (APM) 9000027-001Outline and Installation drawing 9000024-001W 1 Harness Assembly Drawing 9000050-001W6 Cable Assy 9000038-001W7 Coax Cbl GPS-Arinc 7517941-901Power Supply/Interconnect Harness Assembly Drawing 9000005-001A1 Interconnect CCA drawing 9000010-001A1 Interconnect CCA drawing 7517923A3A1 Spectrum Filter Assembly Drawing 7517925-902A2 Processor CCA Drawing 7517925-903A2 Processor CCA Drawing 9000015-001A4 Power Supply/Modulator CCA Drawing 7517935-902A3 Transmitter Drawing 7517935-910A3/A2 Transmitter CCA Drawing 7517945-902A5 Receiver I/O CCA Drawing 7517945-903A5 Receiver I/O CCA Drawing 7517945-904A5 Receiver I/O CCA Drawing 9000020-001A7 TAWS CCA Drawing 9000025-001A8 GPS CCA Drawing IT7517900Integrated test Specification for the TCAS SECURITY NOTATION SPEC NO. 8000253-001 B CAGE CODE 1WYD3 REV LTR SEE THE TITLE PAGE FOR PROPRIETARY AND DATA RIGHTS NOTATIONS. Rev Ltr Test No.Operator limitsTest DescriptionWork Steps AW/CRITICAL NOTATION SUPPLEMENTS 2 SECURITY NOTATIONPAGE ENGINEERING SPECIFICATION EB7517987Product Test Software Release Numbers and CRCs 3. GENERAL INFORMATION 3.1 General Requirements All tests shall be performed under the following conditions: Temperature = 25+/- 5 Deg C Relative humidity = 95% maximum Pressure = between 20 and 32 in Hg 4. POWER REQUIREMENTS 4.1 115 V ac, 400 =/- 10 Hz, 200 W minimum, voltage variable from 90 to 140 V ac. 4.2 28 Vdc, 200 W minimum, voltage variable from 16 to 35 V dc. 5. TEST EQUIPMENT 5.1 TCAS 2000 MTS – Part No. T336255 Mod B • Aircraft interface unit – Part No. T336253 • RF interface unit – Part No. T335254 • PDL panel – Part No. T336259 • Tray assembly – Part No. T336255-26 5.2 T2CAS PC Test Software – Part No. 9000237 • Identified equipment is included in TCAS 2000 MTS, P/N T336255 Mod B 5.3 T2CAS TAWS Card Test Station – • TAWS Processor Test Fixture – Part No. 9000117-001 • Emulator – Wind River Vision Ice II • Power Supplies – Part No. 9000118-001 • PC – Standard PC running Windows 9x, 2000, or NT • Cables oPart No. 9000288 (APM Cable) oPart No. 9000227 (Test Discretes Cable) oPart No. 9000289 (RS232 Cable) oPart No. 9000290 (PCI Bus Test Adapter) oLATTICE Part No. pDS4102-DL2 LATTICE adapter cable (connects to parallel port on PC, other end has straight single in-line Berg pin header with pin 5 cut out for keying) SECURITY NOTATION SPEC NO. 8000253-001 B CAGE CODE 1WYD3 REV LTR SEE THE TITLE PAGE FOR PROPRIETARY AND DATA RIGHTS NOTATIONS. Rev Ltr Test No.Operator limitsTest DescriptionWork Steps AW/CRITICAL NOTATION SUPPLEMENTS 3 SECURITY NOTATIONPAGE ENGINEERING SPECIFICATION • Software oVisionCLICK Rev. 7.90A from Wind River (used to load IO_FPGA and HBIT files) oLATTICE ispVM System Software version 12.0 (used to program CPLD) 5.4 T2CAS Miscellaneous Test Equipment • ATA 8840 Extraction Tool – used to extract TAWS CCA from UUT • TAWS extender CCA – Part No. 9000070-001 • EDDIT Tool – Part No. 9000286-102 (Software used to verify T2CAS software loads) 6. TEST SETUP 6.1 Power up the MTS and allow it to warm up appropriately. Verify that test equipment used is calibrated and functioning properly. 6.2 Connect the test equipment to the UUT. Set IEEE-488 addresses as follows (in Hex): *Aircraft interface unit (A2 CCA in AIU)16 *Aircraft interface unit 2 (A4 CCA in AIU)17 *RF interface unit25 *HP 8648B signal generator19 *Cal instruments AC power supply 2001L01 *HP 8990A peak power analyzer07 *HP 6032A DC power supply05 *HP34970A Data Acquisition Switch Unit09 *HP34970A Data Acquisition Switch Unit10 *HP34970A Data Acquisition Switch Unit11 *HP34970A Data Acquisition S…

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ENGINEERING SPECIFICATION SECURITY NOTATION SPEC NO. IT7517900 CAGE CODE 55939 THIS TITLE PAGE CONTAINS PROPRIETARY AND DATA RIGHTS NOTATIONS. N REV LTR DOCUMENTTYPE INTEGRATED TEST SPECIFICATION DIVISION I DEPARTMENT NO. BCAS I 4517 PRODUCT LINE NO. 3841 CLASS INITIAL RELEASE DATE A 24 JUN 97 CONTRACT NO. TITLE INTEGRATED TEST SPECIFICATION FOR THE TCAS RT-950/951 COMPUTER UNIT, PART NO. 7517900-VAR, AND TCAS RT-952 COMPUTER UNIT, PART NO. 7517905-VAR PREPARED BY: DATE M. Smith 24 June 97 APPROVED FORSCM DATE REFAWAEB/PSAEB NO. CHECKER APPROVED BYTECHNICAL DATE MANAGER P. Bobrowitz 24 June 97 APPROVED BY ENGINEERING DEPARTMENT MANAGER DATE APPROVED FOR SQA DATE APPROVED BY: DATE PRODUCT DESIGN CHECKER (FOR REF, SPCL COGNIZANCE OF QE SUPVR (FOR REF, SPCL CONT CONT PER EPM 1-A-40) PER EPM 1-A-40) FOR PAGE INDEX, SEE PAGE CR-2. REVISION RECORD FOLLOWS PAGE INDEX. THIS IS AN ELECTRO…

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