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25-20-04

COMPONENT MAINTENANCE MANUALWITH

ILLUSTRATED PARTS LIST

Jan 30/2005

B757-200

FWD LEFT CLOSET

Part Number101041-1

101041-101101041-201

THIS DOCUMENT CONTAINS PROPRIETARY INFORMATION

"ANY USE OR DISCLOSURE OF THIS DOCUMENT TO A THIRDPARTY OR ANY REPRODUCTION IS EXPRESSLY PROHIBITED

EXCEPT AS DRIESSEN AIRCRAFT INTERIOR SYSTEM MAYOTHERWISE AGREE IN WRITING"

TP1 REVISION NC

10781 Forbes AvenueGARDEN GROVE, CA 92643

Telephone (714) 265-2911Telefax (714) 265-2301

Telex: 756227Vendor Code: 62225

25-20-04 Jan 30/2005

COMPONENT MAINTENANCE MANUALPART NO. 101041

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TP


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REVNO.

ISSUEDATE

DATEINSERTED BY

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ISSUEDATE

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RETAIN THIS RECORD IN THE FRONT OF MANUAL OR CHAPTER.ON RECEIPT OF REVISIONS, INSERT REVISED PAGES IN THE MANUALAND ENTER REVISION NUMBER, DATE INSERTED, AND INITIALS.

RECORD OF REVISIONS

ROR Page 1

Initial Jan 30/2005 Jan 30/2005 NG

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RECORD OF TEMPORARY REVISIONS

Temporary Page Number Issue Date Date Removed ByRevision No.

RTR Page 1

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SERVICE BULLETIN LIST

Service Original Revision Number Date Bulletin Bulletin Number Issue Date and Date Incorporated

SBL Page 1

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SBL Page 2


Jan 30/200525-20-04 LEP Page 1

LIST OF EFFECTIVE PAGES

* The asterisk indicates pages changed, added, or deletedF = Fold out pages

CHAPTERSECTIONSUBJECT

DATECHAPTERSECTIONSUBJECT

DATEPAGE PAGE

Title TP-1 Jan 30/2005TP-2 Jan 30/2005

Record of Revisions ROR-1 Jan 30/2005ROR-2 Jan 30/2005

Record of Temporary RTR-1 Jan 30/2005Revisions RTR-2 Jan 30/2005Service Bulletin List SBL-1 Jan 30/2005

SBL-2 Jan 30/2005List of Effective Pages LEP-1 Jan 30/2005

LEP-2 Jan 30/2005Table of Contents TOC-1 Jan 30/2005

TOC-2 Jan 30/2005List of Tables LOT-1 Jan 30/2005

LOT-2 Jan 30/2005List of Illustrations LOI-1 Jan 30/2005

LOI-2 Jan 30/2005List of Abbreviations LOA-1 Jan 30/2005

LOA-2 Jan 30/2005Introduction INTRO-1 Jan 30/2005

INTRO-2 Jan 30/2005Description and 1 Jan 30/2005Operation 2 Jan 30/2005

3 Jan 30/20054 Jan 30/20055 Jan 30/20056 Jan 30/20057 Jan 30/20058 Jan 30/2005

Testing and Fault 1001 Jan 30/2005Isolation 1002 Jan 30/2005Wiring Diagm 2001 Jan 30/2005

2002 Jan 30/2005Disassembly 3001 Jan 30/2005

3002 Jan 30/2005Cleaning 4001 Jan 30/2005

4002 Jan 30/20054003 Jan 30/20054004 Jan 30/2005

Check 5001 Jan 30/20055002 Jan 30/2005

Repair 6001 Jan 30/20056002 Jan 30/20056003 Jan 30/20056004 Jan 30/20056005 Jan 30/20056006 Jan 30/20056007 Jan 30/20056008 Jan 30/2005

6009F Jan 30/20056010F Not used

Assembly 7001 Jan 30/20057002 Jan 30/2005

Fits and Clearances 8001 Jan 30/20058002 Jan 30/2005

Illustrated Parts List 10001 Jan 30/200510002 Jan 30/200510003 Jan 30/200510004 Jan 30/2005

Numerical Index 10005-1 Jan 30/200510005-2 Jan 30/200510005-3 Jan 30/200510005-4 Jan 30/2005

IPL Figure 1 10006-1F Jan 30/200510006-2F Not used10006-3 Jan 30/200510006-4 Jan 30/200510006-5 Jan 30/200510006-6 Jan 30/200510006-7 Jan 30/200510006-8 Jan 30/2005

IPL Figure 2 10016-1F Jan 30/200510016-2F Not used10016-3 Jan 30/200510016-4 Jan 30/2005

IPL Figure 3 10017-1F Jan 30/200510017-2F Not used10017-3 Jan 30/200510017-4 Jan 30/2005

IPL Figure 4 10018-1F Jan 30/200510018-2F Not used10018-3 Jan 30/2005

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LEP Page 2

LIST OF EFFECTIVE PAGES

* The asterisk indicates pages changed, added, or deletedF = Fold out pages

CHAPTERSECTIONSUBJECT

DATECHAPTERSECTIONSUBJECT

DATEPAGE PAGE

IPL Figure 4 (cont'd) 10018-4 Jan 30/2005IPL Figure 5 10019-1F Jan 30/2005

10019-2F Not used10019-3 Jan 30/200510019-4 Jan 30/2005

Removal 12001 Jan 30/200512002 Jan 30/2005

Installation 13001 Jan 30/200513002 Jan 30/2005

Servicing 14001 Jan 30/200514002 Jan 30/200514003 Jan 30/200514004 Jan 30/2005

Storage 15001 Jan 30/200515002 Jan 30/2005


Jan 30/200525-20-04 TOC Page 1

TABLE OF CONTENTS

PARAGRAPH TITLE PAGE

Description and Operation.....................................................................................................................1Testing and Fault Isolation...............................................................................................................1001Wiring Diagram................................................................................................................................2001Disassembly.....................................................................................................................................3001Cleaning............................................................................................................................................4001Check.................................................................................................................................................5001Repair................................................................................................................................................6001Assembly...........................................................................................................................................7001Fits and Clearances.........................................................................................................................8001Illustrated Parts List........................................................................................................................10001Removal..........................................................................................................................................12001Servicing.........................................................................................................................................14001Storage...........................................................................................................................................15001

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TOC Page 2



Jan 30/200525-20-04 LOT Page 1

LIST OF TABLES

TABLE PAGE

1 Associated Documents..............................................................................................................12 Leading Particulars.....................................................................................................................54001 Recommended Cleaning Agents and Materials....................................................4001, 40026001 Repair Materials...................................................................................................................60088001 Standard Torque Values.....................................................................................................800114001 Recommended Servicing Agents and Materials..............................................14001, 14002

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LOT Page 2



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LIST OF ILLUSTRATIONS

FIGURE PAGE

1 General Arrangement..............................................................................................................22 Closet Attachments..................................................................................................................63 Closet Provisions.....................................................................................................................72001 Wiring Diagram...................................................................................................................20036001 Trim and Finish...................................................................................................................6009IPL 1 Final Assembly..............................................................................................................10006-1IPL 2 Door Assembly..............................................................................................................10016-1IPL 3 Door Assembly..............................................................................................................10017-1IPL 4 Door Assembly..............................................................................................................10018-1IPL 5 Door Assembly..............................................................................................................10019-1

LOI Page 1

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LOI Page 2


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LIST OF ABBREVIATIONS

The following abbreviations are used in this component maintenace manual:

A ampereA/C aircraftAC alternating currentAR as requiredASSY assemblyATA Air Transportation Association of AmericaBF buyer furnishedBFE buyer furnished equipmentC CelciusCCW counter-clockwiseCFM cubic feet per minuteCG center of gravityCL centerlineCMM Component Maintenance ManualCW clockwiseDC direct currentetc et cetera (and so on)F FahrenheitFAA Federal Aviation AdministrationFig FigureFPM feet per minuteFPS feet per secondFWD forwardGND groundGPM gallons per minuteHg inches of mercuryHz hertz (cycles per second)ID identificationIN inchIPL Illustrated Part ListINSTL InstallationKVA kilovolt amperesLBL left butt lineLBS poundsLEP List of Effective PagesLH left-handMAX maximumMIN minimumMISC miscellaneous

LOA Page 1

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MM millimeterNAS National Aerospace StandaNHA next higher assemblyNo. numberNS/FSB No Smoking/Fasten Seat BeltOUTBD outboardPN part numberPSIA pounds per square inch absolutePSID pounds per square differential pressurePSIG pounds per square inch gaugePWR powerRef. referenceRBL right butt lineRH right-handRF For reference onlySB Service BulletinSF supplier furnishedSFE seller-furnished equipmentSPS Standard Production SpecificationSTA stationTR Temporary RevisionTYP typicalV voltsW wattsWL waterlineWT weight

LOA Page 2


Jan 30/200525-20-04 INTRO Page 1

INTRODUCTION1. Scope of Manual

This component maintenance manual provides instructions for maintenance of FWD LeftCloset Part Number 101041. Instructions are provide for maintenance duties rangingfrom on-board cleaning through simple checks and minor repairs to complete disassembly of the unit for comprehensive shop overhaul. Repairs beyond the scope of this manualshould be referred to the manufacturer.This manual has been compiled in accordance with ATA Specification 100.

2. Manufacturing

This product is manufactured and supported by:

Driessen Aircraft Interior Systems Inc.10781 Forbes AvenueGARDEN GROVE, CA 92843Telephone (714) 265-2911Fax (714) 265-2301 or (714) 265-1802E-mail: [email protected]

3. Layout of Manual

Instructions contained in this manual include:

A. The Description and Operation section provides general descriptions, safetyconsiderations, maintainability, operations, and leading particulars of the Closet.Nomenclature used in this section is consistent with that used throughout this manual.

B. In Testing and Fault Isolation, checks and tests required to determine the conditionof the Closet are contained.

C. Under Disassembly, the disassembly procedures for parts requiring removal to allowfor visual inspection and for parts that can be removed and/or replaced are detailed.

D. The Cleaning section lists cleaning agents/materials, as well as instructions for"In-Service Cleaning", "Field Maintenance", and "Periodic Maintenance" of the Closet.

E. Methods and criteria for determining the serviceability of individual parts is covered inthe Check section.

F. Procedures and materials necessary to repair/replace worn or damaged componentsand restore the Closet to a serviceable condition can be found under Repair.

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H. The Assembly section includes materials required and procedures (consistent with theDisassembly section) for the assembly of the Closet.

J. The Fits and Clearances section lists critical fit clearance tolerances for parts.

K. The Illustrated Parts List section:

(1) An itemized breakdown of parts used on the Closet which are illustrated asnecessary to provide for their identification.

(2) A numerical index listing all spare parts by part number.

(3) A vendor list identifying the manufacturer of a part(s) not produced by Driessen,including their name, address and Cage Code; and

(4) A brief introduction on how to use this portion of the manual.

L. The Removal section provides Closet removal instructions from the aircraft.

M. The Installation section provides Closet installation instructions from the aircraft.

N. The Servicing section provides restoration procedures of the Closet.

P. The Storage section provides storing procedures of the Closet while not installed inthe aircraft.

4. Revisions

A. This manual will be updated in accordance with ATA Specification 100, Section 1-4-0Issuance and Revision Service Policy.

B. Service Bulletins will be issued separately; however, manual revisions will reflect theimpact of applicable Service Bulletins.

5. Shop Verification

The section of this manual have been at the manufacturer's facility by performing the Closetfuctional test, test report number: 440041-201-1.

INTRO Page 2


Jan 30/200525-20-04

DESCRIPTION AND OPERATION1. General

The FWD Left Closet part number 101041 Series is a major component of the Galleysystem installed on Boeing 757-200.

The Closet is an integrally-bonded structure fabricated from fiberglass-sandwich panels,aluminum extrusions, and a removable, aluminum workdeck. The panel joints areaccomplished by "mortise and tenon joints" and the fiberglass phenolic/Nomex honeycombpanels are fabricated in the accordance with Driessen Standard Process Specification. TheCloset design is modular in nature with functional components designated to specificcompartments.

Reference the table below and Driessen Drawing Number 101041 for further information.

Table 1Associated Documents

Page 1

FWD LEFT COAT CLOSET P/N 101041-1 P/N 101041-101 P/N 101041-201

BOEING ASSOCIATED DOCS. DRAWING NO. DRAWING NO. DRAWING NO.

COORDINATION DRAWING 65C15998 SHT. 48 THRU 51 65C15998 SHT. 48 THRU 51GENERAL DESING SPECCONTOUR AT STA 380.00 & 378.00 413N3610 SHT. 2 413N3610 SHT. 2 413N3610 SHT. 2CONTOUR AT STA 404.00 413N3610 SHT. 19 413N3610 SHT. 19 413N3610 SHT. 19

AMERICAN ASSOCIATED DOCS. DRAWING NO. DRAWING NO. DRAWING NO.

CLOSET SPEC CONTROL EBE1002 EBE1002 EBE1002

DRIESSEN ASSOCIATED DOCS. DRAWING/ PART No. DRAWING/ PART No. DRAWING/ PART No.

GENERAL ARRANGEMENT 100041-3 100041-103 100041-203CLOSET ASSEMBLY 101041-1 101041-101 101041-201STRUCTURE ASSEMBLY 102041-11 102041-11 102041-111STRUCTURE DETAILS 103041 103041 103041BONDED STRUCTURE 104041-11 104041-11 104041-111ELECTRICAL INSTALLATION 107041-11 107041-11 107041-11TRIM AND FINISH 119041-3 119041-5 119041-5 (S/N 001-084)

119041-7 (S/N 085 (NT743) AND

SUBSEQUENT)

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Page 2

GENERAL ARRANGEMENTFigure 1


Jan 30/200525-20-04

2. Description

A. General

The FWD Left Closet facilitates for storing emergency equipments and coats.

B. FWD Left Closet Lower Attachments

The Closet employs four (4) hardpoints.Refer to Figure 2- Closet Attachments.

C. FWD Left Closet Upper Attachments

The Closet employs one (1) hardpoint.Refer to Figure 2- Closet Attachments.

D. FWD Left Closet Provisions

See Figure 3 - Closet Provisions.

Page 3

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Page 4

3. Safety Considerations

A. The Closet assembly incorporates safety design features such as rounded externalcorners, flush fittings, minimum projections and component retaining devices to preventobjects from flying when subjected to ultimate load conditions.

B. All movable components of the Closet, such as hinged doors, incorporate a positivelatching provision capable of retaining the component in the closed or stowed positionduring acceleration. All doors that are exposed when installed include secondarylatches.

C. General warning placards, emergency placards, crew instructions placards, and weightplacards are located in conspicuous places and are readable from normal workingpositions.

D. Material used in construction of the Closet is to be fire retardant. Additionally, areassubject to fire hazard (such as waste container stowage compartments, wastereceptacles, etc) are designed and manufactured to contain and prevent the spreadof fire.

4. Maintainability

The Closet is designed so that inspection, adjustment, service and removal/replacement ofparts requires no special tools. Convenient access is provided to the attachment fittings andvarious service facility connections at the airplane interface.

5. Operation

WARNING: DO NOT USE SIDE-HINGED DOORS AS A BRACE OR HANDHOLD.DO NOT USE DOORS AS A STEP LADDER. CLOSET DOORS AREDESIGNED TO BE USED IN SUCH A MANNER AND SUCH USE MAYRESULT IN INJURY TO PERSONNEL, AS WELL AS DAMAGE TO THEUNIT.

CAUTION: IF ITEMS DEPOSITED WITHIN A STORAGE COMPARTMENT ARETOO NUMEROUS OR BULKING TO ALLOW THE DOOR TO CLOSE.DO NOT ATTEMPT TO FORCE THE DOOR CLOSED. FORCEDCLOSURE OF DOORS MAY RESULT IN EXCESSIVE WEAR AND/ORDAMAGE TO THE CLOSET. REMOVE AS MANY ITEMS AS NECESSARYTO ALLOW SUFFICIENT CLEARANCE FOR THE DOOR TO CLOSE.


Jan 30/200525-20-04 Page 5

A. Doors

Turn the retainer 1/4 turn clockwise to unlock the doors with retainers. Once unlocked,the doors are opened by operating the pull latch(es). Doors without retainers are openedby operating the pull latch(es) only.

6. Leading Particulars

Table 2 provides a list of leading particulars for the FWD Left Closet.

Unit Part Number Height Width Depth Weight*

FWD Left 101041-1 79.22 in 43.83 in 26.00 in 391 lbs Closet 101041-101 (2012.19 mm) (1113.28 mm) (660.4 mm) (9931.4 kg) 101041-210

Table 2 Leading Particulars

* Estimated gross weight.

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Closet AttachmentsFigure 2

Page 6


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Closet ProvisionsFigure 3

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Page 8


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Page 1001

TESTING AND FAULT ISOLATION

1. General

Testing and Fault Isolation will not be required. If structural damage are found, the FWD LeftCloset must be repaired or replaced.

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Page 1002


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Page 2001

WIRING DIAGRAM1. General

Check each lead, system input and output for electrical continually in accordance withFigure 2001.

If all requirements of test procedures cannot be completed successfully, the Closet ofcomponent is defective.

Figure 2001


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DISASSEMBLY

1. General

The Closet is an integrally-bonded structure which is fabricated from sandwich panelsand aluminum extrusions. The unit cannot be disassembled without affecting its structureintegrity. As the paneling used to construct the unit is extremely strong and durable,disassembly instructions found herein are limited to removal of the closet from theaircraft and removal of high-wear, easily damaged components of disassembly needed toaccess those items requiring repair and/or replacement. Individual panel repairs may beaccomplished using the repair procedures outlined in the REPAIR section, starting on page6001.

The Closet should be disassembled only to the degree necessary to replace parts,carry out repairs and/or overhaul the unit. Complete disassembly is neither anticipated norrecommended.

Refer to FITS AND CLEARANCES section on page 8001 for applicable torque value.

2. Disassembly

CAUTION: MANY OF THE ELECTRICAL PARTS ON THE UNIT ARE SENSITIVE TOSTATIC ELECTRICITY. PERSONNEL MUST GROUND THEMSELVESBEFORE WORKING ON THESE PARTS.

WARNING: PRIOR TO STARTING ANY ELECTRICAL DISMANTLING, DISCONNECTIONAND/OR DISASSEMBLY, ENSURE THAT ALL POWER TO DISPLAY UNITASSEMBLY HAS BEEN REMOVED.

NOTE: Disassembly sequence is straight forward and self explanatory.

(a) Refer to IPL Figure 1 (Final Assembly) to disassemble.

(b) Refer to IPL Figure 2 (Door Assembly, P/N 127041-11) to disassemble.

(c) Refer to IPL Figure 3 (Door Assembly, P/N 128041-11) to disassemble.

(d) Refer to IPL Figure 4 (Door Assembly, P/N 129041-11/-21) to disassemble.

(e) Refer to IPL Figure 5 (Door Assembly, 126041-11) to disassemble.

Page 3001


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Jan 30/200525-20-04

CLEANING

1. General

The Closet must be cleaned before it is checked or repaired. Cleaning will expose defectsand/or damage as well as the size and location of necessary repairs. Cleaning removesunwanted material which can harm the unit’s performance and appearance.

2. Cleaning Materials

Only use recommended cleaning agents and materials (or appropriate equivalents). Takecare to comply with all cautions and warnings.

Equivalent susbstitutes may be used for listed items.

WARNING: SOME AGENTS AND MATERIALS CAN BE DETRIMENTAL TODECORATIVE TRIMS AND/OR FINISHES, AS WELL AS HARMFUL TOPERSONNEL, IF HANDED IMPROPERLY.

NOTE: GLASS AND MIRROR SURFACES, USE HOUSE HOLD CLEANERS,AMMONIATED DETERGENTS OR GLASS CLEANERS MAY BE USED.(DO NOT USE CLEANERS THAT CONTAIN ABRASIVES OR ALKALIS ASTHEY WILL MAR THE SURFACE).

Table 4001Recommended Cleaning Agents and Materials

Material Identification SourceAir, compressed Any approved source

Aliphatic Naphtha Federal Specification TT-N-95 Commercially available

Benzene Federal Specification VV-B-230 Commercially available

Brushes, small soft-bristled Commercially available

Brushes, non-metallic Commercially available

Cleaner, degreaser Kleenol-30 Mission Kleensweep Prod.2434 Birk DaleLos Angeles, CA

Chlorine compound Clorox or HTH Commercially available

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Table 4001Recommended Cleaning Agents and Materials (cont'd)

Material Identification SourceCloth, lint free Commercially available

Compound, corrosion MIL-C-38334 Commercially availableremoving

Detergent, commercial Super Soilax or Electrol-Sol Commercially available

Disinfectant Lysol Commercially available

Ethanol Alcohol Federal Specification O-E-760 Commercially available

Isobutyl Alcohol Federal Specification TT-B-846 Commercially available

Isopropyl Alcohol Federal Specification TT-I-735 Commercially available

Solvent Rho-clene 7688 Rho-Chem Corp.425 Isis AvenueInglewood, CA

Toluene Federal Specification TT-T-584 Commercially available

Xylene Federal Specification TT-X-916 Commercially available

3. In-Service Cleaning

This procedure is nomally performed by the flight attendants while the aircraft isin-service. Refer to Table 4001 for recommended cleaning agents and materials.

A. Wipe-up all spilled liquid immediately with a clean, soft cloth.

CAUTION: CLEANING CLOTHS ARE TO BE DAMP, NOT WET. EXCESSWATER CAN DAMAGE ELECTRICAL COMPONENTS.

B. Wipe all exposed Closet surfaces with a clean, damp cloth, including the insidecompartments and all working surfaces.

C. Clean all inserts, properly stow all waste materials, and clean all work areas.


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4. Field Maintenance

After each flight, ground crew maintenance shall include these steps for cleaning theCloset. Refer to Table 4001 for recommended cleaning agents and materials.

A. Wipe the inside surfaces of all compartments and work areas. Use a mild disinfectingdetergent and a clean, soft cloth. Be extra careful to fully clean any food handlingsurfaces or areas, such as work counters, coffee makers, drinking fountains, etc.

B. Vacuum the work area completely, particularly corners and crevices where soil canbecome trapped and accumulate.


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CHECK

1. General

A. Visually check all parts under a strong light for physical damage, such as nicks, dents,delamination cuts, cracks, burns, scoring, corrosion, stripped or crossed threads, andother defects. Replace any part when doubt of it's serviceability exists.

B. Procedures detailed in this section shall be performed as a normal function of periodicmaintenance (See Section 4000).

NOTE: EXCESSIVE WEAR SHALL BE DEFINED AS ANY OBVIOUS DEFORMATIONOR DETERIORATION OF A PART WHICH MAY RENDER THE EQUIPMENTINOPERATIVE. WHERE DOUBT EXISTS CONCERNING THESERVICEABILITY OF A PART, THE PART SHALL THEN BE CONSIDEREDUNSERVICEABLE.

2. Mechanical/Structural

A. Visually check for wear, or any defect that might impair the function or appearance ofthe unit.

B. Check all moving parts such as doors, latches, pull-out tables, etc. for distortion,excessive wear, burns, corrosion or scoring which might damage equipment orprevent efficient operation.

C. The structure consist of an integrally bonded unit. The manufacturer recommendsthat the unit be returned for major repairs needed to the bonded honeycomb structure.

D. Where major structure riveted or welded parts are suspect of metal fatigue or cracks,the dye penetrant method in accordance with Specification MIL-I-6866B, must beemployed. In the case of riveted assemblies suspected of damage such as elongatedrivet holes not visisble to the naked eye, the radiographic method in accordance withMIL-STD-453, must be used.

Page 5001

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Page 5002



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1. General

A. Except for those permissible repairs outlined below, the repair of a detailed part orcomponent is not considered practical.

2. Riveted Parts

A. Permissible limitations on size of rivet holes, where rivets were drilled out ondisassembly, are controlled by standard shop-practice use of oversized replacementrivets.

NOTE: THE MINIMUM PITCH AND DISTANCES FOR RIVETS ARE DETERMINEDBY THE ORIGINAL DESIGN AND SHOULD BE CLOSELY OBSERVEDDURING REPAIR.

3. Welded Parts

A. To replace damaged spot or tack-welded parts, cut away spot or tack in the damagedpart by spot-facing. Spot or tack-weld the replacement part to the undamaged partbetween old spots or tacks.

CAUTION: AVOID CUTTING INTO METAL OF ANY ADJOINING PARTS.

B. Spot-welding shall be accomplished in accordance with Specification MIL-W-6858 withtwo or four spots at a minimum edge distance of .25 inch.

4. Placard Replacement

A. The approximate location of each placard is to be shown on the Placard Installation orFinal Assembly drawing, unless specified by other documents.

(1) Proper bonding strength of pressure sensitive placards can only be achieved onclean surfaces.

(2) All contaminants must be removed by cleaning area with proper cleaner. Care shouldbe taken to insure compatibility of cleaner and material to be cleaned.

(3) Metals such as stainless steel and aluminum should be degreased and abraded ifnecessary to provide a smooth clean surface.

(4) Placards with adhesive ahould be applied at temperatures between 60 and 110 F.

REPAIR

Page 6001

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Jan 30/2005

(5) To install placards with pressure-sensitive adhesive, remove backng paper andapply firm even pressure.

(6) Placards requiring rivets shall be installed using blind rivets, per SPS 103.

5. Panel Repairs

A. Corrosion of non-appearance surfaces such as hardware associated with panels may bearrested by cleaning and applying a protective coating.

(1) Clean affected area with Rho-clene solvent by hand, wiping to remove any organicsoil.

(2) Remove corrosion products by brushing with a non-metallic bristle brush or bysanding. Rinse with clean water and dry thoroughly.

(3) Apply protective coating to affected areas.

B. Repair procedure for damaged honeycomb panel when the damaged area is 6 inch orless, and the affected area is limited to the panel skin on one side only plus theunderlying core material.

(1) Remove damaged skin and core material by cutting a round or square hole six (6)inches or less. Do not cut into the panel skin on the opposite side.

(2) Construct a plug using the same panel material and thickness by cutting the material2 inches larger than the panel hole. Cut one side of the material skin and core to .12inch smaller than the panel hole.

(3) Cold bond the plug in place using Crest 270 A/B. Sand smooth, then finish to matchthe rest of the panel.

C. Repair procedure for damaged honeycomb panel when the area is 6 inches in diameteror less, and both sides of the panel skin are affected.

(1) Cut a round hole up to 6 Inches through the panel, removing the damaged panelmaterial.

(2) Construct a plug using the same panel material and thickness. Bond in place usingCrest 270A/B.

(3) Mark a 2.50 inch border around the hole on each side of the panel. Cut two sheetsof fiberglass, to fit the borders, each having the same thickness as the panel skin.

Page 6002


Jan 30/200525-20-04 Page 6003

Bond the sheets in place using Crest 270A/B. Feather the edges of the fiberglassand refinish.

(4) For panel damage more than 6 inches in diameter, consult Driessen Engineering forwritten repair instructions.

D. Procedure for the replacement of Inserts. This procedure describes and providesinstruction to replace bonded insert in Honeycomb Panels.

(1) Remove damaged insert by warming Insert with a Heatgun until adhesive weakens.Remove damaged Insert by manually pulling with small hand pliers.

(2) Remove paper backing from SLT600 Shu-Tab and press Insert on to Tab, aligningholes in tab with holes in insert.

(3) Place Shur-Tab Insert Assembly in installation hole. Apply adequate force to insurethat tab will adhere to face of panel.

6. Decorative Area Repairs

A. Remove dents in metal decor panels by planishing lightly with a small hammer from thereverse side. Plastic-coated panels should be worked against an anvil covered with athin sheet of rubber or similar material to maintain decorative surface appearance.Painted panels may require additional refinishing by repainting.

B. Remove dents from stainless steel surfaces as in paragraph 5.A. However, access todent must be provided by removing a section of backing panel. Cut out a small area ofpanel back skin and core opposite the dent, leaving inner panel intact. Fill in the cutoutby “plugging”, after removing the dent. Refinish stainless steel surface per paragraph 5C.,if necessary.

C. Remove scratches or other discontinuities in satin-brushed stainless steel surfaces (orother satin-brushed metal surfaces) by finishing and blending in. Use a medium grade,satin finishing abrasive and work in same direction as original.

D. Repair damage to painted surfaces as follows:

(1) Fill in any objectionable scratches, gouges, etc., on substrate, using a filling compund.Sand smooth after compund sets up.

(2) Remove all loosely adhering paint or particles substrate by sanding around damagedarea or by “feathering in” edges of existing coating. Use a fine grade, abrasive paperor cloth.

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Jan 30/2005Page 6004

(3) Clean area with Kleenol-30 and dry with a clean cloth before solvent evaporates.

(4) Spray on the appropriate coating, according to applicable trim and finish to thetouch-up area. It is advisable to first apply a primer coat of protective coating if baremetal has been left exposed during the process of repair work.

(5) Remove blemishes from decorative metal surfaces with an original peened or non-directional finish as follows:

(a) Stop the growth of cracks by drilling a small (.04 inch diameter) hole, one on eachend of the crack. Apply only to cracks that occur in welds or other areas of metalcomponents such that only the appearance of hygienic features of unit areaffected.

(b) Remove protective coating over entire area that will be painted. Wipe clean withKleenol-30. Mask adjoining surfaces to protect from overspray.

(c) Fill cracks, stop holes and scratches with a filling compound. Sand smooth withfine paper after compound sets.

(d) Remove sanding residue and handling soil with Kleenol-30 solvent. Spray ontouch-up coating. Allow to dry for one hour at room temperature.

(e) Re-apply protective coating where removed.

7. Replacement of Decorative Materials

A. Removal of Damaged Decorative Laminates

(1) Remove all sealant on edges adjoining metal extrusion.

(2) If extrusion is overlapping the adhesive laminate, cut laminate along edge ofextrusion.

(3) Use a heat gun to warm up decorative laminates to weaken adhesive.

(4) Starting in one corner, peel decorative away from wall.

(5) When all decorative is removed, removed remains of adhesive with Rho-clenesolvent.

B. Cleaning of Wall prior to installing Decorative Material


Jan 30/200525-20-04 Page 6005

(1) Dampen a cloth with solvent, Rho-clene, and wipe surface clean.

(2) Use a clean dry cloth to dry the surface.

CAUTION: DO NOT ALLOW THE SOLVENT TO EVAPORATE TO DRYNESS.

(3) Repeat the above procedures, until there is no discoloration, on a clean, dry cloth. Donot touch the cleaned surfaces with bare hands.

C. Application of Filler Material (Refer to Table 6001)

(1) Clean small localized areas, such as voids and gaps per paragraph 6.B.

(2) Apply filler material and smooth.

(3) Allow filler to dry and sand flush with panel or desired.

D. Adhesive

(1) Selection and Application

(2) Selection of Adhesives - Depending on the covering material, either contract cementor Bonding film has to be chosen.

(a) Contact Cement should be used on hard, non-pliable covering materials .010"thick and heavier.

(b) Bonding Film 2.4 is to be used with coft pliable covering materials up to .010"thick, and or when tests indicate that out-gassing of the Contact Cement causesbubbles or discoloration of the covering material.

(3) Application of Contact Cement

(a) Clean surface to be bonded per paragraph 6.B.

(b) Apply a thin, even coat of adhesive with a spray gun, roller or brush to the surfaceto be covered and the back side of the Decorative Material.

(c) Avoid a heavy layer of Cement to prevent stringing and clumping. A thin coat ofCement is more effective that a thick layer.

(d) Allow adhesive to dry for 15-25 minutes.

25-20-04


Jan 30/2005

(e) Apply covering material per paragraph 6.E.

(4) Application of Bonding Film

(a) Clean surface per paragraph 6.B.

(b) Cut film with scissors, knife or any other sharp blade as follows:

1. Refer to Engineering Blueprint for exact panel dimensions.

2. Add 4" to height and width dim.

(5) Film Application Methods

(a) Direct Method - (Film smaller than 1 sq. ft.)

1. Remove the entire liner from the adhesive side of the film.

2. Align the film and press one edge to the surface with finger pressure.

3. With a plastic applicator, squeeze the remaining unapplied portion using firm,overlapping strokes.

(b) Scored Line Method (Film smaller than 4 sq. ft.)

1. Leave the liner on the film, expose 1"-2" area of adhesive and register the filmalong the registery line.

2. Press adhesive to the surface with finger pressure.

3. Squeeze the film into place with firm, overlapping strokes across the width ofthe film, while removing the remainder of the liner a few inches at a time toprevent pre-adhesion.

(c) Top Horizontal Hinge Method (Film larger than 4 sq. ft.)

1. Leave the liner on the film.

2. Tape the film into position with small pieces of masking tape. Apply 2"-3" tapeover the top edge to serve as a hinge.

3. Make a cut about half-way through the tape hinge at both ends.

Page 6006


Jan 30/200525-20-04

4. Raise the film up over the top hinge and peel the liner back a few inches ata time, while squeegeeing the surface with firm, overlapping strokes,beginning at the top center and working down and outward toward each edge.

5. Hold the film away from the surface with one hand and allow the adhesive totouch only as pressure is applied.

6. Resqueegee the edges.

(d) Center Hinge Method (Film Larger than 4 sq. ft.)

1. Leave the liner on the film.

2. Tape the film into position with small pieces of masking tape. Apply 1" or 2"tape hinge through the center of the film, either vetically or horizontally.

3. Fold half the film back over the hinge, peel the liner off of the film (back to thetape hinge), cut the liner along the hinge and discard.

4. Fold the film back down and squeegee the surface beginning at the centerfrom the page hinge, and work outward and away from the tape hinge usingfirm, overlapping strokes.

5. Hold away from the surface with one hand and allow the adhesive to touchonly as pressure is applied.

6. Remove the tape hinge.

7. Fold over half of the film, remove the liner and apply as above.

(e) If air bubbles are present after application of bonding film, puncture the film atone end with a sharp needle point tool. Press out entrapped air towardpuncture.

(f) Remove polyethylene release liner.

(g) Apply covering material per paragraph 6.E.

E. Application of Decorative Covering Material

(1) Align covering material, and press one edge to the film with plastic applicator.

(2) Squeegee the remaining unapplied portion using film, overlapping strokes.

Page 6007

25-20-04


Jan 30/2005

(3) See Figure 6001 - Trim and Finish for the appropriate location of decorativematerials used on this unit.

Page 6008

Table 6001Repair Materials

MATERIAL PART NUMBER MANUFACTURER REMARKS (DISTRIBUTOR)

2- Part Epoxy Crest 270A & 270B Crest Prod. Mix Ratio: 50 by 50Lord Corp. volume18203 Mt. Baldy Cir.Fountain Valley, CA 92708

Core, Honeycomb P/N 2 1/8 3.0 Advanced Honeycomb Driessen P/N:San Marcos, CA 3140036 thru 3140040

Facing, Sandwich L-525-7781 J.D. Lincoln Inc. Driessen P/N: Fiberglass, Costa Mesa, CA 3140061 Reinforced, Laminates SPH2296L-7781 Culver City Composites Driessen P/N: (Pre-preg 50" wide) CPH2265L-7781 Culver City, CA 3140080

Fiberglass Style 7781 J.D. Lincoln Inc. Fabric Costa Mesa, CA

Contact Cement N123 Monarch Industries Driessen P/N:Brand: Stabond 16631 Milliken Ave. 3150040

Irvine, CA 92606

Polyester Material Filter 77 (APF White) Akemi Plastics Filler Compound Eaton Rapids, MI

Tedlar Film TWH-20BE3 (White) E.I. Dupont Driessen P/N:TGH-15BL3 (Grey) Buffalo, New York 3160186, 3160182

Solvent Rho-clene 7688 RHO-CHEM Corp.Inglewood, CA

Degreaser/Cleaner Kleenol-30 Mission Kleensweep2434 Birk DaleLos Angeles, CA


Jan 30/200525-20-04

ASSEMBLY

1. General

The unit is an integrally bonded structure which is fabricated from sandwich panels andaluminum extrusions. During assembly, it is recommended that low cost items, such ascotter pins, screws, washers, nuts, grommets, etc., be replaced when possible to preventfuture maintenance requirements due to failure of such items. It is essential whenreplacing components, that they be identical to the items being replaced. If componentsubstitutions are being considered, Driessen Aircraft Interiors Systems Incorporated mustbe notified.

Prior to assembling Closet, inspect all parts for wear and/or damage which could resultin failure of the Closet or any of its component assemblies. Mechanically fastened,individual component parts, not bonded to the structure should be assembled by qualifiedpersonnel using standard shop practices.

WARNING: PRIOR TO STARTING ANY ELECTRICAL INSTALLATION, CONNECTIONAND/OR ASSEMBLY, ENSURE THAT ALL POWER TO AIRCRAFTELECTRICAL INTERFACES HAVE BEEN SHUT OFF.

CAUTION: YOU MUST GROUND YOURSELF BEFORE YOU WORK ON THEELECTRICAL PARTS OF THE UNIT. THIS IS BECAUSE MANY OF THEELECTRICAL PARTS ARE SENSITIVE TO STATIC ELECTRICITY.

NOTE: After assembly, make sure that all CLEANING, CHECK AND REPAIRprocedures found in their respective sections for all component parts andsubsystems are completed.

2. Assembly

NOTE: CAREFULLY INSPECT ALL RIVETED, SPOT WELDED, OR BONDEDASSEMBLIES AND COMPONENTS PRIOR TO INSTALLATION/ASSEMBLY.DO NOT REMOVE THESE ITEMS UNLESS REQUIRED DUE TO DAMAGEOR OTHER NEED FOR REPLACEMENT. IF REPLACEMENT IS REQUIRED,REFER TO THE APPLICABLE PORTIONS OF "REPAIR" FOR DETAILEDINSTRUCTIONS.

CAUTION: EXERCISE EXTREME CARE WHEN REMOVING SCREWS OR BOLTSTHAT ATTACH A PART TO THE SYNTHETIC PANELING. THREADEDINSERTS, WHICH ARE INSTALLED IN THE PANELING TO RECEIVE

Page 7001


25-20-04 Jan 30/2005

SCREWS OR BOLTS, ARE INSTALLED IN PANELING WITH POTTINGCOMPOUND. UNNECESSARY DAMAGE TO THESE INSERTS WILLREQUIRE REPLACEMENT WITH LARGER INSERTS.

NOTE: Assembly sequence is straight forward and self explanatory.

(a) Refer to IPL Figure 1 ( Final Assembly) to assemble.

(b) Refer to IPL Figure 2 (Door Assembly, P/N 127041-11) to assemble.

(c) Refer to IPL Figure 3 (Door Assembly, P/N 128041-11) to assemble.

(d) Refer to IPL Figure 4 (Door Assembly, P/N 129041-11/-21) to assemble.

(e) Refer to IPL Figure 5 (Door Assembly, 126041-11) to assemble.

Page 7002

Jan 30/200525-20-04


FITS AND CLEARANCES

1. General

The torque values (Refer to Table 8001) used in accordance with Driessen StandardProcess Specification ( SPS 128).

Page 8001

Table 8001Torque Values

A. How to Use the Fits and Clearances Table

NOTE: Repair or replace the parts which are not within the limits given (refer to) DISASSEMBLY, REPAIR and ASSEMBLY.

(1) These torque values apply to nut tightening only. These values are also applicable toself-locking bolts. When tightening is to be done by rotating the bolt, the high limit of±10% shall be used. Bolts installed in interference fit may not be rotated to tighten nut.

BOLT AND STEEL, CORROSION RESISTANT STEEL TITANIUM (3) (5)NUTMATERIAL

NUT STYLE FOR55,000

PSIMIN.

SCREWS

SELF LOCKING, CASTELLATED, ANDPLATE NUTS (4)

SELF LOCKING, EXTERNALWRENCHING (4)

NUT TYPENUTEXAMPLESBOLTSTRENGTH

AN310,LH7559,NAS679 AN320, NAS1022 MS21042 H2O, H96

125,000 PSI 125,000 PSI 160,000 PSI 120,000 PSI MINIMUM MINIMUM MINIMUM MINIMUM

TORQUE RANGETHREAD SIZE IN. - LB IN. - LB IN. -LB IN. - LB IN. - LB IN. - LB IN. - LB IN. - LB

(1) (2) (1) (2) (1) (2) (1)2-56 OR 2-64 2-3 3.5-4.5 -- 3.5-4.5 -- -- -- --4-40 OR 4-48 5-6 6.8 -- 6.8 -- -- -- --6-32 OR 6-40 9-12 12-15 -- 12-15 -- -- -- --8-32 OR 8-36 12-15 15-17 20 15-17 20 -- -- --10/32 20-25 40 18-20 25 30-35 -- --1/4-28 50-70 100 30-40 60 65-90 100 90-1255/16-24 100-140 225 60-85 140 130-180 200 180-2503/8-24 160-190 390 95-110 240 220-360 410 300-5007/16-20 450-500 840 270-300 500 370-610 690 510-8401/2-20 480-690 1100 290-410 660 630-950 1070 870-13009/16-18 800-1000 1600 480-600 960 1000-1300 1470 1300-15005/8-16 1100-1300 2400 660-780 1400 1400-1700 1900 1900-22003/4-16 2300-2500 5000 1300-1500 3000 2400-3100 3500 3300-43007/8-14 2500-3000 7000 1500-1800 4200 3700-4900 5500 5100-67001-12 OR 1-14 3700-5500 10,000 2200-3300 6000 5100-7900 8900 7000-10,9001-1/8-12 5000-7000 15,000 3000-4200 9000 6900-9500 10,700 9500-13,0001-1/4-12 9000-11,000 25,000 5400-6600 15,000 11,500-14,000 15,750 18,800-19,2001-3/8-12 7000-9000 20,000-24,0001-1/2-12 10,000-12,000

TENSION SHEER TENSION TENSION

25-20-04 Jan 30/2005


Page 8002

(2) Maximum torque allowed for alignment of castellated nut and hole for cotter pin orother safely devise insertion.

(3) Unlubricated except as required by drawing callout or the standard drawing page.

(4) Unless specified on the drawing, or other columns of this table, use these torqueranges for listed nuts, and plate nuts, bolts, and other bolt-nut combinations for equalor greater tensile strength. See applicable standard drawings and procurementspecifications for strength and dimensional information.

(5) These torque values are applicable for installing nuts and bolts plated in accordancewith QQ-P-416. Type I or Type II.


Jan 30/200525-20-04

ILLUSTRATED PARTS LIST

1. General

This section contains an illustrated parts list, definitions for the column headings of theillustrated parts list, vendor codes / addresses, numerical index, assembly and detailillustrations.

2. Illustrated Parts List

The illustrated parts list consists of an itemized breakdown of parts used on the Closet whichare illustrated as necessary to provide for their identification. The column headings of theparts list are defined as follows:

A. "Fig. / Item" (Figure / Item) Column

The number listed under "Fig." is the figure number of the assembly illustration used toillustrate the listed parts. The numbers listed under "Item" are the item numbersidentifying the parts used on the assembly and detail illustrations. Where a part is notillustrated, the item number of that part will be preceded with a dash (-). Where itemnumber variants are listed in the "Fig. / Item" column, it will be preceded by a dash (-).

B. "Part Number" Column

The number listed under "Part Number" is the same as the manufacturer's drawingnumber for that part or the same as the number listed in the manufacturer's assemblydrawing "List of Materials" or the same as the number listed in the manufacturer partscatalog.

C. "Airline Part No." Column

This column is left open, and is to be used by the customer for their own parts numberingsystem.

D. "Nomenclature" Column

The part name listed under "Nomenclature" is the same as the manufacturer's drawingtitle for that part or the same as the part name listed in the manufacturer's assemblydrawing "list of materials" or the same as the part name listed in the manufacturer's partscatalog with any necessary and qualifying descriptions. Nomenclatures are intended toshow the relationship of a part with its assembly. When a nomenclature is followed bythe words "Buy P/N...", that part is no longer procurable. When applicable, a vendor'scode number is listed after the part name. See Vendor's Code / Address on page

Page 10001

25-20-04


Jan 30/2005

10003.

E. "Eff. Code" (Effectivity Code) Column

When two or more main assembly variations are listed, a different "usable on" code letteris assigned to each main assembly and is listed in the "EFF CODE" column. All parts tobe used on a specific assembly are identified by the same code letter as the appropriatemain assembly. This column is left blank for all parts that are common to all mainassemblies.

F. "Units Per Assy" (Units Per Assembly) Column

The quantities listed under "Units Per Assy" are the number of units required per nexthigher assembly. For a bulk number of units, the letters "A/R" are entered to indicate"as required". The letters "REF" are entered to indicate that the unit is listed forreference purposes only.

Identical items are listed separately to indicate their order of disassembly, the quantitiesof identical items within a main assembly must be added to obtain a total quantity permain assembly. The quantities listed for attaching parts are to attach one of the partsthey are attaching. Attaching parts will be listed in the parts list after the item they attach.The quantity listed will be per next higher assembly. Attaching parts will not be illustratedwhere their sequence of installation is obvious.

G. Vendor Codes and Addresses

A part not manufactured by Driessen is assigned a code number which is preceded withthe letter "V", and placed in parentheses following the nomenclature of the part. Thecodes used are defined by the U.S. Federal Supply Code for Manufacturers DocumentH4/H8. The Vendor parts to be used in this manual will list their vendor codes andaddresses in the table on page 10003.

H. Numerical Index

The purpose of the Numerical Index is to enable the user to locate any part by partnumber. The figure and item number the part is used in are listed as well as the totalquantity required in that particular figure. Parts are listed in numerical order starting onpage 10005.

Page 10002


Jan 30/200525-20-04 Page 10003

VENDOR LISTING CODE ADDRESS CODE ADDRESS

VC5307 INNOVINT AIRCRAFT INTERIOREINRICHTUNGS GMBHHOLZMUEHLENSTR, 84-86D22041 HAMBURG - GERMANY

VOUEP1 RYAN HERCO16424 ISHIDA AVEGARDENA, CA 90248

V03296 NMC FASTENING SYSTEMSDIVISION OF NYLON MOLDING1617 S. CALIFORNIA AVE.MONROVIA, CA 91016-4621

V06090 RAYCHEM CORP.300 CONSTITUTION DR.MENLO PARK, CA 94025-1111

V08733 CAMLOC FASTENER CORP.LOS ANGELES, CA

V08756 EVERPURE INC.660 N. BLACKHAWK DR.WESTMONT, IL 60559-1116

V12623 WHITEY CO.318 BISHOP RD.HIGHLANDS HEIGHTS, OH 44143

V17023 BRUCE INDUSTRIES INC.101 EVANS AVE.DAYTON, NV 89403

V2V320 FLAME ENTERPRISES, INC.20945 OSBORNE ST.CANOGA PARK, CA 91304-1847

V25281 OETIKER INC.71-77 OKNER PKWYLIVINGSTON, NJ 07039

V26405 MARATHON SPECIAL PROD.13300 VAN CAMP RD.BOWLING GREEN , OH 43402

V27045 SABRE INDUSTRIES INC.120 W. PROVIDENCIA AVE.BURBANK, CA 91502

V27998 GEOMETRICAL STRUCTURES26670 CAWSTON AVE.HEMET, CA 92343

V28107 SYLVANIA ELECTRIC PRODS.SEMICONDUCTOR DIV.HILLSBORO, NH 03244

V3A054 MC MASTER-CARR9630 NORWALK BLVD.SANTA FE SPRINGS, CA 90670

V3D883 AIR COLD SUPPLY141 W. 23RD ST.LOS ANGELES, CA 90007

V31845 SEALTH AEROMARINE16001 MILLCREEK BLVD., SEMILLCREEK, WA 98012

V34742 TYEE AIRCRAFT INC.3008 100TH ST. SWEVERETT, WA 98204

V34941 HARPER ENGINEERING CO.200 S. TOBIN ST.RENTON, WA 98055

V5N982 BURBANK AIRCRAFT SUPPLY10671 LANARK ST.SUN VALLEY, CA 91352-4033

V51941 SKYLOCK INDUSTRIES, INC.904 S. ALTA VISTA AVE.MONROVIA, CA 91016-3318

V52607 ACTRON MFG INC.1841 RAILROAD ST.CORONA, CA 91720

25-20-04


Jan 30/2005Page 10004

VENDOR LISTING CODE ADDRESS CODE ADDRESS

V56501 THOMAS & BETTS1001 FRONTIER RD.BRIDGEWATER, NJ 08807

V56958 YOUNG ENGINEERS INC.P.O. BOX 278LAKE FORREST, CA 92630-0278

V57177 PROMPTUS ELECTRONIC520 HOMESTEAD AVE.MOUNT VERNON, NY 10550

V62701 ZEVCO INC.22982 ALCALDE DR.,SUITE 101P.O. BOX 3615LAGUNA HILLS, CA 92654

V63794 COONER MFG. CO.9186 INDEPENDENCE AVE.CHATSWORTH, CA 91311

V71468 ITT CANON DIV.666 E. DYER RD.SANTA ANA, CA 92702

V71771 CORY COMPONENTS INC.350 HAMPTON DR.VENICE, CA 90291

V72619 DIALIGHT CORP.203 HARRISON PL.BROOKLYN, NY 11237

V76188 CONTROL DESIGN SUPPLY1168 KNOLLWOOD CIR.ANAHEIM, CA 92801

V76374 MECHANICAL PRODUCTS1824 RIVER ST.P.O. BOX 729JACKSON, MI 49204

V8F937 SYLVANIA MINIATURELIGHTING PROD.W. MAIN ST.HILLSBORO, NH 03244

V8Z509 CALIFORNIA FILTRATION PROD.14480 HOOVER ST.WESTMINSTER, CA 92683

V82255 DAY RAY PRODUCTS1133 MISSION ST.SO. PASADENA, CA 91030-3211

V84830 LEE SPRINGS CO.1462 62ND ST.BROOKLYN, NY 11219

V89488 BOBRICK WASHROOM EQUIP.11611 HART ST.N. HOLLYWOOD, CA 91605-5802

V4001 AEROWORKS2727 S. CRODDY WAYSUITE DSANTA ANA, CA. 92704


Jan 30/200525-20-04

PART AIRLINE FIGURE ITEM TOTAL NUMBER STOCK NUMBER REQ

NUMERICAL INDEX

Page 10005-1

AN960-10L 1 -35 A/RAN960-516 1 315 A/RAN960-8 1 -345 A/RAN960-8L 1 130 2AN960D10L 1 -450 2BAC27NPA0274 1 525 1CTB-4ID 1 -180 3MS20253P2-0698 2 20 1MS20253P2-1510 3 20 1

4 20 1MS20253P2-4330 5 10 3MS21042-L5 1 325 2MS25281-8 1 120 2MS35206-243 1 -340 A/RMS35206-248 1 125 2MS35207-261 1 -30 A/RMS35207-262 1 -480 8MS35207-263 1 -60 2MS35207-267 1 -75 2NAS1801-3-16 1 -445 2NAS42DD-3-32 1 135 2NAS43DD5-48 1 -80 2NAS514P632-8 5 -35 A/RNAS514P832-5 2 15 A/RNAS514P832-6 1 -190 A/RNAS514P832-8 1 -300 A/RNAS6605-14 1 550 4S417N503-10 1 140 1S417N503-15 1 -140A 1SJ3526-1 1 535 5SJ3527-1 1 530 5101041-1 1 -1 REF101041-101 1 -1A 1101041-11 1 -540 1101041-201 1 -1B 1102041-11 1 -5 1102041-111 1 -5A 1103041-11 1 40 1103041-19 1 25 2103041-23 1 70 2


25-20-04 Jan 30/2005


NUMERICAL INDEX

Page 10005-2

103041-3 1 55 2107041-11 1 -115 1107041-3 1 150 1126041-11 1 265 1

5 -1 REF126041-17 5 45 1126041-19 5 55 1

5 135 1126041-21 5 -20 1126041-25 5 190 2126041-27 5 40 1

5 120 1126041-29 5 125 1126041-3 5 175 1126041-31 5 -100 1126041-33 5 5 1126041-35 5 15 2126041-41 5 -185 1126041-47 5 70 2

5 150 2126041-5 5 95 1126041-7 5 80 5

5 160 6126041-9 5 50 1

5 130 1127041-11 1 185 1

2 -1 REF127041-13 2 30 1127041-15 2 40 1127041-17 2 25 1127041-3 2 75 1127041-5 2 45 1127041-7 2 50 1127041-9 2 35 1128041-11 1 205 1

3 -1 REF128041-13 3 30 1128041-15 3 40 1128041-17 3 25 1128041-3 3 75 1


Jan 30/200525-20-04


NUMERICAL INDEX

Page 10005-3

128041-5 3 45 1128041-7 3 50 1128041-9 3 35 1129041-11 1 225 1

4 -1 REF129041-13 4 25 1129041-21 1 245 1

4 -1A REF129041-23 4 -70A 1129041-3 4 70 1129041-5 4 40 1129041-6 4 45 1129041-7 4 35 1129041-9 4 30 1130041-11 4 60 1131041-11 1 335 2132041-11 1 410 1132041-21 1 425 1132041-3 1 365 1132041-5 1 380 1132041-7 1 395 1133041-11 1 350 1134041-11 1 465 11371004-B507 1 -490A 115501-11 1 145 1200024-11 1 285 1200024-3 1 -295 1202009-11 1 545 4210002-3 2 55 3

3 55 34 50 4

210002-5 5 60 45 140 4

210003-135 2 65 23 65 2

210009-3 2 10 13 10 14 10 2

215015-3 2 5 13 5 1


25-20-04 Jan 30/2005Page 10005-4


NUMERICAL INDEX

215015-3 4 5 2215024-3 5 25 1

5 105 1216002-5 1 310 2216005-3 1 330 2216018-3 1 -290 1220006-11 1 510 1220006-21 1 490 1221003-11-3712 1 475 1228001-3 1 10 6228003-7 1 15 2228003-9 1 20 2236001-3 1 85 1236020-14-6 1 105 1236020-40-18 1 110 1236020-5-2 1 100 1236039-120-54 1 90 1236040-100-45 1 95 1248003-19 1 -305 2248003-5 1 -200 A/R248-136-16005-02 1 -170 1251007-3 5 195 6251011-3 1 320 23M4945 5 180 148-1825-02 1 -160 148-7190 1 -175 148-7191 1 -165 148-719-1 1 -155 26400 1 -195 A/R65-5458-12 1 440 165-5458-13 1 -460 265-5458-20B 1 -440A 165-5458-21B 1 -460A 266-4302-1 1 -455 2


FIG.ITEM PART NUMBER

AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE

-

IND
1 -1 101041-1 1 FINAL ASSY, FWD LEFT CLOSET A REF -1A 101041-101 1 FINAL ASSY, FWD LEFT CLOSET B 1 -1B 101041-201 1 FINAL ASSY, FWD LEFT CLOSET C 1 -5 102041-11 2 STRUCTURE ASSY A,B 1
-5A 102041-111 2 STRUCTURE ASSY C 1
10 228001-3 3 STRIKER 6 15 228003-7 3 STRIKER 2 20 228003-9 3 STRIKER 2 25 103041-19 3 BRACKET 2
ATTACHING PARTS
-30 MS35207-261 3 SCREW, PAN HD, # 10-32 X .375 LG 6 -35 AN960-10L 3 WASHER 6
***
40 103041-11 3 BRACKET, COAT ROD 1
ATTACHING PARTS
***
55 103041-3 3 BLOCK, REINFORCE 2
ATTACHING PARTS
***
70 103041-23 3 SPACER, BLOCK 2
ATTACHING PARTS
-75 MS35207-267 3 SCREW, PAN HD, # 10-32 X 1.00 LG 2 -80 NAS43DD5-48 3 SPACER 2
***
85 236001-3 2 PLACARD, ID 1 90 236039-120-54 2 PLACARD, COAT ROD LOAD 1 95 236040-100-45 2 PLACARD, FLOOR LOAD LIMT 1 100 236020-5-2 2 PLACARD, MAX STOW WEIGHT 1 105 236020-14-6 2 PLACARD, MAX STOW WEIGHT 1 110 236020-40-18 2 PLACARD, MAX STOW WEIGHT 1 -115 107041-11 2 ELECTRICAL INSTL 1 120 MS25281-8 3 CLAMP 2
ATTACHING PARTS
125 MS35206-248 3 SCREW, PAN HD, # 8-32 X .88 LG 2 130 AN960-8L 3 WASHER 2 135 NAS42DD-3-32 3 SPACER 2
***
140 S417N503-10 3 SIGN, NSFSB A 1
Jan 30/200525-20-04 Page 10006-3

ITEM NOT ILLUSTRATED



AIRLINEPART NO.

UNITSPER

ASSY

EFFCODE

NOMENCLATUREIND

1 (BOEING FURNISHED, DRIESSENINSTALLED)(S/N 001-015)

-140A S417N503-15 3 SIGN, NSFSB B,C 1
(BOEING FURNISHED, DRIESSENINSTALLED)(S/N 016 AND SUB)
145 15501-11 3 COVER, NSFSB 1
150 107041-3 3 TUBE 1 -155 48-719-1 3 RECEPTACLE, LOCKING 2
-

-160 48-1825-02 3 PIN, CONTACT 1
-165 48-7191 3 RECEPTACLE, LOCKING 1 -170 248-136-16005-02 3 SOCKET, CONTACT 1 -175 48-7190 3 RECEPTACLE, LOCKING 1 -180 CTB-4ID 3 TIES, MARKER 3 185 127041-11 2 DOOR ASSY, MISC STOWAGE 1
(SEE IPL FIG. 2 FOR BREAKDOWN) ATTACHING PARTS

-190 NAS514P832-6 2 SCREW, FLAT HD, # 8-32 X .38 LG 3
-195 6400 2 WASHER 3 -200 248003-5 2 NUT, BLIND 3
***
205 128041-11 2 DOOR ASSY, BREATHING COMPT 1

-215 6400 2 WASHER 5 -220 248003-5 2 NUT, BLIND 5
***
225 129041-11 2 DOOR ASSY, EMERGENCY EQUIP 1

-235 6400 2 WASHER 4 -240 248003-5 2 NUT, BLIND 4
***
245 129041-21 DOOR ASSY, EMERGENCY EQUIP 1

-255 6400 2 WASHER 4 -260 248003-5 2 NUT, BLIND 4
25-20-04 Jan 30/2005Page 10006-4




AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE

-

IND

1 ***
265 126041-11 2 DOOR ASSY, TRI-FOLD 1

-275 6400 2 WASHER 10 -280 248003-5 2 NUT, BLIND 10
***
285 200024-11 2 HOLDER INSTL, DOOR 1 -290 216018-3 3 HOLDER, DOOR 1 -295 200024-3 3 PLATE 1
ATTACHING PARTS
-300 NAS514P832-8 3 SCREW, FLAT HD, # 8-32 X 1/2 LG 2 -305 248003-19 3 NUT, BLIND 2
***
310 216002-5 2 RETAINER, 1/4 TURN 2
-310A A35583-7 2 RETAINER, 1/4 TURN (V52607) REF
(OPTIONAL P/N FOR 216002-5) ATTACHING PARTS
315 AN960-516 2 WASHER 2
320 251011-3 2 SPACER, RETAINER 2 325 MS21042-L5 2 NUT 2
***
330 216005-3 2 RETAINER, 1/4 TURN 2
-330A A35579-1R 2 RETAINER, 1/4 TURN (V52607) REF
(OPTIONAL P/N FOR 216005-3)
335 131041-11 2 BUMPER ASSY 2
ATTACHING PARTS
-340 MS35206-243 2 SCREW, PAN HD, # 8-32 X .38 LG 6
-345 AN960-8 2 WASHER 6
***
350 133041-11 2 BUMPER ASSY 1
ATTACHING PARTS
-355 MS35206-243 2 SCREW, PAN HD, # 8-32 X .38 LG 8 -360 AN960-8 2 WASHER 8
***
365 132041-3 2 KICKSTRIP A,B 1
ATTACHING PARTS
-370 NAS514P832-6 2 SCREW, FLAT HD, # 8-32 X .38 LG A,B 8 -375 AN960-8 2 WASHER A,B 8
***
380 132041-5 2 KICKSTRIP A,B 1
Jan 30/200525-20-04 Page 10006-5




AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATUREIND

1 ATTACHING PARTS
-385 NAS514P832-6 2 SCREW, FLAT HD, # 8-32 X .38 LG A,B 8
-

-390 AN960-8 2 WASHER A,B 8
***
395 132041-7 2 KICKSTRIP A,B 1
ATTACHING PARTS
-400 NAS514P832-6 2 SCREW, FLAT HD, # 8-32 X .38 LG A,B 4
-405 AN960-8 2 WASHER A,B 4
***
410 132041-11 2 KICKSTRIP ASSY A,B 1
ATTACHING PARTS
***
425 132041-21 2 KICKSTRIP ASSY A,B 1
ATTACHING PARTS
***
440 65-5458-12 2 HANDLE, ASSIST A 1
(BOEING FURNISHED, DRIESSENINSTALLED)
(S/N 001-015)
-440A 65-5458-20B 2 HANDLE, ASSIST B,C 1
(BOEING FURNISHED, DRIESSENINSTALLED)(S/N 016 AND SUB) ATTACHING PARTS
-445 NAS1801-3-16 2 BOLT 2
-450 AN960D10L 2 WASHER 2 -455 66-4302-1 2 COLLAR 2

-460 65-5458-13 2 NUT A 2
(BOEING FURNISHED, DRIESSENINSTALLED) (S/N 001-015)
-460A 65-5458-21B 2 NUT B,C 2

25-20-04 Jan 30/2005Page 10006-6


(BOEING FURNISHED, DRIESSENINSTALLED)(S/N 016 AND SUB) ***



AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATUREIND

1 465 134041-11 2 BUMPER ASSY, JOINT-LINE A 1
ATTACHING PARTS
-470 NAS514P832-6 2 SCREW, FLAT HD, # 8-32 X .38 LG A 10
***
475 221003-11-3712 2 ROD, COAT 1
ATTACHING PARTS
-480 MS35207-262 2 SCREW, PAN HD, # 10-32 X .44 LG 8
-485 AN960-10L 2 WASHER 8
***
490 220006-21 2 POCKET ASSY A,B 1
-490A 1371004-B507 2 POCKET, LITERATURE C 1

-

ATTACHING PARTS-495 MS35206-243 2 SCREW, PAN HD, # 8-32 X .38 LG C 4
-500 NAS514P832-6 2 SCREW, FLAT HD, # 8-32 X .38 LG A,B 4 -505 AN960-8 2 WASHER C 4
***
510 220006-11 2 PANEL A,B 1
ATTACHING PARTS
-515 MS35206-243 2 SCREW, PAN HD, # 8-32 X .38 LG A,B 4 -520 AN960-8 2 WASHER A,B 4
***
525 BAC27NPA0274 2 MARKER, ALUM FOIL 1

530 SJ3527-1 2 LOOP, BACKING B 5
535 SJ3526-1 2 HOOK B 5 -540 101041-11 2 KIT, LOOSE ITEM (K1) 1 545 202009-11 3 SEAT TRACK, FITTING ASSY 4 550 NAS6605-14 3 BOLT, # 5/16 X 1.344 LG 4
(FITTING ASSY ATTACHINGHARDWARE)

555 AN960-516 3 WASHER 4

Jan 30/200525-20-04 Page 10006-7


(FITTING ASSY ATTACHINGHARDWARE)


25-20-04 Jan 30/2005Page 10006-8




AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE

-

IND
2 -1 127041-11 1 DOOR ASSY, MISC STOW COMPT REF (SEE IPL FIG. 1 FOR NHA)
5 215015-3 2 LATCH 1
10 210009-3 2 PLATE, BACKING 1
ATTACHING PARTS
15 NAS514P832-5 2 SCREW, FLAT HD, # 8-32 X 5/16 LG 2
***
20 MS20253P2-0698 2 PIN, HINGE 1 25 127041-17 2 HINGE, HALF 1
(M/F 219002)
30 127041-13 2 EXTRUSION, HINGE SIDE 1
(M/F 219006)
35 127041-9 2 EXTRUSION, LATCH SIDE 1
(M/F 3090012)
40 127041-15 2 EXTRUSION, EDGE DOOR 1
(M/F 3090012)
(M/F 3090012)
(M/F 3090012)
55 210002-3 2 BRACKET, CORNER 3
ATTACHING PARTS
***
65 210003-135 2 BRACKET, CORNER 2
ATTACHING PARTS
***
75 127041-3 2 PANEL 1
Jan 30/200525-20-04 Page 10016-3



25-20-04 Jan 30/2005Page 10016-4




AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATUREIND
3 -1 128041-11 1 DOOR ASSY, FWD CLOSET REF (SEE IPL FIG. 1 FOR NHA)
5 215015-3 2 LATCH 1
-

ATTACHING PARTS
***
20 MS20253P2-1510 2 PIN, HINGE 1 25 128041-17 2 HINGE, HALF 1
(M/F 219002)
30 128041-13 2 EXTRUSION, HINGE SIDE 1
(M/F 219006)
(M/F 3090012)
(M/F 3090012)
(M/F 3090012)
(M/F 3090012)
ATTACHING PARTS
***
65 210003-135 2 BRACKET, CORNER 2
ATTACHING PARTS
***
75 128041-3 2 PANEL 1
Jan 30/200525-20-04 Page 10017-3



25-20-04 Jan 30/2005Page 10017-4




AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATUREIND
4 -1 129041-11 1 DOOR ASSY, FWD CLOSET A REF
-

(SEE IPL FIG. 1 FOR NHA)
-1A 129041-21 1 DOOR ASSY, FWD CLOSET B REF
5 215015-3 2 LATCH 2
ATTACHING PARTS
***
20 MS20253P2-1510 2 PIN, HINGE 1
25 129041-13 2 HINGE, HALF 1
(M/F 219002)
(M/F 219006)
(M/F 3090084)
(M/F 3090012)
(M/F 3090012)
ATTACHING PARTS
***
60 130041-11 2 BRACKET, O2 BOTTLE A 1
ATTACHING PARTS
-65 MS35207-261 2 SCREW, PAN HD, # 10-32 X .38 LG A 4
***
70 129041-3 2 PANEL A 1
-70A 129041-23 2 PANEL B 1

Jan 30/200525-20-04 Page 10018-3



25-20-04 Jan 30/2005Page 10018-4




AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATUREIND

5 -1 126041-11 1 DOOR ASSY, FWD LEFT CLOSET REF

-

5 126041-33 2 HINGE, HALF 1
(M/F 219002)
10 MS20253P2-4330 2 PIN, HINGE 3 15 126041-35 2 SPACER 2 -20 126041-21 2 DOOR ASSY 1 25 215024-3 3 BOLTING SYSTEM ASSY 1
ATTACHING PARTS
-30 NAS514P832-5 3 SCREW, FLAT HD, # 8-32 X 5/16 LG 4 -35 NAS514P632-8 3 SCREW, FLAT HD, # 6-32 3
***
40 126041-27 3 EXTRUSION 1
(M/F 219007)
45 126041-17 3 EXTRUSION 1
(M/F 3090009)
50 126041-9 3 EXTRUSION 1
(M/F 3090009)
55 126041-19 3 EXTRUSION 1
(M/F 3090009)
ATTACHING PARTS
***
70 126041-47 3 PLATE, GUIDE 2
ATTACHING PARTS
***
80 126041-7 3 CHANNEL, “U” 5
ATTACHING PARTS
-85 NAS514P832-8 3 SCREW, FLAT HD, # 8-32 5 -90 248003-5 3 NUT, BLIND 5
***
95 126041-5 3 PANEL 1
-100 126041-31 2 DOOR ASSY 1
105 215024-3 3 BOLTING SYSTEM ASSY 1
ATTACHING PARTS
-110 NAS514P832-5 3 SCREW, FLAT HD, # 8-32 X 5/16 LG 4 -115 NAS514P632-8 3 SCREW, FLAT HD, # 6-32 3
Jan 30/200525-20-04 Page 10019-3




AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE

-

IND

5 ***
120 126041-27 3 EXTRUSION 1
(M/F 219007)125 126041-29 3 EXTRUSION 1

(M/F 219007)
130 126041-9 3 EXTRUSION 1
(M/F 3090009)
135 126041-19 3 EXTRUSION 1
(M/F 3090009)
ATTACHING PARTS
***
150 126041-47 3 PLATE, GUIDE 2
ATTACHING PARTS
***
160 126041-7 3 CHANNEL, “U” 6
ATTACHING PARTS
-165 NAS514P832-8 3 SCREW, FLAT HD, # 8-32 6 -170 248003-5 3 NUT, BLIND 6
***
175 126041-3 3 PANEL 1 180 3M4945 3 TAPE, DOUBLE FACED 1 -185 126041-41 2 DOOR ASSY 1 190 126041-25 3 EXTRUSION 2
(M/F 219007)
195 251007-3 3 SPACER 6
25-20-04 Jan 30/2005Page 10019-4



Jan 30/200525-20-04

1. General

The Closet is an integrally-bonded structure which is fabricated from sandwich panelsand aluminum extrusions. The unit cannot be diassembled without affecting its structureintegrity. As the paneling used to construct the unit is extremely strong and durable,disassembly instructions found herein are limited to removal of the Closet from theaircraft and removal of high-wear, easily damaged components of disassembly needed toaccess those items requiring repair and/or replacement. Individual panel repairs may beaccomplished using the repair procedures outlined in the REPAIR section, starting on page6001.

The Closet should be disassembled only to the degree necessary to replace parts, carry outrepairs and/or overhaul the unit. Complete disassembly is neither anticipated norrecommended.

Refer to FITS AND CLEARANCES section on page 8001 for applicable torque value.

2. Removal

CAUTION: MANY OF THE ELECTRICAL PARTS ON THE UNIT ARE SENSITIVE TOSTATIC ELECTRICITY. PERSONNEL MUST GROUND THEMSELVESBEFORE WORKING ON THESE PARTS.

WARNING: PRIOR TO STARTING ANY ELECTRICAL DISMANTLING, DISCONNECTIONAND/OR DISASSEMBLY, ENSURE THAT ALL POWER TO DISPLAY UNITASSEMBLY HAS BEEN REMOVED.

A. Closet Structure Disassembly

NOTE: CAREFULLY INSPECT ALL RIVETED SPOT WELDED, OR BONDEDASSEMBLIES AND COMPONENTS PRIOR TO DISASSEMBLY ORREMOVAL. DO NOT REMOVE THESE ITEMS UNLESS REQUIRED,DAMAGED OR NEED REPLACEMENT. IF REPLACEMENT ISREQUIRED, REFER TO SECTION 6001 OF THIS MANUAL FORDETAILED INSTRUCTIONS.

Page 12001

REMOVAL


25-20-04 Jan 30/2005

CAUTION: EXERCISE EXTREME CARE WHEN REMOVING SCREWS ORBOLTS ATTACHING A PART TO THE SYNTHETIC PANELING.THREADED INSERTS, WHICH ARE INSTALLED IN THE PANELINGTORECEIVE SCREWS OR BOLTS, ARE INSTALLED IN PANELINGWITH POTTING COMPOUND. UNNECESSARY DAMAGE TOINSERTS WILL REQUIRE REPLACEMENT WITH LARGER INSERTS.

Page 12002


Jan 30/200525-20-04

1. General

The unit is an integrally bonded structure which is fabricated from sandwich panels andaluminum extrusions. During assembly, it is recommended that low cost items, such ascotter pins, screws, washers, nuts, grommets, etc., be replaced when possible to preventfuture maintenance requirements due to failure of such items. It is essential whenreplacing components, that they be identical to the items being replaced. If componentsubstitutions are being considered, Driessen Aircraft Interiors Systems Incorporated mustbe notified.

Prior to assembling Closet, inspect all parts for wear and/or damage which could resultin failure of the unit or any of its component assemblies. Mechanically fastened, individualcomponent parts, not bonded to the structure should be assembled by qualified personnelusing standard shop practices.

WARNING: PRIOR TO STARTING ANY ELECTRICAL INSTALLATION, CONNECTIONAND/OR ASSEMBLY, ENSURE THAT ALL POWER TO AIRCRAFTELECTRICAL INTERFACES HAVE BEEN SHUT OFF.

CAUTION: YOU MUST GROUND YOURSELF BEFORE YOU WORK ON THEELECTRICAL PARTS OF THE UNIT. THIS IS BECAUSE MANY OF THEELECTRICAL PARTS ARE SENSITIVE TO STATIC ELECTRICITY.

NOTE: After assembly, make sure that all CLEANING, CHECK AND REPAIRprocedures found in their respective sections for all component parts andsubsystems are completed.

2. Installation

A. Closet Installation

NOTE: CAREFULLY INSPECT ALL RIVETED, SPOT WELDED, OR BONDEDASSEMBLIES AND COMPONENTS PRIOR TO INSTALLATION/ASSEMBLY.DO NOT REMOVE THESE ITEMS UNLESS REQUIRED DUE TO DAMAGEOR OTHER NEED FOR REPLACEMENT. IF REPLACEMENT IS REQUIRED,REFER TO THE APPLICABLE PORTIONS OF "REPAIR" FOR DETAILEDINSTRUCTIONS.

Page 13001

INSTALLATION


25-20-04 Jan 30/2005

CAUTION: EXERCISE EXTREME CARE WHEN REMOVING SCREWS OR BOLTSTHAT ATTACH A PART TO THE SYNTHETIC PANELING. THREADEDINSERTS, WHICH ARE INSTALLED IN THE PANELING TO RECEIVESCREWS OR BOLTS, ARE INSTALLED IN PANELING WITH POTTINGCOMPOUND. UNNECESSARY DAMAGE TO THESE INSERTS WILLREQUIRE REPLACEMENT WITH LARGER INSERTS.

Page 13002

(1) Position the Closet in between the following coordinates:

STA=378.00 mm (9601.2 in), STA=404.00 mm (10261.6 in)LBL=19.00 mm (482.6 in), LBL=52.00 mm (1320.8 in).


Jan 30/200525-20-04

SERVICING

1. General

The Closet must be serviced before it is checked or repaired. Servicing will restore theunit’s performance and appearance.

2. Servicing Materials

Only use recommended servicing agents and materials (or appropriate equivalents). Takecare to comply with all cautions and warnings.

Equivalent susbstitutes may be used for listed items.

WARNING: SOME AGENTS AND MATERIALS CAN BE DETRIMENTAL TODECORATIVE TRIMS AND/OR FINISHES, AS WELL AS HARMFUL TOPERSONNEL, IF HANDED IMPROPERLY.

Table 14001Recommended Servicing Agents and Materials

Material Identification SourceAir, compressed Any approved source

Aliphatic Naphtha Federal Specification TT-N-95 Commercially available

Benzene Federal Specification VV-B-230 Commercially available

Brushes, small soft-bristled Commercially available

Brushes, non-metallic Commercially available

Cleaner, degreaser Kleenol-30 Mission Kleensweep Prod.2434 Birk DaleLos Angeles, CA

Chlorine compound Clorox or HTH Commercially available

Cloth, lint free Commercially available

Compound, corrosion MIL-C-38334 Commercially availableremoving

Page 14001


25-20-04 Jan 30/2005Page 14002

3. Servicing While Disassembled

Perform these steps at any time the galley is disassembled, partial or complete overhaulof the closet performed. Areas not normally exposed are to be thoroughly cleaned andsanitized at this time.

WARNING: AVOID BREATHING THE VAPORS OR FUMES FROM ANY CLEANINGSOLVENT. GOGGLES, GLOVES, A MASK AND PROTECTIVECLOTHING ARE TO BE WORN TO PREVENT IRRITATION FROMPROLONGED CONTACT WITH CLEANING AGENTS. CLOTHESSHOULD BE CHANGED IF SOLVENTS SPILLED ON THEM.

PROTECTIVE EYE SHIELDS OR GOGGLES ARE TO BE WORN WHENCLEANING WITH COMPRESSED AIR. DEBRIS AND/OR HIGHPRESSURE AIR CAN CAUSE SERIOUS EYE INJURY. PERSONNELSHOULD BE WARNED OF AREAS WHERE HAZARDOUS MATERIALSOR PROCEDURES ARE IN USE.

CAUTION: DO NOT ALLOW CLEANING FLUIDS TO RUN INTO CONNECTORS,SWITCHES, TUBING COVERING WIRES OR ELECTRIC PANELS.USE ONLY RECOMMENDED CLEANING AGENTS OR EQUIVALENTSWITH SPECIFIC INSTRUCTIONS TO PREVENT DAMAGE TO THEDECORATIVE FINISHES AND TRIM.

Table 14001Recommended Servicng Agents and Materials (cont'd)

Material Identification SourceDetergent, commercial Super Soilax or Electrol-Sol Commercially available

Disinfectant Lysol Commercially available

Ethanol Alcohol Federal Specification O-E-760 Commercially available

Isobutyl Alcohol Federal Specification TT-B-846 Commercially available

Isopropyl Alcohol Federal Specification TT-I-735 Commercially available

Solvent Rho-clene 7688 Rho-Chem Corp.425 Isis AvenueInglewood, CA

Toluene Federal Specification TT-T-584 Commercially available

Xylene Federal Specification TT-X-916 Commercially available


Jan 30/200525-20-04 Page 14003

A. Structure Assembly

CAUTION: STRUCTURE ASSEMBLIES ARE FABRICATED FROM A MULTI-PLYHONEYCOMB PANEL. DO NOT EMPLOY CLEANING PROCEDURESOUTLINED FOR METAL PARTS (SUCH AS FITTINGS, ANGLES, ETC)OR DAMAGED TO THE DECORATIVE FINISH OF THE HONEYCOMBPANELING MAY RESULT.

(1) Clean Panels

(a) Remove dirt, grease and oil deposits from paneling with a clean cloth saturatedin Isopropyl or Ethanol Alcohol.

(b) Stubborn stains may be cleaned with abrasive cleaning agents, such ashousehold scouring poweder (ammoniated or chlorinated) in combination witha dampened cloth. Use with care to avoid damaging decorative surfaces. Donot use any type of abrasive scouring pad.

(c) Remove difficult scuffs and/or stains from surfaces which appear metallic usingan appropriate cleaning solvent.

(d) Remove solvent using a soft, lint-free cloth soaked in Rho-clene. Stubbornresidue may removed with Kleenol-30.

(2) Clean Metal Parts

(a) Remove dirt, grease and oil from metal structural parts with a clean clothsaturated with Toluene, Benzene or Xylene cleaning solvent.

(b) Wipe clean parts with a lint-free cloth to removed solvent film or residue.

(3) Remove Corrosion

(a) Use a cloth saturated in a liquid solution of 50% distilled water and 50%corrosion-removing compound.

(b) Flush the treated area thoroughly with warm, potable water.

(c) Dry with compressed air.

(d) Mark all areas cleaned for corrosion in this manner for inspection per theCHECK procedure and treatment as specified in REPAIR.


25-20-04 Jan 30/2005Page 14004


Jan 30/200525-20-04


Page 15001

1. Storage Instructions

A. The Closet assembly is essentially corrosion resistant and therefore no specialpreservation is required.

B. Close and latch all doors. Wrap assembly in waterproof wrapping paper (FederalSpecification UU-P-271, or equivalent) or plastic cover. Use tape Federal SpecificationJAB-P-217, or equivalent) to secure wrapping paper or cover.

C. Identify unit by part number, serial number and date of maintenance or overhaul on atag or in a convenient location on wrapper. Store in a cool, dry place away from directsunlight and heat.

STORAGE

25-20-04 Jan 30/2005



Page 15002