GB8NC861AAircraft Transceiver

OPERATING MANUAL 2B-08-00 Page 1 Oct 1/97 DIGITAL AUTOMATIC FLIGHT CONTROL SYSTEMS RADIO TUNING 2B--08--10: OVERVIEW The radio function in the Planeview was developed, using the Multifunction Control Display Unit (MCDU) for the EPIC radio tuning function. The system is designed to have a radio tuning function that matched, as closely as possible, the behavior of the Honeywell Radio Management Unit (RMU) and the Rockwell Collins Radio Tuning Unit (RTU). The resulting design is described below. Throughout this document the screen images presented make minimal use of color on the display.This documentdescribes ageneric colorsetinwhichgreenis usedto indicateactive values versus whitefor normal text, whileamberandredare used to draw the crewís attention or to provide warnings. It assumed that the reader is familiar with the general characteristics of the MCDU and basic radio operations (e.g., active/preset frequency tuning, frequency spacing and formats, DME HOLD, and the unique characteristics and controls of the various types of communications and navigation radios). Information to User: The User’s Manual or Instruction Manual for an intentional or unintentional radiator shall caution the User that changes or modifications not expressly approved by the party responsible for compliance, could void the User’s authority to operate the equipment. OPERATING MANUAL 2B-08-00 Page 2 Oct 1/97 DIGITAL AUTOMATIC FLIGHT CONTROL SYSTEMS 1. MCDU Controls The radio tuning function is operated using a subset of the controls available on the MCDU, shown in Figure 27. DNEXT and PREV Function Keys-- NEXT and PREV function keys move to adjacent pages where more than one page of the same title is used DRADIOFunction Key-- The RADIO function key activates the radio tuning function and displays the RADIO 1/2 page, DTuning Knob-- The tuning knob is used to dial infrequencies orother numeric values. Figure 27 OPERATING MANUAL 2B-08-00 Page 3 Oct 1/97 DIGITAL AUTOMATIC FLIGHT CONTROL SYSTEMS 2. Page Organization The radio tuning function is accessed via the RADIO function key on the MCDU, which displays the RADIO 1/2 page. All other pages are accessed from RADIO 1/2 using the line select keys or the NEXT and PREV function keys, shown in Figure 28. Figure 28 Movement between the RADIO 1/2 and RADIO 2/2 pages is done with the NEXT and PREV function keys, while access to the COM DETAIL, TCAS/XPDR, and NAV DETAIL pages is via line select keys from RADIO 1/2 and access to the HF DETAIL, MLS DETAIL, and ADF DETAIL pages are via line select keys from RADIO 2/2. OPERATING MANUAL 2B-08-00 Page 4 Oct 1/97 DIGITAL AUTOMATIC FLIGHT CONTROL SYSTEMS 3. MCDU Tuning Description Allofthepages thatcorrespond toa particularradio type(e.g., VHFcommunications orADF) are arranged as shown in Figures 29,30, and31, andtypically consistof adetails pagealong with two memory pages. The details pages allow the specific features of each radio to be configured and provide access to the memory pages associated with each radio type. Figure 30 shows the pages associated with the VHF communications radios. Figure 29 OPERATING MANUAL 2B-08-00 Page 5 Oct 1/97 DIGITAL AUTOMATIC FLIGHT CONTROL SYSTEMS Figure 30 shows the pages associated with the VHF navigation radios. Figure 30 Figure 31 shows the pages associated with the TCAS/transponder subsystem Figure 31 OPERATING MANUAL 2B-08-00 Page 6 Oct 1/97 DIGITAL AUTOMATIC FLIGHT CONTROL SYSTEMS Figure 32 shows the arrangement of pages associated with the high--frequency (HF) communications radios. Figure 32 OPERATING MANUAL 2B-08-00 Page 7 Oct 1/97 DIGITAL AUTOMATIC FLIGHT CONTROL SYSTEMS Figure 33 shows the page associated with the automatic direction finder (ADF). Figure 33 OPERATING MANUAL 2B-08-00 Page 8 Oct 1/97 DIGITAL AUTOMATIC FLIGHT CONTROL SYSTEMS Figure 34 shows the pages associated with the Microwave Landing System (MLS) receiver. Figure 34 The RADIO MENU is used for manually tuning the radios. Pushing the RADIO key on the MCDU displays the RADIO MENU page 1/2. OPERATING MANUAL 2B-08-00 Page 9 Oct 1/97 DIGITAL AUTOMATIC FLIGHT CONTROL SYSTEMS 2B--08--20: BASIC OPERATION In keeping with the titling and numberingconventions usedby MCDU functions, eachMCDU page is arranged with a centered title at the top and a page number in the upper--right corner. Page numbers are formatted as the current page number (among those with the same page title), a slash î/î, and the number of pages with the same title. For example, there are two pages entitled îRADIO,î the first is labeled RADIO 1/2, as shown in Figure 35, and the second RADIO 2/2. The bottom line on each page displays the characters entered on the MCDU keypad and is called the scratchpad. The scratchpad is shared across all MCDU client functions,and is not under the control of the radio tuning function. The text area adjacent to each line select key (LSK) on the MCDU is referred to as a field, and identified by the LSK it is associated with. For example, the active frequency for VHF COM radio 1 (shown as COM1, 123.200) on the RADIO 1/2 page is in field 1L. Figure 35 OPERATING MANUAL 2B-08-00 Page 10 Oct 1/97 DIGITAL AUTOMATIC FLIGHT CONTROL SYSTEMS Pushing the NEXT or PREV key when this page is displayed displays the RADIO MENU page 2/2, shown in Figure 36. Figure 36 When the scratchpad is empty, pressing a line select key will either move the format cursor to the adjacent field, or perform the function indicated by the icon that appears near the key. The icons and their functions are described below. îSwapî frequencies. This symbol indicatesthat exchanges between the active and preset frequencies for the associated radio can be made. This has the effect of saving the currently active frequency in the preset memory, and tuning the radio to the frequency previously stored as the preset Page indicator. When this icon is displayed, pushing the adjacent LSK changes the display to another page. The page to be displayed is either labeled explicitly or it …

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Information to User: The User’s Manual or Instruction Manual for an intentional or unintentional radiator shall caution the User that changes or modifications not expressly approved by the party responsible for compliance, could void the User’s authority to operate the equipment.

FCC ID: GB8NC861A MFA p0240003, d0260025 Date of Report: Date of Submission: June 14, 2002 June 25, 2002 Federal Aviation Administration Spectrum Engineering Division ASR-1 800 Independence Ave. S.W. Washington, D.C. 20591 Attention: George Sakat Applicant: Honeywell Inc, Commercial Flight Systems Group FCC ID: GB8NC861A Equipment: MODEL NC-861A consisting of COM Transmitter and VOR/LOC Receiver, Glide Slope Receiver, Marker Beacon Receiver and COM Receiver FCC Rules: 87 Gentlemen: As required under FCC Rule Part 87.147(d) please consider this letter, sent on behalf of the Applicant, as notification of the filing of an application Form 731 for the certification of the referenced equipment. Attached for your records, please find: 1. copy of the FCC Application Form 731 and full Test Data Report 2. copy of the proof of electronic filing to FCC with EA# 3. copy of the covering letter to the Commission 4. copy of the Agent Authorization letter for the writer to act on behalf of the Applicant. We trust the enclosed complies with your requirements. Should you need any further clarification, kindly contact the writer. Sincerely yours, Morton Flom, P. Eng. MF/cvr enclosure(s) cc: Applicant cc: FCC via Electronic Filing cc: Industry Canada VIA CERTIFIED MAIL

The following statement will be placed in the System Description and Installation manual on page 1-4: This device complies with parts 15, of the FCC rules. Operation is subject to the following conditions [1] this device may not cause harmful interference and [2] this device must accept any interference received., including interference that may cause undesired operation.

THEORY OF OPERATION This theory of operation covers the Honeywell Models TR-866 ( ) COM, NV-875( ) NAV and the NC-861( ) NAVCOM. Theory of operation The Honeywell NC-86xx series of radios are a series of aircraft radios intended to be used as “third” or auxiliary navigation and communication radios. The NC-861B, as tested, consists of the following: 1. VHF com transceiver capable of both 25 Khz and 8.33 Khz channel spacing with an extended frequency range of 118.00 Mhz to 151.975Mhz. The nominal transmitter power is 16W. 2. The VOR/LOC section is capable of VOR and localizer reception in the range of 108.00Mhz to 117.95Mhz. 3. The Glide slope receiver section is capable of reception in the range of 328.6Mhz to 335.4Mhz. 4. The Marker section is capable of reception at 75Mhz. The specific variations are as listed in table I. Table I dash noVoice ComData COM FunctionsNAV Functions 25Khz 8.33Khz Ext Freq Mode 0 ACARS Mode A ACARS Mode 2ILS CAT II VORVDBILS Cat III -801XXXX -802XXXXX -803XXXXX -804XXXXXX -805XXXXXXX -806XXXX -811XXXXX -812*XXXXXX -813XXXXXX -814XXXXXXX -815XXXXXXXX -816XXXXXXX -821XXXXXX -822XXXXXXX -823XXXXXXX -824XXXXXXXX -825XXXXXXXXX -826XXXXXXXX *Unit tested VOR/COM receiver The Com Transceiver and the VOR receiver share a common IF amplifier. This precludes operating the Com receiver and the VOR at the same time. The received RF signal from either the VOR or Com antenna is routed through the first RF preselector and amplifier stage. The stage gain of this section is approximately 20dB. The delayed AGC is applied to these stages to enhance the clarity of the received signal and to expand the dynamic range of the receiver. The signal is then further processed in the second preselector stage. The bandwidth limits are set in the first and second preselector stages depending upon the function selected. The mixer uses high side injection, that is, the local oscillator (LO) operates above the received frequency. This is done to minimize any possible interaction with the other receivers. The LO is a Voltage Controlled Oscillator with a high and low band. The low band tunes from 129.825MHz to 151.825MHz., for received frequencies of 108.00 to 130.00MHz. The high band LO tunes from 151.825MHz to 173.800MHz for received frequencies of 130MHz to 151.975MHz. After mixing the receiver RF with the LO, the signal is further amplified in the IF portion of the receiver. The IF operates at 21.825Mhz for all received signals in this portion of the radio. AGC control is applied here to compensate for varying received signal strengths. The IF differential driver is the final IF stage. The output of this driver is applied t the Analog to digital converter and from there the signal is sent to the appropriate system for further processing. Selection of radio operating functions are controlled by way of a 429 serial data bus. VHF Com Transmitter The VHF com transmitter receives its inputs from the receiver VHF synthesizer and uses a reference frequency of 52.5MHz. The high and low VCOs have the capability to cover the entire range of 108 to 152MHz. The transmitter only operates in the range of 118.00 to 151.975MHz. Either the high or low synthesizer is selected depending upon the transmit frequency selected. The VCO is set up in a phase locked loop to stabilize the frequency sent to the RF amplifiers. The modulation is received in digitized format and translated into I and Q signals, where they are injected into the vector modulator. The modulated RF signal is sent to 2 stages of preamplifiers and a stage of final amplification where it is then routed to the VHF antenna. The pre-driver, driver and final stages all have current sense circuitry to monitor their respective current draw. These signals are used to control the biasing of each stage to keep them in a class A operation. The forward and reverse power detectors are used to monitor the integrity of the transmitted signal. Glide Slope receiver The glide slope receiver operates in the range of 328.6Mhz to 335.4Mhz. Signals form the antenna are first sent to an RF preselector and amplifier. This stage uses a single stage of RF amplification. It also uses two stages of delayed AGC to enhance the dynamic range of the receiver. The received RF signal is then sent to the mixer which uses high side injection of the LO. The IF amplifier stages operate at 75 MHz, and the LO operates at 404 to 410 MHz. The actual frequency is determined by the VOR/LOC tuning and is paired with the localizer tuning. Localizer frequencies are the odd decimal frequencies in the range of 108.10 to 112.95 MHz. (108.10, 108.1 5, 108.30, 108.35 etc.) The last stage of IF is a differential driver and the output of this stage is sent to an A/D converter for further processing. Marker receiver The marker receiver is a “0” based converter. That is it receives the 75MHz signal and does not convert it to an IF frequency. The marker receiver uses a two level sensitivity setting for proper operation at high altitude and low altitude flight operations. The signal is received from the antenna and sent through a roofing filter and then through a 75MHz crystal filter. Only one stage of AGC is used in this system. The bandwidth of the crystal filter is +/- 31KHz. From there the 75MHz signal is sent to the differential driver. The output of the driver is sent to the A/D converter for further processing.

ENGINEERING SPECIFICATION DOCUMENT TYPE ~ ' INTEGRATED TEST SPECIFICATION ..... :~ ...... ~, ~,~, ~ .... ~ Dw~S~°NAEs - BELL RD. I DEPARTMENT NO.450480 PRODUCT UN~O.3823 ~TLE NO. IT7026201 A CAGE CODE 55939 REV LTR TH~ ~TLE PAGE CONTA~S AND DATA ~GHTS N~A~ONS. ......... ~ ~ ~" ~'~ ...... ~ "~ ""~ ~:"~ ~" ~'~ ~" ~"~'~/~'~"~'~':~ ~ "~;:~ I C~SS INmAL RELEASE DATE A MAR 02 2002 CONTRACT N~ . . i 4 INTEGRATED TEST SPECIF~AT~N FOR THE VHF DATA RADIO TR-86X, PART NO 7026201 PREPARED BY: DATE M, Howk 2~6/02 APPROVED FOR SCM DATE REF AWAEBIPSAEB NO. CHECKER , ....... , ....... ...... ........... i~ ..... !~ ..... ~!~ ~:~:~ ~;~ ~ ~ :~ ...... ~/~ APPROVED BY TECH~CAL ..... DATE APPROVED BY ENGINEERING DATE MANAGER i DEPARTMENT MANAGER J. Schneider ................... 2/26/02 APPROVED FOR SQA DATE APPROVED BY: DATE ~ ........ ~ ~1 PRODUCT DESIGN CHeCKeR (FOR REF~ SPC~ ~ COGNIZANCE OFOESUPVR ~ORRE~, SPCL ~ CONT PER EPM 1-A4~ CONT PER EPM I-A~ I ......... I FOR PAGE INDEX, SEE PAGE CR-2~ REVISiONRECO~DFOL~0WS ~AGE INDEX. .... THB B AN ELECTRONIC FAC~MILE OF THEO~GINAECR~ ~NFILEWlTH~0CUMEN~CONTROL PROP~ETARYNO~CE TH~ DOCUMENT AND THE INFORMATION D~CLOSED'HERE~ ~REPROP~E~R~ DATA OF HONE~E~ INTERNATIONAL INC:NEI~ER ~OMENTNOR TREiNFORMATION i CONTAINED HER~N SHA~ BEREPRODUCE~ USE~ OR~SCLOSED TO OTHERS W~HOUT THE WRI~EN AUTHORI~ON~HONE~EL[ ~E~ONAL IN~ NONCE (18 USC 190~ THB DOCUMENT ~ BEING FU~ISHED~NFiD~CE BY ............ • AND THE PROBBmONS OF ~8 ~C~§0~ .... Copy~ght 2002 HONE~ELL ~TE~AT~NAL ~ , ,, ~R~,~ ~~ ................................................ ~ ~ ................. ;~ ................ ~;~ I'ione,, , 'ell I AW/C CAL NOTA ON SECU TY N? TATION I" TITLEPAGE I PAGECR-1 : 1510%000 (REV 970213 BCAS ASF590~ENG_SPEC.DO~ (REV 07/1~2000 OFcg7~DATA ~RVI~E~Y~NELL INTERNATIONAL ~C: SEE THE TITLE PAGE FOR PROPRIETARY AND RIGHTS NOTA~ON~ , ~ ~ ~ ~ ,,~,~ .~,~.,,~,~,~ ; ~, , ~ Rev Rev Rev Rev Rev Page Ltr Page Ltr Page Ltr Page Ltr Page Ltr Title 32 77 CR-1 A 33 A 78 34 79 Page 35 80 Index 36 81 CR-2 A 37 82 Revision 38 83 39 84 Record 40 85 CR-3 A 41 86 Ta~e of 42 87 Conten~ 43 88 i - 44 89 45 90 1 - 46 - 91 2 - 47 - 92 3 . 48 A 93 4 - 49 - 94 5 - 50 A 95 6 . 51 - 96 7 - 52 - 97 8 - 53 A 98 9 A 54 - 99 10 A 55 - 100 11 56 - 12 57 _ Append~ A A-0 13 58 - A-1 14 59 - 15 60 A Append~ B 16 61 - B-0 17 62 - B-1 18 63 - B-2 19 64 - B-3 20 65 B-4 21 A 66 B-5 22 A 67 B-6 23 68 24 A 69 Append~ C 25 A 70 C-0 26 A 71 C-1 27 72 C-2 28 A 73 A C-3 29 A 74 C-4 30 75 C-5 31 A 76 C-6 ~ ~ ~ ~ A A 0-7 - C-8 Append~ D D-0 A D-1 A D-2 A D-3 A D-4 A D-5 A D-6 A D-7 A D-8 A TOTAL PAGES: 131 A A A - A A • ~[i; ~ ,~- ~ .... ~ ~ 15102-000 (REV 970213 BCAS ASF~0~ENG_SPE~DO~ (NEW ~OFC~ATA SERVICE~ HONEYWELL INTERNATIONAL ~ -~ CR-2 PAGE SECU~TY NOTA~ON SPEC ENGINEERING SPECIFICATION NO. ~7026201 CAGE CODE 55939 SEE mE ~E PAGE FOR PROP~ETARYAND DATA ~G~S NOTA~ON~ A REV LTR ....... ~ ~ ~" ........... I REV LTR PAGE A SEE PAGE INDEX SHEET CR~ C.O. 200200797A (NA) DESCRIPTION DATE AND APPROVAL 0~'~~ ~ ~P~ ~ Hone ell 5200-018 (REV 970213 BCAS ASF5900/ENG_SPEC.DOT AWlC~CAL NOTA~ON I REVISION RECORDS SECU~TY NOTA~ON I = ~EW I~OF~DATA SER~CES, HONEYWE~ INTERNATION~ INC. CR-3 PAGE SECURITY NOTATIONSPEC NO. IT7026201 SEE PAGE INDEX FOR THIS SHEET REV LETTER CAGE CODE 55939 REV LTR SEE THE TITLE PAGE FOR PROPRIETARY AND DATA RIGHTS NOTATIONS. REV LTR AW/CRITICAL NOTATION TABLE OF CONTENTS i SECURITY NOTATIONPAGE 5200-032 (REV 970213 BCAS ASF5900/ENG_SPEC.DOT) (NEW 1/1/99-OFC97-DATA SERVICES) HONEYWELL INTERNATIONAL INC. ENGINEERING SPECIFICATION TABLE OF CONTENTS TitlePage 1.SCOPE ...................................................................................................................1 2.REFERENCE DOCUMENTS....................................................................................1 2.1ASSEMBLY PRINTS................................................................................................................... 1 2.2B LOCK AND SIGNAL BLOCK DIAGRAMS....................................................................................... 2 2.3P RODUCT SPECIFICATION.......................................................................................................... 7 2.4G OVERNING DOCUMENTS.......................................................................................................... 7 3.GENERAL INFORMATION ......................................................................................8 4.POWER REQUIREMENTS .................................................................................... 10 5.TEST EQUIPMENT OR EQUIVALENT ................................................................... 10 5.1ALTERNATE TEST EQUIPMENT.................................................................................................. 10 5.2T EST SOFTWARE.................................................................................................................... 10 6.TEST SETUP ........................................................................................................ 11 6.1INITIAL SETUP....................................................................................................................... 11 6.2T EST SETUP #1 ..................................................................................................................... 12 6.3TEST SETUP #2 ..................................................................................................................... 12 6.4T EST SETUP # 3 .................................................................................................................... 12 7.TEST REQUIREMENTS ........................................................................................ 17 APPENDIX A CALIBRATION TR-86X............................................................................. A-0 APPENDIX B CALIBRATION TR-86X............................................................................. B-0 APPENDIX C QUALITY CONTROL FUNCTIONAL TEST REPORT................…

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ENGINEERING SPECIFICATION SECURITY NOTATION SPEC NO. IT7026202 CAGE CODE 55939 XC REV LTR THIS TITLE PAGE CONTAINS PROPRIETARY AND DATA RIGHTS NOTATIONS. DOCUMENT TYPE INTEGRATED TEST SPECIFICATION DIVISION DEPARTMENT NO. AES - BELL RD. 450480 PRODUCTLINENO. 3855 CLASS il ,.,T, AL RELEASE DATE A MAR 01 2002 CONTRACT NO. TITLE INTEGRATED TEST SPECIFICATION FOR THE NV-875 VOR/ILS DATA LINK (VIDL), PART NO. 7026202 PREPARED BY: DATE T. Sisco/R. Paulsen 3/1/02 APPROVED FOR SCM DATE REF AWAEB/PSAEB NO. I CHECKER APPROVED BYSECTIONHEAD DATE J. Schneider 3/1/02 APPROVED FOR SQA DATE PRODUCT DESIGN CHECKER (FOR REF, SPCL CONT PER EPM 1-A-40) APPROVED BY ENGINEERING DEPARTMENT MANAGER DATE APPROVED BY: DATE COGNIZANCE OF QE SUPVR (FOR REF, SPCL CONT PER EPM 1-A-40) FOR PAGE INDEX, SEE PAGE CR*2. REVISION RECORD FOLLOWS PAGE INDEX. THIS IS AN ELECTRONIC FACSIMILE OF THE CR-1 ON FILE WITH DOCUMENT CONTROL PROPRIETARY NOTICE THIS DOCUMENT AND THE INFORMATION DISCLOSED HEREIN ARE PROPRIETARY DATA OF HONEYWELL INC. NEITHER THIS DOCUMENT NOR THE INFORMATION CONTAINED HEREIN SHALL BE REPRODUCED, USED, OR DISCLOSED TO OTHERS WITHOUT THE WRITTEN AUTHORIZATION OF HONEYWELL INC 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 HONEYWELL INC, THE INFORMATION DISCLOSED HEREIN FALLS WITHIN EXEMPTION (b) (4)OF5 USC 552 AND THE PROHIBITIONS OF 18 USC 1905. Copyright 1999 Honeywell Inc. All Rights Reserved AW/CRITICAL NOTATION Hone vell SECURITY NOTATION 15101-0o0 (REV 970213 BCAS ASF5900/ENG_SPEC.DOT) (REV 07/18/2000 :OFC97LDATA SERVICES) HONEYWELL INTERNATIONAL INC. CR-1 PAGE ENGINEERING SPECIFICATION SECURITY NOTATION SPEC NO. IT7026202 CAGE CODE 55939 SEE THE TITLE PAGE FOR PROPRIETARY AND DATA RIGHTS NOTATIONS. THE LATEST REVISION OF EACH SHEET IS INDICATED ON THE PAGE INDEX. XC REV LTR Rev Rev Rev Rev Page Ltr Page Ltr Page Ltr Page Ltr Page Rev Ltr Title 26 XB 67 XC CR-1 XC 27 XB 68 XC 28 XB 69 XB Page 29 XB Index 30 XB Appendix A CR-2 XC 31 XB A-0 XB 32 XB A-1 XC Revision 33 XB A-2 XB Record 34 XB A-3 XB CR-3 XC 35 XB A-4 XB 36 XC Table of 37 XB Appendix B Contents 38 XB B-0 XB i XB 39 XB B-1 XB ii XB 40 XB B-2 XB 41 XB B-3 XC 1 XB 42 XB B-4 XC 2 XB 43 XB B-5 XB 3 XB 44 XB B-6 XB 4 XB 45 XB B-7 XB 5 XB 46 XB B-8 XB 6 XC 47 XB B-9 XB 7 XB 48 XB B-10 XB 8 XB 49 XB B-11 XB 9 XB 50 XB B-12 XB 10 XB 51 XB B-13 XB 11 XB 52 XB B-14 XB 12 XB 53 XB B-15 XB 13 XB 54 XB B-16 XB 14 XB 55 XB B-17 XB 15 XB 56 XB B-18 XB 16 XB 57 XB B-19 XB 17 XB 58 XB B-20 XB 18 XB 59 XB B-21 XB 19 XB 60 XB B-22 XB 20 XB 61 XB B-23 XB 21 XB 62 XB B-24 XB 22 XB 63 XB B-25 XB 23 XB 64 XB B-26 XB 24 XB 65 XB B-27 XB 25 XB 66 XC Appendix C C-0 XB C-1 XB C-2 XB C-3 XB Appendix D D-0 XB D-1 XB D-2 XB D-3 XB D-4 XB D-5 XB TOTAL PAGES: 117 I AW/CRITICAL NOTATION Hone3 'ell ,.o x SECURITY NOTATION 1510%000 (REV 9702"~3 BCAS ASF59001ENG_SPEC.DOT~, (REV 071~812000 -OFCgT-:DATA SERVICES) HONEYWELL INTERNATIONAL INC. CR-2 PAGE ENGINEERING SPECIFICATION SECURITY NOTATION SPEC NO. IT7026202 CAGE CODE 55939 XC REV LTR SEE THE TITLE PAGE FOR PROPRIETARY AND DATA RIGHTS NOTATIONS. REV PAGE DESCRIPTION DATE AND APPROVAL LTR XB SEE PAGE INDEX SHEET CR-2 XC SEE PAGE INDEX SHEET CR-2 C.O. 200200821A (NA) VARIOUS CHANGES THRU-OUT DOC. R. Paulsen ,~ 3/22/02 y ~/~ o~ AW/CRITICAL NOTATION Hone 'ell I .EVlS,O.. co.os SECURITY NOTATION 15101-000 (REV 970213 BCAS ASF5900/ENG_SPEC.DOT) (REV 07/1812000 -OFC97-DATA SERVICES) HONEYWELL INTERNATIONAL INC. CR-3 PAGE SECURITY NOTATIONSPEC NO. IT7026202 SEE PAGE INDEX FOR THIS SHEET REV LETTER CAGE CODE 55939 REV LTR SEE THE TITLE PAGE FOR PROPRIETARY AND DATA RIGHTS NOTATIONS. REV LTR XB AW/CRITICAL NOTATION TABLE OF CONTENTS i SECURITY NOTATIONPAGE 15101-000 (REV 970213 BCAS ASF5900/ENG_SPEC.DOT) (REV 07/18/2000 -OFC97-DATA SERVICES) HONEYWELL INTERNATIONAL INC. ENGINEERING SPECIFICATION Table of Contents TitlePage 1.SCOPE.....................................................................................................................1 2.R EFERENCE DOCUMENTS...........................................................................................1 3.G ENERAL INFORMATION.............................................................................................3 4.P OWER AND SIGNAL REQUIREMENTS.........................................................................5 5.T EST WIRING CONNECTIONS AND BLOCK DIAGRAMS....................................................8 6.T EST SETUP........................................................................................................... 16 7.T EST REQUIREMENTS.............................................................................................. 18 8.T EST SPECIFICATION/PROCEDURE DEFINITIONS......................................................... 19 A PPENDICES APPENDIX ASOFTWARE LOADING PROCEDURE..........................................................A-0 A PPENDIX BCALIBRATION PROCEDURE.....................................................................B-0 A PPENDIX CQUALITY CONTROL FUNCTIONAL TEST REPORT.......................................C-0 A PPENDIX DIT7026202-801 TO IT7510134-855 CROSS REFERENCE...........................D-0 SECURITY NOTATIONSPEC NO. IT7026202 SEE PAGE INDEX FOR THIS SHEET REV LETTER CAGE CODE 55939 REV LTR SEE THE TITLE PAGE FOR PROPRIETARY AND DATA RIGHTS NOTATIONS. REV LTR XB TABLE OF CONTENTS (cont) TitlePage AW/CRITICAL NOTATION TABLE OF CONTENTS ii SECURITY NOTATIONPAGE 15101-000 (REV 970213 BCAS ASF5900/ENG_SPEC.DOT) (REV 07/18/2000 -OFC97-DATA SERVICES) HONEYWELL INTERNATIONAL INC. ENGINEERING SPECIFICATION TEST NO. 1.0POWER UP......................................................................................................................................20 2.0PILOT ACTIVATED SELF TEST (PAST) .......................................................................................21 3.0BENCH PAGE, SOFTWARE VERSION …

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ENGINEERING SPECIFICATION DOCUMENT TYPE DIVISION AES - BELL RD. ENGINEERING BULLETIN SECURITY NOTATION SPEC NO. IT7026236 XA CAGE CODE 55939 REV LTR THIS TITLE PAGE CONTAINS PROPRIETARY AND DATA RIGHTS NOTATIONS, r 'CLASS I INITIAL RELEASE DATE DEPARTMENT NO. PRODUCT LINE NO. 450480 3829 A l APR 0 5 2002 CONTRACT NO. TITLE INTEGRATED TEST SPECIFICATION FOR TRANSMITTER CCA 7026236:90× ! L. Ro 'gu , B. Brettner /~t.._~)~o~, , APPROVED FOR SCM DATE APPROVED FOR SQA ,DATE APPROVED BY: DATE I ' , I REF AWAEB/PSAEB NO.I CHECKER PRODUCT DESIGN CHECKER (FOR REF, SPCL COGNIZANCE OFQE SUPVR (FOR REF, SPCL I CONT PER EPM 1oA-40) CONT PER EPM 1-A'40) i EB7026149 I ' .I FOR PAGE INDEX. SEE PAGE CR'2. REVISION RECORD FOLL0WS'P~E]'ND'EX. ...................... PROPRIETARY NOTICE THIS DOCUMENT AND THE INFORMATION DISCLOSED HEREIN ARE PROPRIETARY DATA OF HONEYWELL INTERNATIONAL INC. NEITHER THIS DOCUMENT NOR THE iNFORMATiON CONTAINED HEREIN SHALL BE REPRODUCED, USED, OR DISCLOSED TO OTRERS WITHOUT THE WRITTEN AUTHOR ZAT ON OF HONE~ELL INTERNATIONAL iNCl ......... NOTICE FREEDOM OF INFORMATION ACT (5 USC 552) AND DISCLOSURE OF CONFIDENCE' INFORMATION GENE~LLY (18 USC 1905) THIS DOCUMENT IS BEING FURNISHED IN CONFIDENCE BY HONEYWELL INTERNATIONAL INC. THE INFORMATION DISCLOSED HEREIN FALLS WITHIN EXEMPTION (b) (4) OF 5 USC 552 AND THE PROHIBITIONS OF 18USC !905, .......... Copyright 2002 HONEYWELL INTERNATIONAL INC. AW/CRITICAL NOTATION Honeywell SECURITY NOTATION PAGE 15101-000 (REV 970213 BCAS ASF5900/ENG SPEC.DOT) (REV 07/1812000 OFC97-:DATA SERV]CES~RONE~'WEEL INrEP, N,~TiC}N',~L [NC. .......... SECURITY NOTATION ( 'SPEC .... ........... ' .... I I NO- IT7026236 XA ENGINEERING CAaE SPECIFICATION I CODE SS939 REV,TR , SEE THE TITLE PAGE FOR PROPRIETARY AND DATA RIGHTS NOTATIONSI THE LATEST REVISION OF EACH SHEET IS INDICATED ON THE PA~E iNDEX; ......................... Rev Rev Rev Rev Rev Page Ltr Page Ltr Page Ltr Page Ltr Page Ltr Title CR-1 XA Page Index OR-2 XA Revision Record OR-3 XA Table of Contents i XA ii XA 1 XA 2 XA 3 XA 4 XA 5 XA 6 XA 7 XA 8 XA 9 XA 10 XA 11 XA 12 XA 13 XA 14 XA 15 XA 16 XA 17 XA 18 XA 19 XA 2O XA 21 XA 22 XA 23 XA 24 XA 25 XA 26 XA APPENDIX A A-0 XA A-1 XA A-2 XA A-3 XA A-4 XA APPENDIX B B-0 XA B-1 XA B-2 XA B-3 XA TOTAL PAGES 40 ,, ,,, , ,,, ,,, , , : .... ,.:,, ,, ,, • , , I AW/CRITICAL NOTATION HOIIll PAGE INDEX ca-2 SECURITY NOTATION PAGE 15"102-000 (REV 970213 BCA$ ASF5900/ENG SPEC.DOT) (NEW l/l/99-OFC97-OATA SERVICES) HONEYWELL INTERN~Ti~NAL'IN~ .................. ENGINEERING SPECIFICATION .... • ~• i ̧ - ....... •i" •; ~ ~ •~ •'• • ..... ........ ~ ..... ~ ~• Y'i Y•• ̧ ̧' ~: ..... •• •~ ̧ ̧ ̧ ̧ SECURITY NOTATION SPEC l NO. IT7026236 XA CAGE CODE 55939 REVLTR SEE THE TITLE PAGE FOR PROPRIET~RYAND~DAT~RIGRTS~NO~A~t'ONS. ..................... i ...... .,, • , , ,,, ~,, , REV ' LTR ! PAGE DESCRIPTION ~,, , , , AWIC RITICAL NOTATION Honeywell SECURITY NOTATION DATE AND APPROVAL REVISION RECORDS CR-3 PAGE 5200-018 (REV 970213 BCAS ASF5g00/ENG_SPEC.DOT) (NEW ltl/99-OFC97LDATA SERVICES) HON~EY~E[[ iN"I'E~NATi(]~/~.[ ii,~(~ SECURITY NOTATIONSPEC NO. IT7026236 SEE PAGE INDEX FOR THIS SHEET REV LETTER CAGE CODE 55939 REV LTR SEE THE TITLE PAGE FOR PROPRIETARY AND DATA RIGHTS NOTATIONS. REV LTR AW/CRITICAL NOTATION TABLE OF CONTENTS i SECURITY NOTATIONPAGE 5200-032 (REV 970213 BCAS ASF5900/ENG_SPEC.DOT) (NEW 1/1/99-OFC97-DATA SERVICES) HONEYWELL INTERNATIONAL INC. ENGINEERING SPECIFICATION TABLE OF CONTENTS TitlePage 1.SCOPE...................................................................................................................................1 2.REFERENCE DOCUMENTS......................................................................................................1 3.GENERAL INFORMATION........................................................................................................2 3.1STANDARD TESTING ENVIRONMENT...............................................................................2 3.2TEMPERATURE EXTREMES............................................................................................2 3.3BURN-IN.....................................................................................................................2 3.4LOW SPEED CONTROL BUS OVERVIEW..........................................................................2 4.POWER AND SIGNAL REQUIREMENTS...................................................................................4 5.RECOMMENDED TEST EQUIPMENT (OR EQUIVALENT)..........................................................4 6.TEST SETUP...........................................................................................…

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