CMM 25-29-76

MILLENNIUM 87836 SERIES PASSENGER SEATS FOR AMERICAN AIRLINES B737 AIRCRAFT PART NUMBERS 87836301 87836304 87836311 87836314 87836321 87836324 87836331 87836334 87836341 87836344 87836351 87836354 87836431 87836434 87836441 87836444 87836451 87836454 87836631 87836634 87836641 87836644 87836651 87836654 COMPONENT MAINTENANCE MANUAL WITH ILLUSTRATED PARTS LIST ORIGINALLY ISSUED JAN 27, 1999 B/E AEROSPACE, SEATING PRODUCTS GROUP 1455 Fairchild Road Winston-Salem, North Carolina 27105 PHONE: (336) 767-2000 TELEX 80-6467, 4612021 SITA CODE: INT FBCR FAX: (336) 744-3283 CAGE CODE: V92802 Revision 5 DOC ID# 2338 25-29-76 Feb 10, 2009 Controlled ALERT THIS COMPONENT MAINTENANCE MANUAL IDENTIFIES REPLACEMENT PARTS AND REPAIR PROCEDURES SPECIFICALLY ENGINEERED FOR SEATING PRODUCTS MANUFACTURED BY B/E AEROSPACE, SEATING PRODUCTS GROUP. B/E PARTS ARE MANUFACTURED UNDER STRINGENT QUALITY CONTROL PROCESSES. USING NON-B/E PARTS MAY JEOPARDIZE YOUR WARRANTY AND RESULT IN DEGRADED SEAT PERFORMANCE. MODIFICATIONS TO B/E SEATING PRODUCTS WHICH HAVE NOT BEEN APPROVED BY B/E ENGINEERING MAY INVALIDATE THE TSO. ALL MODIFICATIONS SHOULD BE COORDINATED IN ADVANCE TO AVOID THIS POSSIBILITY. PLEASE REFER TO NO. 25-29-76-2338 IN ALL CORRESPONDENCE TO B/E AEROSPACE REGARDING THIS COMPONENT MAINTENANCE MANUAL AND ILLUSTRATED PARTS LIST. Controlled B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 REVISION NUMBER R5 DATED FEBRUARY 10, 2009 HIGHLIGHTS This Component Maintenance Manual (CMM) with Illustrated Parts List (IPL) has been reviewed for technical changes resulting from B/E Service Bulletins, B/E Service Letters, configuration changes and part improvements. Any existing Temporary Revisions (TRs) against this CMM have been incorporated with this revision. This CMM and IPL have been revised and reformatted. Please replace your old copies of this manual with this Revision Number 5 dated February 10, 2009. A brief description of the major changes follows. SECTION AND PAGES CHANGE DESCRIPTION Title Updated to reflect current revision. List of Effective Pages Updated to reflect current revision. Revision of Records Updated to reflect current revision. Service Bulletin List SB 25-20-3169 added to Service Bulletin List. Table of Contents Updated in line with IPL Page Numbering. Introduction Updated to the latest Standards. Description and Operation Updated to the latest Standards. Seat Identities updated from ‘ABC’ to ‘123’. Illustrations updated to reflect latest revision of the envelope drawing. Schematic and Wiring Diagrams Updated to the latest Standards. Disassembly Updated to the latest Standards and in line with IPL. Cleaning Updated to the latest Standards. Inspection/Check Updated to the latest Standards. Assembly Updated to the latest Standards and in line with IPL. Fits and Clearances Updated to the latest Standards. Special Tools, Fixtures & Equipment Updated to the latest Standards. Illustrated Parts List Front Section updated to the latest Standards. IPL updated to include SB 25-20-3169 and general update for errors or changes in the Bills of Materials. Alpha-numberic index updated accordingly. R5 25-29-76 Controlled Page 1 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 2 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM 87836 SERIES LIST OF EFFECTIVE PAGES SECTION PAGE Title Page DATE Feb 10, 2009 List of Effective Pages LEP-1 LEP-2 LEP-3 LEP-4 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Record of Revisions RR-1 RR-2 Feb 10, 2009 Feb 10, 2009 Record of Temporary Revisions RTR-1 RTR-2 Feb 10, 2009 Feb 10, 2009 Service Bulletin List SB-1 SB-2 Feb 10, 2009 Feb 10, 2009 Table of Contents TOC-1 TOC-2 Feb 10, 2009 Feb 10, 2009 Introduction INTRO-1 INTRO-2 INTRO-3 INTRO-4 INTRO-5 INTRO-6 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Description and Operation 1 2 3 4 5 6 7 8 9 10 11 12 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 SECTION PAGE Testing and Fault Isolation 1001 1002 1003 1004 1005 1006 1007 1008 1009 1010 DATE Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 SCHEMATICS AND WIRING DIAGRAMS 2001 Feb 10, 2009 2002 Feb 10, 2009 2003 Feb 10, 2009 2004 Feb 10, 2009 2005 Feb 10, 2009 2006 Feb 10, 2009 2007 Feb 10, 2009 2008 Feb 10, 2009 2009 Feb 10, 2009 2010 Feb 10, 2009 2011 Feb 10, 2009 2012 Feb 10, 2009 2013 Feb 10, 2009 2014 Feb 10, 2009 2015 Feb 10, 2009 2016 Feb 10, 2009 2017 Feb 10, 2009 2018 Feb 10, 2009 2019 Feb 10, 2009 2020 Feb 10, 2009 Disassembly R5 Controlled 3001 3002 3003 3004 3005 3006 3007 3008 3009 3010 25-29-76 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Page LEP-1 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM 87836 SERIES SECTION PAGE DATE Cleaning 4001 4002 4003 4004 4005 4006 4007 4008 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Inspection/Check 5001 5002 Feb 10, 2009 Feb 10, 2009 Repair 6001 6002 6003 6004 6005 6006 6007 6008 6009 6010 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 7001 7002 7003 7004 7005 7006 7007 7008 7009 7010 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Fits and Clearances 8001 8002 Feb 10, 2009 Feb 10, 2009 Assembly Special Tools, Fixtures, and Equipment 9001 Feb 10, 2009 9002 Feb 10, 2009 Illustrated Parts List 10001 10002 Feb 10, 2009 Feb 10, 2009 R5 SECTION PAGE Illustrated Parts List (Continued) 10003 10004 10005 10006 10007 10008 10009 10010 10011 10012 10013 10014 10015 10016 10017 10018 10019 10020 10021 10022 10023 10024 10025 10026 10027 10028 10029 10030 10031 10032 10033 10034 10035 10036 10037 10038 10039 10040 10041 10042 10043 10044 10045 10046 10047 10048 10049 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 25-29-76 LEP-2 Feb 10, 2009 Controlled DATE B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM 87836 SERIES SECTION PAGE Illustrated Parts List (Continued) 10050 10051 10052 10053 10054 10055 10056 10057 10058 10059 10060 10061 10062 10063 10064 10065 10066 10067 10068 10069 10070 10071 10072 10073 10074 10075 10076 10077 10078 10079 10080 10081 10082 10083 10084 10085 10086 10087 10088 10089 10090 DATE Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 SECTION PAGE Illustrated Parts List (Continued) 10091 10092 10093 10094 10095 10096 10097 10098 10099 10100 10101 10102 10103 10104 10105 10106 10107 10108 10109 10110 10111 10112 10113 10114 10115 10116 DATE Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 Feb 10, 2009 MAINTENANCE AND SERVICING 14001 Feb 10, 2009 14002 Feb 10, 2009 14003 Feb 10, 2009 14004 Feb 10, 2009 14005 Feb 10, 2009 14006 Feb 10, 2009 14007 Feb 10, 2009 14008 Feb 10, 2009 14009 Feb 10, 2009 14010 Feb 10, 2009 14011 Feb 10, 2009 14012 Feb 10, 2009 R5 Controlled 25-29-76 Page LEP-3 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM 87836 SERIES THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled LEP-4 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM 87836 SERIES RECORD OF REVISIONS REV NO. ISSUE DATE 00 Jan 27, 1999 01 Jan 22, 2001 02 Dec 21, 2001 03 Mar 04, 2002 04 Apr 29, 2004 05 Feb 10, 2009 DATE INSERTED BY REV NO. ISSUE DATE DATE INSERTED BY R5 25-29-76 Controlled Page RR-1 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM 87836 SERIES THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page RR-2 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 RECORD OF TEMPORARY REVISIONS TEMPORARY REV NO. PAGE NUMBER ISSUE DATE INSERT DATE BY R5 25-29-76 Controlled DATE REMOVED BY Page RTR-1 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page RTR-2 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 SERVICE BULLETIN LIST Service Bulletins are documents produced by B/E Aerospace engineering, authorizing a customer to perform modification work on B/E seating products. B/E Aerospace files all Service Bulletins with the Federal Aviation Administration (FAA). All Service Bulletins which direct mandatory implementation will be incorporated into the CMM. Optional Service Bulletins are implemented at the discretion of the customer. B/E Aerospace will incorporate only those optional Service Bulletins which the customer informs us have been implemented. Incorporation occurs in two possible ways: A. Scheduled Revision - At this time, B/E Aerospace will incorporate part number changes, Service Bulletins and other customer requested changes. B. Temporary Revision - Part number changes which occur between sceduled revisions will be addressed by temporary revision. These temporary revisions are minimal in nature and are designed to facilitate procurement of correct parts. Temporary Revisions will be incorporated with the next scheduled revision. SB NUMBER REV TITLE DATE DATE INCORP 25-20-1314 E LIMIT SEATBACK ROTATION JAN 14, 1999 JAN 22, 2001 25-20-1308 E INSTRUCTION FOR MOVING THE GROUND STUD ON THE ISPS BOX JAN 19, 1999 JAN 22, 2001 25-20-1332 NEW Y-BELT ATTACHMENT REMOVAL JAN 25, 1999 JAN 22, 2001 25-20-1331 A RESTORE RESTRICTIVE PLACARDS FOR AT&T PHONES JAN 28, 1999 JAN 22, 2001 25-20-1334 NEW INSTRUCTIONS TO SECURE HEELCAP IN THE CENTER CONSOLE FEB 01, 1999 JAN 22, 2001 25-20-1294 A INSTRUCTIONS FOR REPLACING LEG ANTI-RATTLE NUT FEB 07, 1999 JAN 22, 2001 25-20-1367 NEW REPLACE SEAT CONTROL LEVER MAR 11, 1999 JAN 22, 2001 25-20-1402 NEW APR 12, 1999 JAN 22, 2001 25-20-2049 A AUG 11, 1999 JAN 22, 2001 25-20-2057 NEW REPLACE ENDBAY ARMCAP AUG 16, 1999 JAN 22, 2001 25-20-2075 NEW REPLACE FOODTRAY HOOKS AUG 30, 1999 JAN 22, 2001 25-20-2105 NEW IN-ARM FOODTRAY LIFT HANDLE REPAIR OCT 08, 1999 JAN 22, 2001 25-20-2213 B REPLACE BACK PIVOT BOLT JAN 13, 2000 JAN 22, 2001 R5 25-29-76 Controlled Page SB-1 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 SB NUMBER REV TITLE DATE DATE INCORP 25-20-2344 NEW SERVICE BULLETIN CONSOLIDATION JUN 15, 2000 JAN 22, 2001 25-20-2101 B CENTER COCKTAIL TRAY REINFORCEMENT AUG 17, 2000 JAN 22, 2001 25-20-2411 NEW ARMCAP REPLACEMENT AUG 18, 2000 JAN 22, 2001 25-20-2644 NEW REPLACE HEADREST MECHANISM JUL 25, 2002 APR 29, 2004 25-20-2670 A REMOVE PHONE & REPLACE ARMCAP JAN 17, 2002 APR 29, 2004 25-20-2672 NEW SAFETY PLACARD CHANGE OCT 28, 2002 APR 29, 2004 25-20-2726 C BACK ATTACHMENT BOLT REPLACEMENT APR 29, 2002 APR 29, 2004 25-20-2750 A BACK CUSHION REPLACEMENT CONVERTS 878364XX TO 878366XX NOV 27, 2002 APR 29, 2004 25-20-2786 A CENTER MODULE INSTALLATION HARDWARE CHANGE JUL 22, 2002 APR 29, 2004 25-20-3169 B MILLENNIUM SEAT CONTROL ASSEMBLY BEZEL CHANGE MAY 10, 2005 FEB 10, 2009 R5 25-29-76 Controlled Page SB-2 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 TABLE OF CONTENTS SECTION PAGE LIST OF EFFECTIVE PAGES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEP-1 RECORD OF REVISIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RR-1 RECORD OF TEMPORARY REVISIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RTR-1 SERVICE BULLETIN LIST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SB-1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO-1 DESCRIPTION AND OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 TESTING AND FAULT ISOLATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1001 SCHEMATIC AND WIRING DIAGRAMS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2001 DISASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3001 CLEANING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4001 INSPECTION/CHECK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5001 REPAIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6001 ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7001 FITS AND CLEARANCES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8001 SPECIAL TOOLS, FIXTURES AND EQUIPMENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9001 ILLUSTRATED PARTS LIST INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10001 IPL Figure 1: Double Seat Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10020 IPL Figure 2: Headrest Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10028 IPL Figure 3: Back Installation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10034 IPL Figure 4: Back Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10038 IPL Figure 5: Back Assembly W/O Cushion . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10040 IPL Figure 6: Seatpan and Kickpanel Installation . . . . . . . . . . . . . . . . . . . . . . . . 10044 IPL Figure 7: Seatpan Assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10046 IPL Figure 8: Foodtray Installation - Endbay . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10050 IPL Figure 9: Foodtray Assembly - Endbay. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10052 IPL Figure 10: Endbay - Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10054 IPL Figure 11: Endbay Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10056 IPL Figure 12: Seat Control Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10066 IPL Figure 13: Pivot Assembly - Foodtray. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10070 IPL Figure 14: Endbay Placard Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10072 IPL Figure 15: Center Console Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10074 IPL Figure 16: Center Console Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10076 IPL Figure 17: Placard Assembly - Center Console . . . . . . . . . . . . . . . . . . . . . . 10088 IPL Figure 18: Lifevest Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10090 IPL Figure 19: Escape Path Lite Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10094 IPL Figure 20: Phone & SEB Box Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . 10096 IPL Figure 21: Power Box Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10098 IPL Figure 22: Baggage Bar and Installation. . . . . . . . . . . . . . . . . . . . . . . . . . . . 10104 IPL Figure 23: Frame Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10106 IPL Figure 24: Leg Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10110 IPL Figure 25: Spreader Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10114 MAINTENANCE AND SERVICING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14001 R5 25-29-76 Controlled Page TOC-1 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page TOC-2 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 INTRODUCTION 1. Purpose and Scope of This Manual This Component Maintenance Manual (CMM) contains descriptive information, maintenance procedures and an Illustrated Parts List (IPL) for American Airlines B737 aircraft, MILLENNIUM 87836 Series passenger seats manufactured by B/E Aerospace, Seating Products Group, 1455 Fairchild Road, Winston-Salem, North Carolina 27105. 2. Maintenance Concept A. This CMM supports seat maintenance activities that may be reasonably done by first-tier maintenance personnel. This includes routine servicing and maintenance needed to maintain the B/E Aerospace seating system in a satisfactory operating condition throughout its life cycle. Areas addressed in this CMM include: (1) Required inspections and checks designed to ensure safety and operational readiness. (2) Fault isolation procedures for identifying components that may need adjustment or replacement. (3) Step-by-step disassembly and assembly instructions enabling technicians to remove and replace line replaceable assemblies. (4) Commonly recurring adjustment and repair procedures. (5) Required tools and equipment. (6) Tolerances and torque values. (7) Detailed illustrations of the major assemblies and installations, with listings of all procurable items replaceable within the scope of the maintenance instructions. (8) Information regarding the incorporation of Service Bulletins/Letters. B. This CMM does not support the maintenance of riveted, welded or bonded assemblies. Repair of these types of assemblies requires a set of specialized skills and equipment typically unavailable at the line maintenance level. Since these assemblies have very low incidences of failure under normal operating conditions, they are treated as the lowest replaceable assemblies in the maintenance concept for this seat. R5 25-29-76 Controlled Page INTRO-1 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 3. Arrangement of This CMM This CMM is arranged in the following sections to facilitate the presentation of maintenance instructions. SECTION 4. PAGE BLOCK Description and Operation 1-999 Testing and Fault Isolation 1001-1999 Schematic and Wiring Diagrams 2001-2999 Disassembly 3001-3999 Cleaning 4001-4999 Inspection/Check 5001-5999 Repair 6001-6999 Assembly 7001-7999 Fits and Clearances 8001-8999 Special Tools, Fixtures, and Equipment 9001-9999 Illustrated Parts List 10001-10999 Maintenance and Servicing 14001-14999 List of Abbreviations The following abbreviations may be used in this CMM: ABBREVIATION EXPANSION A/C Aircraft AR As Required A/R Armrest ASSY Assembly B/C Business Class BCK Back BMFT Back-Mounted Foodtray B/O Breakover BTM Bottom CFE Customer-Furnished Equipment CSK Countersunk R5 25-29-76 Controlled Page INTRO-2 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 ABBREVIATION EXPANSION CTR Center DBL Double DET Detailed DET BKDN Detailed Breakdown DPCU Digital Passenger Control Unit DSEBI Digital Seat Electronics Box Interface E/B Endbay EFF Effectivity EMI Electro-Magnetic Interference ENVIR Environmental EPL Emergency Path Light F/C First Class FH Firehard FIG Figure FLDG Folding F/R Front Row F/T Foodtray FT-LB Foot-Pounds FWD Forward HCEB Handicapped Endbay HD Head HEX Hexagonal HMAR Hatch-Mounted Armrest IAFT In-Arm Foodtray IAT In-Arm Table I/B Inboard INBD Inboard IN-LB Inch-Pounds INSTL Installation IPL Illustrated Parts List ISPS In-Seat Power Supply LH Left Hand R5 25-29-76 Controlled Page INTRO-3 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 ABBREVIATION EXPANSION LK Lock LKG Locking LRU Line Replaceable Unit LWR Lower MC Mechanical Lock MUX Multiplexer N/A Not Applicable NHA Next Higher Assembly NP Non-Procurable NRW Narrow O/B Outboard OUTBD Outboard PAX Passenger PCU Passenger Control Unit P/N Part Number PPUI PC Power Use Indicator PVT Pivot QUAD Quadruple QUINT Quintuple REC Recline REF Refer To RF Reference Only RH Right Hand RJU Remote Jack Unit RR Rear SB Service Bulletin SCF Scarf SEB Seat Electronics Box SEU Seat Electronic Unit SGL Single SL Service Letter SLFLKG Self-Locking STA Stationary R5 25-29-76 Controlled Page INTRO-4 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 ABBREVIATION EXPANSION STD Standard SUPSD Superseded SUPSDS Supersedes SVDU Super Visual Display Unit T/C Tourist Class T/N Tool Number TPL Triple U/O Used On UPR Upper VDB Video Distribution Box VGS Variable Geometry Seat W/ With W/O Without R5 25-29-76 Controlled Page INTRO-5 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page INTRO-6 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 DESCRIPTION AND OPERATION 1. Configuration The Millennium business class seats for American Airlines, B737 aircraft have been manufactured in 24 versions. The seat versions are listed in tables 1-1 to 1-4. The aircraft configuration is extracted from the envelope drawing 35812 and is shown in figures 1-1 to 1-4. Typical seat dimensions are shown in figures 2-1 and 2-2. Standard Millennium seat components are shown at figure 3-1. R5 25-29-76 Controlled Page 1 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 TABLE 1-1 B737 20 BUSINESS CLASS PASSENGER, W/ PHONES, CONFIGURATION 1 SEAT IDENT SEAT PART NUMBER 1 87836301 2 SEAT DESCRIPTION SEAT WEIGHT SEAT QTY SEAT ASSEMBLY, LH STD 130 2 87836304 SEAT ASSEMBLY, RH STD, W/ AISLE LIGHT 130 2 3 87836311 SEAT ASSEMBLY, LH STD, OFFSET FRONT STUD 130 1 4 87836314 SEAT ASSEMBLY, RH STD, OFFSET FRONT STUD, W/ AISLE LIGHT 130 1 5 87836321 SEAT ASSEMBLY, LH NARROW 130 2 6 87836324 SEAT ASSEMBLY, RH NARROW, W/ AISLE LIGHT 130 2 NOTE: All seat weights are in lbs, with a tolerance of ± 3%. Figure 1-1 B737 20 Business Class Passenger Configuration 1 (Envelope Drawing 35812) R5 25-29-76 Controlled Page 2 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 TABLE 1-2 B737 20 BUSINESS CLASS PASSENGER, NO PHONES, CONFIGURATION 2 SEAT IDENT SEAT PART NUMBER SEAT PART NUMBER SEAT DESCRIPTION SEAT SEAT WEIGHT QTY 7 87836331 87836431 SEAT ASSEMBLY, LH STD 130 2 8 87836334 87836434 SEAT ASSEMBLY, RH STD, W/ AISLE LIGHT 130 2 9 87836341 87836441 SEAT ASSEMBLY, LH STD, OFFSET FRONT STUD 130 1 10 87836344 87836444 SEAT ASSEMBLY, RH STD, OFFSET FRONT STUD, W/ AISLE LIGHT 130 1 11 87836351 87836451 SEAT ASSEMBLY, LH NARROW 130 2 12 87836354 87836454 SEAT ASSEMBLY, RH NARROW, W/ AISLE LIGHT 130 2 NOTE: All seat weights are in lbs, with a tolerance of ± 3%. Figure 1-2 B737 20 Business Class Passenger Configuration 2 (Envelope Drawing 35812) R5 25-29-76 Controlled Page 3 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 TABLE 1-3 B737 20 BUSINESS CLASS PASSENGER, W/ PHONES, CONFIGURATION 3 SEAT IDENT SEAT PART NUMBER 1 87836301 2 SEAT DESCRIPTION SEAT WEIGHT SEAT QTY SEAT ASSEMBLY, LH STD 130 2 87836304 SEAT ASSEMBLY, RH STD, W/ AISLE LIGHT 130 2 3 87836311 SEAT ASSEMBLY, LH STD, OFFSET FRONT STUD 130 1 4 87836314 SEAT ASSEMBLY, RH STD, OFFSET FRONT STUD, W/ AISLE LIGHT 130 1 5 87836321 SEAT ASSEMBLY, LH NARROW 130 2 6 87836324 SEAT ASSEMBLY, RH NARROW, W/ AISLE LIGHT 130 2 NOTE: All seat weights are in lbs, with a tolerance of ± 3%. Figure 1-3 B737 20 Business Class Passenger Configuration 3 (Envelope Drawing 35812) R5 25-29-76 Controlled Page 4 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 TABLE 1-4 B737 12 BUSINESS CLASS PASSENGER, NO PHONES, CONFIGURATION 4 SEAT IDENT SEAT PART NUMBER SEAT DESCRIPTION SEAT WEIGHT SEAT QTY 13 87836641 SEAT ASSEMBLY, LH STD, W/ OFFSET FRONT STUD, NO PHONE, CP LUMBAR CUSHION 130 1 14 87836644 SEAT ASSEMBLY, RH STD, W/ OFFSET FRONT STUD, AISLE LIGHT, NO PHONE, CP LUMBAR CUSHION 130 1 15 87836651 SEAT ASSEMBLY, LH NRW, NO PHONE, CP LUMBAR CUSHION 130 2 16 87836654 SEAT ASSEMBLY, RH NRW, AISLE LIGHT, NO PHONE, CP LUMBAR CUSHION 130 2 17* 87836631 SEAT ASSEMBLY, LH STD, NO PHONE, CP LUMBAR CUSHION 130 N/A 18* 87836634 SEAT ASSEMBLY, RH STD, AISLE LIGHT, NO PHONE, CP LUMBAR CUSHION 130 N/A * These seats are listed for certification purposes only and are not shown on any configuration NOTE: All seat weights are in lbs, with a tolerance of ± 3%. Figure 1-4 B737 12 Business Class Passenger Configuration 4 (Envelope Drawing 35812) R5 25-29-76 Controlled Page 5 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 2. SEAT DIMENSIONS Figures 2-1 to 2-2 show the seat dimensions and useful information from the envelope drawing 35812. All dimensions are in inches unless otherwise stated. Figure 2-1 Seat Dimensions - Front View (Envelope Drawing 35812) R5 25-29-76 Controlled Page 6 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 See Detail 'B' See Detail 'A' DETAIL 'A' DETAIL 'B' TRACK BREAK LEGS 3. Description Figure 2-2 Seat Dimensions - Side View & Details (Envelope Drawing 35812) R5 25-29-76 Controlled Page 7 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 A. General The seats described in this CMM are forward facing and are of the types stated in Table 1. Figure 3 shows the main assemblies found on the double seats. For the operator, the seat has been designed on a modular basis to allow for ease of maintenance. The seat is comprised of the following six major modules: Frame Assembly Seat Pan Assemblies Back Assemblies Headrest Assemblies Endbay Assemblies Center Console Assembly. All of these modules (excluding the frame assembly) can be easily removed from the seat on the aircraft with a minimum of tools. The module can then be quickly replaced by a substitute module and any maintenance work can be carried out away from the aircraft. R5 25-29-76 Controlled Page 8 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 Headrest Assembly Back Assembly Foodtray Assembly Seat Control Assembly Seat Belt Bottom Cushion Endbay Assembly Center Console Assembly Lifevest Assembly Seatpan Assembly Frame Assembly Baggage Bar Figure 3-1 Double Seat Assembly R5 25-29-76 Controlled Page 9 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 B. Standard Features The Millennium seats have the following standard features: Machined aluminum primary structure Fabric bottom diaphragm suspension system Life vest pouch under center console Quick release anti-rattle track fitting Articulating bottom support Side restraint baggage bar. C. Endbay Assembly (With Foodtray Table) The endbay assembly features leather covered self-skinned armcaps and injection moulded rubstrips. The seat control assemblies are side mounted on the endbay assembly. Open the armcap to access the foodtray assembly which includes a slide and swivel feature. CAUTION: DO NOT PUT OBJECTS COLDER THAN 10 DEGREES CELSIUS (50 DEGREES FAHRENHEIT) OR HOTTER THAN 71 DEGREES CELSIUS (160 DEGREES FAHRENHEIT) ON THE FOODTRAY TABLE ASSEMBLY. THIS WILL HELP PREVENT DAMAGE TO THE FOODTRAY. TEMPERATURES COLDER THAN 10 DEGREES CELSIUS (50 DEGREES FAHRENHEIT) OR HOTTER THAN 71 DEGREES CELSIUS (160 DEGREES FAHRENHEIT) CAN CAUSE THE FOODTRAY TO WARP AND POSSIBLY COME APART. D. Center Console (With Lifevest Pouch Assembly) The center console is the central divider in the double seats. It features an injection moulded cocktail table, swivelling injection moulded peanut trays and a leather self skinned armcap. The console also features side-mounted telephone handsets and power ports located at the front of the console. The lifevest pouch assembly is located under the console and is accessible from the front of the seat. It is clearly visible to the passenger and easy to open. E. Back Assembly The back assembly features adjustable recline, adjustable lumbar support and rear magazine pockets. The lumbar support allows passengers to contour the back cushion profile to suit their needs. R5 25-29-76 Controlled Page 10 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 F. Headrest Assembly The headrest assembly provides the passenger with increased comfort. The headrest is adjustable vertically to allow for variation in passenger height. Also the side supports (headrest ears) can be rotated to provide side support for the passenger’s head. G. Seat Pan Assembly The seat pan assembly supports the passenger with a fabric-based bottom support. It also includes an articulating feature for increased comfort. R5 25-29-76 Controlled Page 11 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 4. Seat Assembly Operation A. Back Recline To move any back assembly from the upright to the recline position, activate the recline control lever and apply pressure against the backrest. When the control lever is released the backrest is restrained from any further movement. To re-erect the backrest, activate the recline control lever, release pressure from the backrest and it will return automatically to the normal upright position. The recline unit incorporates an override device which will allow the backrest to be moved from recline position to any angle up to and including the normal upright position by the application of a nominal load at the backrest top. B. Headrest Operation The headrest may be adjusted manually by sliding the headrest up or down as required. A friction device ensures that the headrest remains in the chosen position. The headrest ears can be adjusted manually by rotating the ears to the required position. Again, friction ensures that the ears remain in the chosen position. C. Foodtray Deployment Open the endbay/console armcap, and pull on the foodtray table handle to rotate the table to its vertical position. The table can now be swung into its deployed position ready for use. Close the armcap. In the deployed position, the foodtray table can slide forward and aft to allow for passenger comfort. The table is bi-fold, and can be used with either one or two leaves opened, as required. D. Attachment of the Seat Assemblies The seat assembly is attached to the aircraft seat tracks by securing the legs, fore and aft, with studs and track fittings. R5 25-29-76 Controlled Page 12 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 TESTING AND FAULT ISOLATION 1. Proper Assembly Proper assembly of the passenger seat will preclude the necessity for elaborate testing procedures. Complete disassembly of the seat is not usually required. Disassembly should proceed only so far as to correct malfunctions or replace damaged and worn parts. After assembly check all seat functions to ensure that each performs smoothly with no excessive binding or other evidence of faulty assembly. 2. Seat Back Recline Mechanism Seat backs recline through the operation of a recline control lever with pressure applied in an aft direction on the back. When the recline control lever is pulled with no pressure exerted on the back, the seat should return to its full upright position. If the seat back fails to operate in the above fashion, refer to REPAIR for corrective action. Refer to the envelope drawings in this CMM for recline operation. On mechanical locks, check clutch engagement in the recline lock by placing the seat back in the upright position and applying pressure in an aft direction. If the seat back reclines slightly and a click is audible, refer to REPAIR. 3. Breakover Seat backs are locked out from breakover by the use of a nut and bolt. 4. Seat Attachment To Aircraft The seat assemblies should lock securely to the floor track at the lock mechanisms and studs at the bottom of the leg assemblies. If the lock mechanisms or studs do not lock firmly into the floor tracks, refer to FITS AND CLEARANCES. Check for floor track wear as illustrated in Figure 8001 and Figure 8002. 5. Table 1001, Fault Isolation Table The Fault Isolation Tables are broken down into (3) specific categories: A. Fault - defines the problem B. Probable Cause - defines the most likely cause C. Corrective Action - provides the corrective action to be taken in the order that most likely would correct the problem. R5 25-29-76 Controlled Page 1001 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 TABLE 1001 FAULT ISOLATION TABLE FAULT PROBABLE CAUSE AND FAULT ISOLATION ENDBAY ARM TOO 1. Front/rear bolts loose LOOSE/TOO MUCH PLAY 2. Front and rear washers/ spacers worn FAULT FOODTRAY (IN-ARM) DIFFICULT TO RAISE UP IN VERTICAL POSITION FAULT FOODTRAY (IN-ARM) IN VERTICAL POSITION TOO LOOSE PROBABLE CAUSE AND FAULT ISOLATION Forward pivot assembly worn or damaged PROBABLE CAUSE AND FAULT ISOLATION CORRECTIVE ACTION Tighten front and rear bolts and torque to proper value per torque tables in FITS AND CLEARANCES. Replace worn washers/spacers, replace attaching hardware and torque to proper value per torque tables in FITS AND CLEARANCES. CORRECTIVE ACTION a. Remove front endbay arm escutcheon to access the forward pivot assembly. b. Inspect for bent or damaged parts. c. Replace damaged components. If necessary, replace the entire forward pivot assembly. CORRECTIVE ACTION Set screw loose Tighten set screw securing foodtray link pin. Foodtray link pin broken or damaged a. Remove set screw that secures foodtray link pin b. Drive out broken/damaged foodtray link pin c. Insert new link pin d. Install setscrew to hold pin in place R5 25-29-76 Controlled Page 1002 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FAULT FOODTRAY (IN-ARM) WILL NOT SWIVEL OR ROTATE FAULT FOODTRAY (IN-ARM) WILL NOT SLIDE FREELY IN DOWN OR HORIZONTAL POSITION FAULT FOODTRAY (IN-ARM) NOT LEVEL (SIDE-TOSIDE) PROBABLE CAUSE AND FAULT ISOLATION CORRECTIVE ACTION 1.Slider rod in down position Replace foodtray swivel. If the inside forward pivot assembly problem still exist, go to step 2. 2.Extension spring broken or missing Replace extension spring. If problem still exist, go to step 3. 3.Foodtray latch broken Replace foodtray latch. If problem still exist, go to step 4. 4. Foodtray pivot bushing broken, bent or damaged Replace foodtray pivot bushing. If problem persists, go to step 4. 5. Forward pivot assembly broken, bent or damaged Replace foodtray forward pivot assembly PROBABLE CAUSE AND FAULT ISOLATION CORRECTIVE ACTION Slide rod bent or damaged PROBABLE CAUSE AND FAULT ISOLATION Leveling screws not properly adjusted Replace bent/damaged slide rod and O-rings. CORRECTIVE ACTION a. Grasp foodtray assembly by foodtray lift handle and lift foodtray assembly straight up and out of endbay arm. b. Leave foodtray assembly in vertical position so that (2) setscrews on inner foodtray are exposed (looking straight down on foodtray assembly). c. Adjust setscrews either in or out until both inner and outer foodtray leaf assemblies are visually level. d. Repeat process until both foodtray leaf assemblies are level with one another. R5 25-29-76 Controlled Page 1003 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FAULT FOODTRAY (IN-ARM) NOT LEVEL (FRONT-TOBACK) FAULT FOODTRAY INNER AND OUTER LEAF ASSEMBLIES BROKEN AT HINGE PROBABLE CAUSE AND FAULT ISOLATION Leveling screws not properly adjusted PROBABLE CAUSE AND FAULT ISOLATION CORRECTIVE ACTION a. Leave foodtray assembly in vertical position and locate leveling adjustment screw. This screw is located at bottom of slide plate assembly, just below and to the left of setscrew attaching foodtray assembly to forward pivot assembly. b. Adjust leveling adjustment screw in or out until foodtray assembly is level (180°) with cocktail table. CORRECTIVE ACTION Foodtray leaf hinge(s) broken Replace foodtray leaf hinge(s). FAULT PROBABLE CAUSE AND FAULT ISOLATION HEADREST IS DIFFICULT TO INSTALL Friction bushings adjusted too tightly CORRECTIVE ACTION Adjust friction bushings so that headrest slide plate assembly slides on easily. NOTE: The headrest slide plate assembly locking nut located on the headrest assembly should be properly torqued so that the headrest can be consistently moved by a force between 10-12 pounds. FAULT PROBABLE CAUSE AND FAULT ISOLATION HEADREST EARS ARE DIFFICULT TO BEND 1/4 - 28 Hex head bolt and locking nut over-torqued. CORRECTIVE ACTION Torque to allow headrest ear to be consistently moved with 12-15 pounds of force exerted at the end of the ear. R5 25-29-76 Controlled Page 1004 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FAULT HEADREST FORWARD TILT TOO LOOSE OR TOO TIGHT FAULT LIFEVEST SHROUD ASSEMBLY ACCESS DOOR WILL NOT OPEN AND CLOSE PROPERLY FAULT LIFEVEST SHROUD ASSEMBLY ACCESS DOOR LOOSE FAULT MUX BOX COVER LOOSE PROBABLE CAUSE AND FAULT ISOLATION CORRECTIVE ACTION Pivot bolt and nut under or over torqued Torque to allow forward tilt pressure of 8-20 pounds (Ref SB 25-20-2644) PROBABLE CAUSE AND FAULT ISOLATION CORRECTIVE ACTION Pull latch broken or defective Replace pull latch and mounting screws PROBABLE CAUSE AND FAULT ISOLATION CORRECTIVE ACTION Loose screws on hinge assembly Replace loose screws on hinge assembly PROBABLE CAUSE AND FAULT ISOLATION CORRECTIVE ACTION Screw(s) damaged Replace mux box cover screw(s). R5 25-29-76 Controlled Page 1005 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FAULT SEAT BACK WILL NOT RECLINE PROBABLE CAUSE AND FAULT ISOLATION CORRECTIVE ACTION 1. P.L. Porter cable assembly loose from actuator end of hydrolok a. Inspect recline hydrolok actuator to see whether control cable has slipped out of actuator slot, or actuator has slipped off hydrolok. b. Reinstall cable to actuator slot or actuator to hydrolok. c. If problem persists, go to step 2. 2. P.L. Porter recline cable out of cable lever slot in seat control assembly a. Remove the (2) screws attaching seat control bezel to endbay assembly. b. Replace control cable into cable lever slot and test for proper operation. c. If problem persists, go to step 3. 3. P.L. Porter cable assembly broken a. Replace control cable assembly b. Adjust cable tension. c. Test recline control button for proper recline operation. d. If problem persists, go to step 4. 4. Hydrolok damaged/ inoperative a. Replace recline control hydrolok b. Reattach cable assembly at actuator and control cable lever ends of seat assembly. Route cable harness according to cable routing guidelines. c. Test recline control for proper operation. d. Adjust as necessary to ensure cable remains in slots (both ends) and that hydrolok is adjusted for proper tension. NOTE: The most common recline problems are due to improperly adjusting the hydrolok cable for proper tension during installation. If tension is not accurately adjusted, the cable simply slips out of the actuator end of the cable assembly and in some cases, the control button end of the cable assembly. Ensuring proper adjustment during maintenance activity will ensure fewer problems of this nature. NOTE: Refer to REPAIR section, beginning on page 6001, for more detailed instructions on removal and installation of seat control components. R5 25-29-76 Controlled Page 1006 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FAULT SEAT LEGREST INOPERATIVE PROBABLE CAUSE AND FAULT ISOLATION CORRECTIVE ACTION 1. P.L. Porter cable not installed to actuator slot in gaslock or hydrolok a. Inspect gaslock/hydrolok actuator to see if cable has slipped out of actuator slot. b. Reinsert cable assembly and test seat legrest control lever for proper operation. c. If problem still persists, go to step 2. 2. P.L. Porter legrest cable not installed to cable lever slot in seat control assembly a. Remove the (2) screws attaching seat control bezel to endbay assembly. b. Inspect to see if control cable has slipped out of the legrest control cable lever slot. c. Install control cable into cable lever slot and test the legrest control button. d. If problem persists, go to step 3. 3. P.L. Porter cable assembly broken a. Replace control cable assembly. b. Adjust cable to proper tension. c. Test legrest control button for proper operation. Id. If problem persists, go to step 4. 4. Gaslock damaged/ inoperative a. Replace gaslock. b. Install cable assembly at actuator and control cable lever ends of seat assembly. c. Test legrest control for proper operation. d. Adjust cable tension as necessary. NOTE: Refer to REPAIR section, beginning on page 6001, for more detailed instructions on removal and installation of seat control components. R5 25-29-76 Controlled Page 1007 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FAULT SEAT FOOTREST INOPERATIVE PROBABLE CAUSE AND FAULT ISOLATION CORRECTIVE ACTION 1. P.L. Porter cable assembly loose from actuator end of mechanical lock a. Inspect mechanical lock actuator to see if cable has slipped out of actuator slot. b. Install cable to actuator slot. c. Test seat footrest control button for proper operation. d. If problem persists, go to step 2. 2. P.L. Porter footrest cable detached from cable lever slot in seat control assembly a. Remove the (2) screws attaching seat control bezel to endbay assembly. b. Inspect to see if control cable has slipped out of footrest control cable lever slot. c. Install control cable into cable lever slot and test footrest control button for proper operation. d. If problem persists, go to step 3. 3. P.L. Porter cable assembly broken a. Replace P.L. Porter control cable assembly. b. Adjust cable tension. c. Test footrest control button for proper operation. Id. If problem persists, go to step 4. 4. Mechanical lock damaged/ inoperative a. Replace mechanical lock. b. Install P.L. Porter cable assembly at actuator and control cable lever ends of seat assembly. Route cable harness according to guidelines. c. Test footrest control for proper operation. d. Adjust cable tension as necessary. NOTE: Refer to REPAIR section, beginning on page 6001, for more detailed instructions on removal and installation of seat control components. R5 25-29-76 Controlled Page 1008 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FAULT SEAT LUMBAR INOPERATIVE PROBABLE CAUSE AND FAULT ISOLATION CORRECTIVE ACTION 1. P.L. Porter cable assembly detached from lumbar valve tube a. Remove lumbar cushion assembly from seat back assembly. b. Check to make sure that cable assembly is connected to lumbar valve tube. Reconnect if necessary. c. Test lumbar control lever button for proper operation. d. If problem persists, go to step 2. 2. Lumbar cable assembly detached from cable lever slot in seat control assembly a. Remove the (2) screws attaching seat control bezel to endbay assembly. b. Inspect to see if control cable has slipped out of lumbar control cable lever slot. c. Install control cable into cable lever slot and test lumbar control button. d. If problem persists, go to step 3. 3. P.L. Porter cable assembly broken a. Replace P.L. Porter control cable assembly. b. Adjust cable to proper tension. c. Test lumbar control button for proper operation. Id. If problem persists, go to step 4. 4. Lumbar valve tube broken/ defective a.Remove spring clip attaching lumbar valve assembly to inflatable lumbar cushion. b. Install replacement lumbar valve assembly. c. Install P.L. Porter control cable to lumbar valve assembly. d. Test for proper operation. e. If problem persists, go to step 5. 5. Lumbar cushion assembly defective a. Replace lumbar cushion assembly. b. Test for proper operation. NOTE: Refer to REPAIR section, beginning on page 6001, for more detailed instructions on removal and installation of seat control components. R5 25-29-76 Controlled Page 1009 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FAULT SEAT ASSEMBLY READING LIGHT DOES NOT WORK PROBABLE CAUSE AND FAULT ISOLATION Reading light has no power CORRECTIVE ACTION Disconnect the fiber optic cables by loosing the setscrews that secure the cable plugs, remove and replace the failed reading light source assembly. NOTE: The reading light is built into the seat back assembly and cannot be easily replaced. If the reading light fails, it will more than likely be due to the power source and not the fiber optic cables and reading light assembly. NOTE: For troubleshooting electronic customer furnished equipment, please refer to the appropriate vendor furnished maintenance documentation. R5 25-29-76 Controlled Page 1010 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 SCHEMATIC AND WIRING DIAGRAMS 1. General A. Cable Routing This section contains installation, maintenance and service procedures for properly routing and securing electrical cables on aircraft seating equipment. These general practices apply to all series of aircraft passenger seats manufactured by B/E Aerospace. Refer to aircraft manufacturer’s specifications for OEM requirements and more detail (see table below). Figure 2020 contains diagrams and installation/maintenance procedures specific to American Airlines B737 MILLENNIUM 87836 Series passenger seats. OEM Specification Document Boeing Electrical Bonding BAC5117 Installation of Electrical Wiring BAC5158 (1) Routing Principles (a) Cables shall be as accessible as possible to allow for ease of maintenance and inspection since most repairs are carried out on the aircraft. (b) Route cables to avoid possible damage from passenger contact, underseat carry on storage and shifting, spills, and/or mechanical movement of seat components. Refer to Figure 2001. R5 25-29-76 Controlled Page 2001 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 RECLINE MECHANISM STRUCTURE UNACCEPTABLE ACCEPTABLE SEAT FRONT BEAM CABLE Figure 2001 (c) When seat parts can rotate between each other, route the cables parallel to the rotation axis. Refer to Figure 2002. ACCEPTABLE UNACCEPTABLE Figure 2002 (d) Route cables to minimize the need for protective methods and materials like wrap or sleeves. R5 25-29-76 Controlled Page 2002 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (e) Route cables with enough slack to prevent mechanical strain on wires, terminals, connections, junctions and supports. Refer to Figure 2003. CONNECTOR 0.25" MINIMUM STRAIN POINTS SMOOTH TRANSITION SPACER CABLE TIE WRONG RIGHT SEAT BEAM Figure 2003 (f) When cables cross or are in proximity to seat moving parts, route them on either side of those moving parts. (g) Locate the breakout of individual cables adjacent to cable support or clamping points. This minimizes the amplitude of vibration transmitted to the breakout wires from the main harnesses. (h) Route cables exiting a connector in a straight line for at least 0.25 inches before making a bend. Refer to Figure 2003. R5 25-29-76 Controlled Page 2003 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 SERVICE LOOP (TYPICAL) SEB Figure 2004 (j) (2) Provide service loops to allow for adjustment, service or removal of connectors or components with minimal disassembly. Refer to Figure 2004. Clearances (a) Install cables with enough clearance to prevent chafing against the sharp edges of structure, equipment, etc. (1/8” minimum clearance unless secondary protection is provided). (b) When not specifically controlled, the slack portion of the cable bundles may contact smooth flat surfaces and smooth radii of 1/8” or larger of either metal or plastic. (c) Route power wiring for motorized equipment, in-seat power, or reading lights separately from IFE and communication wiring. Sensitive signal or communication wiring should have at least a one-inch separation from electrical wiring. When a one-inch separation is not possible, enclose the power wiring in a metallic shield grounded to seat structure to minimize EMI. Refer to Figure 2005. R5 25-29-76 Controlled Page 2004 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 CABLES CABLE TIE WITH SPACERS 1'' SEAT BEAM Figure 2005 (3) Bend Radius (a) For coaxial cable, use a minimum bend radius of ten times the cable diameter. In restricted places, the bend radius for coaxial cable may be a minimum of six times the cable diameter. Too severe a bend in coaxial cable can damage the cable and cause loss of signal. For standard wire cable, the bend radius will be a minimum of three times the cable diameter, but six times the cable diameter is preferred. (b) The bend radius of a cable bundle will not be less than six times the diameter of the largest cable in the bundle. (c) Clamping or the pressure of cable rubbing against structure causes bend sensitivity and reduced cable life. Increase bend radius to maximize cable life. NOTE: (4) If the cable jacket or sheathing becomes crimped, the bend radius is too small. Cable Slack (a) Distribute slack evenly throughout the length of the cable bundle. (b) In applicable areas, ensure there is enough cable slack to allow the following operations: (i) Replacement of terminations and/or connectors (ii) Movement of hinged or sliding joints R5 25-29-76 Controlled Page 2005 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (c) (iii) Removal and replacement of face mounted equipment (iv) Coupling and uncoupling of connectors (v) Movement of equipment to perform adjustment, servicing or removal. Provide drip loops so that liquids will not drip on or into electrical equipment. Do not use drip loops unless cable routing will permit liquids to run down the wiring into the connector. Drip loops are not required on wires or connectors that terminate in a potted connector.Take care to prevent the drip loop from chafing on adjacent structure or equipment. If chafing can occur, that section of wire or cable must be sleeved or tape wrapped. Do not use drip loops to take up excess wire length. Refer to Figure 2006. DRIP LOOP Figure 2006 (5) Cable Ties (a) Untangle cables as much as practical before tying them into groups. Lay cable groups parallel when practical before tying them into bundles. (b) In underseat baggage stow areas, place cable out of reach of passenger and install ties as necessary to ensure no slack in this area. (c) The use of nylon straps (Tyraps, Panduit, etc.) attached directly to smooth structure is acceptable. (d) Cut off cable ties square and flush with the cable tie head to prevent injury. Refer to Figure 2007. R5 25-29-76 Controlled Page 2006 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 WRONG RIGHT TRIMMED CABLE TIES Figure 2007 (e) Where a cable or cables break out of a cable bundle, each group shall be tied together and/or secured at a maximum distance of 1 inch from the break out point. Refer to Figure 2008. CABLE TIES 1'' 6" TO 8" 1" 1" Figure 2008 (f) Do not use cable ties in areas where the head of the cable tie can press against and abrade adjacent wires, or where the clamping pressure results in deformation of a coaxial cable. Refer to Figure 2009. R5 25-29-76 Controlled Page 2007 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 WRONG CABLE TIE HEAD Figure 2009 (g) (6) (7) When cable ties intrude into the foam of the seat (e.g., seat back), turn the head of the cable tie to one side to minimize risk of damage to the seat cushion. Spacing Ties for Bundle Support (a) Space ties on cable bundles a minimum of 6” and a maximum of 8” apart. (b) Ties may be placed as required to provide adequate support at bends, breakout and locations where cables are adjacent to moving parts. Clamping (a) Cable bundles should never be attached directly to the structure. Instead, use stand-offs and spacers. Refer to Figure 2010. CABLE TIE SPACER CABLE TIE SEAT REAR BEAM Figure 2010 R5 25-29-76 Controlled Page 2008 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (8) (b) Select the smallest clamp size that (1) holds the wiring securely, (2) allows no abrasive movement, and (3) neither crushes nor pinches the wire. (c) Use standard clamps. Clamping and installation should be done in a way that facilitates the removal and replacement of cable assemblies. (d) Tie and support wire or cable bundles to prevent mechanical strain on individual wires or terminations. (e) When the diameter of the cable is smaller than what the clamp can securely hold, use nylon tape to wrap the cable before clamping. (f) Do not use hook and loop fasteners to secure cable bundles. Connectors (a) Minimize the handling of connectors and cabling at all times to reduce the possibility of connector damage. (b) Minimize the bending of wire conductors. Cables containing any wire with damaged insulation should be replaced. (c) Wiring should be periodically inspected for signs of unacceptable damage such as cuts, breaks, cracked or burnt insulation or excessive kinks. (d) Periodically inspect connectors for signs of contamination with metal particles, water, dirt, grease, oil, carbon or adhesive. (e) Periodically inspect connectors for bent or corroded contacts. Do not straighten bent connector contacts. Do not reject tarnished silver, gold or rhodium plating on contacts. (f) Use standard snug fitting dust caps to protect the uncoupled end of connectors from mechanical damage and contamination. Install the dust covers on all connectors to prevent damage. (g) When performing service requiring disconnecting connectors, protect connectors from contamination by metal particles, water, dirt, grease and oil. Use polyethylene bags. (h) Route cables to minimize mechanical strain on connectors and cabling. (j) Protect cables against breakage at connections by providing enough slack and using mechanical clamping as needed to relieve strain. (k) Install connectors to prevent their usage as steps, hand holds, or footrest, and to prevent mechanical strain on attached cables. (l) Securely attach each connector on the seat structure using one of the following methods: R5 25-29-76 Controlled Page 2009 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (i) Plastic straps (Tyraps, Panduit, etc.) (ii) Clamps (iii) Structure provision (raceway, bracket, etc.). (m) Mount connectors horizontally to allow for drainage and prevent the trapping of liquid or condensation. (9) Handling of ESD (Electrostatic Discharge)-Sensitive Parts and Assemblies (a) Protect parts and assemblies from damage and contamination during all transportation and storage periods. They must be capable of meeting the requirements of the drawing and specification to which they were manufactured. Damage may consist of bends, dents, deformations, loose or missing fasteners, broken or kinked wires, and electrostatic discharge damage. Contamination consists of foreign materials such as dirt, dust, chips, filings, loose material, solder particles, grease, oil paint and moisture. (b) Use suitable cushioning and wrapping materials for equipment protection. NOTE: 2. Cushioning and wrapping materials may vary, depending on the environment in which they are to be used. Grounding of Seats and Seat Equipment This section contains installation, maintenance and service procedures for properly grounding seats and seat electrical/electronic components. Seat tracks on modern transport aircraft are not designed to carry ground. All electrical seat and seat related components should be grounded via the aircraft’s electrical system. Proper grounding and bonding techniques used on the metal portions of the seat group are essential to ensure adequate grounding. NOTE: B/E Aerospace seating products are manufactured to conform to the aircraft manufacturer’s electrical grounding specifications that are/were current at the time of manufacture. Specifications continue to change, and not all products currently in service conform to present specifications. For information on upgrading seat electric/ electronic equipment grounding to current manufacturing specifications, contact B/E Aerospace’s Seating Aftermarket Operations (SAO) for options and quotes. Although properly maintained seating products continue to meet certification, evolving OEM specifications may result in the application of different grounding specifications during a prolonged schedule of manufacture and delivery. R5 25-29-76 Controlled Page 2010 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (1) Grounding to A/C Electrical System (a) Main static ground for the seat is the grounding connection through the seat-toseat cable. This main static ground may be either a contact in the seat-to-seat connector or a #10 stud connected to a ground cable from the seat-to-seat cable. Refer to Figure 2011 for an example. 7 - SPARE 2 - AC RETURN 1 - SINGLE-PHASE 115VAC 3 - STATIC GROUND 6 - STATIC GROUND 5 - NOT USED 115VAC 400Hz 4 - NOT USED Figure 2011 (b) Static ground connection to the ECU from ground stud(s) on the seat structure may be accomplished through a ground strap that is a component of the seat-toseat wiring harness or via ground fittings on the ECU enclosure itself. Refer to Figure 2012 for an example. R5 25-29-76 Controlled Page 2011 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 JXX JXX JXX 0 0 0 0 0 TWO REDUNDANT GROUND FITTINGS 0 0 0 ECU 3 6 J1 J2 SEAT-TO SEAT CABLE 3 6 SEAT-TOSEAT CABLE BONDED TO SEAT PRIMARY GROUND Figure 2012 (c) Ground stud(s) on the seat’s metallic frame provide for ground strap terminal connections. Refer to Figure 2013. R5 25-29-76 Controlled Page 2012 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 ISPS (PC POWER) SEAT STRUCTURE OUTPUT 1 4 5 3-PHASE POWER READING LIGHT 3 3 6 SECONDARY BONDING STUD (OPTIONAL) INPUT 3-PHASE POWER MOTOR 1 4 5 X 3 X 6 PRIMARY BONDING STUD (#10) 3 CONTROLLER AIRCRAFT STATIC GROUND AT SIDEWALL FLOORBOX DISCONNECT AIRCRAFT SEAT Figure 2013 R5 25-29-76 Controlled Page 2013 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (2) Ground Studs, Types Utilized (a) Direct Ground Stud - A ground stud installation where necessary terminal(s) is/ are installed simultaneously with the ground stud. The ground stud must be removed to remove the terminal(s). Refer to Figures 2014 and 2015. SELF-LOCKING NUT PRESSURE WASHER TERMINAL CORROSIVE PROTECTIVE WASHER CLEANED SURFACE METAL STRUCTURE CORROSIVE PROTECTIVE WASHER FASTENER Figure 2014 - Direct Ground Stud with Single Terminal SELF-LOCKING NUT PRESSURE WASHER TERMINAL CLEANED SURFACE CORROSIVE PROTECTIVE WASHER METAL STRUCTURE CORROSIVE PROTECTIVE WASHER FASTENER Figure 2015 - Direct Ground Stud with Multiple Terminals R5 25-29-76 Controlled Page 2014 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (b) Preinstalled Ground Stud - A ground stud installation that allows terminals (installed by separate process) to be installed and/or removed without removing the ground stud. (c) Standard Ground Stud - A ground stud comprised of standard fasteners, washers and nuts. Refer to Figures 2016 and 2017. SELF-LOCKING NUT PRESSURE WASHER TERMINAL PRE-INSTALLED GROUND STUD METAL STRUCTURE CORROSIVE PROTECTIVE WASHER PRESSURE WASHER Figure 2016 - Standard Ground Stud with Single Terminal SELF-LOCKING NUT PRESSURE WASHER TERMINAL METAL STRUCTURE PRE-INSTALLED GROUND STUD PRESSURE WASHER CORROSIVE PROTECTIVE WASHER Figure 2017 - Standard Ground Terminal with Multiple Terminals R5 25-29-76 Controlled Page 2015 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (3) Grounding Procedures (a) Each seat must be provided with a #10 ground stud to ground equipment and structure not otherwise attached to main static ground. (b) If a ground stud needs to be installed or reinstalled, refer to Boeing document BAC5117 for specifications on surface preparation, materials and testing. (c) When more than one terminal is installed on one ground stud, put the largest terminal next to the corrosion protective washer and stack the other terminals in order of decreasing size. Fan the terminals around the stud whenever possible. Refer to Figure 2018. (d) A maximum of six terminals may be installed on a single ground stud, whether primary or secondary bonding stud. (e) For restricted spaces, a ground strap terminal may be bent 90 degrees one time only. Ensure that enough clearance exists between the terminal shank and the ground stud to allow installation and removal without further bending. Repeated bending of a terminal may cause it to break. (f) Corrosion protective and pressure (locking) washers must be used on ground studs. Refer to Figures 2014 through 2017. (g) When more than two ground terminals are installed on a ground stud, corrosive protective flat washers must be installed on each side of each terminal. Refer to Figure 2018. HEX NUT FLAT WASHERS EACH SIDE OF TERMINAL BASE MATERIAL NOT SHOWN HEX NUT Figure 2018 (h) Terminals can be turned over to assist installations. (j) Nuts on ground studs must be properly torqued. Refer to Tables 2001 and 2002 and aircraft OEM specifications. R5 25-29-76 Controlled Page 2016 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 Table 2001 Self-Locking Electrical Nut Torque Values STUD SIZE TIN COATED COPPER TERMINAL ON ALUMINUM MINIMUM MAXIMUM 10-32 28 IN-LB 35 IN-LB 1/4-28 65 IN-LB 70 IN-LB 5/16-24 135 IN-LB 145 IN-LB Table 2002 Plain Electrical Nut Torque Values NUT SIZE MINIMUM MAXIMUM 10-32 35 IN-LB 40 IN-LB 1/4-28 85 IN-LB 105 IN-LB 5/16-24 150 IN-LB 180 IN-LB (k) If a ground terminal is removed from a ground stud with more than one terminal, the other terminals must be resecured with the ground stud to the seat using proper procedures. This will apply when a component of the seat may be removed for repair or replacement at a later date. (l) Whenever a ground terminal is removed and reinstalled or replaced, or whenever a ground stud is installed or replaced, use an ohmmeter to verify that resistance to ground is within an acceptable range. (Figure 2019 illustrates a method for testing for resistance to ground with an ohmmeter.) Refer to aircraft OEM specs for details of stud sizes and maximum resistance. OHMMETER METAL STRUCTURE APPROX 0.25" Figure 2019 R5 25-29-76 Controlled Page 2017 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 3. Installation POWER BOX INSTALLATION 48250 38" PWR HARNESS TO J2 CONN ON BOX 38" PWR HARNESS TO J3 CONN ON BOX ELECTRICAL BOX & SHROUD ASSEMBLY Figure 2020 R5 25-29-76 Controlled Page 2018 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 POWER BOX INSTALLATION 48250 POWER PORT POWER J-BOX Figure 2021 R5 25-29-76 Controlled Page 2019 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 SEB INSTALLATION 48299 WIRING HARNESS (MAS) MUX PLATE SEB MUX SHROUD Figure 2022 R5 25-29-76 Controlled Page 2020 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 DISASSEMBLY 1. General WARNING: BEFORE SERVICING SEATS HAVING POWER COMPONENTS, DISCONNECT POWER TO THE SEAT TO AVOID ELECTRICAL SHOCK. CAUTION: DO NOT REMOVE RIVETED ASSEMBLIES OR SUBASSEMBLIES UNLESS DAMAGE MAKES IT NECESSARY TO REPLACE A PROCURABLE PART. (REFER TO THE ILLUSTRATED PARTS LIST FOR A LIST OF PROCURABLE PARTS.) IF YOU REMOVE AND INSTALL RIVETS AGAIN AND AGAIN, YOU WILL DAMAGE ADJACENT SURFACES AND MAKE THE RIVET HOLES LARGER. CAUTION: DO NOT DISASSEMBLE RIVETED, CEMENTED, OR BONDED SUBASSEMBLIES. IF THE ASSEMBLY IS DAMAGED AT THESE POINTS, YOU MUST REPLACE THE ENTIRE ASSEMBLY. A. This section gives complete disassembly instructions for the full seat assembly. If you must repair or replace a part or subassembly, disassemble only as much as necessary to repair or replace the damaged part or subassembly. B. Read all instructions and look at the related illustrations before starting disassembly. C. Identify all parts with a label as you remove them. D. TESTING AND FAULT ISOLATION (Page Block 1000) contains procedures you can use to make an analysis of the operation and condition of subassemblies. It contains a table that identifies possible malfunctions and gives procedures to correct the malfunctions. E. SCHEMATIC AND WIRING DIAGRAMS (Page Block 2000) contains procedures, notes, warnings and cautions for the electrical system. F. INSPECTION/CHECK (Page Block 5000) contains procedures you can use to inspect parts and subassemblies. Inspections will help you make a decision to set adjustments, clean subassemblies and repair or replace damaged parts. G. REPAIR (Page Block 6000) contains procedures you can use to make small repairs. 2. Removal of the Seat Assembly from the Aircraft CAUTION: DO NOT SLIDE THE SEAT ASSEMBLY ACROSS ABRASIVE SURFACES; THIS WILL CAUSE TOO MUCH WEAR ON THE TRACK STUDS AND FITTINGS. Seat assemblies are attached to the aircraft seat tracks with a stud and anti-rattle clamp located at the bottom of the forward leg and a track fitting assembly located at the bottom of the rear leg. See Figure 3001 for examples. R5 25-29-76 Controlled Page 3001 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 SCREW LEG (REAR) LEG (FRONT) REAR TRACK FITTING ANTI-RATTLE NUT STUD Figure 3001 A. Loosen the stud under the front of the leg by loosening the anti-rattle nut. B. Loosen the screw on top of the rear track fitting. This loosens the plunger that attaches the studs to the aircraft seat tracks. C. Push the seat assembly either forward or aft one-half inch and lift it off the aircraft seat tracks. NOTE: Track savers are recommended to protect the track fittings when the seat is removed from the aircraft. They can be ordered from B/E Aerospace. R5 25-29-76 Controlled Page 3002 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 3. General Disassembly A. Disassembly of the Seat (1) Bottom Cushion and Seat Belt Removal Refer to IPL Figure 1 (2) (a) Remove the bottom cushion assemblies (15) by firmly pulling away from the hook and pile fastening on the seat diaphragm. Remove the bottom cover assembly (10) from the bottom cushion (15) by disengaging the hook and pile fastening. (b) Remove the seatbelts, buckles and tips (20,25). Headrest & Dress Cover Removal Refer to IPL Figure 1 (3) (a) Remove the headrest assemblies (35) by sliding the headrest upwards and releasing the latch. Remove the headrest cover (30) from the headrest assembly (35) by disengaging the hook and pile fastening. (b) Remove the back cover assemblies (40) and literature pocket covers (45) by disengaging the hook and pile fastening. Remove the lumbar covers (50) and lumbar cushion assemblies (55). Disassembly of the Headrest Assembly Refer to IPL Figure 2 (4) (a) Remove the ear assemblies (10,15) from the center body assembly (5) by removing bolt (20), washers (25,30), spacer (35) and nut (40). (b) Remove the slide plate assembly (45A) from the center body assembly (5) by removing bolt (90), washers (95,100), spacer (105) and nut (110). (c) Remove the headrest release latch (80) by removing the screw (85) and the dowel pin (75). (d) Remove the pivot bracket (55) from the headrest slide plate (50) by removing the screws (60), the washers (65) and the spacers (70). Back Assembly Removal Refer to IPL Figure 3 (a) Detach the seatpan assembly from the back assembly (refer to paragraph 6). (b) Remove the control lines from the Hydrolok. R5 25-29-76 Controlled Page 3003 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (5) (c) Disconnect the Hydrolok from the spreader assembly by removing nuts (85) and washers (90). (d) Detach the back assembly (5A) from the spreader assembly, at the Hydrolok side, by removing bolt (10A), washers (15,40), shackle fitting (20), bushing (25), spacers (30,35) and nut (45). (e) Detach the back assembly (5) from the spreader assembly, at the nonHydrolok side, by removing bolt (50A), washer (55), shackle fitting (60), bushing (65) and spacer (70). (f) Carefully lift the back assembly away from the seat assembly. Disassembly of the Back Assembly Refer to IPL Figures 4 and 5 (6) (a) Debond and remove back the cushion assembly (4-10), back pad (4-20), fireblock (4-25) and fabric support assembly (4-15) as required. (b) Remove the Hydrolok (5-25) by removing screw (5-30A) and nut (5-35). (c) Remove the recline arm (5-10) by removing bolts (5-16), washers (5-20, 5-22) and nuts (5-24). (d) Remove the spring assemblies (5-40,5-45) by removing screws (5-50). (e) Remove the headrest friction plate (5-90) by removing covers (5-110), screws (5-95), nuts (5-107), springs (5-97), washers (5-100A) and friction block (5105B). (f) Remove the roller support bracket (5-55) and the roller assemblies (5-70A) by removing the covers (5-110), screws (5-60), spacers (5-65), bushings (5-80) and spacers (5-85). (g) Remove the screws (5-135) and washers (5-140). Seatpan and Kickpanel Removal Refer to IPL Figure 6 (a) Remove the kickpanel assembly (30) from the seatpan assembly (5) by removing screws (35) and washers (40). (b) Remove the seatpan assembly (5) from the backrest assembly by removing screws (10A), washers (15), bushings (20) and spacers (25). R5 25-29-76 Controlled Page 3004 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (7) Disassembly of the Seatpan Assembly Refer to IPL Figure 7 (8) (a) Disconnect the bottom diaphragm assembly (5) from the welded seatpan assembly (45) by disengaging the hook and pile fastening. (b) Remove the diaphragm support tube (35) from the pivot arms (50,55) and slide the bottom diaphragm assembly (5) clear off the support tube. Remove the plug caps (40). (c) Remove the bottom diaphragm loop assembly (10) and contour foam pad assembly (15) from the seatpan assembly (45). (d) Remove the pivot arms (50,55) by removing screws (60), washers (65) and nuts (70). (e) Remove the kickplate bracket assemblies (75,80) by removing rivets (85). Removal and Disassembly of the Foodtray Assembly - Endbay Refer to IPL Figure 8 and 9 (9) (a) Remove the foodtray assembly (8-5) from the endbay by removing pin (8-10). (b) Separate the foodtray leaf assembly, outer (9-5) and the foodtray leaf assembly, inner (9-15) by removing pins (9-30) and hinges (9-25). (c) Remove the screws (9-75) and slide rod retainers (9-70) and separate the slide plate assembly (9-35), o-rings (9-55), washers (9-60) and slide rod (9-65). (d) Remove the foodtray lift handle (9-80A) by removing screws (9-85A). Endbay Removal Refer to IPL Figure 10 (a) Disconnect and unroute all the control line to the endbay. (b) Remove bolt (30) and washer (35) at the front spreader. (c) Remove the endbay assembly (5) by removing bolts (10) and screw (15). (d) Carefully lift the endbay assembly (5) away from the frame assembly. (10) Disassembly of the Endbay Assembly Refer to IPL Figure 11 (a) Remove the armcap assembly (5B) by removing screws (25) and washers (30). R5 25-29-76 Controlled Page 3005 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (b) Remove the upper heelcap (60) by removing screws (65). (c) Remove the seat control assembly (45A) by removing screws (50) and washers (55). Unroute control lines and lift the control assembly (45A) clear of the endbay. (d) To disassemble the seat control assembly (45A), refer to IPL Fig. 12. (e) Remove the endbay escutcheon (75) by removing screws (80). (f) Remove the frontcap rubstrip (70) by pressing down firmly on the upper tab and unhooking it from the endbay assembly. (g) Remove the rearcap rubstrip (95) by removing screws (100). (h) Remove the endbay rubstrip (85) by sliding the rubstrip forward to disengage the screws (90) from the keyways. (j) Remove the screw (150A). (k) Remove the inner shroud (135) by removing plastic rivets (140). (l) Remove the lowercap shroud (105) and outer shroud (110) by removing screws (125) and rivets (115,120). (m) Remove the bracket, lower shroud (160) by removing rivets (165). (n) Remove the armcap hinge assembly (240) by removing rivets (245). (p) Remove the armcap hinge spacer (250) by removing rivets (255). (q) Loosen screws (200). (r) Remove the pivot assembly (205) by removing bolt (210), spacers (215A), washer (220) and nut (225). Remove set screw (230). (s) To disassemble the pivot assembly (205), refer to IPL Fig. 13. (t) Separate the endbay panels, inner and outer (190,195) by removing screws (200). Remove the bolt (185) and washer (180). (11) Center Console Removal Refer to IPL Figure 15 (a) Disconnect the telephone harnesses and power port harnesses. (b) Remove the center console assembly (5) by removing screws (10) and washers (15, -16). Lift the console clear of the seat assembly. R5 25-29-76 Controlled Page 3006 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (12) Disassembly of the Center Console Assembly Refer to IPL Figure 16 (a) Remove the heelcap (5) by removing screw (15) and pushing upwards to remove the screws (10) out of the keyways. (b) Remove the armcap assembly (170) from the center console by removing screw (180) and sliding the armcap back and lifting away from screws (175). (c) Remove the PCUs (50). (d) Remove the remote jacks (55) by removing screws (65) and bezels (60). (e) Remove the cocktail table assembly (20) by removing screws (40), sliding the cocktail table assembly forward and lifting screws (30) out of the keyways. (f) Remove the power port outlets (125) by removing screws (130). (g) Remove the front shroud assembly (135) by turning the studs (145) and pulling the shroud downwards to remove screws (165) from the keyways. (h) Remove the peanut tray assemblies (70,75) by removing screw (80) and washer (85), spacers (90,95A), bushing - spacer (100) and bushing - pivot (105). (j) Remove the handsets (185), cradles (190), screws (195), cord reels (200), cables (205) and guides (210). (k) Remove the screws (230). (l) Remove the side shrouds (215,220) by removing plastic rivets (225). (13) Lifevest Assembly Removal Refer to IPL Figure 15 (a) Remove the lifevest assembly (20) by removing screws (25) and washers (30) and nuts (35). Lift the lifevest assembly, clear off the seat assembly. (14) Disassembly of the Lifevest Assembly Refer to IPL Figure 18 (a) Remove the shroud, lifevest (15) by removing screws (25), spacer pads (20), washer (30) and nuts (35). R5 25-29-76 Controlled Page 3007 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (15) Phone and SEB Box Removal Refer to IPL Figure 20 (a) Cut the lock straps (20). (b) Remove the mux shroud assembly (35) by quarter turning the studs. (c) Unroute the harnesses (5) or phone cords (10,15) back to the SEB (40) or phone box (45A) and disconnect. (d) Remove the SEB (40) and filter assembly (60) or the phone box (45A). (e) Remove the mux plate assembly (50) by removing screws (55). (16) Power Box Removal Refer to IPL Figure 21 (a) Disconnect and unroute the harnesses (5), removing lock straps (10) and spiral wrap (15) as required. (b) Remove the shroud assembly (20) by quarter turning the studs (30). (c) Remove the power supply (40A) and power J-box (45) by removing screw (50). (d) Remove shims (55). (e) Remove the bracket assembly (60) by removing screws (80), bushings (85) and nuts (90). (17) Baggage Bar Removal Refer to IPL Figure 22 (a) Remove screw (60). (b) Remove screw (40A), washer (45), bushing (50) and nut (55A). (c) Remove screws (15,25), washers (20,30), doubler (10) and nuts (35). (d) Rotate and lift the baggage bar (5) clear off the frame assembly. (18) Disassembly of the Frame Assembly Refer to IPL Figure 23 (a) Remove the spreader assemblies (15,20) by removing bolts (35) and nuts (40). Slide the spreader assemblies (15,20) clear off the beams (5,10). R5 25-29-76 Controlled Page 3008 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (b) Remove the leg assemblies (45) by removing bolts (50), washers (55) and nuts (60). Slide the leg assemblies (45) clear off the beams (5,10). (c) Remove the spreader assemblies (25,30) by removing bolts (35) and nuts (40). Slide the spreader assemblies (25,30) clear off the beams (5,10). (19) Disassembly of the Leg Assembly Refer to IPL Figure 24 (a) Remove the set screw (20), nylon ball (25), stud (15) and anti-rattle nut (10). On the offset leg assemblies, remove the track adaptor assembly (80) by removing the screw (105). (b) Remove the track fitting assembly (50) by removing screw (55A), washers (60,65) and nut (70). (c) Remove the leg doublers (30) by removing screw (35), washer (40) and nut (45). (d) Fit the track fitting saver cover (75) to the removed track fitting (50) in order to protect the studs. R5 25-29-76 Controlled Page 3009 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 3010 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 CLEANING 1. General External surfaces and upholstery should be periodically checked and cleaned. The table on Page 4002 lists cleaning agents and materials used on the seat assembly. Since each cleaning agent has specific features and limitations, carefully follow the instructions given on any product container to ensure best results. The normal cleaning method for seat covers is to remove them from the seat and commercially dry clean with perchlorethane. NOTE: 2. Before dry cleaning, mate the hook attachment with the opposing piece of pile. List of Cleaning Materials and Usage WARNING: SOLVENT CLEANING AGENTS MUST BE USED IN A WELL VENTILATED AREA. AVOID PROLONGED SOLVENT CONTACT WITH SKIN AND AVOID BREATHING VAPORS. OBSERVE APPROPRIATE FIRE REGULATIONS. WARNING: READ AND FOLLOW ALL LABEL DIRECTIONS FOR THE CLEANING MATERIALS IN USE. SOME PRODUCTS CAN BE HAZARDOUS TO HEALTH UNLESS SPECIAL PRECAUTIONS ARE FOLLOWED. CAUTION: DO NOT USE THE FOLLOWING TYPES OF CLEANING AGENTS: CITRUS CLEANERS, TRICHLORETHYLENE, TRICLENE, METHYL ETHYL KETONE (MEK), METHYL ISO BUTYL KETONE (MIBK), LYES, ALKALINE CLEANERS, TOLUOL, BENZOL, ACETONE AND CARBONTETRACHLORIDE. CAUTION: READ AND FOLLOW ALL LABEL DIRECTIONS FOR THE CLEANING MATERIALS IN USE. SOME PRODUCTS MAY CAUSE DAMAGE TO FABRICS OR FINISHES WHEN USED INCORRECTLY. CAUTION: ALWAYS TEST A CLEANING AGENT ON A SMALL, INCONSPICUOUS AREA TO BE SURE IT WILL NOT STAIN OR DAMAGE THE FABRIC OR FINISH. NOTE: Follow the instructions on the product label for the appropriate application and dilution requirements. Hot water enhances the cleaning power of most cleaning compounds. R5 25-29-76 Controlled Page 4001 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 Usage Cleaning Agent Upholstery Isopropyl alcohol, grain alcohol (ethanol), wood alcohol (methanol), naptha, white kerosene, petroleum, ether, heptane, freon TF, mild soap and water, upholstery shampoo Metal: Dirt and Grime Mild soap and water, chlorinated dry cleaning solvent Metal: Grease and Oil Hexane, isopropyl alcohol, grain alcohol (ethanol), chlorinated dry cleaning solvent Fabric-Backed Vinyl Mild soap and water Leather Commercial saddle soap Ultraleather™ Mild soap and water Plastic: Dirt and Grime Mild soap and water, plastic cleaner PCU Isopropyl alcohol, mild detergent, aliphatic naptha Painted Surface Isopropyl alcohol, soapy water (recommended) Tape Adhesive Residue Isopropyl alcohol Equivalent substitutes may be used for cleaning agents listed above. 3. Upholstery Cleaning (For Spots and Small Areas) Both wool and synthetic fabric seat covers require periodic dry cleaning. See Section 11 in this page block for detailed cleaning recommendations. A. Vacuum upholstery thoroughly or brush with a medium stiff bristle upholstery or clothes brush. Do not pound or beat upholstered covers, as this does not effectively clean the upholstery and can hasten the wear. NOTE: Vigorous rubbing may be required to obtain uniform stain removal and to avoid a spotty or blotchy appearance after drying. B. Remove dry or water-borne soil with upholstery shampoo. Dilute the upholstery shampoo as directed on its container and apply to a small area (approximately one square foot) with a small, clean brush. Liberal application will assist in loosening deeply imbedded dirt. C. Oily grease spots are best removed with solvent-type cleaning agents or with solventimpregnated powder. Test the material to be cleaned by first applying the cleaning agent to a small inconspicuous area of the material. Use cleaning agents sparingly, without saturating fabric, to avoid spotting and damage. Apply the cleaning agent with a soft, clean cloth and avoid spreading stains by working from the outer edges of the stain toward the center. D. After using upholstery shampoo, solvent-type cleaning agents, or solvent-impregnated powder, roll a clean turkish towel or other absorbent cloth into a cylindrical shape and wipe off the cleaned area. Rotate the rolled cloth frequently to present a clean section to the fabric surface. R5 25-29-76 Controlled Page 4002 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 4. Bare Metal Parts Cleaning Moisten a clean, dry cloth with a chlorinated dry cleaning solvent and thoroughly wipe metal parts. Repeat as required to remove stubborn accumulations of dirt and grease. Dry with a fresh, clean, dry cloth. 5. Fabric-Backed Vinyl Cleaning Clean fabric-backed vinyl with a mild soap and water solution and wipe clean and dry. Do not use solvent-type of cleaners on vinyl. 6. Leather Cleaning CAUTION: DO NOT USE DETERGENTS, CITRUS CLEANERS, OR SOLVENTS FOR CLEANING LEATHER. Clean leather covers with commercial saddle soap. 7. Ultraleather™ Cleaning CAUTION: DO NOT USE HEAVY DETERGENTS, CITRUS CLEANERS, OR SOLVENTS FOR CLEANING ULTRALEATHER™. DO NOT MACHINE WASH THIS MATERIAL. A. Spot clean with mild soap and water. Air dry or quick dry with warm setting of a hair dryer. Disinfect with a 5:1 bleach solution. Dry cleanable by conventional methods using commercial dry cleaning solvents. B. Remove stains for coffee, tea, red wine, liquor, soft drinks, milk, ketchup, steak sauce, soy sauce, mayonnaise, butter salad, chocolate, cosmetic foundation, lipstick, face cream, suntan oil/lotion, shoe polish and urine using a mild detergent. C. Use a mild cleaning fluid on stains like machine oil and on more stubborn stains when mild detergent is not enough. 8. Plastic Cleaning CAUTION: CITRUS CLEANERS AND CLEANING AGENTS CONTAINING CHLORINATED HYDROCARBONS WILL MAR PLASTIC AND CAUSE DAMAGING CHANGES TO ITS CHEMICAL COMPOSITION. THE USE OF ANY SUCH CLEANING AGENTS WILL REDUCE THE SERVICE LIFE OF PLASTIC PARTS AND VOID WARRANTY CLAIMS. A. Use extreme care when cleaning any plastic surface. Never use abrasive soaps and bleach. Instead, clean all plastic surfaces with a mild soap and water solution or a recommended plastic cleaner. R5 25-29-76 Controlled Page 4003 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 B. Mix liquid soap or plastic cleaner with water to the suggested concentration, depending on the strength needed for cleaning. Apply the solution directly to the plastic and rub with a clean, lint-free cloth to loosen dirt and debris. Wipe with a fresh, clean, lint-free cloth or rinse with water and dry with a turkish towel. 9. Painted Surface Cleaning Clean painted surfaces with non-abrasive soaps or isopropyl alcohol. 10. Adhesive Residue Cleaning CAUTION: DO NOT USE SOLVENTS AS A CLEANER FOR ADHESIVE RESIDUE. SOLVENTS WILL WEAKEN THE BONDED SURFACES. Use a soft cloth wet with small amounts of isopropyl alcohol to remove adhesive residue (i.e., double-sided tape residue). Once the area is clean and free from adhesive residue, use a soft, dry, lint-free cloth to completely dry the area. 11. PCU Cleaning WARNING: PERFORM DE-ACTIVATION PROCEDURES AS DETAILED IN THE DISASSEMBLY CHAPTER OF THE APPROPRIATE AIRCRAFT MANUAL. WARNING: ALIPHATIC NAPTHA IS FLAMMABLE. USE NAPTHA ONLY IN A WELL VENTILATED AREA AWAY FROM FLAMES OR ELEVATED TEMPERATURES. WARNING: USE STANDARD SAFETY PRECAUTIONS FOR HANDLING FLAMMABLE MATERIALS. A. Lightly brush all accessible electrical parts, connections, and wiring with a soft bristle, nonmetallic brush. B. Use dry, filtered air at moderate pressure (25 psi maximum) to blow away loosened dust and dirt. C. Clean all accessible areas with a clean, lint-free cloth or soft bristle brush moistened in aliphatic naptha. D. Allow parts to thoroughly air dry before returning to service. 12. Wool and Synthetic Fabric Cleaning B/E Aerospace provides the following information as a guideline for the care and maintenance of fabric seat covers. Repeated cleaning of the seat covers can reduce the flammability retardant characteristics of the dress cover assembly and, in turn, affect the flammability characteristics of the cushion-cover system. Some cleaning processes may reduce the flammability protection more than others. Please follow the fabric manufacturer’s instructions for dress cover fabric cleaning. The flammability requirements for the dress cover assembly R5 25-29-76 Controlled Page 4004 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 and all other components of the cushion-cover system are defined by 14CFR25.853 (a) and (c). CAUTION: MONITOR SEAT COVERS FOR FLAMMABILITY PERFORMANCE OVER THE LIFE CYCLE PER THE REQUIREMENTS LISTED IN THE PREVIOUS PARAGRAPH. THIS MONITORING PROCESS IS THE RESPONSIBILITY OF THE AIRLINE. A. Flame-Resistant Synthetic Upholstery Fabrics NOTE: (1) As a rule, synthetic fabrics do not require pretreatment because of the inherent non-staining characteristics of the fibers. Laundry machines Use a laundry machine with a load capacity of approximately 40 pounds. Machines with larger loading capacities tend to accelerate abrasion of the fabric. (2) Detergents Use only non-ionic detergents. (3) (4) Fabric preparation for laundering (a) Cover hook tape with pile tape to avoid fabric damage during laundering. (b) Turn covers inside out before laundering. Laundering procedure NOTE: Load the laundry machine to approximately 33% of rated capacity. Loading machines higher than 33% may impair cleaning efficiency and accelerate abrasion of the fabric. Underloading may impair flame retardant properties because of detergent absorption. Follow the guidelines in the following table for laundry machine settings: Cycle First Wash Temperature 85° F Add 1 ounce all-in-one non-ionic detergent Intermediate Rinse 85° F Cycle Time 10-15 minutes 5-10 minutes Second Wash 85°-105° F 0.4 ounce all-in-one 10-15 minutes non-ionic detergent Final Rinse 85° F Drying 131° F maximum Variable; remove promptly when dry to avoid wrinkling. R5 25-29-76 Controlled Page 4005 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 B. Flame-Resistant Wool and Wool-blend Upholstery Fabrics (1) Sort fabrics by stain characteristics and pretreat stains as described below: Type Examples Water soluble Tea, coffee, red wine, fruit, urine Pretreatment method a. Moisten the stain with water. b. Work the spotting reagent into the stain with a spatula or tamping brush. c. Blow steam through the spot. d. Follow steam with forced air and simultaneous vacuuming. Protein-type water soluble Milk, chocolate, blood a. Moisten the stain with water. b. Work the spotting reagent into the stain with a spatula or tamping brush. c. Blow steam through the spot. d. Follow steam with forced air and simultaneous vacuuming. Water in-soluble Ink, lipstick, nail polish, shoe polish a. Work the spotting reagent into the stain (dry fabric) with a spatula or tamping brush. b. Dry clean the fabric before the reagent dries. CAUTION: USING AN ANIONIC OR ALKALINE REAGENT CAN IMPAIR THE FLAME RETARDANT CHARACTERISTICS OF THE FABRIC AND ADVERSELY AFFECT CERTIFICATION. Unknown stains a. Use a commercial, non-ionic stain removal kit that includes procedures for removing unknown stains. b. Test the cleaner on a small area for colorfastness before proceeding. (2) Laundry machines: (a) Use a dry cleaning machine with a load capacity of 20-65 pounds. Machines with larger loading capacities tend to accelerate fabric abrasion. R5 25-29-76 Controlled Page 4006 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (3) (4) (b) Load machines to about 70% of rated capacity. Loading machines higher than 70% may impair cleaning efficiency and accelerate fabric abrasion. Underloading may result in impairment of flame retardant properties because of detergent absorption or excessive shrinkage. (c) Use a non-ionic dry cleaning detergent. (d) Although the dry cleaning process is designed to be waterless, Lantal Textiles, a manufacturer, states that the addition of some water is necessary to reduce the long-term buildup of perspiration salts and sebum, which will cause a reduction in flame retardancy. (e) The temperature of the dry cleaning solvent should be 65°-70° F. Maintain this temperature throughout the dry cleaning process. Higher temperatures can cause undue shrinkage. Preparing fabric for dry cleaning: (a) Cover hook tape with pile tape to avoid fabric damage during dry cleaning. (b) Turn covers inside out. Dip-wash/filter-rinse dry cleaning procedures: STAGE Dip wash PROCEDURE a. Wet the fabric with solvent containing 3-5 grams per liter of detergent. b. Add water mixed with detergent (see the detergent or manufacturer’s recommendation) to the cage with a hopper or automatic metering pump. c. Circulate solvent without filtering for 7-10 minutes. d. Pump out the solvent and centrifuge the fabric. Filter rinse a. Add distilled solvent and circulate continuously from the cage to the button trap to the pump to the filter to the cage for 3-5 minutes. b. Centrifuge for 2 minutes then dry. (5) Drying temperature Tumble dry flame-retardant wool and wool blend fabrics with a maximum outlet air temperature of 120° F. R5 25-29-76 Controlled Page 4007 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 4008 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 INSPECTION/CHECK 1. Visual Inspection of Parts A. All new or existing parts should be visually inspected before being installed to the seat. Use a strong light and a 5x to 7x magnifying glass. When inspecting for damage or corrosion, an inspection mirror must be used to determine the condition of all exposed surfaces. B. Refer to the manufacturer's instructions for detailed inspection, test and overhaul procedure of recline locks and controls. 2. Seat Assembly Serviceability Inspection Following any significant repair work or disassembly of the seat assembly, perform the following checks. Replace any part that fails to meet the requirements of the check with a serviceable part. If a defective part is repairable, note the defect and assign the part for repair. DETAILED INSPECTION (ACCEPT/REJECT EACH ITEM LISTED) Check for required tags on seat assembly. If modifications have been made to seat per service documentation, check that proper tags and /or entries have been applied. Visually check that all parts are clean and free of all cracks, corrosion, deterioration and free from obvious signs of damage. Check back assemblies and installations Check for proper recline function. Check for proper installation and function of Hydrolok. Visually check for missing parts, broken parts and parts that are not securely attached or fastened. Check hardware and metal parts for orientation, tightness and burrs. Check literature spring tension. Check foodtray assemblies Check foodtray latch functions securely. Check foodtray deploys and stows properly. Check food table top shrouds for nicks, cracks, stains, or burrs. NOTE: Burrs, nicks and scratches are defined as material raised above the normal surface which, if not removed, would prevent complete and proper mating of parts and sealing surfaces. Where nicks and scratches allow bare metal to show through a protective finish, note defect and assign part for repair. Dents or other damage must not impair finish or functional operation of any part. Check foodtray surfaces for serviceable appearance. Check seatbelts and seatbelt shackles for serviceability, proper installation and tightness of attaching hardware. R5 25-29-76 Controlled Page 5001 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 DETAILED INSPECTION (ACCEPT/REJECT EACH ITEM LISTED) Endbay/Arm Check PCU for function and proper installation. Check armrest tension and lockout. Check recline buttons for proper function. Check cable routings. Check hardware and metal parts for proper direction, tightness and sharp edges/burrs. Check paint and finishes for chipping and worn spots. Note condition of bonding on parts and assemblies. Bottom diaphragm Check for proper installation Check for proper tension. Diaphragm should not have sags or appear loose. Check for tears or other damage to fabric Check for part identification Baggage bar Check baggage bar for serviceable appearance Check to make certain baggage bar plugs are installed. Check all hardware for tightness, burrs and sharp edges SEB Check all SEB hardware and metal surfaces for sharp edges Check for proper cable routing Check connectors for proper installation Dress Covers Check all dress covers for cleanliness and serviceability Check dress cover labels for number of cleanings NOTE: Refer to CLEANING section for information on flammability retardancy as affected by dry cleaning. Check all dress covers for proper fit and alignment Check rear track fittings and front track studs for secure attachment to the floor track. Also check for wear or deformation of these parts. Check lifevest and lifevest pouch for serviceability R5 25-29-76 Controlled Page 5002 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 REPAIR 1. General Common repair procedures for seating products typically involve replacement of high-wear, aesthetic components, such as armcaps, cushion covers and shrouds. Removal and installation of many of these parts may be accomplished using the Assembly and Disassembly sections or by referring to the figures in the Illustrated Parts List. This section describes tasks which may require an additional amount of procedural information. PROCEDURE Repair Damaged Surfaces Remove and Install Headrest Adjust Headrest Adjust Headrest Ear Assemblies Remove and Replace Seat Control Cable Assemblies Adjust Back Recline Remove and Replace Recline Control Hydrolok Remove and Replace Gaslock Remove and Replace Lumbar Valve Tube R5 25-29-76 Controlled Page 6001 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 REPAIRING DAMAGED SURFACES 1 Minor Surface Damage (Light Alloy and Steel Components) A. Blend out minor surface damage using abrasive cloth. NOTE: Minor surface damage is considered to be abrasions and scratches. B. If applicable, restore the surface treatment in accordance with local regulations. 2. Minor Surface Damage (Thermoformed Plastic Panels) A. Clean plastic surface with alcohol or an alphatic solvent such as mineral spirits, heptane or hexane. B. Fill any surface irregularities with catalyzed polyester resin filler. NOTE: Catalyze only the amount of filler that will be used immediately because the material will begin to harden within five minutes. An automotive body repair surfacing putty may be used as a fill material. C. Level with spatula before filler hardens and restore texture by stippling with a stiff bristle brush. D. After filler has fully hardened (10 to 15 minutes), rub the area lightly with an abrasive cloth to blend repair into adjacent areas. 3. Screw Threads A. Slightly rough or burred threads may be cleaned up using a thread file, or small three corner file, on external threads, and a plug tap of correct size for internal threads. B. Components having stripped threads, or threads which cannot be suitably cleaned up as described above, must be replaced by an approved spare. 4. Removal of Surface Corrosion A. Light alloy components (1) Remove corrosion using an abrasive cloth. (2) If applicable restore the surface treatment in accordance with local regulations. B. Steel components Remove corrosion using a coarse grade wire brush, steel wool or abrasive cloth. R5 25-29-76 Controlled Page 6002 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 5. Upholstery - Fabric WARNING: DO NOT USE NYLON OR COTTON THREAD. THE BACK AND BOTTOM CUSHION ASSEMBLIES USED ON THE SEAT MODELS IDENTIFIED IN THIS MANUAL, ARE CERTIFIED TO CONFORM TO AWN59. CHANGING OF EITHER DRESS COVER OR FIRE BLOCKER MATERIALS MAY CAUSE CUSHIONS TO FAIL THE REQUIREMENTS OF AWN59 AND WILL EFFECTIVELY VOID THE BACK OR BOTTOM CUSHION CERTIFICATION. A. Excessively worn or damaged dress covers must be discarded. B. Flotation straps may be repaired using Kevlar thread. Small cuts and tears can be repaired in the same manner. R5 25-29-76 Controlled Page 6003 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 REMOVE, INSTALL AND ADJUST HEADREST 1 2 7 3 6 5 4 Item Description Item Description 1 Headrest assembly 5 Release latch 2 Bolt 6 Slide plate assembly 3 Headrest ear assembly 7 Friction bushings 4 Lock nut FOR SPECIFIC PARTS INFORMATION, SEE IPL FIGURE 2 AND FIGURE 5. R5 25-29-76 Controlled Page 6004 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 NOTE: For specific parts information, refer to Figure 2 and Figure 5 of the Illustrated Parts List. 1. Removing and Installing Headrest A. Slide headrest (1) up until it is not quite fully extended. B. Lift release latch (5) with finger and continue to slide headrest (1) up until it releases. A firm, steady pull is necessary to disengage the slide plate assembly (5). C. To install, align slide plate assembly (5) with friction bushings (7), then push downward firmly. NOTE: Headrest should install with a downward pressure of 8-20 pounds. 2. Adjusting Headrest Adjust headrest (1) for installation pressure required by tightening or loosening friction bushings (7). 3. Adjusting Headrest Ear Assemblies NOTE: Headrest ear assemblies (3) are designed to be adjustable with a pressure of 12-15 pounds. Regulate amount of pressure required to adjust headrest ear assemblies(3) by tightening or loosening bolt (2) and lock nut (4). R5 25-29-76 Controlled Page 6005 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 REMOVE, INSTALL AND ADJUST BACK RECLINE HYDROLOCK 2 12 11 1 3 4 5 6 10 9 8 7 Item Description Item Description 1 Screw 7 Washer 2 Recline arm 8 Washer 3 Washer 9 Jam nut 4 Nut 10 Actuator 5 Hydrolok 11 Bracket 6 Jam nut 12 Spreader FOR SPECIFIC PARTS INFORMATION, SEE IPL FIGURE 3 AND FIGURE 5. R5 25-29-76 Controlled Page 6006 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 NOTE: For specific parts information, refer to Figure 3 and Figure 5 of the Illustrated Parts List. 1. Removing Recline Hydrolok A. Place seat in the fully upright position to remove tension from the hydrolok. B. Remove clip on actuator from the threaded end of the hydrolok. Retain for reuse. C. Remove screw (1), washer (3) and nut (4) securing hydrolok (5) to recline arm (2). Retain for reuse. D. Remove jam nut (9) and washer (8) from threaded end of hydrolok (5). Retain for reuse. E. Remove hydrolok (5) from bracket (11) mounted to side of spreader. F. Remove washer (7) and jam nut (6) from hydrolok (5). Retain for reuse. 2. Installing Back Recline Hydrolock A. Install jam nut (6) and washer (7) to hydrolok (5). B. Install hydrolok (5) into bracket (11) mounted on side of spreader. C. Install washer (8) and jam nut (9) as shown. D. Install hydrolok (5) to recline arm (2) with screw (1), washer (3) and nut (4). E. Install clip-on actuator (10) to threaded end of hydrolok (5). F. Test operation. 3. Adjusting Back Recline A. Loosen jam nut (9) used to secure hydrolok (5) to bracket (11). B. Position seat back to desired number of degrees of recline angle. C. Tighten jam nut (9). D. Test operation. R5 25-29-76 Controlled Page 6007 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 REMOVE AND INSTALL CONTROL CABLE ASSEMBLY 2 1 3 5 4 6 Item Description Item Description 1 Control lever 4 Cable Assembly 2 Seat control bezel 5 Screw 3 Cable Lever 6 Extension spring NOTE: Some illustrated parts are not individually procurable, but are component parts of procurable assemblies. FOR SPECIFIC PARTS INFORMATION, SEE IPL FIGURE 12 R5 25-29-76 Controlled Page 6008 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 NOTE: For specific parts information, refer to Figure 12 of the Illustrated Parts List. 1. Removing Control Cable Assembly NOTE: Retain all parts removed during this procedure for reuse. A. Identify and tag all control cables to be removed. B. Relieve tension on cable assembly (4) by returning component to the normal position. C. Remove actuator from hydrolok. D. Remove screw (5) from lever cable (3). E. Remove control lever (1). F. Carefully remove extension spring (6) from either end. G. Remove cable assembly (4) from lever cable (3). 2. Installing Control Cable Assembly CAUTION: MAKE SURE THAT YOU ATTACH CONTROL CABLE(S) IN THE CORRECT POSITION. CONTROL CABLES HAVE SPECIFIC LENGTHS, DEPENDING ON FUNCTION. INCORRECT INSTALLATION WILL PREVENT PROPER OPERATION AND MAY CAUSE DAMAGE TO SEAT MECHANISMS. A. Make sure that affected component is in the normal position. B. Route the cable properly through the seat and endbay and secure with original cable clamp(s) or new cable tie(s). C. Install cable assembly (4) to lever cable (3). D. Attach extension spring (6). E. Install control lever (1) through seat control bezel (2). F. Install lever cable (3) and screw (5). G. Install actuator to hydrolok. H. Adjust tension and test for proper operation. R5 25-29-76 Controlled Page 6009 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 6010 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 ASSEMBLY 1. General Assembly procedures can vary slightly for different Millennium seat models. A. Before assembly, inspect all parts for wear and/or damage that could cause failure of the seat assembly or any of its component assemblies. Always replace attaching parts (cotter pins, screws, washers, nuts, grommets, cable holders, etc.) with new parts. Replacing these low-cost items will help decrease maintenance that is necessary when these items fail. B. LoctiteTM products or equivalent are required for seat assembly. 2. Installation of Seat Assembly on Aircraft A. Clean floor tracks, studs, and track fittings when seats are moved. This will prevent unwanted wear on fastener assemblies. B. To attach the seat assemblies to the aircraft, put the track studs and track fittings at the bottom of the leg assemblies into matching notches in the floor track. C. Slide the seat assembly forward or aft approximately one-half inch until the locking mechanism on the track fitting can be pressed into an access hole. WARNING: BE SURE TO TIGHTEN ALL SCREWS, BOLTS AND NUTS TO THE CORRECT TORQUE VALUE. IF YOU DO NOT USE THE CORRECT TORQUE VALUE, THE SEAT OR PARTS OF THE SEAT COULD BECOME LOOSE. THIS COULD CAUSE DAMAGE OR INJURY. IF THE TORQUE VALUE IS NOT SHOWN, USE THE TORQUE VALUES GIVEN IN TABLE 8001 IN THE FITS AND CLEARANCES SECTION (PAGE BLOCK 8000). WHEN YOU TIGHTEN A NUT AND BOLT THAT ARE USED TOGETHER, MEASURE THE TORQUE VALUE ON THE NUT. IF YOU CANNOT GET ACCESS TO THE NUT OR A NUT IS NOT USED, MEASURE THE TORQUE ON THE BOLT. D. To lock the track fitting into position, tighten the Allen screw, which will push the arm against the top surface of the aircraft floor tracks. E. Tighten the anti-rattle nut under the forward leg hand tight plus 1/4-turn. R5 25-29-76 Controlled Page 7001 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 3. Storage Instructions A. General The seat is essentially corrosion resistant and special preservation is not required. B. Procedures 4. (1) Wrap the seat assembly in waterproof wrapping paper (Federal Specification UU-P217 or equivalent) or a plastic cover. Use tape (Federal Specification JAN-P-127 or equivalent) to secure the wrapping paper or cover. (2) Identify the seat assembly part number and overhaul date on a tag or in a convenient location on the seat assembly wrapper. (3) Store the seat assembly in a cool, dry place away from sunlight and heat sources. Assembly Procedures (1) Assembly of the Leg Assembly Refer to IPL Figure 24 (2) (a) Attach the front stud (15) and anti-rattle nut (10) to the leg, machined (5). Secure with set screw (20) and nylon ball (25). On the offset leg assemblies, attach the track adaptor assembly (-80) with the screw (-105). (b) Attach the leg doublers (30) with screw (35), washer (40) and nut (45). (c) Attach the track fitting assembly (50) with screw (55), washers (60,65) and nut (70). (d) Fit the track fitting saver cover (75) to the track fitting (50) in order to protect the studs. Assembly of the Frame Assembly Refer to IPL Figure 23 (a) Attach the center spreader assemblies (25,30) with bolts (35) and nuts (40). Apply loctite 271 to the threads protruding out of the end of the nut. Torque bolts to 70-80 IN.LBS. (b) Attach the leg assemblies (45) with bolts (50), washers (55) and nuts (60). (c) Attach the outboard and inboard spreader assemblies (15,20) with bolts (35) and nuts (40). Apply loctite 271 to the threads protruding out of the end of the nut. Torque bolts to 70-80 IN.LBS. R5 25-29-76 Controlled Page 7002 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (3) Installation of the Baggage Bar Refer to IPL Figure 22 (4) (a) Rotate and move the baggage bar (5) into position on the frame assembly. (b) Attach the baggage bar (5) to the spreaders with screw (40A), washer (45), bushing (50), nut (55A) and screw (60). (c) Attach the baggage bar (5) to the leg assemblies with screws (15,25), washers (20,30), doubler (10) and nuts (35). Installation of the Power Box Refer to IPL Figure 21 (5) (a) Attach the bracket assembly (60) with screws (80), bushings (85) and nuts (90). (b) Install the power supply (40A) and power J-box (45) with screws (50) and shims (55). (c) Connect and route the harnesses (5), attaching lock straps (10) and spiral wrap (15) as required. (d) Install the shroud assembly (20) and quarter turn the studs (30) to lock the shroud into position. Installation of the Phone Box Refer to IPL Figure 20 (6) (a) Attach the mux plate assembly (50) with screws (55). (b) Install the SEB (40) and filter assembly (60) or phone box (45A). (c) Install the pile (30). (d) Install and route the harnesses (5) or the phone cords (10,15) through the frame assembly, installing spiral wrap (25) and lock straps (20). (e) Install the mux shroud assembly (35) and quarter turn the studs to lock the shroud into position. Assembly of the Center Console Assembly Refer to IPL Figure 16 (a) Attach the peanut tray assemblies (70,75) with screws (80), washers (85), spacers (90,95A), bushing - spacer (100) and bushing - pivot (105). R5 25-29-76 Controlled Page 7003 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (b) Attach the side shrouds (215,220) with plastic rivets (225). (c) Install screws (230). (d) Install the cradles (190) with screws (195). (e) Install the handsets (185), cord reels (200), cables (205) and guides (210). (f) Attach the screws (165) to the front shroud assembly (135). Align the screws (165) in the keyways on the console structure and slide the front shroud assembly upwards to engage the screws. Adjust the screws (165), as required, to produce a snug fit. When the screws have been properly adjusted and the front shroud assembly is in place, turn the studs (145) to lock the front shroud assembly into position. (g) Install the power port outlets (125) with screws (130). (h) Attach the screws (30) and washers (35) to the cocktail table assembly (20). Align the screws (40) in the keyways on the console structure and slide the cocktail table assembly backwards to engage the screws. Adjust the screws (30), as required, to produce a snug fit. When the screws have been properly adjusted and the cocktail table assembly is in place, attach screws (40). (j) Attach screws (175) to the console structure. Align the keyways on the armcap assembly (170) onto the screws (175) and slide the armcap assembly (170) into position. Adjust the screws (175), as required, to produce a snug fit. When the screws (175) have been properly adjusted and the armcap assembly (170) is in place, attach screw (180). (k) Attach the screws (10) to the heelcap assembly (5). Align the screws (10) in the keyways on the console structure and slide the heelcap assembly (5) downwards to engage the screws. Adjust the screws (10), as required, to produce a snug fit. When the screws (10) have been properly adjusted and the heelcap assembly (5) is in place, attach screw (15). (l) Install the PCUs (50). (m) Install the remote jacks (55) with screws (65) and bezels (60). (7) Installation of the Center Console Assembly Refer to IPL Figure 15 (a) Align the center console assembly (5) onto the frame assembly and attach with screws (10) and washers (15, 16). (b) Route and install telephone and power port harnesses. R5 25-29-76 Controlled Page 7004 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (8) Assembly of the Lifevest Assembly Refer to IPL Figure 18 (a) (9) Attach the shroud, lifevest (15) with screws (25), spacer pads (20), washer (30) and nuts (35). Installation of the Lifevest Assembly Refer to IPL Figure 15 (a) Align the lifevest assembly (20) on the frame assembly. (b) Attach the lifevest assembly (20) with screws (25), washers (30) and nuts (35). (10) Assembly of the Endbay Assembly Refer to IPL Figure 11 (a) Install the nutplates (260,270,280, 286) with rivets (265,275,285, 287). (b) Align the pivot assembly (205) and spacers (215A) with the endbay panels, inner and outer (190,195). Attach with bolt (210), washer (220) and nut (225). (c) Install set screw (230). (d) Attach the endbay panels (190,195) together with screws (200). (e) Attach the bolt (185) and washer (180). (f) Install the hook and pile fastenings (290,295,300) and foam pad (155). (g) Install the armcap hinge assembly (240), endbay stiffener (235), armcap hinge spacer (250) with rivets (245,255). (h) Install the hat section (170) with rivets (175). (j) Install the bracket, lower shroud (160) with rivets (165). (k) Attach the lower cap shroud (105) and outer shroud (110) with screws (125) and rivets (115,120). Install pile (130). (l) Attach the innershroud (135) with rivets (140) and hook (145). (m) Attach the screw (150A). (n) Install screws (90). Attach the endbay rubstrip (85) by sliding the rear rubstrip so as to engage screws (90) on the keyways. (p) Attach the rearcap rubstrip (95) with screws (100). R5 25-29-76 Controlled Page 7005 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (q) Attach the frontcap rubstrip (70) by pressing into position at the front of the endbay assembly. (r) Attach the endbay escutcheon (75) with screws (80). (s) Attach the seat control assembly (45A) with screws (50) and washers (55). Route the control line through the endbay. (t) Attach the upper heelcap (60) with screws (65). (u) Attach the armcap assembly (5) with screws (25) and washers (30). (v) Attach the placard, mount bezel (35B) with screws (40). (11) Installation of the Endbay Refer to IPL Figures 10 (a) Carefully lift the endbay assembly (5) into position on the frame assembly. (b) Attach the endbay assembly (5) with bolts (10) and screw (15). (c) Tighten the bolt (30) at the front stretcher. (d) Install pocket cover (20) and pile (25). (e) Route the control line to the back assembly and connect as required. (12) Assembly and Installation of the Foodtray Assembly Refer to IPL Figures 8 and 9 (a) Join the outer foodtray leaf assembly (9-5) and the inner foodtray leaf assembly (9-15) with hinges (9-25) and pins (9-30). Install the set screws (9-20) and dowel pins (9-10). (b) Assemble the slide plate assembly (9-35), o-rings (9-55), washers (9-60) and slide rod (9-65) and attach with screws (9-75) and slide rod retainers (9-70). Install set screws (9-45) and slide cap (9-50). (c) Attach the foodtray lift handle (9-80A) with screws (9-85A). (d) Install the foodtray assembly (8-5) onto the endbay assembly with pin (8-10). (e) Adjust set screws (9-20,9-45) as required. R5 25-29-76 Controlled Page 7006 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (13) Assembly of the Back Assembly Refer to IPL Figures 4 and 5 (a) Attach the nutplates (5-115) with rivets (5-120). (b) Attach the recline arm (5-10) with bolts (5-16), washers (5-20, 5-22) and nuts (524). (c) Attach the Hydrolok (5-25) with screw (5-30A) and nut (5-35). (d) Attach the spring assemblies (5-40,5-45) with screws (5-50). (e) Attach the roller support bracket (5-55) with the roller assemblies (5-70A), screws (5-60), spacers (5-65), bushings (5-80) and spacers (5-85). Install covers (5-110). (f) Attach the headrest friction plate (5-90) with screws (5-95), nuts (5-107), springs (5-97), washers (5-100A) and friction block (5-105B). Install covers (5-110). (g) Install hook (5-125,5-130). (h) Install the screws (5-135) and washers (5-140). (j) Install the fabric support assembly (4-15) onto the back assembly (4-5) with adhesive. (j) Install the back pad (4-20), the back cushion assembly (4-10) and fireblock (-25) onto the back assembly (4-5) with adhesive. (14) Installation of the Back Assembly Refer to IPL Figure 3 (a) Carefully lift the back assembly (5A) onto the seat assembly. (b) Attach the back assembly (5A) to the spreader assembly, at the non-Hydrolok side, with bolt (50A), washer (55), shackle fitting (60), bushing (65) and spacers (70). NOTE: Torque item (50A), bolt, to 80 ± 5 IN-LB. (c) Attach the back assembly (5A) to the spreader assembly, at the Hydrolok side, with bolt (10A), washers (15,40), shackle fitting (20), bushing (25), spacers (30,35) and nut (45). NOTE: Torque item (10A), bolt, to 80 ± 5 IN-LB. (d) Attach the spacer (80A) and bolt (75). R5 25-29-76 Controlled Page 7007 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (e) Connect the Hydrolok to the spreader assembly with nuts (85) and washers (90). (f) Attach the back assembly to the seatpan assembly (refer to paragraph 16). (g) Connect the control lines at the Hydrolok. (15) Assembly of the Seatpan Assembly Refer to IPL Figure 7 (a) Install the kickplate bracket assemblies (75,80) with rivets (85). (b) Attach the pivot arms (50,55) with screws (60), washers (65) and nuts (70). (c) Install the bottom diaphragm loop assembly (10) and contour foam pad assembly (15) onto the seatpan assembly (45) and secure with the zipper. (d) Attach the plug caps (40) to the diaphragm support tube (35). Slide the bottom diaphragm assembly (5) on to the support tube. Align the diaphragm support tube (35) on the pivot arms (50,55). (e) Attach the bottom diaphragm assembly (5) to the welded seatpan assembly (45) by engaging the hook and pile fastening. Secure with the zipper. (16) Installation of the Seatpan Assembly Refer to IPL Figure 6 (a) Attach the seatpan assembly (5) to the backrest assembly with screws (10A), washers (15), bushings (20) and spacers (25). (b) Attach the kickplate assembly (30) with screws (35) and washers (40). (17) Assembly of the Headrest Assembly Refer to IPL Figure 2 (a) Install the pivot bracket (55) to the headrest slide plate (50) by installing the screws (60), the washers (65) and the spacers (70). (b) Install the headrest release latch (80) by installing the screw (85) and the dowel pin (75). (c) Attach the slide plate assembly (45A) to the center body assembly (5) with bolt (90), washers (95,100), spacer (105) and nut (110). (d) Attach the ear assemblies (10,15) to the center body assembly (5) with bolt (20), washers (25,30), spacer (35) and nut (40). R5 25-29-76 Controlled Page 7008 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 (18) Installation of the Headrest & Dress Covers Refer to IPL Figure 1 (a) Attach the lumbar covers (50) and lumbar cushion assemblies (55) . (b) Fit the back cover assemblies (40) and the literature pocket covers (45) and engage the hook and pile fastening. (c) Fit the headrest covers (30) onto the headrest assemblies (35) and engage the hook and pile fastening. (d) Attach the headrest assemblies (35) to the backrest assemblies by aligning the slide plate onto the rollers and sliding the headrest downwards until the latch engages. NOTE: Ensure that 12-15 lbs. of torque will allow the ear to be consistently rotated (Ref SB 25-20-2644). NOTE: Ensure that 10-12 lbs. of torque will allow the headrest to slide consistently. NOTE: The force must be exerted at the end of the ear and top of the headrest. NOTE: Ensure that forward tilt pivot is set at 8-20 lbs (Ref SB 25-20-2644). (19) Installation of the Bottom Cushion and Seat Belt Refer to IPL Figure 1 (a) Fit the bottom cover assembly (10) to the bottom cushion (15) and engage the hook and pile fastening. Fit the bottom cushion assemblies to the seatpan diaphragm by firmly engaging the hook and pile fastenings. (b) Attach the seatbelts, buckles and tips (20,25). R5 25-29-76 Controlled Page 7009 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 7010 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FITS AND CLEARANCES 1. General Normal maintenance of the seat assemblies does not require fit and clearance information. 2. Torque Tables A. Threaded Fastener Torque Ranges When specific torque values are not shown on the applicable drawing, use the torque values in Table 8001 as a guide when you tighten nuts, studs, bolts, and screws. When you tighten a nut and bolt that are used together, measure the torque value on the nut. If you cannot access the nut or a nut is not used, measure the torque on the bolt. (1) Standards and Specifications for Values (a) Self-Locking Fasteners A self-locking fastener supplies more resistance when it is turned on a thread. Because of this, you must add the prevailing torque value to the standard torque value to get the correct torque value for a self-locking fastener. This will help prevent unwanted vibrations that can work the fastener loose. (See Table 8001.) NOTE: (b) The prevailing torque value is taken from IFI 100/107, PrevailingTorque Type Steel Hex Nuts, Grade B, Industrial Fasteners Institute, 1987. B/E Aerospace supplied the values for Self-Locking Fasteners, sizes 4-40 and 6-32. Standard Fastener Values Most standard fastener values are from the Standard Aircraft Handbook. Refer to it for any fastener not listed in Table 8001. NOTE: B/E Aerospace supplied the values for Standard Fasteners, sizes 440 and 6-32. R5 25-29-76 Controlled Page 8001 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 Table 8001 Threaded Fastener Torque Values THREAD/IN THREAD TYPE STANDARD FASTENERS (IN-LB) MIN-MAX PREVAILING TORQUE (IN-LB) MAX REFERENCE ONLY SELF-LOCKING FASTENERS (IN-LB) MIN-MAX 4-40 Coarse 3-5 3 6-8 6-32 Coarse 7-10 8 15-18 8-32 Coarse 12-15 12 24-27 10-32 Fine 20-25 13 33-38 1/4-28 Fine 50-70 30 80-100 5/16-24 Fine 100-140 60 160-200 R5 25-29-76 Controlled Page 8002 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 SPECIAL TOOLS, FIXTURES AND EQUIPMENT 1. Tools A. No special tools, fixtures or equipment are required to maintain B/E Aerospace passenger seats. Only common hand tools are required to assemble and/or disassemble the seats. Refer to Table 9001 for a list of suggested common hand tools. NOTE: Equivalent substitutes may be used for tools listed in Table 9001. B. Special fabricated hand tools can be used to perform specific tasks such as the removal of bushings or the tightening of an eyebolt. However, their use is not required. See Table 9002 for a list of suggested fabricated hand tools. NOTE: Equivalent substitutes may be used for items listed in Table 9002. Table 9001 Suggested Common Hand Tools HAND TOOLS QUANTITY REQUIRED 7/16" Opened, Closed Ended Wrench 2 9/16" Opened, Closed Ended Wrench 2 11/32" Opened, Closed Ended Wrench 2 1/2" Opened, Closed Ended Wrench 2 7/16" Thin Wall Socket - 3/8" Drive 2 3/8" Thin Wall Socket - 3/8" Drive 2 1/2" Thin Wall Socket - 3/8" Drive 2 9/16" Thin Wall Socket - 3/8" Drive 2 Ratchet, 3/8" Drive 1 4" Ratchet Extension, 3/8" Drive 1 6" Ratchet Extension, 3/8" Drive 1 8" Ratchet Extension, 3/8" Drive 1 Rubber Tipped Hammer 1 Ball Peen Hammer 1 Scratch Awl 1 #1 Flat Screwdriver 1 #2 Flat Screwdriver 1 #2 Phillips Head Screwdriver 1 R5 25-29-76 Controlled Page 9001 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 Table 9001 (Continued) Suggested Common Hand Tools HAND TOOLS QUANTITY REQUIRED #3 Phillips Head Screwdriver 1 Allen Wrench Set 1 Allen Wrench Set - Metric 1 Snap Ring 1 Cleat Coil Pliers 1 Tape Measure, 6' 1 Wire Cutters 1 Razor Knife 1 Reamer Set 1 Channel Lock 1 File Set 1 Scissors 1 Pliers 1 Needle Nose Pliers 1 Tie Wire Cutters 1 Table 9002 Special Fabricated Hand Tools HAND TOOLS 2. QUANTITY REQUIRED Bushing Knocker 1 Eyebolt Turner #1 1 Fixtures There are no special fixture requirements. 3. Equipment There are no special equipment requirements. R5 25-29-76 Controlled Page 9002 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 ILLUSTRATED PARTS LIST 1. Introduction A. Purpose This Illustrated Parts List (IPL) helps to find and identify procurable parts of the seats. A procurable part is one that can be purchased as a replacement part. B. How to Use the IPL Each IPL figure has an illustration that uses item numbers to identify parts of the seat that can be replaced. Each illustration is followed by a parts list that shows all of the parts in item number sequence. Each parts list has the following columns: FIG. ITEM The number at the top of this column identifies the IPL Figure. The other numbers are item numbers. An item number is given to each part that can be replaced and is shown on the illustration. A dash (-) before an item number shows that the part is not shown on the illustration. PART NUMBER Identifies installations, assemblies and parts by number. If a part number is followed by (NP), that part is not procurable. AIRLINE PART NO. Blank column for airline use. NOMENCLATURE Identifies parts by name and is indented to show how parts are related to the primary assembly. See the next page for more details. EFF CODE Identifies which parts are used on the primary assemblies. The primary assemblies are shown at the start of the IPL figure. An effectivity code letter is given to each primary assembly. Each part used on a primary assembly is given the effectivity code letter of that primary assembly. If a part is used on all of the primary assemblies, it is not given an effectivity code. The effectivity codes in each IPL figure apply only to that figure and are not related to the effectivity codes in any other IPL figure. UNITS/ASSY Identifies the quantity of each part used on the primary assembly. R5 25-29-76 Controlled Page 10001 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 The Nomenclature column uses bullet indents (•) to show the relationship between parts, as in the examples that follow: Assembly or Installation This is the primary assembly/installation and is not indented. • Subassembly/Detail Part This is a subassembly or detail part of the primary assembly/installation. It is indented with one bullet (•). If parts with two bullets (• •) follow the subassembly, they are part of the subassembly. • • Sub-subassembly/Detail Part A sub-subassembly/detail part of the subassembly. It is indented with two bullets (• •). If you can purchase the one indent subassembly/part, this part will be included. If parts with three bullets (• • •) follow the sub-subassembly, they are part of the sub-subassembly. • • • Detail Part 2. Detail part for the sub-subassembly. It is indented with three bullets (• • •). If you can purchase the two-indent part, this part will be included. ATTACHING PARTS Shows that the parts listed after it attach the part or parts before it. *** Shows the end of an ATTACHING PARTS list. Also used at the end of individual IPL parts listing tables. Vendor Codes Vendor Code numbers are specified in the current issue of Federal Supply Code for Manufacturers, Catalogue Handbooks H4-1, H4-3 and/or NATO codes, and are available on the Internet at https://www.bpn.gov/bincs/search_info.asp. 3. Trim and Finish Codes All seat part numbers and some parts in the IPL include a Trim and Finish (T & F) code at the end of the part number. Be sure to include the T & F codes when purchasing replacement parts. Example: part number 1002913-001AG01 where AG01 is the part’s T & F code. 4. LPxxxxx Parts Versus MSxxxxx Parts The “LP” in LPxxxxx part numbers indicates that the part (typically a fastener such as a bolt, screw or nut) has “lockpatch” material applied to the threads to make the part self-locking. When such a part is used, the lockpatch is compressed, creating a much stronger metal-tometal contact and positive resistance to vibration and loosening. YOU CAN REPLACE AN LPxxxxx PART WITH AN EQUIVALENT MSxxxxx PART ONLY IF YOU USE A LOCKING MATERIAL (SUCH AS LOCTITETM) ON THE THREADS OF THE MSxxxxx PART. For example, you may use part number MS27039 in place of part number LP27039 only when you apply LoctiteTM to the threads before installation. R5 25-29-76 Controlled Page 10002 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 5. Alpha/Numerical Index - PART NUMBER AA-710-27 (NP) AN316-6R AN3-24A AN4-10A AN4-10A AN4-10A AN4-20A AN4-20A AN4-20A AN4-24A AN4-25A AN4-30A AN4-33A AN4-4A AN960-10 AN960-10 AN960-10L AN960-416 AN960-416 AN960-416 AN960-416 AN960-416 AN960-416 AN960-416 AN960-416 AN960-416 AN960-416L AN960-516 AN960-616L AN960-616L AN960-6L AN960-6L AN960-6L AN960-8 AN970-3 AN970-3 AN970-3W AN970-4 APPPHC810 B14-498026 B14-498026 BAC29PPS42096 BALL-NYLON AIRLINE PART NO. IPL FIG 5 3 23 5 10 11 23 3 11 2 2 3 2 3 6 15 7 24 5 3 3 3 10 11 11 15 6 24 25 13 18 18 11 11 22 22 22 25 5 2 2 16 24 ITEM 6 85 35 15 30 185 50 50 210 -20A 20 10 90 75 40 30 65 40 20 15 40 55 35 180 220 15 15 60 30 25 30 -30A 30 55 30 45 20 -20A 110 25 95 45 25 R5 25-29-76 Controlled TTL REQ 1 2 2 2 1 1 2 1 1 1 1 1 1 1 4 2 2 1 2 1 1 1 1 1 1 6 2 2 1 1 2 3 5 2 2 1 2 1 6 4 4 1 1 Page 10003 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER C169 C23CE-4300-02 C23CE-4300-04 C23PH-6001-02-9E C23PH-6001-03-9E C23PH-6004-01-0 C23PM-6200-01 C23PU-6920-01 C23PU-6967-01 CBF1310-1 CP19270045 CSP-42 CSP-42 CSP-43 CSP-43 CSP-43 CSP-43 CSP-43 CSP-43 CSP-43 CSP-43 CSP-43 CSP-43 CSP-43 CSP-44 CSP-44 CSP-44 CSP-44 CSP-44 CSP-45 CSP-46 DA10135-001 DB01-009 DS12X375 F000009 FHA-032-24 HT1/4FR-B HT3/8FR-B HT3/8FR-B HV17500-09 K1000-3 LC040D03M LE02B01M LP24693-29 LP24693-31 AIRLINE PART NO. IPL FIG 16 20 20 20 20 16 16 16 16 1 1 16 16 18 18 18 11 16 16 16 16 16 16 16 11 16 16 16 16 16 16 20 9 2 19 21 20 19 21 5 5 5 12 12 12 ITEM 166 -45 45A 10 15 205 185 190 200 -195 15 270 365 45 70 110 255 240 260 315 355 375 385 440 245 265 280 305 345 -115 -440A -60 55 75 10 -65 -25 15 -15 25A 115 97 25 20A -20 R5 25-29-76 Controlled TTL REQ 2 1 1 1 1 2 2 2 2 1 2 2 2 3 2 18 7 6 6 3 6 4 4 2 6 4 12 2 4 2 2 1 3 1 10 1 AR AR AR 1 6 2 2 2 2 Page 10004 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER LP24693-S28 LP24694-S185 LP27039-0805 LP27039-0806 LP27039-0812 LP27039-1-05 LP27039-4-06 LP27039-4-20 LP35206-225 LP4-11A LP565A1032H3 LP565A1032H6 M13100001-2-6 M1-99-128 MC54045-85 MF6000-06 MK1000-3 MK1000-08 MK2000-06 MK2000-08 MK2000-3 MS16997-20 MS20470AD8-24A MS21042-3 MS21042-3 MS21042-3 MS21042-4 MS21083N6 MS21083N6 MS21083N6 MS21090-0621 MS21209F4-15L MS21266-1N MS24671-8 MS24693-4B MS24693-S25 MS24693-S25 MS24693-S27 MS24693-S27 MS24693-S274 MS24694-S104 MS24694-S118 MS27039-0806 MS27039-0806 MS27039-0807 AIRLINE PART NO. IPL FIG 9 24 11 16 16 2 25 10 9 10 9 11 22 18 12 11 16 11 11 11 18 16 24 21 22 23 3 17 24 13 21 16 18 16 16 11 11 17 11 16 16 11 16 16 11 ITEM 85 -105 90 10 80 85 15 15 75 10 20 230 -55 5 15 260 460 -286 280 270 75 195 -35 -75 35 40 45 15 100 30 50 390 90 65 130 40 125 10 65 175 -227 -150 30 165 100 R5 25-29-76 Controlled TTL REQ 2 1 2 4 1 1 1 1 4 2 2 1 1 1 1 2 2 2 4 2 2 4 2 1 3 2 1 2 2 1 1 4 AR 1 2 3 2 2 2 2 1 1 4 2 2 Page 10005 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER MS27039-0808 MS27039-1-04 MS27039-1-05 MS27039-1-06 MS27039-1-08 MS27039-1-08 MS27039-1-08 MS27039-1-09 MS27039-1-13 MS27039-1-13 MS27039-1-14 MS27039-1-14 MS27039-1-14 MS27039-1-17 MS27039-1-17 MS27039-1-23 MS27039-1-24 MS27039-4-08 MS27039-4-09 MS27039-4-10 MS27039-4-10 MS27039-4-14 MS27039-4-15 MS27039-4-16 MS27039-4-17 MS27039-4-20 MS27039-4-24 MS35206-227 MS35206-227 MS35335-31 MS35335-35 MS35338-44 MS35650-302 MS35650-30ST MS51957-30 MS51957-30 MS51957-44 NAS1096-2-6 NAS1149F0332P NAS1149F0332P NAS1149F0363P NAS1149FN816P NAS387-632-10P NAS42DD6-33 NAS602-8B AIRLINE PART NO. IPL FIG 16 18 16 22 6 16 16 20 21 22 22 22 15 22 16 5 5 16 5 5 16 5 5 6 6 11 11 11 16 16 3 15 5 21 18 18 16 11 5 16 16 2 11 5 11 ITEM 180 10 455 -40 35 250 420 55 80 60 25 40A 25 15 400 95 60 -230A 50 140 230 -30 30A -10 10A 200 150A 25 40 85 90 -16 107 -70 25 -25A 15 50 100A 425 35 65 80 85 -50A R5 25-29-76 Controlled TTL REQ 1 2 2 1 4 3 2 2 2 1 1 1 1 2 2 2 4 2 4 2 2 1 1 2 2 2 1 5 2 1 2 6 2 1 2 3 1 2 2 4 2 2 2 4 2 Page 10006 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER NAS623-3-3 NAS623-3-5 NAS623-4-12W NAS623-4-18W NAS623-5-18W NAS6604-11 NAS6604-26 NAS6604-48W NAS679A3W NAS679A4W NAS679A4W NAS679A4W NP24693-S28 NP565A632H4 NP565A832H4 NP565D8H4 NPS27039-0808 RD-AM7901-01 RD-AX4331-10 RD-AX4331-11 RD-AX6430-08 RD-AX6733-08 RND-3/4-16-18 SSC-32 SSC-32 SSC-32 SSC-43 SSC-43 SSP-32 SSP-32 SSP-32 SSP-32 SSP-32 SSP-32 SSP-42 TY-26M TY-26M-0 TY-26M-0 TYPE-P-212 0201720-001 0201806-021 021975-003 040058 042002 042002-BLACK AIRLINE PART NO. IPL FIG 7 7 15 24 24 15 3 3 7 23 5 11 9 13 9 24 2 20 20 20 16 16 7 11 11 11 16 16 7 18 5 11 11 16 11 19 20 21 16 11 11 19 16 7 11 ITEM 60 -60A -10 35A 55 10A 50A 10A 70 60 35 225 85A 35 45 20 60 5 40 -40A 55 50 40 275 285 -287 290 335 -85 80 120 175 265 465 165 -10A 20 10 -445 -305 -310 5 330 20 -300 R5 25-29-76 Controlled TTL REQ 2 2 6 1 1 6 1 1 2 2 1 1 2 2 1 1 2 1 1 1 2 2 2 2 2 2 6 1 2 2 12 2 2 2 4 10 2 6 AR 2 1 1 AR AR AR Page 10007 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER 042003-BLACK 042003-BLACK 042020 042020 042020-BLACK 042020-BLACK 042028 042028-BLACK 042031-BLACK 042031-BLACK 042031-BLACK 042032-BLACK 042032-BLACK 1002937 1003344-001 1003344-003 1003345-001 1003440-001 1068-1 1069-1-1 126967-01 127306-01CAA 127307-01CAA 127473-01CAA 22303107 22303121 21048-01 22NKM-02 22NKM-02 22NKM-02 22NKM-02 22NKM-02 22NKM-62 22NKM-62 22NKTM-02 27SR0012-BLACK 27SR0020-BLACK 27SR0020-BLACK 27SR0020-BLACK 27SR0030-BLACK 3/16-X-3/16 35812 (NP) 40844027 41544013 42ND12-048 AIRLINE PART NO. IPL FIG 11 16 20 10 18 11 18 5 7 5 11 7 11 5 1 1 5 2 21 16 5 21 21 21 24 24 16 22 15 16 16 16 18 18 21 11 11 11 16 11 9 1 25 24 25 ITEM -130 -120 30 25 -85 295 115 125 -25 130 -145 -30 290 16 -55A -50A 105B 50 -40 125 -25 5 45 40A 15 90 210 55A 35 255 410 430 35 -35A 90 -20 115 140 225 120 10 -5 25 75 -40 R5 25-29-76 Controlled TTL REQ AR AR AR AR AR AR AR AR AR AR AR AR AR 2 2 2 1 1 1 2 1 2 1 1 1 2 4 1 1 3 2 2 2 3 2 5 4 2 4 2 2 RF 1 1 1 Page 10008 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER 43-13-1-24 43711053 44146005 44146006 44146007 44146008 44146013 45017005 45469001 46812003 46812015 47000407L056800 47000408L056800 48200001 48200001 48200002 48200002 48200021 48200021 48200022 48200022 48200403 48200403 48200404 48200404 48200405 48200405 48200406 48200406 48201001 48201001 48201002 48201002 48201003 48201003 48201004 48201004 48201023 48201023 48201024 48201024 48201101 48201102 48201203 48202001 AIRLINE PART NO. IPL FIG 16 9 24 24 24 24 24 8 22 16 16 12 12 23 1 23 1 23 1 23 1 23 1 23 1 23 1 23 1 23 25 23 25 23 25 23 25 23 25 23 25 25 25 10 23 ITEM -150 30 85 -85A -85B -85C 95 10 10 -110A -110 -30B -30C -1 180 -1A -180A -1F -180F -1G -180G -1D -180D -1E -180E -1B -180B -1C -180C 15 -1E 20 -1F -25 -1 -30 -1B 25A -1A 30A -1C 45 -45A 20 5 R5 25-29-76 Controlled TTL REQ 2 4 1 1 1 1 1 1 1 1 1 1 1 RF 1 RF 1 RF 1 RF 1 RF 1 RF 1 RF 1 RF 1 1 RF 1 RF 1 RF 1 RF 1 RF 1 RF 1 1 1 1 Page 10009 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER 48202005 48202201 48202205 48203015 48203015 48203015 48203025 48203025 48203025 48203057 48203069 48203081 48203111 48203113 48203129 48203401 48203407 48203415 48203435 48203447 48203601 48203602 48204133 48204134 48204301 48204303 48205051 48205053 48205115 48205125 48205131 48205137 48205139 48205143 48205155 48207101 48207201 48210105 482120138872S01 482120138872S01 482120138872S01 482120148872S01 482120148872S01 482120148872S01 482120148872S01 AIRLINE PART NO. IPL FIG 23 23 23 6 7 1 6 7 1 5 7 7 25 25 7 25 25 7 7 7 7 7 5 5 3 3 2 2 2 5 2 5 5 2 5 24 24 1 1 10 11 1 1 10 11 ITEM 10 -5A -10A 5 -1 80 -5A -1A -80A -70 45 15 -10A 10 35 5 -55 5 10 -5A 50 55 -10A 10 65 25 45 -45A 55 55 80 90 -105 -55A -105A 5 30 55 110 5 -1 115 -115A -5A -1A R5 25-29-76 Controlled TTL REQ 1 1 1 RF RF 2 RF RF 2 4 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 1 1 1 1 2 1 1 2 2 1 RF RF 1 1 RF RF Page 10010 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER 482123138872S01 482123138872S01 482123138872S01 482124138872S01 482124138872S01 482124138872S01 482124148872S01 482124148872S01 482124148872S01 482124238872S01 482124238872S01 482124238872S01 482130118872S01 482130118872S01 482130118872S01 482130138872S01 482130138872S01 482130138872S01 482130218872S01 48213033L056800 48213035 482130438872S01 482130458872S01 48213047 48213049 48213053 48213055L056800 482130578872S01 482130588872S01 48213059 48213063 482130678872S01 482130698872S01 482130718872S01 482130718872S01 48213107T0569FM 48213109T0568FM 48213110T0568FM 48213115 48213117T0569FM 48213119 48213121 48213123 48213125 48213129 AIRLINE PART NO. IPL FIG 1 10 11 1 10 11 1 10 11 1 10 11 18 1 15 18 1 15 16 16 16 16 16 16 16 16 16 16 16 16 16 16 16 16 16 18 16 16 16 18 16 16 16 16 16 ITEM -110A -5B -1B -110B -5C -1C -115B -5D -1D -110C -5E -1E -1A -145A -20A -1C 145 20 -20A 135 -340A -5B 5A -275A 275 -235A -135A 70 75 235 470 -170B -170C 170A -170D 15 215 220 -370A -15A 310 -395A -415A 245 -285A R5 25-29-76 Controlled TTL REQ 1 RF RF 1 RF RF 1 RF RF 1 RF RF RF 1 RF RF 1 RF 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 1 Page 10011 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER 48213133 48213135 48213135 48213139 48213140 48213143F207100 48213144F207100 48213145 48213146 48213147L056800 48213149L056800 48213151L056800 482131538872S01 48213155 48213157 48213171 48213177F207100 48213179F207100 48213183 48213185 48213187 48213197 48213199 48213217 48213218 48213333L056900 48213345 48213347 482134258872S01 48213427T0569FM 48213429T0569FM 48213435 48213473 48213475 482135178872S01 48213761 48213771 48214147T0568JM 48219023 48219023 48219024 48219024 48219209 48219209 48219210 AIRLINE PART NO. IPL FIG 18 18 18 16 16 16 16 16 16 16 16 16 16 16 16 16 16 16 18 16 16 16 16 18 18 17 16 16 16 18 18 16 16 16 16 18 16 16 4 5 4 5 4 5 4 ITEM 95 100 105 320 325 -71 -76 300 295 60 -140A 140 -5 380 435 350 -25A 25 -95A 415 395 370 285 -100A -105A 5 100 105 20 -1 -1B 340 -450A 450 -170 60 360 -60A 5A -1A -5C -1C 5 -1 -5B R5 25-29-76 Controlled TTL REQ 1 1 1 1 1 1 1 1 1 2 1 1 1 1 2 1 1 1 1 1 1 1 1 1 1 1 1 1 1 RF RF 1 1 1 1 1 1 2 1 RF 1 RF 1 RF 1 Page 10012 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER 48219210 48220005 48220025 48220025 48221005 48222005 48223215 48224001 48224002 48225001 (NP) 48225001 (NP) 48225005 (NP) 48225005 (NP) 48226001 48226001 48226003 48226003 48226004 48226004 48226005 48226005 48226006 48226006 48227001 (NP) 48227001 (NP) 48227101 48229001 48229003 48229005 48229005 48229007 48229007 48229015 48229017 48229019 48229025 48229029 48229031 48229033 48229035 48229037 48229039 48229043 48229063 482310258872S01 AIRLINE PART NO. IPL FIG 5 2 1 2 2 5 4 2 2 1 3 1 3 23 24 23 24 23 24 23 24 23 24 6 1 6 25 24 5 5 3 3 6 2 2 2 16 13 13 16 16 3 9 16 11 ITEM -1B -1 35 -1A 5 5 10 15 10 60 -1 60A -1A 45 -1 -45A -1A -45B -1B -45C -1C -45D -1D -1 75 20 20 65 65 -100 35 70 25 35 105 70 405 20 15 -95 90 30 60 95A -5A R5 25-29-76 Controlled TTL REQ RF RF 2 RF 1 1 1 1 1 2 RF 2 RF 2 RF 1 RF 1 RF 1 RF 1 RF RF 2 2 1 2 4 2 1 2 2 1 1 2 2 1 1 2 1 1 2 2 1 Page 10013 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER 482310268872S01 482310278872S01 482310288872S01 48231049 482310618872S01 482310628872S01 482310678872S01 482310688872S01 482310738872S01 482310738872S01 482310748872S01 482310748872S01 48231075 48231076 48231077S0568ES 48231078S0568ES 48231079S0568ES 48231080S0568ES 482310878872S01 482310918872S01 48231101 48231102 48231103 48231104 48231115T0568ST 48231119T0568ST 48231123T0568ST 48231127 48231129T0568ST 48231153 482311838872S01 482311838872S01 482311838872S01 482311848872S01 482311848872S01 482311848872S01 48231185L056900 48231201 48231202 48231203 48231217 48231219 48231303 48231305T0568FM 48231306T0568FM AIRLINE PART NO. IPL FIG 11 11 11 11 11 11 11 11 11 13 11 13 13 13 9 9 9 9 9 9 11 11 11 11 9 9 9 9 9 9 1 8 9 1 8 9 11 11 11 11 11 11 9 11 11 ITEM -5D -10A -10C 240 -5 -5C -10 -10B 205 1 -205A -1A 5 -5A 40 -40A 35 -35A 15 5 190 -190A 195 -195A 17 6 7 25 -8 65 95 5 -1 100 -5A -1A -35A 160 -160A 170 250 -235 50 110 -110A R5 25-29-76 Controlled TTL REQ 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 1 1 1 1 RF 1 1 RF 1 1 1 1 1 1 1 1 1 Page 10014 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER 48231307T0568FM 48231308T0568FM 48231309T0569FM 48231310T0569FM 48231311T0568FM 48231312T0568FM 48231405 48231409T0569FM 48231419 48231601A0578AN 48231603S0568ES 48231607A0568ES 48231613A0578ES 48231641A0568ES 482317018872S01 482317028872S01 48231751L056900 48231752L056900 48233001L056900 48233002L056900 48233003L056800 48233005L056900 48233007L056900 48233101L056900 482350038872S01 482350038872S01 482350038872S01 482350338872S01 482350338872S01 482350338872S01 482370098872S01 482370098872S01 482370098872S01 482370198872S01 482370198872S01 482370198872S01 48238065 48238075 48245005L056800 48245005L056800 48245008L056800 48245008L056800 482450358872S01 482450358872S01 482450388872S01 AIRLINE PART NO. IPL FIG 11 11 11 11 11 11 11 11 9 11 13 9 9 9 11 11 11 11 11 11 11 11 11 11 1 15 16 1 15 16 1 15 16 1 15 16 5 5 11 12 11 12 11 12 11 ITEM 135 -135A 105 -105A -15 -15A 155 -105B 9 75 10 70 80 80A 5B -5E 35B -35C 85 -85A 60 95 70 -35 -130A -5B -1B -130B -5C -1C 130 5 -1 -130C -5A -1A 40 45 -45 -1 -45B -1B 45A -1A -45C R5 25-29-76 Controlled TTL REQ 1 1 1 1 1 1 1 1 1 1 1 2 1 1 1 1 1 1 1 1 1 1 1 1 1 RF RF 1 RF RF 1 RF RF 1 RF RF 1 1 1 RF 1 RF 1 RF 1 Page 10015 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER 482450388872S01 482450478872S01 482450478872S01 482450488872S01 482450488872S01 48245103L056800 48245104L056800 48245203L056800 48245204L056800 48245303 48245401L056800 48245402L056800 48245601 48248001 48248002 48248003 48248004 48251051 48251052 48251053 48251054 48251105 48251106 48250009 (NP) 48250009 (NP) 48250010 (NP) 48250010 (NP) 482541018872S01 (NP) 482541018872S01 482541028872S01 482541028872S01 48257019 (NP) 48257019 (NP) 48258015F081139 482590150887200 48260005H161800 482630010887200 482640010887200 482640010887200 48265001 (NP) 48265001 (NP) 48266051 48277117 48287017 48287017 AIRLINE PART NO. IPL FIG 12 11 12 11 12 12 12 12 12 12 12 12 12 20 20 20 20 21 21 21 21 21 21 21 1 21 1 1 8 1 8 1 10 1 1 1 17 1 17 1 15 4 1 4 3 ITEM -1C 45D -1E -45E -1F 30 -30A -5 -5B 10A 5A -5C -10 50 -50A 35 -35A 60 -60A 20 -20A 25 -25A -1 -165 -1A -165A 85 -1 90 -1A 105 -1 10 40 30 20 135 -1 125 -1 15 120 -1 5 R5 25-29-76 Controlled TTL REQ RF 1 RF 1 RF 1 1 2 2 2 2 2 2 1 1 1 1 1 1 1 1 1 1 RF 1 RF 1 1 RF 1 RF 2 RF 2 2 2 1 1 RF 1 RF 1 2 RF RF Page 10016 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER 48287018 48287018 48287027 48287027 48287027 48287028 48287028 48287028 48289005 48528201 48528201 48528202 48528202 48528203 48528203 48528204 48528204 48539101 48539105 48553201 48606073 48606077 48269001 (NP) 48269001(NP) 48273002 (NP) 48273002 (NP) 48278001F081139 48292005H161800 48294001 (NP) 48294001 (NP) 48299005 (NP) 48299005 (NP) 48299006 (NP) 48299006 (NP) 48299007 (NP) 48299007 (NP) 48299008 (NP) 48299008 (NP) 48299031 (NP) 48299031 (NP) 48299032 (NP) 48299032 (NP) 48925003 48925004 489280078872S01 AIRLINE PART NO. IPL FIG 4 3 1 4 3 1 4 3 4 22 1 22 1 22 1 22 1 18 18 21 5 5 15 1 19 1 1 1 22 1 20 1 20 1 20 1 20 1 20 1 20 1 7 7 6 ITEM -1B -5B 65 -1A 5A 70 -1C -5C 20 5 175 -5A -175A -5B -175B -5C -175C -55 55A 55 80 70A -2 140 -1 -150 50 45 -1 170 -1 -160 -1A -160A -2A -155 -2B -155A -1B -160B -1C -160C -75 -80 30 R5 25-29-76 Controlled TTL REQ RF RF 1 RF RF 1 RF RF 1 RF 1 RF 1 RF 1 RF 1 1 1 2 4 4 1 1 RF 1 2 2 RF 1 RF 1 RF 1 RF 1 RF 1 RF 1 RF 1 1 1 1 Page 10017 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER 489320078872S01 (NP) 489320078872S01 (NP) 49688121 49688137 49688181 49688183 49688187 49688189 49688191 502864-201-2251 502864-203-2251 52NKE-064 52NKTE-048 52NKTE-048 52NKTE-054 52NTE-048 52NTE-048 5710-80-024 82-19-160-16 82-19-160-16 82-32-101-20 82-32-201-20 82-46-101-41 878363018872S01 878363048872S01 878363118872S01 878363148872S01 878363218872S01 878363248872S01 878363318872S01 878363348872S01 878363418872S01 878363448872S01 878363518872S01 878363548872S01 878364318872S01 878364348872S01 878364418872S01 878364448872S01 878364518872S01 878364548872S01 878366318872S01 878366348872S01 878366418872S01 878366448872S01 AIRLINE PART NO. IPL FIG 6 1 18 18 18 18 18 18 18 1 1 25 24 5 24 2 2 5 21 16 16 21 16 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 ITEM -2 -81 65 20 40 50 -40A -50A -20A 20 25 35 45 -24 70 40 110 -75 30 -145 -160 35 -155 1 -1A -1B -1C -1D -1E -1F -1G -1H -1J -1K -1L -1M -1N -1P -1Q -1R -1S -1T -1U -1V -1W R5 25-29-76 Controlled TTL REQ RF 2 1 2 2 1 2 1 2 2 2 1 1 2 1 1 1 8 3 2 2 3 2 RF RF RF RF RF RF RF RF RF RF RF RF RF RF RF RF RF RF RF RF RF RF Page 10018 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 PART NUMBER 878366518872S01 878366548872S01 91080005 91080006 91080007 91080008 91101205 96006003 96006021 96040253 96040303 96265003 96265003 96265005 97123007 98035003 98038001 98038233 98038233 98080001 98511007 98511007 99217105 99217115 AIRLINE PART NO. IPL FIG 1 1 24 24 24 24 24 3 3 21 22 3 3 16 24 23 11 5 5 11 2 2 1 1 ITEM -1X -1Y -80 -80A -80B -80C 50 80 80A 85 -50 20 60 -226 10 55 -215 -22 135 215A 30 100 -190 -185 R5 25-29-76 Controlled TTL REQ RF RF 1 1 1 1 1 1 1 2 1 1 1 2 1 2 2 8 8 2 2 2 1 1 Page 10019 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 30 35 40 45 50 55 60 70 135 30 35 105 115 120 90 100 40 45 50 55 60 65 20 25 20 25 10 15 120 75 80 170 175 125 130 140 145 75 80 105 110 10 15 180 85 95 Double Seat Assembly Figure 1 R5 25-29-76 Controlled Page 10020 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 6.Detailed Parts List FIG. ITEM 1 PART NUMBER 1 -1A 878363018872S01 878363048872S01 -1B 878363118872S01 -1C 878363148872S01 -1D -1E 878363218872S01 878363248872S01 -1F 878363318872S01 -1G 878363348872S01 -1H 878363418872S01 -1J 878363448872S01 -1K 878363518872S01 -1L 878363548872S01 -1M 878364318872S01 -1N 878364348872S01 -1P 878364418872S01 AIRLINE PART NOMENCLATURE NO. 1234567 DOUBLE SEAT ASSEMBLY Seat Assembly BE1.0-2-57, LH DBL STD Seat Assembly BE1.0-2-57, RH DBL STD, W/ Aisle Light Seat Assembly BE1.0-2-57, LH DBL STD, Offset Front Stud Seat Assembly BE1.0-2-57, RH DBL STD, Offset Front Stud, W/ Aisle Light Seat Assembly BE1.0-2-54, LH DBL, NRW Seat Assembly BE1.0-2-54, RH DBL, NRW, W/ Aisle Light Seat Assembly BE1.0-2-57, LH DBL STD (SUPSD by Item -1M, REF SB 25-20-2670) Seat Assembly BE1.0-2-57, RH DBL STD W/ Aisle Light (SUPSD by Item -1N, REF SB 25-20-2670) Seat Assembly BE1.0-2-57, LH DBL STD, Offset Front Stud (SUPSD by Item -1P, REF SB 25-20-2670) Seat Assembly BE1.0-2-57, RH DBL STD, Offset Front Stud, W/ Aisle Light (SUPSD by Item -1Q, REF SB 25-20-2670) Seat Assembly BE1.0-2-54, LH DBL, NRW (SUPSD by Item -1R, REF SB 25-20-2670) Seat Assembly BE1.0-2-54, RH DBL, NRW, W/ Aisle Light (SUPSD by Item -1S, REF SB 25-20-2670) Seat Assembly BE1.0-2-57, LH DBL STD, No Phone (SUPSDS Item -1F, REF SB 25-20-2670) (SUPSD by Item -1T, REF SB 25-20-2750) Seat Assembly BE1.0-2-57, RH DBL STD W/ Aisle Light, No Phone (SUPSDS Item -1G, REF SB 25-20-2670) (SUPSD by Item -1U, REF SB 25-20-2750) Seat Assembly BE1.0-2-57, LH DBL STD, Offset Front Stud, No Phone (SUPSDS Item -1H, REF SB 25-20-2670) (SUPSD by Item -1V, REF SB 25-20-2750) EFF CODE UNITS PER ASSY A B RF RF C RF D RF E F RF RF G RF H RF J RF K RF L RF M RF N RF P RF Q RF - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10021 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 AIRLINE UNITS PART NOMENCLATURE EFF PER NO. 1234567 CODE ASSY DOUBLE SEAT ASSEMBLY R RF Seat Assembly BE1.0-2-57, RH DBL STD, Offset Front Stud, W/ Aisle Light, No Phone (SUPSDS Item -1J, REF SB 25-20-2670) (SUPSD by Item -1W, REF SB 25-20-2750) 878364518872S01 Seat Assembly BE1.0-2-54, LH DBL, NRW, S RF No Phone (SUPSDS Item -1K, REF SB 25-20-2670) (SUPSD by Item -1X, REF SB 25-20-2750) 878364548872S01 Seat Assembly BE1.0-2-54, RH DBL, NRW, T RF W/ Aisle Light, No Phone (SUPSDS Item -1L, REF SB 25-20-2670) (SUPSD by Item -1Y, REF SB 25-20-2750) FIG. ITEM PART NUMBER 1 -1Q 878364448872S01 -1R -1S -1T 878366318872S01 Seat Assembly BE1.0-2-57, LH DBL STD, No Phone, W/ CP Lumbar Cushion (SUPSDS Item -1M, REF SB 25-20-2750) Seat Assembly BE1.0-2-57, RH DBL STD, W/ Aisle Light, No Phone, W/ CP Lumbar Cushion (SUPSDS Item -1N, REF SB 25-20-2750) Seat Assembly BE1.0-2-57, LH DBL STD, Offset Front Stud, No Phone, W/ CP Lumbar Cushion (SUPSDS Item -1P, REF SB 25-20-2750) Seat Assembly BE1.0-2-57, RH DBL STD, Offset Front Stud, W/ Aisle Light, No Phone, W/ CP Lumbar Cushion (SUPSDS Item -1Q, REF SB 25-20-2750) Seat Assembly BE1.0-2-54, LH DBL, NRW, No Phone, W/ CP Lumbar Cushion (SUPSDS Item -1R, REF SB 25-20-2750) Seat Assembly BE1.0-2-54, RH DBL, NRW, W/ Aisle Light, No Phone, W/ CP Lumbar Cushion (SUPSDS Item -1S, REF SB 25-20-2750) -1U 878366348872S01 -1V 878366418872S01 -1W 878366448872S01 -1X 878366518872S01 -1Y 878366548872S01 -5 35812 (NP) • Envelope Drawing RF 10 15 48258015F081139 CP19270045 • Bottom Cover Assembly • Bottom Cushion Assembly 2 2 20 25 502864-201-2251 502864-203-2251 • Seat Belt-Buckle • Seat Belt-Tip 2 2 U RF V RF W RF X RF Y RF Z RF - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10022 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER 1 30 48260005H161800 35 48220025 40 45 50 -50A 482590150887200 48292005H161800 48278001F081139 1003344-003 55 -55A 48210105 1003344-001 60 48225001 (NP) -60A 48225005 (NP) 65 70 48287027 48287028 75 48227001 (NP) 80 48203015 -80A 48203025 -81 489320078872S01 (NP) 85 482541018872S01 (NP) 482541028872S01 (NP) 482311838872S01 482311848872S01 90 95 100 AIRLINE PART NOMENCLATURE NO. 1234567 DOUBLE SEAT ASSEMBLY • Headrest Cover Assembly • Headrest Assembly (See FIG 2 for DET BKDN) • Back Cover Assembly • Literature Pocket Cover Assembly • Cover Assembly, Lumbar • Cover Assembly, Lumbar (POST SB 25-20-2750) • Cushion Assembly, Lumbar • Cushion Assembly, Lumbar (POST SB 25-20-2750) • Back Installation (SUPSD by Item -60A REF SB 25-20-2213) • Back Installation (SUPSDS Item 60 REF SB 25-20-2213) (See FIG 3 for DET BKDN) • Back Assembly LH • Back Assembly RH (See FIG 4 for DET BKDN) EFF CODE UNITS PER ASSY 2 2 A-T U-Z 2 2 2 2 A-T U-Z 2 2 2 2 1 1 • Seatpan Installation (See FIG 6 for DET BKDN) • Seatpan Assembly (SUPSD by Item -80A) • Seatpan Assembly (SUPSDS Item 80) (See FIG 7 for DET BKDN) • Kickpanel Installation (See IPL Fig 6 for DET BKDN) 2 • Foodtray Table Installation, E/B LH 1 • Foodtray Table Installation, E/B RH (See FIG 8 for DET BKDN) 1 • • Foodtray Assembly, E/B LH • • Foodtray Table Assembly, E/B RH (See FIG 9 for DET BKDN) 1 1 2 2 2 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10023 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 AIRLINE PART NOMENCLATURE NO. 1234567 DOUBLE SEAT ASSEMBLY • Endbay, STD - Installation (See FIG 10 for DET BKDN) 482120138872S01 • Endbay Assembly, STD LH (Pre SB 25-20-3169, SUPSD by item 110B for effectivity codes UWY only) FIG. ITEM PART NUMBER 1 105 48257019 (NP) 110 -110A 482123138872S01 • Endbay Assembly, LH, A/L (Pre SB 25-20-3169, SUPSD by item 110C for effectivity codes VXZ only) -110B 482124138872S01 • Endbay Assembly, STD LH (Post SB 25-20-3169, SUPSDS item 110 for effectivity codes UWY only) • Endbay Assembly, LH, A/L (Post SB 25-20-3169, SUPSDS item 110A for effectivity codes VXZ only) • Endbay Assembly, STD RH (Pre SB 25-20-3169, SUPSD by item 115A and -115B) (See FIG 11 for DET BKDN) • Endbay Assembly, STD RH (Post SB 25-20-3169, SUPSDS item 115, effectivity is now A-T only) (See FIG 11 for DET BKDN) • Endbay Assembly, STD RH (Post SB 25-20-3169, SUPSDS item 115, for effectivity codes U-Z only) (See FIG 11 for DET BKDN) • Placard, Seat Control Icon (See FIG 14 for Row & File Placard) -110C 482124238872S01 115 482120148872S01 -115A 482120148872S01 -115B 482124148872S01 120 48277117 125 48265001 (NP) 130 482370098872S01 -130A 482350038872S01 -130B 482350338872S01 -130C 482370198872S01 135 482640010887200 140 48269001(NP) • Center Console Installation (See FIG 15 for DET BKDN) • Center Console Assembly • Center Console Assembly • Center Console Assembly • Center Console Assembly (See FIG 16 for DET BKDN) • Placard Assembly - Center Console (See FIG 17 for DET BKDN) • Lifevest Assembly Instl. (See FIG 15 for DET BKDN) EFF CODE UNITS PER ASSY 2 ACE GJLNQ SUWY BDFH KMPRT VXZ UWY 1 1 VXZ 1 1 1 A-T 1 U-Z 1 A-M 2 1 ABCD GHJK EFLM STYZ N-RU-X 1 1 1 1 1 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10024 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER 1 145 482130138872S01 AIRLINE PART NOMENCLATURE NO. 1234567 DOUBLE SEAT ASSEMBLY • Lifevest Assembly -145A 482130118872S01 • Lifevest Assembly (See FIG 18 for DET BKDN) -150 48273002 (NP) • Escape Path Lite Installation (See FIG 19 for DET BKDN) -155 48299007 (NP) • Phone Installation -155A 48299008 (NP) • Phone Installation (See FIG 20 for DET BKDN) -160 48299005 (NP) -160A 48299006 (NP) -160B 48299031 (NP) • SEB Installation • SEB Installation • SEB Installation -160C 48299032 (NP) • SEB Installation (See FIG 20 for DET BKDN) -165 • Power Box Installation 48250009 (NP) -165A 48250010 (NP) • Power Box Installation (See FIG 21 for DET BKDN) 170 48294001 (NP) 175 48528201 • Baggage Bar Installation (See FIG 22 for DET BKDN) • Baggage Bar LH -175A 48528202 • Baggage Bar RH -175B 48528203 -175C 48528204 • Baggage Bar LH • Baggage Bar RH 180 • Frame Assembly LH STD (SUPSD by item -180F for effectivity code A only) 48200001 EFF CODE UNITS PER ASSY ABCD GHJK NPQR UVWX EFLM STYZ 1 BDFHK MPRT VXZ BDF HKM ACE GJLSY ACE BDF GJLNQ SUWY HKMP RTVXZ 1 BDFHK MPRT VXZ ACEGJ LNQSU WY 1 1 1 1 1 1 1 1 1 1 ACGJ NQUW BDHK PRVX ELSY FMTZ 1 1 1 GNU 1 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10025 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER 1 -180A 48200002 -180B -180C -180D -180E -180F 48200405 48200406 48200403 48200404 48200021 -180G 48200022 -185 99217115 AIRLINE UNITS PART NOMENCLATURE EFF PER NO. 1234567 CODE ASSY DOUBLE SEAT ASSEMBLY HPV 1 • Frame Assembly RH STD (SUPSD by item -180G for effectivity code B only) • Frame Assembly LH Offset CJQW 1 • Frame Assembly RH Offset DKRX 1 • Frame Assembly LH NRW ELSY 1 • Frame Assembly RH NRW FMTZ 1 • Frame Assembly LH STD A 1 (SUPSDS item 180 for effectivity code A only) • Frame Assembly LH STD B 1 (SUPSDS item -180A for effectivity code B only) (See FIG 23 for DET BKDN) • Nameplate (REF SB 25-20-2344) 1 * * * -190 99217105 -195 CBF1310-1 • Modification Tag (POST SB 25-20-2750) • Placard, Lifevest (POST SB 25-20-2750) U-Z 1 U-Z 1 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10026 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10027 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 10 100 20 5 25 30 35 15 90 95 45 30 105 95 25 110 40 Headrest Assembly Figure 2 R5 25-29-76 Controlled Page 10028 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 50 70 55 65 60 80 75 85 Headrest Assembly Figure 2 Continued R5 25-29-76 Controlled Page 10029 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10030 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER 2 AIRLINE NOMENCLATURE PART NO. 1234567 HEADREST ASSEMBLY EFF CODE UNITS PER ASSY A RF B RF -1 48220005 -1A 48220025 Headrest Assembly (SUPSD by Item -1A) Headrest Assembly (SUPSDS Item -1, REF SB 25-20-1402) (See FIG 1 for NHA) 5 48221005 • Center Body Assembly 1 10 15 48224002 48224001 1 1 20 -20A 25 30 35 40 AN4-25A AN4-24A B14-498026 98511007 48229017 52NTE-048 • Ear Assembly • Ear Assembly ATTACHING PARTS • Bolt (SUPSD by Item -20A) • Bolt (SUPSDS by Item 20) • Washer, Bellvelle • Washer, Brass • Washer / Spacer • Nut, Locking 45 48205051 -45A 48205053 50 55 1003440-001 48205115 -55A 48205143 60 65 70 NPS27039-0808 NAS1149FN816P 48229025 1 1 4 2 1 1 * * * • Slide Plate Assembly (SUPSD by Item 45A) • Slide Plate Assembly (SUPSDS Item 45 REF SB 25-20-1402) ATTACHING PARTS • • Slide Plate, Headrest • • Pivot Bracket, Headrest (SUPSD by Item -55A) • • Pivot Bracket, Headrest (SUPSDS Item 55) ATTACHING PARTS • • Screw • • Washer (AN960-8L) • • Washer/Spacer A 1 B 1 1 2 2 2 2 2 * * * 75 80 DS12X375 48205131 • • Dowel Pin • • Release Latch, Headrest ATTACHING PARTS 1 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10031 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM AIRLINE NOMENCLATURE PART NO. 1234567 PART NUMBER 85 LP27039-1-05 • • Screw 90 95 100 105 110 AN4-33A B14-498026 98511007 48229019 52NTE-048 • Bolt • Washer, Bellvelle • Washer, Brass • Washer / Spacer • Nut, Locking EFF CODE UNITS PER ASSY 2 1 * * * 1 4 2 1 1 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10032 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10033 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 45 5 5A 40 35 50 85 55 90 80 60 75 65 70 30 25 20 15 10 Back Installation Figure 3 R5 25-29-76 Controlled Page 10034 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER 3 -1 48225001 (NP) -1A 48225005 (NP) 5 48287017 5A 48287027 -5B 48287018 -5C 48287028 10 AN4-30A 10A NAS6604-48W 15 20 25 30 AN960-416 96265003 48204303 48229039 35 48229007 40 AN960-416 45 MS21042-4 50 AN4-20A AIRLINE NOMENCLATURE PART NO. 1234567 BACK INSTALLATION EFF CODE UNITS PER ASSY Back Installation (SUPSD by Item -1A, REF SB 25-20-2213) Back Installation (SUPSDS Item -1, REF SB 25-20-2213) (See FIG 1 for NHA) A RF B RF Back Assembly LH (Order Separately) (SUPSD by Item 5A) Back Assembly LH (Order Separately) (SUPSDS Item 5) Back Assembly RH (Order Separately) (SUPSD by Item -5C) Back Assembly RH (Order Separately) (SUPSDS Item -5B) (See FIG 4 for DET BKDN) ATTACHING PARTS • Bolt (Order Separately) (SUPSD by Item 10A) • Bolt (Order Separately) (SUPSDS Item 10) (Torque to 80 ± 5 in-lb) • Washer (Order Separately) • Shackle Fitting (Order Separately) • Bushing (Order Separately) • Washer / Spacer (Order Separately) • Washer / Spacer (Order Separately) • Washer (Order Separately) (REF SB 25-20-2213) • Nut (Order Separately) (REF SB 25-20-2213) A RF B RF A RF B RF A 1 B 1 • Bolt (Order Separately) (SUPSD by Item 50A) 1 1 1 1 1 1 1 A 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10035 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE PART NO. 1234567 EFF CODE UNITS PER ASSY B 1 3 50A NAS6604-26 55 60 65 70 AN960-416 96265003 48204301 48229007 75 80 AN4-4A 96006003 80A 96006021 85 90 AN316-6R MS35335-35 • Bolt (Order Separately) (SUPSDS Item 50) (Torque to 80 ± 5 in-lb) • Washer (Order Separately) • Shackle Fitting (Order Separately) • Bushing (Order Separately) • Washer / Spacer (Order Separately) • Bolt (Order Separately) • Spacer (Order Separately) (SUPSD by Item 80A) • Spacer (Order Separately) (SUPSDS Item 80) • Nut, Jam (Order Separately) • Washer (Order Separately) 1 1 1 2 A 1 1 B 1 2 2 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10036 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10037 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 20 10 5 15 Back Assembly Figure 4 R5 25-29-76 Controlled Page 10038 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER 4 -1 48287017 -1A 48287027 -1B 48287018 -1C 48287028 5 48219209 5A 48219023 -5B 48219210 -5C 48219024 10 15 48223215 48266051 20 48289005 -25 PROTEX-RT AIRLINE PART NO. NOMENCLATURE 1234567 BACK ASSEMBLY Back Assembly LH (SUPSD by Item -1A) Back Assembly LH (SUPSDS Item -1) Back Assembly RH (SUPSD by Item -1C) Back Assembly RH (SUPSDS Item -1B) (See FIG 1, 3 for NHA) • Back Assembly W/O Cushion LH (SUPSD by Item 5A) • Back Assembly W/O Cushion LH (SUPSDS Item 5) • Back Assembly W/O Cushion RH (SUPSD by Item -5C) • Back Assembly W/O Cushion RH (SUPSDS Item -5B) (See FIG 5 for DET BKDN) • Back Cushion Assembly • Fabric Support Assembly (Attach with Adhesive Sim Alpha 309) • Back Pad (Attach with Adhesive Sim Alpha 309) • Protex Fireblock (Attach with Adhesive - Sim Alpha 309) (Cover Item 10 and seam between Item 5 and 20) EFF CODE UNITS PER ASSY A RF B RF C RF D RF A 1 B 1 C 1 D 1 1 1 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10039 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 85 55 70A 80 65 60 45 110 105B 107 100A 95 125 90 97 110 50 5 40 115 120 130 50 6 135 20 140 10 135 35 16 30A 25A Back Assembly W/O Cushion Figure 5 R5 25-29-76 Controlled Page 10040 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER 5 -1 48219209 -1A 48219023 -1B 48219210 -1C 48219024 5 6 10 -10A 48222005 AA-710-27 (NP) 48204134 48204133 15 20 -22 -24 AN4-10A (DELETED) 1002937 (ADDED) AN960-416 98038233 52NKTE-048 -25 126967-01 25A HV17500-09 -30 MS27039-4-14 30A MS27039-4-15 35 NAS679A4W 40 45 48238065 48238075 50 MS27039-4-09 16 AIRLINE PART NO. NOMENCLATURE 1234567 BACK ASSEMBLY W/O CUSHION Back Assembly W/O Cushion LH (SUPSD by Item -1A) Back Assembly W/O Cushion LH (SUPSDS Item -1) Back Assembly W/O Cushion RH (SUPSD by Item -1C) Back Assembly W/O Cushion RH (SUPSDS Item -1B) (See FIG 4 for NHA) • Back Frame Assembly • • Oilite Bushing • Recline Arm • Recline Arm ATTACHING PARTS • Bolt (Apply Loctite 242 to threads) • Bolt • Washer • Washer • Nut, Cap EFF CODE UNITS PER ASSY A RF B RF C RF D RF AB CD 1 1 1 1 AC 2 BD 2 BD BD 2 4 2 AC 1 BD 1 AC 1 BD 1 * * * • Hydrolok (HV17500-07) (SUPSD by item 25A) • Hydrolok (V1YSK1) (SUPSDS item -25) ATTACHING PARTS • Screw, Pan Hd (SUPSD by Item 30A) • Screw, Pan Hd (SUPSDS Item -30) • Nut, Lock 1 * * * • Spring Assembly, Lower • Spring Assembly, Upper ATTACHING PARTS • Screw, Pan Hd 1 1 4 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10041 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER 5 AIRLINE PART NO. NOMENCLATURE 1234567 BACK ASSEMBLY W/O CUSHION EFF CODE UNITS PER ASSY * * * 55 48205125 60 65 -70 MS27039-1-24 48229005 48203057 70A 48606077 -75 5710-80-024 80 85 48606073 NAS42DD6-33 • Roller Support Bracket ATTACHING PARTS • Screw, Pan Hd • Washer / Spacer • Roller Assembly (SUPSD by Item 70A) • Roller Assembly (SUPSDS Item -70) • Washer, Seamstrom Stainless (Deleted REF SB 25-20-2644) • Bushing • Spacer 1 AC 4 4 4 BD 4 8 4 4 * * * 90 48205137 95 97 -100 MS27039-1-23 LC040D03M 48229005 100A NAS1149F0332P -105 48205139 -105A 48205155 105B 1003345-001 107 MS35650-302 • Headrest Friction Plate ATTACHING PARTS • Screw, Pan Hd • Spring (Added REF SB 25-20-2644) • Washer / Spacer (SUPSD by Item 100A, REF SB 25-20-2644) • Washer (SUPSDS Item -100, REF SB 25-20-2644) • Headrest Friction Block (SUPSD by Item 105A, REF SB 25-20-2644) • Headrest Friction Block (SUPSDS Item -105, REF SB 25-20-2644) (SUPSD by Item 105B) • Headrest Friction Block (SUPSDS Item -105A) • Nut (Added REF SB 25-20-2644) 1 2 2 2 2 1 AC 1 BD 1 2 * * * 110 APPPHC810 • Cover, Screw 6 115 K1000-3 6 120 SSP-32 • Nutplate ATTACHING PARTS • Rivet, Pop 12 * * * 125 130 042028-BLACK 042031-BLACK • Hook 2.0 peel black • Hook 1.0 peel black AR AR - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10042 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER 5 AIRLINE PART NO. NOMENCLATURE 1234567 BACK ASSEMBLY W/O CUSHION EFF CODE UNITS PER ASSY * * * 135 98038233 140 MS27039-4-10 • Washer (REF SB 25-20-1314) ATTACHING PARTS • Screw (REF SB 25-20-1314) (Apply Loctite 242 to threads) 4 2 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10043 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 25 20 15 10A 30 40 5 35 Seatpan and Kickpanel Installation. Figure 6 R5 25-29-76 Controlled Page 10044 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER 6 -1 48227001 (NP) -2 489320078872S01 (NP) 5 48203015 -5A 48203025 -10 MS27039-4-16 10A MS27039-4-17 15 20 25 AN960-416L 48227101 48229015 AIRLINE PART NO. NOMENCLATURE 1234567 SEATPAN AND KICKPANEL INSTALLATION Seatpan Installation (See FIG 1 for NHA) Kickpanel Installation (REF SB 25-20-2049) (See FIG 1 for NHA) Seatpan Assembly (Order Separately) (SUPSD by Item -5A) Seatpan Assembly (Order Separately) (SUPSDS Item 5) (See FIG 7 for DET BKDN) ATTACHING PARTS • Screw (Order Separately) (SUPSD by Item 10A) • Screw (Order Separately) (SUPSDS Item -10) • Washer (Order Separately) • Bushing (Order Separately) • Washer / Spacer (Order Separately) EFF CODE UNITS PER ASSY A RF B RF A RF A RF A 2 A 2 A A A 2 2 2 B 1 B B 4 4 * * * 30 489280078872S01 35 40 MS27039-1-08 AN960-10 • Kickplate Assembly (Order Separately) ATTACHING PARTS • Screw, Pan Hd (Order Separately) • Washer (Order Separately) * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10045 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 5 20 10 15 35 45 40 Seatpan Assembly Figure 7 R5 25-29-76 Controlled Page 10046 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 45 20 50 65 70 65 60 55 Seatpan Assembly Figure 7 continued R5 25-29-76 Controlled Page 10047 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10048 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER 7 AIRLINE PART NO. EFF CODE UNITS PER ASSY Seatpan Assembly (SUPSD by Item -1A) Seatpan Assembly (SUPSDS Item 1) (See FIG 1 for NHA) A RF B RF A 1 B 1 NOMENCLATURE 1234567 SEATPAN ASSEMBLY -1 48203015 -1A 48203025 5 48203415 -5A 48203447 10 15 20 -25 -30 48203435 48203081 042002 042031-BLACK 042032-BLACK • Bottom Diaphragm Assembly (SUPSD by Item -5A) • Bottom Diaphragm Assembly (SUPSDS Item 5) • Bottom Diaphragm Loop Assembly • Contour Foam Pad Assembly • Hook 5/8 • Hook 1.0 • Pile 2.0 35 40 48203129 RND-3/4-16-18 • Tube, Diaphragm Support • Cap, Plug 1 2 45 48203069 • Seatpan Assembly, Welded 1 50 55 48203601 48203602 1 1 60 NAS623-3-3 -60A NAS623-3-5 65 70 AN960-10L NAS679A3W • Pivot Arm • Pivot Arm ATTACHING PARTS • Screw, Pan Hd (SUPSD by Item -60A) • Screw, Pan Hd (SUPSDS Item 60) • Washer • Nut, Lock 1 1 AR AR AR 2 2 2 2 * * * -75 -80 48925003 48925004 -85 SSP-32 • Kickplate Bracket Assembly LH • Kickplate Bracket Assembly RH (REF SB 25-20-2049) ATTACHING PARTS • Rivet, Pop 1 1 2 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10049 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 10 5 Foodtray Installation - End bay Figure 8 R5 25-29-76 Controlled Page 10050 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER 8 -1 -1A 482541018872S01 (NP) 482541028872S01 (NP) 5 482311838872S01 -5A 482311848872S01 10 45017005 AIRLINE PART NO. EFF CODE UNITS PER ASSY A RF Foodtray Installation - Endbay RH (See FIG 1 for NHA) B RF • Foodtray Assembly LH (Order Separately) • Foodtray Assembly RH (Order Separately) (See FIG 9 for DET BKDN) ATTACHING PARTS • Pin, Foodtray Link (Order Separately) A 1 B 1 NOMENCLATURE 1234567 FOODTRAY INSTALLATION END BAY Foodtray Installation - Endbay LH 1 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10051 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 25 15 17 30 20 5 8 9 10 25 80 80A 7 50 85 85A 70 30 45 55 75 60 70 55 35 40 65 55 75 Foodtray Assembly - Endbay Figure 9 R5 25-29-76 Controlled Page 10052 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM PART NUMBER -1 -1A 482311838872S01 482311848872S01 5 -6 7 8 9 10 15 17 20 482310918872S01 48231119T0568ST 48231123T0568ST 48231129T0568ST 48231419 3/16-X-3/16 482310878872S01 48231115T0568ST LP565A1032H3 25 30 48231127 43711053 35 -35A 40 -40A 45 50 55 60 65 48231079S0568ES 48231080S0568ES 48231077S0568ES 48231078S0568ES NP565A832H4 48231303 DB01-009 48229043 48231153 70 75 48231607A0568ES LP35206-225 9 AIRLINE PART NO. NOMENCLATURE 1234567 FOODTRAY ASSEMBLY - ENDBAY EFF CODE UNITS PER ASSY Foodtray Assembly - Endbay Foodtray Assembly - Endbay (See FIG 1, 8 for NHA) • Foodtray Leaf Assembly - Outer • • Foodtray Laminate (Lower) • • Foodtray Laminate (Cup Holder) • • Foodtray Laminate (Upper) • • Foodtray Foam Filler • • Dowel Pin • Foodtray Leaf Assembly - Inner • • Foodtray Laminate (Upper) • • Setscrew ATTACHING PARTS • Foodtray Leaf Hinge • Pin A B RF RF 1 1 1 1 1 2 1 1 2 2 4 * * * • Slide Plate Assembly • Slide Plate Assembly • • Slide Plate Assembly W/ Bushing • • Slide Plate Assembly W/ Bushing • • Setscrew • • Slide Cap • O-ring • Washer/Spacer • Slide Rod ATTACHING PARTS • Slide Rod Retainer • Screw, Pan Hd A B A B 1 1 1 1 1 1 3 2 1 2 4 * * * 80 48231613A0578ES 80A 48231641A0568ES 85 85A LP24693-S28 NP24693-S28 • Foodtray Lift Handle (SUPSD by Item 80A) • Foodtray Lift Handle (SUPSDS Item 80, REF SB 25-20-2075) ATTACHING PARTS • Screw (SUPSD by Item 85A) • Screw (SUPSDS Item 85, REF SB 25-20-2105) (Use Loctite 290) 1 1 2 2 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10053 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 5 25 15 20 35 10 30 Endbay Installation Figure 10 R5 25-29-76 Controlled Page 10054 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 10 PART NUMBER AIRLINE PART NO. NOMENCLATURE 1234567 ENDBAY INSTALLATION EFF CODE UNITS PER ASSY -1 48257019 (NP) Endbay Installation (See FIG 1 for NHA) RF 5 482120138872S01 RF -5A 482120148872S01 -5B 482123138872S01 -5C 482124138872S01 -5D 482124148872S01 -5E 482124238872S01 10 15 20 LP4-11A LP27039-4-20 48201203 25 042020 30 35 AN4-10A AN960-416 Endbay Assembly, STD LH (Order Separately) Endbay Assembly, STD RH (Order Separately) Endbay Assembly, LH, Aisle Light (Order Separately) Endbay Assembly, STD LH (Added per SB 25-20-3169) (Order Separately) Endbay Assembly, STD RH (Added per SB 25-20-3169) (Order Separately) Endbay Assembly, LH, Aisle Light (Added per SB 25-20-3169) (Order Separately) (See FIG 11 for DET BKDN) ATTACHING PARTS • Bolt (Order Separately) • Screw (Order Separately) • Pocket Cover, Spreader (Order Separately) (REF SB 25-20-1314) • Pile 1.0 Peel (Order Separately) (REF SB 25-20-1314) Bolt (REF IPL FIG 11, Item 185) Washer (REF IPL FIG 11, Item 185) RF RF RF RF RF 2 1 1 AR 1 1 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10055 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 5B 35B 50 40 55 50 55 25 30 45A Endbay Assembly Figure 11 R5 25-29-76 Controlled Page 10056 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 65 125 60 125 90 85 100 95 100 90 80 75 70 120 80 105 120 Endbay Assembly Figure 11 continued R5 25-29-76 Controlled Page 10057 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 115 110 150A 115 135 105 140 Endbay Assembly Figure 11 continued R5 25-29-76 Controlled Page 10058 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 155 170 175 200 190 195 165 160 180 185 Endbay Assembly Figure 11 continued R5 25-29-76 Controlled Page 10059 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 280 260 295 240 290 285 255 275 260 250 265 225 265 220 270 190 280 285 285 245 215A 230 205 215A 280 210 285 195 280 Endbay Assembly Figure 11 continued R5 25-29-76 Controlled Page 10060 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 11 PART NUMBER -1 -1A -1B -1C 482120138872S01 482120148872S01 482123138872S01 482124138872S01 -1D 482124148872S01 -1E 482124238872S01 -5 482310618872S01 -5A 482310258872S01 5B 482317018872S01 -5C 482310628872S01 -5D 482310268872S01 -5E 482317028872S01 -10 482310678872S01 -10A 482310278872S01 -10B 482310688872S01 -10C 482310288872S01 -15 -15A -20 25 30 48231311T0568FM 48231312T0568FM 27SR0012-BLACK MS35206-227 AN960-6L EFF CODE UNITS PER ASSY A B C D RF RF RF RF E RF F RF • Armcap Assembly (SUPSD by Item 5A) • Armcap Assembly (SUPSDS Item -5) (SUPSD by Item 5B) • Armcap Assembly (SUPSDS Item -5A) • Armcap Assembly (SUPSD by Item -5D) • Armcap Assembly (SUPSDS Item -5C) (SUPSD by Item -5E) • Armcap Assembly (SUPSDS Item -5D, REF SB 25-20-2057, -2411) ACDF 1 ACDF 1 ACDF 1 BE 1 BE 1 BE 1 • • Armcap Assembly - Covered (SUPSD by Item -10A) • • Armcap Assembly - Covered (SUPSDS Item -10) • • Armcap Assembly - Covered (SUPSD by Item -10C) • • Armcap Assembly - Covered (SUPSDS Item -10B) • • Armcap Insert, Plastic • • Armcap Insert, Plastic • • Plastic Rivet, Black • Screw • Washer ACDF 1 ACDF 1 BE 1 BE 1 ACDF BE 1 1 5 5 5 AIRLINE NOMENCLATURE PART NO. 1234567 ENDBAY ASSEMBLY Endbay Assembly, STD LH Endbay Assembly, STD RH Endbay Assembly, LH - Aisle Light Endbay Assembly, STD LH (Added per SB 25-20-3169) Endbay Assembly, STD RH (Added per SB 25-20-3169) Endbay Assembly, LH, Aisle Light (Added per SB 25-20-3169) (See FIG 11 for DET BKDN) * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10061 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 11 -35 48233101L056900 -35A 48231185L056900 35B 48231751L056900 -35C 48231752L056900 40 MS24693-S25 PART NUMBER AIRLINE NOMENCLATURE PART NO. 1234567 • Placard Mount Bezel (SUPSD by Item -35A) • Placard Mount Bezel (SUPSDS Item -35) (SUPSD by Items 35B and -35C) • Placard Mount Bezel (SUPSDS Item -35A, REF SB 25-20-2057, 2411) (See FIG 14 for Placard Details) • Placard Mount Bezel (SUPSDS Item -35A REF SB 25-20-2057, 2411) (See FIG 14 for Placard Details) ATTACHING PARTS • Screw, Csk EFF CODE UNITS PER ASSY 1 1 ACDF 1 BE 1 3 * * * -45 48245005L056800 45A 482450358872S01 -45B 48245008L056800 -45C 482450388872S01 -45D 482450478872S01 -45E 482450488872S01 50 -50A 55 NAS1096-2-6 NAS602-8B AN960-8 • Seat Control Assembly (SUPSD by Item 45A) • Seat Control Assembly (SUPSDS Item -45) • Seat Control Assembly (SUPSD by Item -45C) • Seat Control Assembly (SUPSDS Item -45B) (See FIG 12 for DET BKDN) • Seat Control Assembly (Added per SB 25-20-3169) • Seat Control Assembly (Added per SB 25-20-3169) (See FIG 12 for DET BKDN) ATTACHING PARTS • Screw • Screw (Added per SB 25-20-3169) • Washer AC 1 AC 1 B 1 B 1 DF 1 E 1 ABC DEF ABC 2 2 2 * * * 60 48233003L056800 65 MS24693-S27 • Heelcap - Upper ATTACHING PARTS • Screw, Csk 1 2 * * * 70 48233007L056900 • Rubstrip - Frontcap 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10062 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 11 75 48231601A0578AN 80 NAS387-632-10P PART NUMBER AIRLINE NOMENCLATURE PART NO. 1234567 EFF CODE • Escutcheon - Endbay ATTACHING PARTS • Screw, Oval UNITS PER ASSY 1 2 * * * 85 -85A 48233001L056900 48233002L056900 90 LP27039-0805 95 48233005L056900 100 MS27039-0807 • Rubstrip - Endbay • Rubstrip - Endbay ATTACHING PARTS • Screw, Pan Hd ACDF BE 1 1 2 * * * • Rubstrip - Rearcap ATTACHING PARTS • Screw 1 2 * * * 105 -105A -105B 110 -110A 48231309T0569FM 48231310T0569FM 48231409T0569FM 48231305T0568FM 48231306T0568FM 115 120 125 -130 27SR0020-BLACK 27SR0030-BLACK MS24693-S25 042003-BLACK 135 -135A 48231307T0568FM 48231308T0568FM 140 -145 27SR0020-BLACK 042031-BLACK -150 150A MS24694-S118 MS27039-4-24 • Cap Shroud - Lower • Cap Shroud - Lower • Cap Shroud - Lower, Aisle Light • Endbay Shroud - Outer • Endbay Shroud - Outer ATTACHING PARTS • Plastic Rivet • Plastic Rivet • Screw • Pile 5/8 peel AD BE CF ACDF BE 1 1 1 1 1 4 2 2 AR * * * • Shroud - Inner panel • Shroud - Inner panel ATTACHING PARTS • Plastic Rivet • Hook 1.0 peel ACDF BE 1 1 2 AR * * * • Screw (SUPSD by Item 150A) • Screw (SUPSDS Item -150, REF SB 25-20-1332) 1 1 * * * 155 48231405 • Foam Pad 1 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10063 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 AIRLINE NOMENCLATURE PART NO. 1234567 EFF CODE UNITS PER ASSY • Bracket, Lower Shroud • Bracket, Lower Shroud ATTACHING PARTS • Rivet, Pop ACDF BE 1 1 FIG. ITEM 11 160 -160A 48231201 48231202 165 SSP-42 170 48231203 175 SSP-32 • Hat Section, Rubstrip ATTACHING PARTS • Rivet, Pop 180 185 AN960-416 AN4-10A • Washer • Bolt 190 -190A 195 -195A 48231101 48231102 48231103 48231104 200 MS27039-4-20 • Endbay Panel - Outer • Endbay Panel - Outer • Endbay Panel - Inner • Endbay Panel - Inner ATTACHING PARTS • Screw PART NUMBER 4 * * * 1 2 * * * 1 1 * * * ACDF BE ACDF BE 1 1 1 1 2 * * * 205 -205A 482310738872S01 482310748872S01 210 -215 AN4-20A 98038001 215A 98080001 220 225 AN960-416 NAS679A4W • Pivot Assembly - Foodtray • Pivot Assembly - Foodtray (See Fig 14 for DET BKDN) ATTACHING PARTS • Bolt • Washer / Spacer (SUPSD by Item 215A) • Washer / Spacer - Tufnol (SUPSDS Item -215) • Washer • Nut, Lock ACDF BE 1 1 1 2 2 1 1 * * * 230 LP565A1032H6 • Setscrew 1 * * * -235 240 48231219 48231049 245 CSP-44 • Endbay Stiffener • Armcap Hinge Assembly ATTACHING PARTS • Rivet 1 1 6 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10064 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 11 PART NUMBER AIRLINE NOMENCLATURE PART NO. 1234567 EFF CODE UNITS PER ASSY * * * 250 48231217 255 CSP-43 260 MF6000-06 265 SSP-32 270 MK2000-08 275 SSC-32 • Armcap Hinge Spacer ATTACHING PARTS • Rivet 1 7 * * * • Nutplate ATTACHING PARTS • Rivet, Pop 2 2 * * * • Nutplate ATTACHING PARTS • Rivet 2 2 * * * 280 MK2000-06 • Nutplate ATTACHING PARTS • Rivet 285 SSC-32 -286 MK1000-08 -287 SSC-32 290 295 -300 042032-BLACK 042020-BLACK 042002-BLACK • Pile 2.0 peel • Pile 1.0 peel • Hook 5/8 -305 -310 0201720-001 0201806-021 • Proximity Lights-Clear Lens • Backing Plate Assembly 4 2 * * * • Nutplate (Added per SB 25-20-3169) ATTACHING PARTS • Rivet (Added per SB 25-20-3169) DEF 2 DEF 2 * * * AR AR AR * * * CF CF 2 1 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10065 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 30 5A 10A 25 15 20A Seat Control Assembly Figure 12 R5 25-29-76 Controlled Page 10066 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 12 PART NUMBER -1 48245005L056800 -1A 482450358872S01 -1B 48245008L056800 -1C 482450388872S01 -1D 482450478872S01 -1E 482450488872S01 -5 48245203L056800 5A 48245401L056800 -5B 48245204L056800 -5C 48245402L056800 -10 48245601 10A 48245303 15 MC54045-85 -20 LP24693-31 20A LP24693-29 25 LE02B01M AIRLINE PART NO. NOMENCLATURE 1234567 SEAT CONTROL ASSEMBLY Seat Control Assembly (SUPSD by Item -1A) Seat Control Assembly (SUPSDS Item -1) Seat Control Assembly (SUPSD Item -1C) Seat Control Assembly (SUPSDS by Item -1B) Seat Control Assembly (Added per SB 25-20-3169) Seat Control Assembly (Added per SB 25-20-3169) (See FIG 11 for NHA) • Control Lever (SUPSD by Item 5A) • Control Lever (SUPSDS Item -5) • Control Lever (SUPSD by Item -5C) • Control Lever (SUPSDS Item -5B, REF SB 25-20-1367) • Lever Cable (SUPSD by Item 10A) • Lever Cable (SUPSDS Item -10, REF SB 25-20-1367) • Porter Cable Assembly ATTACHING PARTS • Screw (SUPSD by Item 20A) • Screw (SUPSDS by Item -20, REF SB 25-20-1367) EFF CODE UNITS PER ASSY A RF B RF C RF D RF E RF F RF A 2 BE 2 C 2 DF 2 AC 2 BDEF 2 1 AC 2 BDEF 2 • Extension, Spring 2 * * * 30 48245103L056800 • Bezel, Seat Control AB 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10067 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM -30A -30B -30C PART NUMBER 48245104L056800 47000407L056800 47000408L056800 AIRLINE PART NO. NOMENCLATURE 1234567 • Bezel, Seat Control • Bezel, Seat Control • Bezel, Seat Control EFF CODE CD E F UNITS PER ASSY 1 1 1 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10068 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10069 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 10 5 35 15 20 25 30 Pivot Assembly - Foodtray Figure 13 R5 25-29-76 Controlled Page 10070 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 EFF CODE UNITS PER ASSY • Pivot Assembly - Foodtray (See FIG 11 for NHA) • Pivot Assembly - Foodtray (See FIG 11 for NHA) A 1 B 1 48231075 48231076 • Pivot / Bushing Assembly • Pivot / Bushing Assembly A B 1 1 10 48231603S0568ES 15 20 25 30 48229033 48229031 AN960-616L MS21083N6 • Swivel, Foodtray ATTACHING PARTS • Washer / Spacer • Washer / Spacer • Washer • Nut, Lock FIG. ITEM 13 PART NUMBER -1 482310738872S01 -1A 482310748872S01 5 -5A AIRLINE PART NO. NOMENCLATURE 1234567 PIVOT ASSEMBLY - FOODTRAY 1 1 1 1 1 * * * 35 NP565A632H4 • Setscrew 2 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10071 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 ROW & FILE PLACARD SEAT ICON PLACARD (48277117) Endbay Placard Installation Figure 14 R5 25-29-76 Controlled Page 10072 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 ROW & FILE PLACARD PART NO SEAT ROW NO SEAT FILE LETTER SEAT ICON PLACARD PART NO 48277001 3 A 48277117 48277003 3 B 48277117 48277005 3 E 48277117 48277007 3 F 48277117 48277009 4 A 48277117 48277011 4 B 48277117 48277013 4 E 48277117 48277015 4 F 48277117 48277017 5 A 48277117 48277019 5 B 48277117 48277021 5 E 48277117 48277023 5 F 48277117 48277025 6 A 48277117 48277027 6 B 48277117 48277029 6 E 48277117 48277031 6 F 48277117 48277033 7 A 48277117 48277035 7 B 48277117 48277039 7 E 48277117 48277041 7 F 48277117 END BAY PLACARD INSTALLATION R5 25-29-76 Controlled Page 10073 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 5 15 10 15 10 20 35 30 25 30 Center Console Installation Figure 15 R5 25-29-76 Controlled Page 10074 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 15 PART NUMBER -1 48265001 (NP) -2 48269001 (NP) 5 482370098872S01 -5A 482370198872S01 -5B 482350038872S01 -5C 482350338872S01 -10 NAS623-4-12W 10A NAS6604-11 15 -16 AN960-416 MS35338-44 AIRLINE PART NO. NOMENCLATURE EFF 1234567 CODE CENTER CONSOLE INSTALLATION Center Console Installation (See FIG 1 for NHA) Lifevest Assembly Installation (See FIG 1 for NHA) Center Console Assembly, STD (Order Separately) Center Console Assembly, STD (Order Separately) Center Console Assembly, NRW (Order Separately) Center Console Assembly, NRW (Order Separately) (See FIG 16 for DET BKDN) ATTACHING PARTS • Screw (Order Separately) (SUPSD by Item 10A) • Screw (Order Separately) (SUPSDS Item -10) • Washer (Order Separately) • Washer, Split, Lock (Order Separately) UNITS PER ASSY A RF B 1 RF RF RF RF A 6 A 6 A A 6 6 * * * 20 482130138872S01 -20A 482130118872S01 Lifevest Assembly, STD (Order Separately) Lifevest Assembly, NRW (Order Separately) (See FIG 18 for DET BKDN) 25 30 35 MS27039-1-14 AN960-10 22NKM-02 • Screw, Pan Hd (Order Separately) • Washer (Order Separately) • Nut, Cap (Order Separately) RF RF B B B 1 2 1 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10075 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 45 65 50 20 25 60 55 100 95A 35 75 5A 30 30 70 105 95A 90 85 80 10 40 15 360 365 130 125 Center Console Assembly Figure 16 R5 25-29-76 Controlled Page 10076 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 205 210 185 180 225 170A 220 190 195 165 230 215 225 135 140 166 Center Console Assembly Figure 16 continued R5 25-29-76 Controlled Page 10077 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 255 250 265 250 245 265 255 270 245 260 250 235 240 255 Center Console Assembly Figure 16 continued R5 25-29-76 Controlled Page 10078 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 335 280 345 325 330 175 275 280 290 305 315 295 200 310 320 330 300 285 340 Center Console Assembly Figure 16 continued R5 25-29-76 Controlled Page 10079 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 435 405 385 440 410 470 380 370 375 400 430 350 390 425 355 425 395 420 415 390 450 455 460 465 Center Console Assembly Figure 16 continued R5 25-29-76 Controlled Page 10080 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 16 PART NUMBER -1 -1A -1B -1C 482370098872S01 482370198872S01 482350038872S01 482350338872S01 -5 482131538872S01 5A 482130458872S01 -5B 482130438872S01 10 15 LP27039-0806 MS51957-44 AIRLINE PART NO. EFF CODE UNITS PER ASSY Center Console Assembly, STD Center Console Assembly, STD Center Console Assembly, NRW Center Console Assembly, NRW (See FIG 1, 15 for NHA) A B C D RF RF RF RF • Heelcap Assembly (SUPSD by Item 5A) • Heelcap Assembly (SUPSDS Item -5) • Heelcap Assembly ATTACHING PARTS • Screw, Pan Hd • Screw (REF SB 25-20-1334) AB 1 AB 1 CD 1 NOMENCLATURE 1234567 CENTER CONSOLE ASSEMBLY 4 1 * * * 20 -20A 25 -25A 482134258872S01 482130218872S01 48213179F207100 48213177F207100 30 35 40 MS27039-0806 NAS1149F0363P MS35206-227 • Cocktail Table Assembly • Cocktail Table Assembly • • Laminate, Cocktail Table • • Laminate, Cocktail Table ATTACHING PARTS • Screw • Washer (AN960-10) • Screw AB CD AB CD 1 1 1 1 4 2 2 * * * 45 BAC29PPS42096 50 55 60 RD-AX6733-08 RD-AX6430-08 48213147L056800 -60A 48214147T0568JM 65 MS24671-8 • Placard, Safety (REF SB-25-20-1331) • PCU • Remote Jack • Bezel, Headphone Jack (SUPSD by Item -60A) • Bezel, Headphone Jack (SUPSDS Item 60) ATTACHING PARTS • Screw AC 1 2 2 2 2 1 * * * 70 -71 482130578872S01 48213143F207100 • Peanut Tray Assembly • • Laminate, Peanut Tray 1 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10081 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 16 75 -76 PART NUMBER 482130588872S01 48213144F207100 80 85 90 -95 LP27039-0812 MS35335-31 48229037 48229035 95A 48229063 100 105 48213345 48213347 AIRLINE PART NO. NOMENCLATURE 1234567 CENTER CONSOLE ASSEMBLY • Peanut Tray Assembly • • Laminate, Peanut Tray ATTACHING PARTS • Screw • Washer • Washer / Spacer • Washer / Spacer (SUPSD by Item 95A) • Washer / Spacer (SUPSDS Item -95) • Bushing - Spacer • Bushing - Pivot EFF CODE UNITS PER ASSY 1 1 1 1 1 2 2 1 1 * * * -110 -110A 46812015 46812003 -115 -120 CSP-45 042003-BLACK • Bracket Assembly, Tee Support • Bracket Assembly, Tee Support (REF SB 25-20-2101) ATTACHING PARTS • Rivet, Pop • Pile 5/8” Peel AB CD 1 1 2 AR * * * 125 1069-1-1 130 MS24693-4B • Power Port Outlet ATTACHING PARTS • Screw, Black A-C 2 2 * * * 135 -135A 140 -140A -145 -150 -155 -160 48213033L056800 48213055L056800 48213151L056800 48213149L056800 82-19-160-16 43-13-1-24 82-46-101-41 82-32-101-20 165 MS27039-0806 • Shroud Assembly - Front • Shroud Assembly - Front • • Front Shroud • • Front Shroud • • Stud • • Spring • • Washer • • Retainer - Split Ring ATTACHING PARTS • Screw, Pan Hd AB CD AB CD 1 1 1 1 2 2 2 2 2 * * * 166 C169 • Monitor Light Guide CD 2 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10082 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 16 -170 482135178872S01 170A 482130718872S01 -170B 482130678872S01 -170C 482130698872S01 -170D 482130718872S01 175 180 MS24693-S274 MS27039-0808 185 190 C23PM-6200-01 C23PU-6920-01 195 MS16997-20 PART NUMBER AIRLINE PART NO. NOMENCLATURE 1234567 CENTER CONSOLE ASSEMBLY • Armcap Assembly (SUPSD by Item 170A, REF SB 25-20-2670) • Armcap Assembly (SUPSDS Item -170, REF SB 25-20-2670) • Armcap Assembly (SUPSD by Items -170C & -170D, REF SB 25-20-2670) • Armcap Assembly (SUPSDS Item -170B, REF SB 25-20-2670) • Armcap Assembly (SUPSDS Item -170B, REF SB 25-20-2670) ATTACHING PARTS • Screw, Csk • Screw, Pan Hd EFF CODE UNITS PER ASSY A 1 A 1 CD 1 C 1 BD 1 2 1 * * * • Handset, AT&T • Cradle, AT&T ATTACHING PARTS • Screw AC AC 2 2 4 * * * 200 205 210 C23PU-6967-01 C23PH-6004-01-0 21048-01 • Cord Reel, AT&T • Cable, AT&T • Guide, Cord Reel AC AC AC 2 2 4 * * * 215 220 48213109T0568FM 48213110T0568FM 225 27SR0020-BLACK • Shroud - Side • Shroud - Side ATTACHING PARTS • Plastic Rivet 1 1 4 * * * -226 96265005 -227 MS24694-S104 • Shackle Fitting (Removed REF SB 25-20-1332 and replaced by item 230) ATTACHING PARTS • Screw (Removed REF SB 25-20-1332 and replaced by item 230) AB 2 AB 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10083 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 16 PART NUMBER AIRLINE PART NO. NOMENCLATURE 1234567 CENTER CONSOLE ASSEMBLY EFF CODE UNITS PER ASSY AB 2 CD 2 AB CD 1 1 * * * 230 MS27039-4-10 -230A MS27039-4-08 235 -235A 48213059 48213053 240 CSP-43 245 48213125 250 255 260 265 270 MS27039-1-08 22NKM-02 CSP-43 CSP-44 CSP-42 • Screw (Added REF SB 25-20-1332 to replace items -226 and -227) • Screw * * * • Power Port Assembly • Power Port Assembly ATTACHING PARTS • Rivet, Pop 6 * * * • Side Panel ATTACHING PARTS • Screw, Pan Hd • Nut, Cap • Rivet, Pop • Rivet, Pop • Rivet, Pop 2 3 3 6 4 2 * * * 275 -275A 48213049 48213047 280 CSP-44 285 -285A 48213199 48213129 290 SSC-43 295 300 48213146 48213145 305 CSP-44 310 48213119 • Bracket Assembly, Top - Phone • Bracket Assembly, Top - Phone ATTACHING PARTS • Rivet, Pop AB CD 1 1 12 * * * • Bracket, Cocktail Table Mount • Bracket, Cocktail Table Mount ATTACHING PARTS • Rivet, Pop AB CD 1 1 6 * * * • Bracket, Tray Support • Bracket, Tray Support ATTACHING PARTS • Rivet, Pop 1 1 2 * * * • Bracket, Cocktail Table, Front ATTACHING PARTS 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10084 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 16 315 PART NUMBER CSP-43 AIRLINE PART NO. NOMENCLATURE 1234567 CENTER CONSOLE ASSEMBLY • Rivet, Pop EFF CODE UNITS PER ASSY 3 * * * 320 325 330 48213139 48213140 040058 335 SSC-43 • Bracket, RJU • Bracket, RJU • Tape ATTACHING PARTS • Rivet, Pop 1 1 AR 1 * * * 340 -340A 48213435 48213035 345 CSP-44 • Bracket Assembly, PCU • Bracket Assembly, PCU ATTACHING PARTS • Rivet, Pop AB CD 1 1 4 * * * 350 48213171 355 CSP-43 • Bracket, Heelcap ATTACHING PARTS • Rivet, Pop 1 6 * * * 360 48213771 365 CSP-42 • Bracket, Anchor (REF SB 25-20-1334) ATTACHING PARTS • Rivet, Pop 1 2 * * * 370 -370A 48213197 48213115 375 CSP-43 • Bracket, Center Support • Bracket, Center Support ATTACHING PARTS • Rivet, Pop AB CD 1 1 4 * * * 380 48213155 385 CSP-43 • Bracket, Phone Support ATTACHING PARTS • Rivet, Pop 1 4 * * * 390 395 -395A MS21209F4-15L 48213187 48213121 400 MS27039-1-17 • Helicoil • Plate, Rear Mount • Plate, Rear Mount ATTACHING PARTS • Screw, Pan Hd AB CD 4 1 1 2 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10085 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 16 405 410 PART NUMBER 48229029 22NKM-02 AIRLINE PART NO. NOMENCLATURE 1234567 CENTER CONSOLE ASSEMBLY • Washer / Spacer • Nut, Cap EFF CODE UNITS PER ASSY 2 2 * * * 415 -415A 48213185 48213123 420 425 430 MS27039-1-08 NAS1149F0332P 22NKM-02 • Plate, Front Mount • Plate, Front Mount ATTACHING PARTS • Screw, Pan Hd • Washer (AN960-10L) • Nut, Cap AB CD 1 1 2 4 2 * * * 435 48213157 440 -440A -445 CSP-43 CSP-46 TYPE-P-212 • Bracket, Cord Reel ATTACHING PARTS • Rivet, Pop • Rivet, Pop • Tape, Glass Cloth 2 AB 2 2 AR AB CD 1 1 * * * 450 -450A 48213475 48213473 455 MS27039-1-05 • Cover, Blank-Off • Cover, Blank-Off ATTACHING PARTS • Screw, Pan Hd 2 * * * 460 MK1000-3 465 SSP-32 • Nutplate ATTACHING PARTS • Rivet, Pop 2 2 * * * 470 48213063 • Center Support Assembly 1 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10086 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10087 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 5 20 10 15 Placard Assembly - Center Console Figure 17 R5 25-29-76 Controlled Page 10088 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 AIRLINE PART NO. NOMENCLATURE 1234567 PLACARD ASSEMBLY CENTER CONSOLE EFF CODE UNITS PER ASSY FIG. ITEM 17 PART NUMBER -1 482640010887200 Placard Assembly - Center Console (See FIG 1 for NHA) RF 5 48213333L056900 1 10 15 MS24693-S27 MS21083N6 • Bezel, Placard Mount ATTACHING PARTS • Screw, Csk • Nut, Lock 20 482630010887200 • Placard - Adhesive 2 2 * * * 1 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10089 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 115 110 105 75 80 95 110 5 10 55A 60 90 110 100 110 35 20 70 65 45 15 40 50 20 30 25 Lifevest Assembly Figure 18 R5 25-29-76 Controlled Page 10090 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 18 PART NUMBER -1 48213427T0569FM -1A 482130118872S01 -1B 48213429T0569FM -1C 482130138872S01 5 M1-99-128 10 MS27039-1-04 AIRLINE PART NO. NOMENCLATURE 1234567 LIFEVEST ASSEMBLY Lifevest Console Assembly (SUPSD by Item -1A) Lifevest Console Assembly (SUPSDS Item -1) Lifevest Console Assembly (SUPSD by Item -1C) Lifevest Console Assembly (SUPSDS Item -1B) (See Fig 1, 15 for NHA) EFF CODE UNITS PER ASSY A RF B RF C RF D RF • Pull Latch ATTACHING PARTS • Screw, Pan Hd 1 2 * * * 15 -15A 48213107T0569FM 48213117T0569FM 20 -20A 25 -25A 30 -30A 35 -35A 49688137 49688191 MS51957-30 MS51957-30 AN960-6L AN960-6L 22NKM-62 22NKM-62 • Shroud, Lifevest • Shroud, Lifevest ATTACHING PARTS • Pad, Spacer • Pad, Spacer • Screw, Pan Hd • Screw, Pan Hd • Washer • Washer • Nut, Cap • Nut, Cap AB CD 1 1 AB CD AB CD AB CD AB CD 2 2 2 3 2 3 2 3 AB CD 2 2 AB CD 3 1 1 * * * 40 -40A 49688181 49688187 45 50 -50A CSP-43 49688183 49688189 • Hinge - Lifevest Door • Hinge - Lifevest Door ATTACHING PARTS • Rivet, Pop • Hinge Pin • Hinge Pin * * * -55 48539101 • Bracket, Latching - Lifevest (SUPSD by Item 55A) 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10091 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 18 55A 48539105 60 48213761 PART NUMBER AIRLINE PART NO. NOMENCLATURE 1234567 EFF CODE UNITS PER ASSY 1 • Bracket, Latching - Lifevest (SUPSDS Item -55, REF SB 25-20-1308, 1402) • Strap, Lifevest Retention 1 * * * 65 49688121 70 CSP-43 • Bracket ATTACHING PARTS • Rivet, Pop 1 2 * * * 75 MK2000-3 80 SSP-32 • Anchor Nut ATTACHING PARTS • Rivet, Pop 2 2 * * * -85 90 042020-BLACK MS21266-1N • 1” Pile Peel Black • Grommet Edge (Use Loctite - 454 to secure) AR AR * * * 95 -95A 100 -100A 105 -105A 48213133 48213183 48213135 48213217 48213135 48213218 110 CSP-43 • Bracket, Lifevest Stowage • Bracket, Lifevest Stowage • Bracket, Lifevest Side • Bracket, Lifevest Side • Bracket, Lifevest Side • Bracket, Lifevest Side ATTACHING PARTS • Rivet, Pop AB CD AB CD AB CD 1 1 1 1 1 1 18 * * * 115 042028 • Hook, Peel AR * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10092 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10093 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 5 10 15 Escape Path Lite Installation Figure 19 R5 25-29-76 Controlled Page 10094 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 19 PART NUMBER AIRLINE NOMENCLATURE PART NO. 1234567 ESCAPE PATH LITE INSTALLATION EFF CODE UNITS PER ASSY -1 48273002 (NP) Escape Path Lite Installation (See FIG 1 for NHA) RF 5 021975-003 1 10 F000009 -10A TY-26M 15 HT3/8FR-B • Harness Assembly, Escape Path Lite (Order Separately) ATTACHING PARTS • Lock Strap (Order Separately) (SUPSD by Item -10A) • Lock Strap (Order Separately) (SUPSDS Item 10) • Spiral Wrap (Order Separately) 10 10 AR * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10095 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 5 10 30 20 15 55 50 35 40 45A 60 Phone & SEB Box Installation Figure 20 R5 25-29-76 Controlled Page 10096 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 20 PART NUMBER -1 -1A -1B -1C 48299005 (NP) 48299006 (NP) 48299031 (NP) 48299032 (NP) -2A -2B 48299007 (NP) 48299008 (NP) 5 10 15 RD-AM7901-01 C23PH-6001-02-9E C23PH-6001-03-9E 20 -25 30 TY-26M-0 HT1/4FR-B 042020 AIRLINE NOMENCLATURE EFF PART NO. 1234567 CODE PHONE & SEB BOX INSTALLATION SEB Installation SEB Installation SEB Installation SEB Installation (See FIG 1 for NHA) Phone Box Installation Phone Box Installation (See FIG 1 for NHA) • Harness (Order Separately) • Phone Cord (Order Separately) • Phone Cord (Order Separately) ATTACHING PARTS • Lock Strap (Order Separately) • Spiral Wrap (Order Separately) • Pile, 1.0” Peel (Order Separately) UNITS PER ASSY A B C D RF RF RF RF E F RF RF ABCD EF EF 1 1 1 2 AR AR * * * 35 48248003 -35A 48248004 • Mux Shroud Assembly (Order Separately) • Mux Shroud Assembly (Order Separately) ACE 1 BDF 1 AB CD EF 1 1 1 EF 1 ACE 1 BDF 1 * * * 40 -40A -45 RD-AX4331-10 RD-AX4331-11 C23CE-4300-02 45A C23CE-4300-04 • SEB (Order Separately) • SEB (Order Separately) • Phone Box (Order Separately) (SUPSD by Item 45A) • Phone Box (Order Separately) (SUPSDS Item -45) * * * 50 48248001 -50A 48248002 55 MS27039-1-09 • Mux Plate Assembly (Order Separately) • Mux Plate Assembly (Order Separately) ATTACHING PARTS • Screw, Pan (Order Separately) 2 * * * -60 DA10135-001 • SEB EMI Filter Assembly (Order Separately) AB 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10097 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 10 5 Power Box Installation Figure 21 R5 25-29-76 Controlled Page 10098 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 90 85 80 90 40A 55 45 85 60 80 50 20 25 30 35 Power Box Installation Figure 21 continued R5 25-29-76 Controlled Page 10099 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10100 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 21 PART NUMBER -1 48250009 (NP) -1A 48250010 (NP) 5 127306-01CAA 10 TY-26M-0 -15 HT3/8FR-B AIRLINE NOMENCLATURE PART NO. 1234567 POWER BOX INSTALLATION EFF CODE UNITS PER ASSY Power Box Installation (See FIG 1 for NHA) Power Box Installation (See FIG 1 for NHA) A RF B RF • Power Harness (Order Separately) (1068805-5-38) ATTACHING PARTS • Lock Strap, Black (Order Separately) • Spiral Wrap Tube, Black (Order Separately) 2 6 AR * * * 20 48251053 -20A 48251054 25 48251105 -25A 48251106 30 35 82-19-160-16 82-32-201-20 • Shroud Assembly, Electric Box (Order Separately) • Shroud Assembly, Electric Box (Order Separately) • • Shroud, Electric Box (Order Separately) • • Shroud, Electric Box (Order Separately) ATTACHING PARTS • • Stud (Order Separately) • • Retainer (Order Separately) A 1 B 1 A 1 B 1 3 3 * * * -40 1068-1 40A 127473-01CAA 45 127307-01CAA 50 MS21090-0621 • PC Power Port (Order Separately) (SUPSD by Item 40A) • Power Supply (1068-2) (Order Separately) (SUPSDS Item -40) • Power J-Box (1068820-2) (Order Separately) • Screw, Lock (Order Separately) 1 1 1 1 * * * 55 48553201 60 48251051 -60A 48251052 • Shim, Electric Box Bracket (Order Separately) • Bracket Assembly, Electric Box (Order Separately) • Bracket Assembly, Electric Box (Order Separately) 2 A 1 B 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10101 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 21 -65 PART NUMBER FHA-032-24 -70 -75 MS35650-30ST MS21042-3 80 85 90 MS27039-1-13 96040253 22NKTM-02 AIRLINE NOMENCLATURE PART NO. 1234567 • • Stud-Pem (Order Separately) (REF SB 25-20-1308, 1402) • • Nut (Order Separately) • • Nut, Lock (Order Separately) ATTACHING PARTS • Screw, Pan Hd (Order Separately) • Bushing (Order Separately) • Nut, Cap (Order Separately) EFF CODE UNITS PER ASSY 1 1 1 2 2 2 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10102 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10103 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 60 35 20 15 35 5 20 35 30 15 55A 10 25 30 40A 45 Baggage Bar and Installation Figure 22 R5 25-29-76 Controlled Page 10104 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 22 PART NUMBER AIRLINE NOMENCLATURE PART NO. 1234567 BAGGAGE BAR AND INSTALLATION EFF CODE UNITS PER ASSY -1 48294001 (NP) Baggage Bar Installation (See FIG 1 for NHA) RF 5 48528201 RF -5A 48528202 -5B 48528203 -5C 48528204 Baggage Bar LH Seat (Order Separately) Baggage Bar RH Seat (Order Separately) Baggage Bar LH Seat (Order Separately) Baggage Bar RH Seat (Order Separately) (See FIG 1 for NHA) 10 45469001 15 MS27039-1-17 20 25 30 35 AN970-3W MS27039-1-14 AN970-3 MS21042-3 -40 MS27039-1-06 40A MS27039-1-14 45 -50 -55 AN970-3 96040303 M13100001-2-6 55A 22NKM-02 60 MS27039-1-13 • Doubler, Baggage Bar (Order Separately) • Screw, Pan Hd (Order Separately) • Washer (Order Separately) • Screw, Pan Hd (Order Separately) • Washer (Order Separately) • Nut (Order Separately) • Screw, Pan Hd (Order Separately) (SUPSD by Item 40A) • Screw, Pan Hd (Order Separately) (SUPSDS Item -40) • Washer (Order Separately) • Bushing (Order Separately) • Clip nut (Order Separately) (SUPSD by Item 55A) • Nut (Order Separately) (SUPSDS Item -55) • Screw, Pan Hd (Order Separately) RF RF RF 1 2 2 1 2 3 1 1 1 1 1 1 1 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10105 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 15 10 30A 25A 60 20 5 45 35 40 40 50 55 35 45 Frame Assembly Figure 23 R5 25-29-76 Controlled Page 10106 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 23 PART NUMBER AIRLINE NOMENCLATURE PART NO. 1234567 FRAME ASSEMBLY EFF CODE UNITS PER ASSY A B C D E F RF RF RF RF RF RF G H RF RF -1 -1A -1B -1C -1D -1E 48200001 48200002 48200405 48200406 48200403 48200404 -1F -1G 48200021 48200022 Frame Assembly LH STD Frame Assembly RH STD Frame Assembly LH Offset Frame Assembly RH Offset Frame Assembly LH NRW Frame Assembly RH NRW (See FIG 1 for NHA) Frame Assembly LH STD Frame Assembly RH STD 5 -5A 48202001 48202201 • Beam, Front • Beam, Front A-DGH EF 1 1 10 -10A 48202005 48202205 • Beam, Rear • Beam, Rear A-DGH EF 1 1 15 20 -25 48201001 48201002 48201003 25A 48201023 -30 48201004 30A 48201024 35 AN3-24A 40 MS21042-3 • Spreader Assembly • Spreader Assembly • Spreader Assembly (Center) (SUPSD by Item 25A) • Spreader Assembly (Center) (SUPSDS Item -25) • Spreader Assembly (Center) (SUPSD by Item 30A) • Spreader Assembly (Center) (SUPSDS Item -30, REF SB 25-20-2213) (See FIG 25 for DET BKDN) ATTACHING PARTS • Bolt (Apply Loctite 271 to Bolt Threads) • Nut 45 -45A -45B -45C 48226001 48226003 48226004 48226005 • Leg Assembly • Leg Assembly B737 O/B LH • Leg Assembly B737 O/B RH • Leg Assembly B737 I/B LH 1 1 1 1 1 1 2 2 * * * ABE-H C D C 2 1 1 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10107 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 23 -45D 50 55 60 PART NUMBER 48226006 AN4-20A 98035003 NAS679A4W AIRLINE NOMENCLATURE PART NO. 1234567 • Leg Assembly B737 I/B RH (See FIG 24 for DET BKDN) ATTACHING PARTS • Bolt • Washer • Nut EFF CODE UNITS PER ASSY D 1 2 2 2 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10108 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10109 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 40 45 70 5 60 30 35A 60 65 55 65 50 25 75 10 20 15 100 95 85 90 OFFSET LEGS ONLY Leg Assembly Figure 24 R5 25-29-76 Controlled Page 10110 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 24 PART NUMBER AIRLINE NOMENCLATURE PART NO. 1234567 LEG ASSEMBLY -1 -1A -1B -1C -1D 48226001 48226003 48226004 48226005 48226006 Leg Assembly Leg Assembly Offset, B737 O/B LH Leg Assembly Offset, B737 O/B RH Leg Assembly Offset, B737 I/B LH Leg Assembly Offset, B737 I/B RH (See FIG 23 for NHA) 5 48207101 • Leg, Machined 10 97123007 15 20 25 22303107 NP565D8H4 BALL-NYLON • Nut, Anti-Rattle (REF SB 25-20-1294) • Stud • Setscrew • 1/8 dia. EFF CODE UNITS PER ASSY A B C D E RF RF RF RF RF 1 A 1 A 1 1 1 * * * 30 48207201 -35 MS20470AD8-24A 35A NAS623-4-18W 40 45 AN960-416 52NKTE-048 • Leg, Doubler ATTACHING PARTS • Rivet, Solid (SUPSD by Items 35A, 40, 45) • Screw, Pan Hd (SUPSDS Item -35) • Washer • Nut, Cap 2 2 1 1 1 * * * 50 91101205 55 60 65 70 NAS623-5-18W AN960-516 48229003 52NKTE-054 • Track Fitting Assembly ATTACHING PARTS • Screw, Pan Hd • Washer • Washer / Spacer • Nut, Cap 1 1 2 2 1 * * * 75 41544013 • Cover, Track Fitting Saver 1 * * * -80 -80A -80B 91080005 91080006 91080007 • Track Adapter Assembly, O/B LH • Track Adapter Assembly, O/B RH • Track Adapter Assembly, I/B LH B C D 1 1 1 - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10111 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 EFF CODE UNITS PER ASSY • Track Adapter Assembly, I/B RH E 1 44146005 44146006 44146007 44146008 • • Track Adapter O/B LH • • Track Adapter O/B RH • • Track Adapter I/B LH • • Track Adapter I/B RH B C D E 1 1 1 1 90 95 100 22303121 44146013 MS21083N6 BCDE BCDE BCDE 2 1 2 -105 LP24694-S185 • • Stud • • Alignment Plate • • Nut, Lock ATTACHING PARTS • Screw, Csk BCDE 1 FIG. ITEM 24 -80C 91080008 85 -85A -85B -85C PART NUMBER AIRLINE NOMENCLATURE PART NO. 1234567 * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10112 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10113 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 45 35 10 5 30 25 20 15 Spreader Assembly Figure 25 R5 25-29-76 Controlled Page 10114 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 FIG. ITEM 25 PART NUMBER AIRLINE NOMENCLATURE PART NO. 1234567 SPREADER ASSEMBLY -1 48201003 • Spreader Assembly (Center) (SUPSD by Item -1A) • Spreader Assembly (Center) (SUPSDS Item -1, REF SB 25-20-2213) • Spreader Assembly (Center) (SUPSD by Item -1C) • Spreader Assembly (Center) (SUPSDS Item -1B, REF SB 25-20-2213) • Spreader Assembly • Spreader Assembly (See FIG 23 for NHA) -1A 48201023 -1B 48201004 -1C 48201024 -1E -1F 48201001 48201002 5 48203401 • Articulation Roller 10 -10A 48203113 48203111 15 20 LP27039-4-06 48229001 -20A AN970-4 • Shaft, Artic Roller • Shaft, Artic Roller ATTACHING PARTS • Screw • Washer / Spacer (SUPSD by Item -20A) • Washer / Spacer (SUPSDS Item 20) EFF CODE UNITS PER ASSY A RF B RF C RF D RF E F RF RF 1 A-D EF 1 1 1 1 1 * * * 25 40844027 30 35 AN960-616L 52NKE-064 • Eyebolt, Special ATTACHING PARTS • Washer • Nut, Cap A-D 1 A-D A-D 1 1 EF 1 ABE CDF 1 1 BD 1 * * * -40 42ND12-048 • Nut, Spline * * * 45 -45A 48201101 48201102 • Spreader • Spreader * * * -55 48203407 • Spreader Bushing (Added Per SB 25-20-2213) * * * - ITEM NOT ILLUSTRATED R5 25-29-76 Controlled Page 10115 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 10116 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 MAINTENANCE AND SERVICING 1. General A. Description These recommended maintenance procedures are applicable to all Millennium Series seats currently in operation. The following maintenance schedules are recommended for Millennium Series seats. CHECK DAILY MONTHLY CHECK - IN AIRCRAFT LIGHT CHECK - IN AIRCRAFT HEAVY CHECK - OUT OF AIRCRAFT B. Compliance is at the discretion of the customer. Failure to perform proper preventive maintenance may adversely affect serviceability of the seat. C. All procedures may be implemented during normal scheduled maintenance cycles. D. These maintenance procedures do not affect the certification basis of the seat unit. However, failure to replace damaged or defective components could affect the airworthiness of the seat. E. The installation and use of non B/E Aerospace products/components on this seat assembly will affect the certification and warranty of the seat. R5 25-29-76 Controlled Page 14001 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 2. Checks A. Daily Checks NOTE: Limited access time during daily checks, unless specifically indicated, does not normally allow sufficient time for component replacement. Consider the extent of the damage/defect to determine if the component replacement can be deferred until an appropriate scheduled maintenance period, or if the seat should be repaired immediately. Task Time Required 1 Carry out a visual examination of the general condition of seat and seat covers. 2 Check seat track fittings for secure attachment to floor tracks. 3 Check the condition of all life vest pouches or flotation cushions. 4 Check to make sure that recline controls operate correctly. 5 Check all in-arm food tables for damage and correct operation. 6 Check IFE and electrical components for proper operation. 7 Check center console for serviceability of sliding tray assembly and proper functioning of PC power ports. R5 25-29-76 Controlled Page 14002 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 B. Monthly Check - In Aircraft NOTE: Limited access time during monthly checks, unless specifically indicated, does not normally allow sufficient time for component replacement. Consider the extent of the damage/defect to determine if replacement/repair can be deferred until an appropriate scheduled Light or Heavy check, or if the seat should be repaired immediately. Task Time Required 1 Carry out a visual examination of the complete seat assembly (Refer to IPL Figure 1). Examine parts for cuts, nicks, cracks, corrosion, scoring, damaged threads, excessive wear and any defects which may impair the efficient operation of the seat. 2 Seat Covers and Cushions (Refer to IPL Figure 1, 2, 3, 5 and 6) • Replace any cushion covers and seat back covers that have been damaged or are dirty/stained. These can be repaired/cleaned as required. Refer to CLEANING. • Replace hook and pile fasteners on seat covers as required. 3 Seatpan Assembly (Refer to IPL Figure 7 and 8) • Check all seat belt shackles for damage and secure attachment. Repair/replace as necessary. • Check all seat belts for damage and secure attachment. Repair/replace as necessary. • Check/tighten all loose nuts, bolts and screws. Pay particular attention to the baggage bar doubler. Replace any worn or damaged items. • Check the bottom diaphragm. Replace any damaged bottom diaphragm support tube assemblies. • Check to make sure the baggage bar tube plugs are securely fitted. Replace if missing. 4 Leg Assemblies (Refer to IPL Figure 21 or 22) • Check/tighten all loose bolts. Replace any worn or damaged items. • Check serviceability of the rear leg fitting assembly. • Ensure seat track fittings are secure in the floor track. • Ensure spreaders are undamaged. • Check the SEB, including mounting brackets for damage. 5 Rub strips and covers (Refer to IPL Figure 13) • Check rub strips for damage and secure attachment. Slightly damaged areas on rub strips may be trimmed, then replaced at the earliest opportunity. R5 25-29-76 Controlled Page 14003 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 Task 6 Time Required Center Console Assembly (Refer to IPL Figure 16) • Check sliding tray, cocktail table, armcap and heelcap for secure installation and damage. Tighten/repair/replace as necessary. • Check PC power outlet for proper functioning. Repair/ replace as necessary. • Check all shrouds for damage. Repair/replace as necessary. 7 Back Assemblies (Refer to IPL Figure 5 or 6) • Check/tighten all loose bolts and nuts, paying particular attention to the Hydrolok and recline arm installation. Replace any worn or damaged items. • Check headrest assembly for secure installation. Check ear assemblies for 6-8 lb. tension. Adjust as necessary (Refer to REPAIR) • Ensure literature pocket springs are secure and correctly fitted. Replace as necessary. • Adjust seat controls, as required, by adjusting the cable jam nuts. Refer to REPAIR section • Set the seat backs in line to the dimensions shown in DESCRIPTION AND OPERATION. 8 Endbay Assemblies (Refer to IPL Figure 11, 12 and 13) • Replace all damaged or worn armcap assemblies. • Check/tighten all screws and bolts. • Ensure there are no rough edges on screws etc. Blend as necessary. • Check armcap hinges for loose screws and damage. Repair/replace as necessary. • Check remote jack unit (RJU) transducers, if applicable, for security/damage. Replace as necessary. • Check front and rear escutcheons for security/damage. Replace as necessary. • Check all shrouds for damage. Repair/replace as necessary. • Check function of in-arm food table, paying particular attention to table link pins and linkages. • Check in-arm food table alignment. If out of alignment, set by adjusting set screws. R5 25-29-76 Controlled Page 14004 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 C. Light Check - In Aircraft NOTE: Light Check includes all previous checks plus some additional checks. Task Time Required 1 Carry out a visual examination of the complete seat assembly (Refer to IPL Figure 1). Examine parts for cuts, nicks, cracks, corrosion, scoring, damaged threads, excessive wear and any defects which may impair the efficient operation of the seat. 2 Seat Covers and Cushions (Refer to IPL Figure 1, 2, 3, 5 and 6) • Replace any cushion covers and seat back covers that have been damaged or are dirty/stained. These can be repaired/cleaned as required. Refer to CLEANING. • Replace hook and pile fasteners on seat covers as required. 3 Seatpan Assembly (Refer to IPL Figure 7 and 8) • Check all seat belt shackles for damage and secure attachment. Repair/replace as necessary. • Check all seat belts for damage and secure attachment. Repair/replace as necessary. • Check/tighten all loose nuts, bolts and screws. Pay particular attention to the baggage bar doubler. Replace any worn or damaged items. • Check the bottom diaphragm. Replace any damaged bottom diaphragm support tube assemblies. 4 Leg Assemblies (Refer to IPL Figure 21, 22 and 23) • Thoroughly examine the leg assemblies, including spreaders for any signs of corrosion. • Check leg assemblies for damage. Replace any damaged legs. • Check/tighten all loose bolts. Replace any worn or damaged items. • Check serviceability of the rear leg fitting assembly. • Ensure seat track fittings are secure in the floor track. • Ensure spreaders are undamaged. R5 25-29-76 Controlled Page 14005 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 Task 5 Time Required Center Console Assembly (Refer to IPL Figure 16) • Examine sliding tray and cocktail tray for damage/wear to laminate. Replace any damaged assemblies. • Check sliding tray, cocktail table, armcap and heelcap for secure installation and damage. Tighten/repair/replace as necessary. • Check all shrouds for damage. Repair/replace as necessary. • Check front and side shrouds for secure installation. Replace plastic rivets as necessary. • Check PC power outlet for proper functioning. Repair/ replace as necessary. • Check PC power harness. Check connectors and examine harness for obvious signs of chafing or wear. 6 Endbay Assemblies (Refer to IPL Figure 11, 12 and 13) • Replace all damaged or excessively worn armcap assemblies. • Check/tighten all screws and bolts. • Ensure there are no rough edges on screws etc. Blend as necessary. • Check armcap hinges for loose screws and damage. Repair/replace as necessary. • Check remote jack unit (RJU) transducers, if applicable, for security/damage. Replace as necessary. • Check front and rear escutcheons for security/damage. Replace as necessary. • Check all shrouds for damage. Repair/replace as necessary. • Check front and side shrouds for secure installation. Replace plastic rivets as necessary. • Check function of in-arm food table, paying particular attention to table link pins and linkages. • Examine all in-arm food table laminates. Repair/replace any damaged in-arm food tables. • Check in-arm food table alignment. If out of alignment, set by adjusting set screws. R5 25-29-76 Controlled Page 14006 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 Task 7 Time Required Rub strips and covers (Refer to IPL Figure 13) • Check rub strips for damage and security of attachment. If loose, secure using appropriate fastenings: double sided tape, hook and pile, screws and bolts, etc. • As a short term solution, trim damaged areas on rub strips which have only slight damage. They should be replaced at the earliest opportunity. 8 Back Assembly and Installation (Refer to IPL Figure 4, 5 and 6) • Check headrest assembly for secure installation. Check ear assemblies for 6-8 lb. tension. Adjust as necessary (Refer to REPAIR) • Ensure literature pocket springs are secure and correctly fitted. Replace as necessary. • Check/tighten all loose bolts and nuts, paying particular attention to the Hydrolok and recline arm installation. Replace any worn or damaged items. • Check all Hydrolok and recline control mechanical cables. Replace any found defective. • Adjust seat controls, as required, by adjusting the cable jam nuts. Refer to REPAIR section • Set the seat backs in line to the dimensions shown in DESCRIPTION AND OPERATION. 9 Seat Covers and Cushions (Refer to IPL Figure 1, 2, 3, 5 and 6) • Replace any cushion covers and seat back covers that have been damaged or are dirty/stained. These can be repaired/cleaned as required. Refer to CLEANING. • Replace hook and pile fasteners on seat covers as required. R5 25-29-76 Controlled Page 14007 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 14008 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 D. Heavy Check - Out of Aircraft NOTE: Heavy Check includes all previous checks plus some additional checks. Task 1 Time Required Preparation and Cleaning Procedure • Carry out a visual examination of the complete seat assembly (Refer to IPL Figure 1). Thoroughly inspect all components, assemblies and sub-assemblies using a strong light and some means of magnification. Examine parts for cuts, nicks, cracks, corrosion, scoring, damaged threads, excessive wear and any defects which may impair the efficient operation of the seat. 2 Leg Assembly (Refer to IPL Figure 21, 22 and 23) • Check/tighten all fasteners. Replace any defective bolts. • Check leg assemblies for damage caused during removal/ installation of seat in tracks in the aircraft. Replace any defective/ damaged components. • Check all track fitting studs and track fitting assemblies. Replace any defective/damaged components. • Check spreader assemblies for cracks, corrosion or other damage. Replace any damaged spreaders. • Check to make sure that all hardware on SEB is correctly tightened. Check for dust, or other blockage in ventilation areas. 3 Frame Assembly (Refer to IPL Figure 20) • Check/tighten all loose bolts and nuts. Pay particular attention to the Hydrolok and recline arm installation. Replace any worn or damaged items. • Check the baggage bar for damage and replace as necessary. • Check to make sure that baggage bar tube plugs are securely fitted. Replace as necessary. • Check all bottom diaphragm tube assemblies for bending, cracking, corrosion and other signs of damage. Replace as necessary. • Check all seat diaphragms. Replace as necessary. • Check all seat belt linkages for damage and for security of attachment. Replace any damaged/defective items. • Check/tighten all seat belt linkage attachment bolts and nuts. R5 25-29-76 Controlled Page 14009 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 Task 4 Time Required Back Assembly and Installation (Refer to IPL Figure 4, 5 and 6) • Check all bolts and nuts for damage. Replace any worn or damaged items. • Check all Hydrolok assemblies. Replace as necessary. • Adjust seat backs to the dimensions shown in DESCRIPTION AND OPERATION. • Adjust seat controls, as required, by adjusting the cable jam nuts. • Ensure the literature pocket springs are secure and correctly fitted. Replace any defective literature pocket springs. 5 Endbay Assemblies (Refer to IPL Figure 11, 12 and 13) • Check/tighten all bolts. Ensure there are no rough edges on fasteners. Replace as necessary. • Check all recline control mechanical cables. Replace any found defective. • Replace all compartment hinges, unless they have already been replaced since previous heavy check. • Replace all shroud panels, unless they have already been replaced since previous heavy check. Replace all plastic rivets. • Replace all rub strips, unless they have already been replaced since previous heavy check. • Replace all escutcheons, unless they have already been replaced since previous heavy check. • Replace all arm cap assemblies, unless they have already been replaced since previous heavy check. • Check all in-arm food tray cover leaves for damage. Repair/ replace as required. • Check function of in-arm food table, paying particular attention to table link pins and linkages. • Check in-arm food table alignment. If out of alignment, set by adjusting set screws. R5 25-29-76 Controlled Page 14010 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 Task 6 Time Required Center Console Assembly (Refer to IPL Figure 16) • Check PC power harness. Check connectors and examine harness for signs of chafing or wear. Replace as necessary. • Check sliding tray and cocktail table assemblies. Replace as necessary. • Replace front shroud assembly and side shroud panels, unless they have already been replaced since previous heavy check. • Replace all armcap assemblies, unless they have already been replaced since previous heavy check. • Replace all heelcap assemblies, unless they have already been replaced since previous heavy check. 7 Seat Covers and Cushions (Refer to IPL Figure 1, 2, 3, 5 and 6) • Test seat covers for continued flame retardancy. NOTE: Repetitive cleaning and buildup of foreign substances in covers will adversely affect flame retardancy of covers over time. Cover appearance may be adequate while actual serviceability no longer meets regulatory requirements. • Replace any cushion covers and seat back covers that have been damaged or are dirty/stained. These can be repaired/ cleaned as required. Refer to CLEANING. • Replace hook and pile fasteners on seat covers as required. • Replace all back and seat cushion assemblies (Refer to IPL Figure 1, 3, 5 and 6). 8 Electrical • Check all cables for continuity. Replace any cable assemblies that fail continuity checks. • Clean and check all IFE equipment i.e. PCU, MUX box, RJU and SEB cover etc. Replace any damaged/defective components. R5 25-29-76 Controlled Page 14011 Feb 10, 2009 B/E AEROSPACE COMPONENT MAINTENANCE MANUAL MILLENNIUM SERIES 87836 THIS PAGE IS INTENTIONALLY LEFT BLANK. R5 25-29-76 Controlled Page 14012 Feb 10, 2009

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