GB8HS-600Inmarsat Aircraft Telecommunications Systems

This document contains technical data and is subject to U.S. export regulations. These commodities, technology, or software were exported from the United States in accordance with the export administration regulations. Diversion contrary to U.S. law is prohibited. Honeywell Aerospace Electronic Systems CES--Phoenix P.O. Box 21111 Phoenix, Arizona 85036-1111 U.S.A. Printed in U.S.A. Pub. No. A15--5111--006 23--20--31 Title Page T--1 30 May 2002 System Description and Installation Manual HS--600 High Speed Data System SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System PROPRIETARY NOTICE This document and the information disclosed herein are proprietary data of Honeywell. Neither this document nor the information contained herein shall be used, reproduced, or disclosed to others without the written authorization of Honeywell, 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 Honeywell. The information disclosed herein fall within exemption (b) (4) of 5 USC 552 and the prohibitions of 18 USC 1905. S2002 Honeywell is a U.S. registered trademark of Honeywell. All other marks are owned by their respective companies. Copyright 2002 Honeywell All Rights Reserved 23--20--31 Title Page T--2 30 May 2002 Please cut along the dotted line. Please cut along the dotted line. REPORT OF POSSIBLE DATA ERROR FOR HONEYWELL USE ONLY CONTROL NO. DATE RECEIVED Please mail or FAX completed form to Technical Publications Quality Administrator. If returning by mail, please tape this form closed (U.S. postal regulations prohibit the use of staples). If sending by FAX, the Technical Publicationsí U.S. FAX No. is (602 - 436 - 3900). If sending by email, the email address is [email protected]. Local reproduction of this form is encouraged.This form is based on electronic form INF--300, Revision 0 To help us improve the quality of our publication, Honeywell encourages any report of a possible data error. PUBLICATION INFORMATION Publication Number A15--5111--006 Volume No. (Book, or Addendum) ATA Number 23--20--31 Latest Issue Date From Title Page Publication Title High Speed Data Unit Document Type System Description and Installation Manual READER INFORMATION Please check all that apply: hTrainerhTechnicianhLibrarianhEngineerhOther(Please specify) Your Name (optional)Company Name Street Address City, State (Province), Zip Code, Country Telephone No.FAX No. POSSIBLE DATA ERROR Page No. Paragraph Figure No.Table No.Description of Possible Data Error HONEYWELL REPLY DO NOT STAPLE DO NOT STAPLE BUSINESS REPLY MAIL FIRST CLASS PERMIT NO. 3532, PHOENIX, AZ FOLD FOLD POSTAGE WILL BE PAID BY ADDRESSEE Honeywell Aerospace Electronic Systems CES--Phoenix P.O. Box 21111 Phoenix, Arizona 85036-1111 U.S.A. ATTN: Technical Publications Quality Administrator NO POSTAGE NECESSARY IF MAILED IN THE UNITED STATES Please cut along the dotted line. Please cut along the dotted line. CUSTOMER RESPONSE FOR HONEYWELL USE ONLY CONTROL NO. DATE RECEIVED Please mail or FAX completed form to Technical Publications Quality Administrator. If returning by mail, please tape closed (U.S. postal regulations prohibit the use of staples). If sending by FAX, the Technical Publicationsí U.S. FAX No. is (602 - 436 - 3900). If sending by email, the email address is [email protected]. Local reproduction of this form is encouraged. To help us improve the quality of our publications, Honeywell encourages readers to provide input to the customer--satisfaction survey below. We welcome all comments and recommendations. PUBLICATION INFORMATION Publication Number A15--5111--006 Volume No. (Book, or Addendum) ATA Number 23--20--31 Latest Issue Date From Title Page Publication Title High Speed Data Unit Document Type System Description and Installation Manual READER INFORMATION Please check all that apply: hTrainerhTechnicianhLibrarianhEngineerhOther(Please specify) Your Name (optional)Company Name StreetAddress City,State(Province), StreetAddress City,State(Province), Zip Code, Country Telephone No.FAX No. CUSTOMER--SATISFACTION SURVEY Please check the yes or no box to answer the following questions:YesNo 1. Is the Publication technically accurate? jj 2. Is information easy to find? jj 3. Is information complete? jj 4. Are figures easy to use? jj 5. Are tables easy to use jj 6. Is the Publication used for training? jj 7. Do you or your organization wish to remain on distribution for this publication? jj Please rate this publication in comparison to other documents you use. GoodFairPoor jjj Please provide comments, recommendations and/or improvements that you would like to see in this publication. DO NOT STAPLE DO NOT STAPLE BUSINESS REPLY MAIL FIRST CLASS PERMIT NO. 3532, PHOENIX, AZ FOLD FOLD POSTAGE WILL BE PAID BY ADDRESSEE Honeywell Aerospace Electronic Systems CES--Phoenix P.O. Box 21111 Phoenix, Arizona 85036-1111 U.S.A. ATTN: Technical Publications Quality Administrator NO POSTAGE NECESSARY IF MAILED IN THE UNITED STATES SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 23--20--3130 May 2002 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 H shows Honeywell is the incorporator. Revision Number Revision Date Date Put In Manual By Revision Number Revision Date Date Put In Manual By SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 23--20--3130 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary n…

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Honeywell Sales Bulletin 02-07o – Honeywell/Thales Swift64 SATCOM System HS-600 Page 3 of 5 1.3 HP-600 High Power Amplifier (HPA) The 40 W HPA is identical to the unit already in use with the existing MCS system. It is an 8 MCU LRU that will be dedicated for exclusive use with the HSU. 1.4 RF Combiner and Splitter These devices facilitate the ability of the HSU and HPA to share the HGA with the existing MCS system. The RF Combiner attributes are: • Size ¾ 3.53” (89.66mm) height ¾ 5.04” (128.02 mm) width ¾ 10.91” (277.11mm) length • Weight: < 5 pounds (2.27 kg) The Splitter attributes are: • Size ¾ 1.00” (25.40mm) height ¾ 1.75” (44.45 mm) width ¾ 2.00” (50.80mm) length • Weight: < 1 pound (0.45 kg) 1.5 System Block Diagram COMBINER (High Power) D/LNA HGA SD700 SDU (6 MCU) HP600 40W HPA (8 MCU) HS600 Swift64 ( 4 MCU) RF RF RF RF RF RF HP600 40W HPA (8 MCU) RF Splitter R232

FCC ID: GB8HS-600 MFA p0240002, d0250043 Date: May 16, 2002 Federal Aviation Administration Spectrum Engineering Division ASR-1 800 Independence Ave. S.W. Washington, D.C. 20591 Attention: George Sakat Applicant: Honeywell International Inc. Commercial Electronic Systems Inc. – Phoenix Equipment: HS-600 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. 5. LIST OF INFORMATION as requested by you, duly completed 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

> -----Original Message----- > From: Bailey, Peter (AZ77) > Sent: Thursday, August 01, 2002 1:41 PM > To: Dosdall, Charlie (AZ77) > Subject: RE: [Fwd: 16-QAM]FCC ID; GB8HS-600 EA23544 > > Charlie, > > In the designation 38K0D1W, 38K0 identifies the occupied bandwidth as 38.0 > kHz (the position of the K denotes the decimal point); D identifies the > modulation type; 1 indicates that a single channel is involved; W > identifies the type of information to be transmitted (in our case a > combination of stuff like data, telephony, etc.). > > When trying to determine the correct emissions designation for HS-600, I > was unable to find anything in part 87 that pertained directly to 16QAM. > The table in 87.137, for instance, which does contain the designations for > AES equipment, does not mention Quadrature/Amplitude Modulation. However, > in part 2, para. 2.201 which assigns the letter designation for the > modulation type, the letter "D" is used for an "Emission in which the main > carrier is amplitude and angle-modulated either simultaneously or in a > pre-established sequence." This seemed to apply pretty well. Changing > the modulation type to G, which is phase modulation, is not entirely > accurate. > > Pete

With regard to the FCC concerns over the Swift64 Aero HSD service with respect to Part 87 of the FCC Regulations, as these apply to the airborne equipment (i.e., the HS-600 system) providing this service, the following can be said: Inmarsat has filed the appropriate Swift 64 Aero HSD technical parameters with the ITU, which include the following items: Class of Emission Emission Designator Authorized Bandwidth G1D 5K60G1D 25 kHz D1D 40K0D1D 45 kHz D1E 40K0D1E 45 kHz D1W 40K0D1W 45 kHz Figure 11 of Version 1.2 (CN3) to the Inmarsat Min-M SDM is included (with Inmarsat’s permission) to provide additional information regarding the spectral content of the Aero HSD signal. The adjacent channel interference developed by the Swift64 service (as realized in the HS-600 system) complies with the relevant ITU recommendations, which were developed in consultation with other users of this spectrum. The Swift64 Aero HSD service and its maritime equivalent (Fleet77) are already approved and commercially available from Telenor; specifically, the Swift64 Aero HSD service is available through Telenor’s GESs at Southbury, CT; Santa Paula, CA; and Kuantan, Malaysia. If there are any further questions, please do not hesitate to ask.

Glocom Corporation Proprietary This document is proprietary to Glocom Corporation. Use or disclosure of this document or the information contained herein, for any purpose other than internal division use, is not permitted without prior authorization of Glocom Corporation. DOCUMENT: GL1.201.032-0-001-HRD REVISION: 2.0 PROGRAM: GCM-P46 DATE: April 17, 2002 GLOCOMGLOCOM Aero-M4 MES Development Program Core Aero-M4 MTU Radio Module Hardware Specification Issue 2.0 Glocom Corporation Suite 300, 20010 Century Boulevard Germantown, MD 20874 Core Aero-M4 MTU Radio Module Hardware Specification GL1.201.032-0-001-HRD Rev 2.0 April 17, 2002 GLOCOM CORPORATION Page 2 The use or disclosure of this information is subject to the restrictions on the title page. Revision History Design Document Name: Core Aero-M4 MTU Radio Module Hardware Specification Revision Description Approval Date DRAFT Requirements Issue 1.0 G.E. Hosimer May 8, 2000 1.0 Block diagram updated, Tables added. (Minheng Shan) G.E. Hosimer September 11, 2000 1.1 Pre-CDR reconciliation with schematics G.E. Hosimer October 17, 2000 1.2 Updated after Internal CDR G.E. Hosimer December 8, 2000 1.3 a) Change document number; From: GL1.201.032.002-HRD To: GL1.201.032-0-001-HRD b) Correct design document references in Section 1.4. c) Resolve various TBD's, TBR's, and TBA's throughout the body of the text. G.E. Hosimer Minheng Shan February 20, 2001 2.0 Update design detail information for FCC G.E. Hosimer April 17, 2002 Document Attributes: File Name: HRD - RM 2.0 File Size: 955904 bytes Core Aero-M4 MTU Radio Module Hardware Specification GL1.201.032-0-001-HRD Rev 2.0 April 17, 2002 GLOCOM CORPORATION Page 3 The use or disclosure of this information is subject to the restrictions on the title page. Table of Contents 1 INTRODUCTION..................................................................................................................................................................................6 1.1 PURPOSE...........................................................................................................................................................................................6 1.2 SCOPE...............................................................................................................................................................................................6 1.3 CONFORMANCE...............................................................................................................................................................................6 1.4 REFERENCES....................................................................................................................................................................................6 1.5 DEFINITIONS OF TERMS AND ACRONYMS...................................................................................................................................8 2 OVERVIEW.........................................................................................................................................................................................10 2.1 RADIO MODULE DESCRIPTION....................................................................................................................................................10 2.1.1 General Architecture.............................................................................................................................................................10 2.1.1.1 RF Section.....................................................................................................................................................................10 2.1.1.2 IF Section.......................................................................................................................................................................11 2.2 DESIGN CHANGES.........................................................................................................................................................................12 3 FUNCTIONAL REQUIREMENTS...............................................................................................................................................13 3.1 AERO M4 REQUIREMENTS..........................................................................................................................................................14 3.2 HARDWARE REQUIREMENTS.......................................................................................................................................................14 3.2.1 Transmitter Description........................................................................................................................................................15 3.2.1.1 TX RF Section..............................................................................................................................................................15 3.2.1.1.1 TX Power Sensor....................................................................................................................................................15 3.2.1.1.2 TX Power Amplifier...............................................................................................................................................15 3.2.1.1.3 TX RF Filter............................................................................................................................................................15 3.2.1.1.4 TX RF Switch..........................................................................................................................................................16 3.2.1.1.5 TX Variable Gain Amplifier.................................................................................................................................16 3.2.1.1.6 TX RF Amplifier...............................................................................................................................…

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DOCUMENT: TN1.201.032-1-005 REVISION: 2.0 PROJECT: P46 DATE: April 17, 2002 Technical Note Glocom Corporation Suite 300, 20010 Century BLVD Germantown MD 20874 GLOCOM CORPORATION PROPRIETARY AND CONFIDENCIAL This document is proprietary and confidencial to GLOCOM COPRPORATION. Use of this document or disclosure of any information contained herein, for any purpose other than internal division use, is not permitted without prior written consent of GLOCOM CORPORATION. GLOCOM Aero-M4 MTU ISE Power Control Requirements TABLE OF CONTENTS 1 INTRODUCTION........................................................................................................................................................................................3 2 GENERAL REQUIREMENTS....................................................................................................................................................................3 3 INITIAL SETUP...........................................................................................................................................................................................3 4 INITIALIZATION AND SYSTEM CALIBRATION..............................................................................................................................6 5 SYSTEM CALIBRATION PROCEDURE...............................................................................................................................................6 5.1 ECONOMY MODE FLAG.....................................................................................................................................................................9 6 TRANSMISSION MODES AND MTU TX OUTPUT POWER...........................................................................................................9 7 TIMING OF HPA CONTROL AND ISE MTU CARRIER-ON............................................................................................................9 8 COMPENSATING FOR ANTENNA GAIN VARIATIONS.................................................................................................................9 8.1 EIRP LIMITS AND THE NO POWER FLAG.....................................................................................................................................13 9 DYNAMIC POWER CONTROL............................................................................................................................................................17 9.1 NO POWER FLAG..............................................................................................................................................................................18 9.2 EIRP CHANGE RATE LIMITS...........................................................................................................................................................18 9.3 CONCURRENT MTU AND HPA POWER CONTROL EVENTS (OPTIONAL)..............................................................................18 9.4 NUMERICAL REPRESENTATION OF POWER ADJUSTMENT......................................................................................................19 10 CALL PROCESSING...............................................................................................................................................................................19 10.1 EIRP AND ANTENNA GAIN REPORTING......................................................................................................................................19 11 HTCE INTERFACE FLOWCHARTS....................................................................................................................................................19 12 REFERENCES............................................................................................................................................................................................29 APPENDIX A - ISE SYSTEM CALIBRATION TABLES .....................................................................................27 LIST OF FIGURES FIGURE 1- AERO-M4 SATCOM SYSTEM BLOCK DIAGRAM............................................................................................................................3 FIGURE 2 - FLOW OF PARAMETER DATA DURING DYNAMIC POWER CONTROL.......................................................................................18 FIGURE 3 - ISE CALL PROCESS EVENT LADDER DIAGRAM.............................................................................................................................21 FIGURE 4 - SYSTEM CALIBRATION FLOWCHART- STEP 1.............................................................................................................................23 FIGURE 5 - SYSTEM CALIBRATION FLOWCHART- STEP 2.............................................................................................................................24 FIGURE 6 - ANTENNA GAIN COMPENSATION FLOWCHART..........................................................................................................................26 FIGURE 7 - EIRP DETERMINATION FLOWCHART............................................................................................................................................27 FIGURE 8 - HTCE INTERFACE TASK FLOWCHART...........................................................................................................................................28 LIST OF TABLES TABLE 1 - SYSTEM PARAMETERS SETTABLE FROM THE DEBUG PORT.......................................................................................................4 TABLE 2 - POWER CONTROL PARAMETERS FOR THE ISE MTU.....................................................................................................................5 TABLE 3 - MTU TX OUTPUT POWER VS. TRANSMISSION MODE....................................................................................................................9 TABLE 4 - EXAMPLE OF ISE MTU SYSTEM CALIBRATION....…

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T.EUROPA HS-600 B 55939 7519220-802 7519300 01-05-16 CIRCUIT CARD ASSEMBLY- 1 3 STATIC SENS 7519300 INTERCONNECT 1 1 EA 7519221-2 7519221-2 PWB 2 6 EA 7517919-2 7517919-2 P0ST CRES,HEX,CLASS 303 87-004-04 3 8 EA 7516275-422 7516275-422 SCREW PNH CRES 4-40X11-16 4 4 EA 07187 0932-119 0932-119 SPACER 5 2 EA 07187 0424-8 MS35649-244 NUT HEX CRES 4-40 6 2 EA 07187 0770-5 MS15795-803 WASHER CRES 0.125 ID 50 1 EA 7002012-133 7002012-133 CAP 2.7 PF !0.1 PF 500 VDCW V SMD C 1 52 5 EA 7024421-125 7024421-125 C0NN 2 MM V J 12 05 J 14 05 J 22 06 J 42 07 J 52 08 53 5 EA 7024421-55 7024421-55 C0NN J 11 05 J 13 05 J 21 06V J 41 07 J 51 08 54 3 EA 7516241-150 7516241-150 C0NN J 1 11 J 2 11 J 3 11V 55 1 EA 7519243-5 7519243-5 C0NN P 1 10 V 56 2 EA 7025088-6 7025088-6 IDCTR 3.3 nH LL1608-FH *MOISTURE SENSITIVE* L 1 L 2 57 2 EA 7010077-3 7010077-3 C0NNECTR J 4 11 J 5 11 V 701 X EA M7005495 M7005495 MFGSPEC 5 T.EUROPA HS-600 B 55939 7519220-802 7519300 01-05-16 CIRCUIT CARD ASSEMBLY- 2 3 STATIC SENS 7519300 INTERCONNECT SH SH SH 50 C 1 2.7 PF !0.1 PF 500 VDCW SMD 54 J 1 11 54 J 2 11 54 J 3 11 57 J 4 11 57 J 5 11 53 J 11 05 52 J 12 2 MM 05 53 J 13 05 52 J 14 2 MM 05 53 J 21 06 52 J 22 2 MM 06 53 J 41 07 52 J 42 2 MM 07 53 J 51 08 52 J 52 2 MM 08 56 L 1 3.3 nH LL1608-FH *MOISTURE SENSITIVE* 56 L 2 3.3 nH LL1608-FH *MOISTURE SENSITIVE* 55 P 1 10 T.EUROPA HS-600 B 55939 7519220-802 7519300 01-05-16 CIRCUIT CARD ASSEMBLY- 3 3 STATIC SENS 7519300 INTERCONNECT INITIAL RELEASE 8-17-00 A PICTORIAL CHANGES ONLY. 28380 (NA) 12-19-00 B ADDED ITEMS 50 AND 56. CLASS II CHANGES MINOR. 24514 (M) 5-16-01

P.SCHWERMAN MARK III CMU B 55939 7519230-902 7519200 01-09-19 CIRCUIT CARD ASSEMBLY- 1 26 7519200 POWER SUPPLY 1 1 EA 7519231-2 7519231-2 PWB 2 1 EA 7519232-901 7519232-901 CCA STATIC SENSITIVE DEVICE 3 3 1 EA 7519238-901 7519238-901 HEATSINK 3 4 1 EA 7516274-6 7516274-6 PLATE 5 5 EA 7003216-71 7003216-71 P0ST 6 31 EA 7516275-414 7516275-414 SCREW PNH CRES 4-40X7-16 7 16 EA 07187 0770-5 MS15795-803 WASHER CRES 0.125 ID 8 13 EA 7500518-1 7500518-1 WASHER V 9 13 EA 7004588-223 7004588-223 INSUL V 10 2 EA 7004588-224 7004588-224 INSUL V 11 1 EA 7004588-334 7004588-334 INSUL V 12 4 EA 7003467 7003467 PLUG V 13 1 EA 7516274-7 7516274-7 PLATE 14 4 EA 07187 0919-127 MS51957-127 SCREW PNH CRES 8-32X1 1-8 MIL-S-7742 15 4 EA 58960 2504638-11 NAS620C8L WASHER CRES 0.169 ID 16 4 EA 07187 0164-8 0164-8 WASHER CRES 0.178 ID V 51 23 EA 07187 4006200-85 M39014/02-XV CAP 1,000,000 UUF !10% 50 VDCW MIL-C-39014/2 C 44 04 C 45 04 C 46 04 C 47 04 C 50 04 C 51 04 C 52 04 C 53 04 C 56 04 C 57 04 C 58 04 C 59 04 C 83 04 C 84 04 C 85 04 C 86 04 C 87 04 C102 04 C103 04 C109 04 C122 04 C123 04 C125 16 52 11 EA 58960 4077890-1 4077890-1 CAP 0.1 UF !20% 500 VDCW V C 4 02 C 5 02 C 6 02 C 7 02 C 8 02 C 68 01 C 69 01 C 70 01 C 71 01 C 72 01 C 73 01 53 9 EA 7011730-225 7011730-225 CAP 1 UF !10% 25 VDCW V SURFACE MOUNT C 2 14 C 24 06 C 38 02 C 39 02 C 78 09 C343 06 C344 13 C406 06 C461 10 54 78 EA 7011730-437 7011730-437 CAP 0.10 UF !10% 50 VDCW V ASSEMBLY VARIABLES CONTINUED ON FOLLOWING PAGE P.SCHWERMAN MARK III CMU B 55939 7519230-902 7519200 01-09-19 CIRCUIT CARD ASSEMBLY- 2 26 7519200 POWER SUPPLY SURFACE MOUNT C 13 03 C 21 15 C 40 15 C 43 07 C 48 12 C 49 07 C 60 08 C 88 09 C 97 05 C304 07 C305 07 C306 14 C307 14 C308 14 C313 14 C317 03 C318 03 C320 02 C323 07 C324 07 C325 10 C326 13 C327 06 C328 15 C330 15 C333 03 C335 03 C336 07 C337 07 C338 02 C339 02 C340 02 C352 07 C353 15 C354 15 C356 15 C362 12 C364 12 C365 12 C366 10 C367 10 C368 08 C369 08 C373 11 C374 11 C381 12 C382 12 C383 12 C385 08 C386 04 C387 04 C389 12 C390 09 C403 04 C408 05 C411 05 C412 04 C413 04 C414 05 C417 10 C418 10 C422 09 C423 09 C424 06 C425 13 C426 11 C427 11 C429 08 C438 06 C439 06 C442 07 C444 11 C445 07 C448 11 C449 11 C451 11 C455 11 C456 11 55 13 EA 7011730-517 7011730-517 CAP 2200 PF !10% 100 VDCW V SURFACE MOUNT C 11 14 C 42 07 C 77 09 C 96 05 C 98 06 C 99 06 C346 03 C371 11 C384 10 C405 05 C419 10 C430 11 C437 09 56 16 EA 7011730-525 7011730-525 CAP 0.010 UF !10% 100 VDCW V SURFACE MOUNT C 20 03 C 25 06 C 26 07 C 82 05 C100 06 C104 05 C117 04 C319 03 C329 15 ASSEMBLY VARIABLES CONTINUED ON FOLLOWING PAGE P.SCHWERMAN MARK III CMU B 55939 7519230-902 7519200 01-09-19 CIRCUIT CARD ASSEMBLY- 3 26 7519200 POWER SUPPLY C341 07 C347 03 C388 05 C409 05 C420 09 C428 04 C434 10 57 27 EA 7011730-540 7011730-540 CAP 0.10 UF !10% 100 VDCW V SURFACE MOUNT C 10 03 C 12 02 C 37 02 C 41 13 C 54 04 C 75 08 C 80 11 C 89 11 C 91 02 C105 05 C106 05 C124 11 C300 03 C301 03 C302 02 C303 02 C309 11 C312 07 C316 02 C331 07 C332 07 C360 04 C372 04 C394 08 C395 11 C402 02 C404 11 58 25 EA 7011730-646 7011730-646 CAP 220 PF !10% 200 VDCW V SURFACE MOUNT C 14 07 C 22 15 C 65 08 C 76 08 C101 09 C110 10 C311 07 C322 07 C345 03 C348 02 C349 02 C350 02 C351 02 C391 08 C396 08 C416 10 C421 09 C433 05 C440 16 C441 16 C446 17 C450 17 C452 09 C453 17 C454 17 59 21 EA 7011730-700 7011730-700 CAP 0.018 UF !10% 500 VDCW V SURFACE MOUNT C 55 02 C 74 01 C314 02 C315 02 C321 02 C355 03 C357 01 C358 01 C359 01 C361 01 C370 01 C375 01 C376 01 C377 01 C378 01 C397 01 C398 01 C399 01 C400 01 C401 01 C407 01 60 17 EA 7013064-318 7013064-318 CAP 220 UF !20% 10 VDCW V SURFACE MOUNT C 36 16 C 92 08 C 93 08 C 94 08 C 95 08 C107 11 C108 11 C111 11 C112 11 ASSEMBLY VARIABLES CONTINUED ON FOLLOWING PAGE P.SCHWERMAN MARK III CMU B 55939 7519230-902 7519200 01-09-19 CIRCUIT CARD ASSEMBLY- 4 26 7519200 POWER SUPPLY C113 11 C114 11 C115 11 C116 11 C118 11 C119 11 C120 11 C121 11 61 11 EA 7013064-714 7013064-714 CAP 22 MFD !20% 35 VDCW V SURFACE MOUNT C 1 03 C 15 07 C 16 07 C 17 07 C 18 07 C 29 07 C 30 07 C 31 07 C 32 07 C 33 07 C 35 16 62 1 EA 7021790-106 7021790-106 CAP 47 UF !20% 100 VDCW V C 9 02 63 3 EA 7500015-901 7500015-901 CAP 1 UF !10% 100 VDCW V C 19 04 C 28 02 C 34 02 64 9 EA 7500054-101 7500054-101 CAP 100 UUF !5% 50 VDCW V SURFACE MOUNT C 27 07 C 61 12 C 62 12 C 90 10 C334 03 C393 08 C415 05 C447 12 C460 12 65 9 EA 7500054-102 7500054-102 CAP 1000 PF !5% 50 VDCW V SURFACE MOUNT C 3 13 C 23 13 C342 07 C392 08 C410 05 C431 02 C432 16 C435 10 C436 09 66 14 EA 7500054-471 7500054-471 CAP 470 PF !5% 50 VDCW V SURFACE MOUNT C 63 12 C 64 12 C 66 12 C 67 12 C 79 12 C 81 09 C310 03 C363 12 C379 12 C380 12 C443 06 C457 15 C458 13 C459 13 67 10 EA 7011731-20 7011731-20 DI0DE STATIC SENSITIVE DEVICE V SURFACE MOUNT CR 16 13 CR 23 02 CR 25 07 CR 28 13 CR 29 13 CR 33 08 CR 37 11 CR 45 11 CR 49 04 CR 50 04 68 36 EA 7012934-10 7012934-10 DIODE STATIC SENSITIVE DEVICE V MMBD7000L SURFACE MOUNT ASSEMBLY VARIABLES CONTINUED ON FOLLOWING PAGE P.SCHWERMAN MARK III CMU B 55939 7519230-902 7519200 01-09-19 CIRCUIT CARD ASSEMBLY- 5 26 7519200 POWER SUPPLY CR 2 13 CR 3 13 CR 4 03 CR 5 03 CR 6 14 CR 8 02 CR 9 02 CR 11 14 CR 12 06 CR 13 07 CR 20 03 CR 21 07 CR 22 15 CR 24 02 CR 26 12 CR 27 12 CR 32 12 CR 34 12 CR 35 12 CR 39 12 CR 40 05 CR 41 12 CR 42 05 CR 46 06 CR 47 09 CR 52 04 CR 53 16 CR 54 16 CR 55 06 CR 58 16 CR 61 05 CR 62 09 CR 63 10 CR300 15 CR301 02 CR302 15 69 5 EA 7014906-100 7014906-100 DI0DE CR 30 11 CR 38 11 CR 51 11V CR 59 11 CR 60 16 70 1 EA 7018324-100 7018324-100 DIODE STATIC SENSITIVE DEVICE V SURFACE MOUNT CR 48 08 71 5 EA 7018422-160 7018422-160 DI0DE STATIC SENSITIVE DEVICE V SURFACE MOUNT CR 7 02 CR 17 07 CR 19 02 CR 44 11 CR 56 11 72 3 EA 7019611-616 7019611-616 DI0DE STATIC SENSITIVE DEVICE V CR 14 07 CR 15 02 CR 18 07 73 1 EA 7020185-40 7020185-40 RECT CR 31 01 V 74 5…

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