P8CTT-951TCAS

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 Page RR--1 RECORD OF REVISIONS For each revision, put the revised pages in your manual and discard the superseded pages.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--…

Text truncated - open the document above for the full version.

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…

Text truncated - open the document above for the full version.

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.

T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 15 Figure 16 View of A7 TAWS Processor With Bracket Attached Figure 3: Unit Front Name Plate T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 16 Figure 4: Unit Front With Name Plate Showing T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 17 Figure 5: Unit Rear With ARINC Connector

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…

Text truncated - open the document above for the full version.

T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 15 Figure 3: Unit Front Name Plate

T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 18 Figure 6: View of Unit Side With A7 TAWS Processor Showing T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 19 Figure 7: View of Unit Side, A7 TAWS Removed, A2 Processor Assembly Showing T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 20 Figure 8: View of Unit Side, Showing A5 Receiver - I/O Assembly with Shield T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 21 Figure 9: View of Unit Side With A5 Receiver Hinged Outward, Showing A4 Power Supply/Modulator Assembly T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 22 Figure 10: View of Unit Side with A2 Processor Removed Showing A3 Transmitter Assembly With Cover T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 23 Figure 11: View of Unit Side, A5 Receiver and Front Panel Removed, Showing A4 Power Supply/Modulator Assembly T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 24 Figure 12: View of Unit Side, A4 Power Supply/Modulator Assembly Removed, Showing A1 Interconnect Assembly T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 25 Figure 13: View of A3 Transmitter Assembly With Shield Removed T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 26 Figure 14: View of A5 Receiver – I/O Assembly with Shield Removed. Side A T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 27 Figure 15: View of A5 Receiver – I/O Assembly with Cover Removed. Side B T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 28 Figure 16: View of A7 TAWS Processor With Bracket Attached

T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 5 3 GENERAL INFORMATION 3.1 TYPE DESIGNATION The equipment has been designated by ACSS as models TT-95x T 2 CAS Computer Units, P/Ns 9000000-20001 (TT-952), 9000000-55001 (TT-951), 9000000-1001 (TT-950). 3.2 SERVICE AND RULE FOR INTENDED OPERATION Air Traffic Control Part 87, Subpart A 3.3 DESCRIPTION OF EQUIPMENT 3.3.1 TAWS/Windshear Functionality The TAWS/Windshear function is implemented as an independent processor and I/O circuitry from the TCAS function. The TAWS/Windshear circuitry is contained on a unique circuit card assembly (CCA), which is added to the existing TCAS-2000 unit design in a spare card slot The TAWS function uses vertical speed, ground speed, track angle, flight path angle, latitude, longitude, flap status, steep approach status, static air temperature, roll angle, pressure altitude system inputs. A database, which includes terrain data, airport data, aircraft performance data and climb rate models, is used for the determination of the alerts and display of terrain information. The TAWS/Windshear CCA will also provide a reactive windshear alert which meets the requirements of TSO-C117a. The windshear alert is active during take-off and final approach phases and produces aural and visual annunciations. The windshear alert measures vertical and horizontal components of air mass accelerations and determines if a windshear caution or warning should be generated. Windshear alert is not yet implemented; however, all current circuitry and processor will be utilized. 3.3.2 TCAS Functionality 3.3.2.1 Type of Emission 18MOP1D 3.3.2.2 Frequency Range 1030 + 0.01 MHz T 2 CAS FCC Compliance Test Report SPEC NO: CAGE CODE: 8000709-001 1WYD3 REV LTR - ACSS Proprietary Use or disclosure of the information on this sheet is subject to the proprietary notice on the title page. Page 6 3.3.2.3 Power Rating 0.4 to 500 Watts Peak Effective Radiated Power (Pulsed) 3.3.2.4 Final Power Amplifier Solid State Balanced Amplifier (Class C) using two Motorola MRF10501 silicon bipolar transistors. 3.3.2.5 Active Device Functions Function Device Type Manufacturer Oscillator Temperature Compensated Crystal Oscillator (TCXO) 6206 Oscillatek Microwave Low Noise Transistor--Amplifier AT-41511 HP Transmitter Monolithic Amplifier VNA – 25 Mini-Circuit .1 Watt, Microwave Pulse Power Function Device Type Manufacturer Transmitter Transistor--Amplifier, MRF1000MB Motorola 1 watt Microwave Pulse Power Transistor--Amplifier, MRF10005 Motorola 5 watt Microwave Pulse Power Transistor--Amplifier, MRF10031 Motorola 30 watt Microwave Pulse Power Transistor--Amplifier, MRF10120 Motorola 150 watt Microwave Pulse Power Transistor--Amplifier, MRF10502 (2 ea) Motorola 500 watt Pulse Modulator N Channel FET IRFR220 Motorola Modulator N Channel F…

Text truncated - open the document above for the full version.