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COMPONENT MAINTENANCE MANUALWITH

ILLUSTRATED PARTS LIST

Aug 31/2003

BOEING737

GALLEY 1 (AEROMEXICO)

Part Number501165-1

10781 Forbes AvenueGARDEN GROVE, CA 92643

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

Telex: 756227Vendor Code: 62225

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

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COMPONENT MAINTENANCE MANUALPART NO. 501165

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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 Aug 31/2003 Aug 31/2003 ITR

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RECORD OF TEMPORARY REVISIONS

Temporary Page Number Issue Date Date Removed ByRevision No.

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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


Aug 31/200325-34-93 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 Aug 31/2003TP-2 Aug 31/2003

Record of Revisions ROR-1 Aug 31/2003ROR-2 Aug 31/2003

Record of Temporary RTR-1 Aug 31/2003Revisions RTR-2 Aug 31/2003Service Bulletin List SBL-1 Aug 31/2003

SBL-2 Aug 31/2003List of Effective Pages LEP-1 Aug 31/2003

LEP-2 Aug 31/2003Table of Contents TOC-1 Aug 31/2003

TOC-2 Aug 31/2003List of Tables LOT-1 Aug 31/2003

LOT-2 Aug 31/2003List of Illustrations LOI-1 Aug 31/2003

LOI-2 Aug 31/2003List of Abbreviations LOA-1 Aug 31/2003

LOA-2 Aug 31/2003Introduction INTRO-1 Aug 31/2003

INTRO-2 Aug 31/2003Description and 1 Aug 31/2003Operation 2 Aug 31/2003

3 Aug 31/20034 Aug 31/20035 Aug 31/20036 Aug 31/20037 Aug 31/20038 Aug 31/2003

Testing and Fault 1001 Aug 31/2003Isolation 1002 Aug 31/2003

1003 Aug 31/20031004 Aug 31/20031005 Aug 31/20031006 Aug 31/20031007 Aug 31/20031008 Aug 31/2003

Wiring Diagram 2001 Aug 31/20032002 Aug 31/2003

2003F Aug 31/20032004F Aug 31/2003

Disassembly 3001 Aug 31/20033002 Aug 31/2003

Cleaning 4001 Aug 31/20034002 Aug 31/20034003 Aug 31/20034004 Aug 31/20034005 Aug 31/20034006 Aug 31/2003

Check 5001 Aug 31/20035002 Aug 31/20035003 Aug 31/20035004 Aug 31/2003

Check(Cont'd) 5005 Aug 31/20035006 Aug 31/2003

Repair 6001 Aug 31/20036002 Aug 31/20036003 Aug 31/20036004 Aug 31/20036005 Aug 31/20036006 Aug 31/20036007 Aug 31/20036008 Aug 31/2003

6009F Aug 31/20036010F Not used

Assembly 7001 Aug 31/20037002 Aug 31/2003

Fits and Clearances 8001 Aug 31/20038002 Aug 31/2003

Illustrated Parts List 10001 Aug 31/200310002 Aug 31/200310003 Aug 31/200310004 Aug 31/2003

Numerical Index 10005-1 Aug 31/200310005-2 Aug 31/200310005-3 Aug 31/200310005-4 Aug 31/200310005-5 Aug 31/200310005-6 Aug 31/200310005-7 Aug 31/200310005-8 Aug 31/200310005-9 Aug 31/200310005-10 Aug 31/200310005-11 Aug 31/200310005-12 Aug 31/200310005-13 Aug 31/200310005-14 Aug 31/2003

IPL Figure 1 10006-1F Aug 31/200310006-2F Not used10006-3 Aug 31/200310006-4 Aug 31/200310006-5 Aug 31/200310006-6 Aug 31/2003


IPL Figure 3 10015-1F Aug 31/2003

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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 3 (cont'd) 10015-2F Not used10015-3 Aug 31/200310015-4 Aug 31/2003


IPL Figure 5 10030-1F Aug 31/200310030-2F Not used10030-3 Aug 31/200310030-4 Aug 31/2003


IPL Figure 7 10045-1F Aug 31/200310045-2F Aug 31/200310045-3 Aug 31/200310045-4 Aug 31/2003



IPL Figure 10 10048-1F Aug 31/200310048-2F Aug 31/200310048-3 Aug 31/200310048-4 Aug 31/2003

Removal 12001 Aug 31/200312002 Aug 31/2003

Installation 13001 Aug 31/200313002 Aug 31/2003

13003F Aug 31/200313004F Aug 31/200313005F Aug 31/200313006F Aug 31/2003

Servicing 14001 Aug 31/200314002 Aug 31/200314003 Aug 31/200314004 Aug 31/200314005 Aug 31/200314006 Aug 31/2003

Storage 15001 Aug 31/200315002 Aug 31/2003


Aug 31/200325-34-93 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..........................................................................................................................................12001Installation.......................................................................................................................................13001Servicing.........................................................................................................................................14001Storage...........................................................................................................................................15001

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TOC Page 2



Aug 31/200325-34-93 LOT Page 1

LIST OF TABLES

TABLE PAGE

1 Associated Documents..............................................................................................................12 Applicable Inserts........................................................................................................................33 Power Load.................................................................................................................................44 Leading Particulars.....................................................................................................................51001 Test Equipment.........................................................................................................1001, 10021002 Bonding Resistance Measuring Table...............................................................................10031003 Fault Isolation Chart.............................................................................................................10084001 Recommended Cleaning Agents and Materials...................................................4001, 40025001 Check Schedules.................................................................................................................50016001 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 Galley Attachments..................................................................................................................63 Applicable Inserts................................................................................................................7, 82001 Wiring Diagram.......................................................................................................2003 , 20046001 Trim and Finish...................................................................................................................6009IPL 1 Final Assembly..............................................................................................................10006-1IPL 2 Structure Assembly.......................................................................................................10010-1IPL 3 Placard Installation........................................................................................................10015-1IPL 4 Electrical Installation.....................................................................................................10025-1IPL 5 Electrical Assembly......................................................................................................10030-1IPL 6 Plumbing Installation.....................................................................................................10035-1IPL 7 Door Assembly..............................................................................................................10045-1IPL 8 Drawer Installation.........................................................................................................10046-1IPL 9 Waste Chut Assembly..................................................................................................10047-1IPL 10 Light Fixture Assembly.................................................................................................10048-113001 Installation......................................................................................................13003 thru 13006

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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


Aug 31/200325-34-93 INTRO Page 1

INTRODUCTION1. Scope of Manual

This component maintenance manual provides instructions for maintenance of Galley 1Part Number 501165. Instructions are provided for maintenance duties ranging from on-board cleaning through simple checks and minor repairs to complete disassembly of the unitfor comprehensive shop overhaul. Repairs beyond the scope of this manual should bereferred 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 92643Telephone (714) 265-2911Telefax (714) 265-2301 or 714-265-1802Email: [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 galley.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 galley 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 galley.

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

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

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

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

J. The Illustrated Parts List section:

(1) An itemized breakdown of parts used on the stair house 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.

K. The Removal section provides stair house removal instructions from the aircraft.

L. The Installation section provides galley installation instructions from the aircraft.

M. The Servicing section provides restoration procedures of the galley.

N. The Storage section provides storing procedures of the galley 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 sections of this manual have been verified at the manufacturer's facility by performingthe galley functional test, test report number: 840123-1-2.

INTRO Page 2


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DESCRIPTION AND OPERATION1. General

The Galley 1 part number 501165 Series is a major component of the galley systeminstalled on 737-700 (NORTHWEST AIRLINES).

The galley is an integrally-bonded structure fabricated from fiberglass-sandwichpanels, 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. Thegalley design is modular in nature with functional components designated to specificcompartments.

Reference the table below and Driessen Drawing Number 501165 for further information.

Table 1Associated Documents

Page 1

GALLEY No. 1 P/N 501165-1BOEING ASSOCIATED DOCUMENTS DRAWING NO.

GENERAL I.C.D 415A8100 SHT. 156 REV. ACOORDINATION DRAWING 415A8101 SHT. 4 REV. ACONTOUR DWG. 415A8200 SHT. 1 REV. NEWGENERAL DESINGN SPECS. D415A001 REV. G

D6-55698 REV. GELECTRICAL DESIGN SPEC. D6-51331 REV.D

DRIESSEN ASSOCIATED DOCUMENTS DRAWING/PART NO.GENERAL ARRANGEMENT 500165-3FINAL ASSEMBLY 501165-1STRUCTURE ASSEMBLY 102724-211STRUCTURE DETAILS 103724BONDED STRUCTURE ASSEMBLY 104724-211ELECTRICAL DIAGRAM 506165-3ELECTRICAL INSTALLATION 507165-11ELECTRICAL ASSEMBLY 508165-11PLUMBING DIAGRAM 509165-3PLUMBING INSTALLATION 510165-11PLACARD INSTALLATION 518165-11TRIM AND FINISH 519165-3INSTALLATION DRAWING 521165-11

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Page 2

GENERAL ARRANGEMENTFigure 1


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2. Description

A. General

The galley facilitates for stowage of coats and garments.The galley also provides storage space for passanger control items and emergencyequipments. Removable serving carts permits rapid replenishment of food, beveragesand dry sotres during pre- and post- flight operations.

B. Galley Lower Attachments

The galley employs four (4) hardpoints, bolts and washers.Refer to Figure 2- Galley Attachments.

C. Galley Provisions

The Galley is design to handle provisions such as curtain rail. See Fig. 3 ApplicableInserts and Galley Provisions.

3. Safety Considerations

A. The Galley 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 Galley, such as hinged doors, incorporate apositivelatching provision capable of retaining the component in the closed or stowedposition during acceleration. All doors that are exposed when installed includesecondary latches.

C. General warning placards, emergency placards, crew instructions placards, and weight

Page 3

Table 2Applicable Inserts

APPLICABLE INSERTS VENDOR AND P/N DIMENSIONS

STEAM OVEN B/E AEROSPACE 11.22 22.11 21.3272071000 285.0 561.5 541.5

COFFEE MAKER B/E AEROSPACE 6.31 12.12 13.72P/N 411-0001-141 160.3 307.8 348.5

COFFEE MAKER RAIL B/E AEROSPACE N/A N/A N/AP/N 416-0201-27 N/A N/A N/A

CART, HALF SIZE DRIESSEN 11.89 40.55 16.04P/N TL010017 302.0 1030.0 407.4

WASTE CONTAINER DRIESSEN 7.34 20.00 18.87P/N 225006-29 186.4 508.0 479.3

WORK LIGHT DRIESSEN N/A N/A N/A N/A N/A N/A

HOT CUP DRIESSEN N/A N/A N/AP/N DLH549-017 N/A N/A N/A

W H D

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Page4

Table 3Power Load

INSERT / COMPONENT TOTAL POWER LOAD DESCRIPTION WATTS

COFFEE MAKER 2775

STEAM OVEN 3750

WORK LIGHT 35

HOT CUP 500

TOTAL 7060

placards are located in conspicuous places and are readable from normal workingpositions.

D. Material used in construction of the Galley 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

A. The galley is designed so that inspection, adjustment, service and removal/replacementof parts requires no special tools. Convenient access is provided to the attachmentfittings and various service facility connections at the airplane interface.

B. Plumbing

The galley receives potable water through a quick-disconnect fitting, a shutoff valve andwater filter. Waste water and liquids from coffee makers, water boilers and countertopsis drained through galley mounted plumbing lines into the aircraft drain system.

C. Lighting

General illumination for galley areas is accomplished by means of light fixtures in theaircraft ceiling. A light fixture, located above the counter, directly illuminates theworkdeck.


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Unit Part Number Height Width Depth Weight*

Galley 1 501165-1 77.60 in 39.25 in 22.25 in 546 lbs(1971.04 mm) (996.95 mm) ( 565.15 mm) (248 kg)

Table 4 Leading Particulars

* Estimated gross weight.

Page 5

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 STAIR HOUSE. REMOVE AS MANY ITEMS ASNECESSARY TO ALLOW SUFFICIENT CLEARANCE FOR THEDOOR TO CLOSE.

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 4 provides a list of leading particulars for the Galley.

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Galley AttachmentsFigure 2

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Aug 31/200325-34-93Applicable Inserts and Galley Provisions

Figure 3(Sheet 1 of 2)Page 7

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Page 8

Applicable Inserts and Galley ProvisionsFigure 3 (Sheet 2 of 2)


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TESTING AND FAULT ISOLATION

CAUTION: HANDLE, MOUNT AND TEST THE GALLEY AND ITS COMPONENTSWITH CARE TO PREVENT TOOL MARKS, SCRATCHES OR OTHERDAMAGE CAUSED BY TESTING.

1. General

These procedures are designed to test the galley before installation in the aircraft.

If all requirements of test procedures cannot be completed successfully, the galley ofcomponent is defective. Refer to Fault Isolation (in this section) for possible causes andcorrections.

2. Test Equipment

Table 1001 lists the test equipment and materials required for the testing and faultisolation of the galley. Equivalent equipment and/or materials may be substituted for theitems listed.

Table 1001Test Equipment

EQUIPMENT MANUFACTURER RANGE / RATING (Part Number)

Fixture (mounting or holding) Locally Fabricated Not Applicablefor each structure, subassembly

Frequency Converter Commercially available

Dielectric Test Device Hipotronics Inc. 2.5 kV - 3.0 kV(Model: HD 103) 0-50/500/5000 µA (DC)

0-50 µA (AC)2 % Full scale

Digital Ohmeter Valhalla Scientific 200 milliohms-20 kiloohms(Model: 4100 ATC) ± .02% Reading ± 2 digits

Digital Multimeter Commercially available

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Table 1001Test Equipment (cont'd)

EQUIPMENT MANUFACTURER RANGE / RATING (Part Number)

Pressure/Vacuum Gage Commercially available -100 kPA/30" HG200 KPA/30 PSI2% Full Scale Accuracy

Water Tank Commercially available 75 psi max.

Vacuum/Compressor Pump Commercially available 400 PSI max.

Stop Watch or Clock with a sweep Commercially available 23" Hg max VAC, 20 psi max.

Power Supply, Switched Commercially available 115/200 VAC, 400 Hz,3-phase, thermal protected at135 F

3. Electrical Tests

A. Electrical Bonding Test

(1) Measure the resistance value between the top galley static ground and a point onthe aircraft where resistance is less that ten (10) milliohms. The minimumallowable resistance for the galley bonding point to the farthest measuring point ofthe complete galley must not exceed 30 milliohms.

(2) Check the bonding using Figure 2001 from the top galley static ground to eachapplicable point indicated in Table 1002 . When the galley compliment includes morethan one unit of the same type -- two (2) coffee makers or two (2) ovens -- be sure totest each unit separately.

(3) Any ground resistance that exceeds the maximum values given must be rejected.

(a) Take appropriate corrective action -- either rework or replace.

(b) Upon completion of rework or replacement, the test shall be conducted again inthis entire test.

C. Dielectric Strength Test

Test each assembled wire harness for dielectric strength before it is installed in thegalley.

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MEASUREMENT POINT RESISTANCE PER UNIT (All Points Measured to Top Galley Static Ground) (in milliohms)

Table 1002Bonding Resistance Measuring Table

Coffee Maker 15Coffee Maker Rail 10Steam Oven 15Electrical Panel 10Work Counter 10Hot Cup Provisions 15Sump 10Shut-Off Valve 10Work Light 15Ballast 10Water Filter Bracket 15Plumbing Spigot 15

Page 1003

(1) Disconnect all inserts, including the ballast and indicator light, from the galley electrical system.

(2) Close the circuit breakers and set the switches to the ON position.

(3) Attach the connector pins of the wire harness being tested to the positive terminals of the dielectric strength tester through the test cable adaptor.

(4) Attach the negative terminal to the galley ground connection.

(5) Apply 1500 VAC at a uniform rate of 250 to 500 volts per second.

(6) Maintain at 1500 VAC for a period of one (1) minute.

(7) Apply the test voltage between each active conductor and all other conductors connected together.

(8) Test all wire harnesses longer than 15 feet at 100 volts rms, 50 or 60 Hz. All other requirements remain the same.

CAUTION: ALL REPEAT DIELECTRIC STRENGTH TESTS SHALL BE CONDUCTEDAT 80% OF THE SPECIFIED VOLTAGE.


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(9) Any evidence of arcing, sparking or breakdown; current leakage in excess of 2.0milliamperes; or other evidence of insulation damage shall constitute a failure.

(a) Take appropriate corrective action.

(b) Test must be performed again after any corrective action or rework is done.

(10) Any wire harness which passes this test shall immediately be tested for insulation resistance before being disconnected from the test equipment.

D. Insulation Resistance Test

Test each wire harness which passed the dielectric strength.

(1) Verify all inserts, including the ballast and indicator light are disconnected from thegalley electrical system. Disconnect if needed.

(2) Verify the circuit breakers are closed and switched are set to the ON position.Close and set to ON as needed.

(3) Test each harness wire-to-wire and wire-to-ground using 500 VDC for one (1)minute. Insulation between mutually insulated parts must be a minimum of 100megohms.

(4) Reconnect all inserts, ballast, indicator lights, etc., once all wiring harnesses havebeen successfully tested.

(5) Open the circuit breakers and set all switches to the OFF position.

4. Electrical System Functional Tests

Apply 115/200 VAC, 400 Hz, 3-phase power to the galley through the galley-to-aircraftinterface connector. Observe that all installed inserts are operating properly as follows:

A. Coffee Maker Functional Test

(1) Close the coffe maker circuit breaker.

(2) Place the coffee maker power switch in the ON position. The white POWER andamber HEATING indicator lights will come on and the water in the unit will begin toheat.


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(3) Return the coffee maker power switch to the OFF position. The white POWERand amber HEATING indicator lights will go off and the water in the unit will cool.

(4) Open the coffee maker circuit breaker.

B. Work Light Functional Test

(1) Close the circuit breaker for the area light.

(2) Set the area light switch first OFF position.

(3) Set the switch to the DIM position.

(4) Set the switch to the BRT position.

(5) Return the switch to the OFF position.

(6) Verify the level of lighting increases or decreases in brightness accordingly.

(7) Open the circuit breaker the work light.

C. Oven Functional Test

(1) Close the oven circuit breaker.

(2) Place the oven power switch in the ON position. The POWER switch will light upwhen the power is on.

(3) Place the HIGH switch in the ON position. The HIGH switch will light up and thethe oven will begin to heat.

(4) Return the oven power switch to the OFF position, The switch light will go off andthe oven will cool.

(5) Open the oven circuit breaker.

5. Compartment Functional Test (Doors, Drawers, Retainers and Latches)

A. Rotate each retainer and verify that it remains in both the open and closed positions.

B. Tap the center of the door lightly. There should be no excessive rattling.

Page 1005


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C. Unlatch and open each door fully one-at-a-time.

(1) The latch should release smoothly.

(2) The door should close completely without any binding or misalignment.

(3) Each primary and secondary latch shall smoothly and fully engage without marringthe face trim.

(4) Doors shall not strike any adjacent surface when open; unless, a bumper is providedto act as a door stop.

D. Check any drawers in the unit.

(1) The low-friction slides on the drawers should operate smoothly.

(2) The door should close completely without any binding or misalignment.

(3) The open position shop should assure the drawer remains in the unit even when open.

(4) There shall be no excessive transverse or vertical movement.6.

6. Plumbing System Functional Test

A. Water Supply System Test

(1) Put some system in place -- catch basins, external water tank or the aircraft mainwater tanks -- to collect water drainage from the system

(2) Turn water shut-off valve to the OFF position.

(3) Connect the water source to the galley inlet compressor.

(4) Set water pressure to 25 psi.

(5) Turn the water shut-off valve to the ON position.

(6) Install the insert equipment (coffee makers and/or water boilers) and open the outletsof the inserts equipment.

(7) Assure free flow of water from the insert equipment.

Page 1006


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(8) At 25 psi of water pressure, check all connections for leaks.

(9) Remove the insert equipment. The design of the water source interface between thegalley plumbing system and the insert equipment is such that removal of the insertsautomatically shuts off the water supply at the interface.

(10) Increase the water pressure to 50 psi and check all connections for leaks.

(11) Open the drain valve to drain the water in the system.

B. Drain System Test

(1) Put some system in place -- catch basins, external water tank or the aircraft mainwaste water tanks -- to collect water drainage from the system.

(2) Plug the drainage system at the end of the outlet fitting.

(3) Connect the water source to the galley water inlet connector.

(4) Fill the sump and drain lines with water and check all connections for leaks.

(5) Pour water into the drain system through the water boiler or coffee maker drain line.

(6) Assure overflow only occurs through out the work counter sump.

(7) Plug all drains lines with applicable plug and apply 15 psi to the drainage system forone (1) minute.

(8) Check the drain system for ruptures, sinks or permanent distortion.

(9) Disconnect the water supply.

(10) Remove all plugs from the drain lines to drain the system.

7. Fault Isolation

Table 1003 lists possible function faults and the component(s) most likely to cause theproblem. Perform any galley fault isolation procedure in accordance with Table 1003.


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TROUBLE PROBABLE CAUSE CORRECTIVE ACTION

Oven fails to POWER and/or HEATING switch Turn ON.operate. not ON.

Circuit breaker is OPEN. CLOSE the circuit breaker.

Switch(es) or circuit breaker is Replace the damaged or defectivedamaged or defective. component.

Module is damaged or defective. Refer to oven manufacter´sproduc data

Galley lights does not Lighting element is burnt out. Replace the ballast and/or bulb.illuminate.


Switch or circuit breaker is Replace the damaged or defectivedamaged or defective. component.

Table 1003Fault Isolation Chart

Galley door does not Compartment too full. Remove items until sufficient space isclose properly. cleared to close the door.

Attaching screws are loose. Tighten screws on both the door andgalley structure.

Hinged pin is damaged. Replace the hinge pin.

Coffee Maker POWER switch is not ON. Turn ON.does not function.


Switch or circuit breaker is Replace the damaged or defectivedefective. component.

Module is damaged or defective. Refer to beverage maker manufacturer'sproduct data.

Aug 31/200325-34-93


1. 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 galley ofcomponent is defective. Refer to Fault Isolation (in this section) for possible causes andcorrections.

Page 2001

WIRING DIAGRAM

25-34-93 Aug 31/2003


Page 2002



Aug 31/200325-34-93

DISASSEMBLY1. General

The galley is an integrally-bonded structure which is fabricated from sandwich panels andaluminum 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 galley from the aircraftand removal of high-wear, easily damaged components of disassembly needed to accessthose items requiring repair and/or replacement. Individual panel repairs may beaccomplished using the repair procedures outlined in the REPAIR section, starting on page6001.

The galley should be disassembled only to the degree necessary to replace parts, carryout 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 GALLEYASSEMBLY HAS BEEN REMOVED.

NOTE: Disassembly sequence is straight forward and self explanatory.

(a) Refer to IPL Figure 1 (Final Assembly, P/N 501165-1) to disassemble.

(b) Refer to IPL Figure 2 (Structure Assembly, P/N 102724-211) to disassemble.

(c) Refer to IPL Figure 3 (Placard Installation, P/N 518165-11) to disassemble.

(d) Refer to IPL Figure 4 (Electrical Installation, P/N 507165-11) to disassemble.

(e) Refer to IPL Figure 5 (Electrical Assembly, P/N 508165-11)) to disassemble.

(f) Refer to IPL Figure 6 (Plumbing Installation, P/N 510165-11) to disassemble.

Page 3001


25-34-93 Aug 31/2003Page 3002

(g) Refer to IPL Figure 7 (Door Assembly, P/N 527165-11) to disassemble.

(h) Refer to IPL Figure 8 (Drawer Installation, P/N 534165-11) to disassemble.

(i) Refer to IPL Figure 9 (Waste Chute Assembly, P/N 143719-11) to disassemble.

(j) Refer to IPL Figure 10 (Light Fixture Assembly, P/N 239051-21) to disassemble.


Aug 31/200325-34-93

CLEANING

1. General

The galley must be cleaned before it is checked or repaired. Cleaning will exposedefects and/or damage as well as the size and location of necessary repairs. Cleaningremoves unwanted material which can harm the galley'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.

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

Cloth, lint free Commercially available

Compound, corrosion MIL-C-38334 Commercially availableremoving

Page 4001


25-34-93 Aug 31/2003

Table 4001Recommended Cleaning 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

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 galley 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.

4. Field Maintenance

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

A. Remove all perishable items from the galley.

Page 4002


Aug 31/200325-34-93

B. Drain and dry the standing sumps.

C. Remove screens from sumps and clean away any debris.

D. Check drain strainers and remove any waste accumulation.

E. Remove the waste containers and dispose of waste in accordance with field wastedisposal procedures.

F. Clean and dry the waste containers in accordance to standard sanitation practices.

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

G. 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.

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

5. Periodic Maintenance

Performance of this procedure is recommended no less than on a quarterly basis. All thesteps for In-Flight Cleaning and Field Maintenance should be performed before theinstructions which follow are executed.

WARNING: PROTECTIVE EYE SHIELDS OR GOGGLES ARE TO BE WORN WHENCLEANING WITH COMPRESSED AIR. DEBRIS AND/OR HIGHPRESSURE AIR CAN CAUSE SERIOUS EYE INJURY.

CAUTION: SMALL PARTS CAN EASILY BE DAMAGED BY HOLDING THECOMPRESSED AIRJET NOZZLE TOO CLOSE. USE BRUSHESCAREFULLY ON DELICATE PARTS.

A. Cleaning Around and Behind the Beverage Makers

WARNING: BE VERY CAREFUL TO AVOID ELECTRIC SHOCK BYINTERRUPTING THE FLOW OF ELECTRICITY TO THE INSERT ATTHE CIRCUIT BREAKER.

Page 4003


25-34-93 Aug 31/2003

(1) Open the electrical circuit supplying power to the beverage maker.

(2) Disengage and slide out Beverage Maker from coffee maker rail. Proceed todisassemble beverage maker rails from the sump assy by removing hardware in four(4) places (screws, washers and spacers). Retain all hardware for re-installation ofrail after completion of cleaning.

NOTE: IT IS NOT NECESSARY TO COMPLETELY REMOVE THE COFFEEMAKER RAIL(S) FROM C/M COMPARTMENT IN ORDER TO CLEANUNDERNEATH. PLUMBING LINES AND ELECTRICALCONNECTIONS LOCATED AT THE REAR OF THE RAIL(S) MAY BELEFT INTACT.

(3) Blow dust away from small recesses, holes and enclosures using compressed air.

(4) Lift the beverage maker rail and gain ample access to the sump area underneath.Remove hardware securing sump screen(s) and clean/clear out any visible debris.

(5) Remove stains from all surfaces of the sump with an appropriate cleaning solvent.The solvent must then be removed using a soft, lint-free cloth soaked inRho-clene. Stubborn residue may be removed with Kleenol-30.

(6) Hard to remove soil may be cleaned with abrasive cleaning agents, scouringpowders (ammoniated or chlorinated) and non-metallic scouring pads only whenused with care so to avoid damaging anodized surfaces.

WARNING: AVOID BREATHING THE VAPORS OR FUMES FROM ANYCLEANING SOLVENT. GOGGLES, GLOVES, A MASK ANDPROTECTIVE CLOTHING ARE TO BE WORN TO PREVENTIRRITATION FROM PROLONGED CONTACT WITH CLEANINGAGENTS. CLOTHES SHOULD BE CHANGED IF SOLVENTSSPILLED ON THEM.

CAUTION: DO NOT ALLOW CLEANING FLUIDS TO RUN INTO CONNECTORS,SWITCHES, TUBING COVERING WIRES OR ELECTRIC PANELS.

(7) Wipe all surfaces dry with a clean, lint free cloth. Re-install sump screens andbeverage maker(s) using previously removed screws.

(8) Perform all CHECK procedures at this time.

Page 4004


Aug 31/200325-34-93

B. Replacing Water Filter Cartridge

(1) Shut off water supply to the filter at the Shut-off Valve (Turn knob CW to "OFF"position).

(2) Relieve all remaining water pressure in the system by opening spigot downstreamfrom filter.

(3) Release V-Band and disassemble the unit.

(4) Unscrew and discard old cartridge.

(5) Wash indide of water filter shell with diluted cholrine compound (Clorox, HTH, etc.).Tear open top of replacement cartridge plastic wrapper and peel back.

NOTE: TO PREVENT CONTAMINATION, KEEP HANDS OFF OF CARTRIDGE -HOLD WITH PLASTIC WRAPPER.

(6) Remove both the instruction label and colored outlet cap from cartridge.

(7) Screw cartridge into threaded outlet nipple (FINGER TIGHT ONLY).

(8) Remove and discard plastic wrapper.

(9) Reassemble the filter ensuring that the gasket is in place on shell tip. TightenV-Band bolt securely.

(10) Bleed air from system by running three (3) gallons of water at full flow until water is clear.

C. Cleaning Around and Behind Oven

WARNING: BE VERY CAREFUL TO AVOID ELECTRIC SHOCK BYINTERRUPTING THE FLOW OF ELECTRICITY TO THE INSERT ATTHE CIRCUIT BREAKER.

(1) Open the electrical circuit supplying power to the oven.

(2) Disengage and slide out the bracket. Retain all hardware for re-installation of railafter completion of cleaning.

Page 4005


25-34-93 Aug 31/2003

(3) Remove dirt, grease and oil deposits from paneling with a clean cloth saturated inIsopropyl, Isobutyl or Ethanol Alcohol.

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

(b) Remove difficult scuffs and/or stains from surfaces which appears metallicusing an appropriate cleaning solvent.

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

(4) 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 all surfaces dry with a clean, lint free cloth to remove solvent film orresidue. Re-install oven(s) using previously removed hardware.

(c) Perform all CHECK procedures at this time.

Page 4006


Aug 31/200325-34-93

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. Inspection and the following maintenance must be performed according to therequirements listed in Table 5001 - Check Schedules.

Page 5001

Table 5001Check Schedules

INSPECTIONCHECK SCHEDULE

A. Structure

B. Joints

C. Upper and Lower Attachments

D. Rubstrip and Tee Assembly, Carts

E. Workdecks and Work Counters

F. Air Filters and Vents

G. Mechanical(1) Slide Extractor(2) 1/4 Turn Retainer(3) Door Assembly

H. Electrical(1) Switched, Circuit Breakers and Fans(2) Wire Bundle Assemblies(3) Terminal Lugs, Connectors and Terminal Boards(4) Bulbs, Flourescent tubes, cap, lenses and LED

J. Placards

A B C D E


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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. Check Procedures

A. Structure

(1) Check the structure of the galley for scratches, cracks, holes and other damage.

CAUTION: ANY SIGNS OF CRACKS OR HOLES IN THE PANELS, THE GALLEYMUST BE SHUT DOWN AND REMOVE FROM THE AIRCRAFT.

(a) To remove the galley from the aircraft, refer to Section 3000, DISASSEMBLY ofthis manual.

(b) To repair the panels, refer to Section 6000, REPAIR of this manual.

(c) To replace panels, contact Driessen engineering.

(2) Check the decorative material is satisfactorily bonded. If damage, Refer to SECTION6000 of this manual for repair procedure.

(3) Check the galley for corrosion, especially milled or metal components and dampcompartments.

(4) Check trims, kickstrips and protective kickstrips are not loose.

(5) Check trims all areas in the galley are clean.

B. Joints

(1) Check all screwed joints of the galley are satisfactorily attached. Tighten unloosescrews or bolts. Refer to Section 8000, FITS AND CLEARANCES for correct torquevalues.

(2) Check all riveted connections are satisfactorily. If rivets are loose, remove all rivetsand replace.

Page 5002


Aug 31/200325-34-93

C. Upper and Lower attachments

(1) Check upper and lower attachments are not damaged and satisfactorily attached.

(2) Check upper and lower attachments for sign of vibrations. If these markings exist,replace attachment.

(3) Check carefully all attachment for corrosion. Floor fittings must be inspected carefully.Replace if necessary.

(4) Check floor seals between galley and aircraft floor. If seal is broken or deteriorated,replace it.

(5) Check tie rods of upper attachment for easy movement. Tighten unbolts to its correcttorque value by referring to Section 8000, Fits and Clearances of this manual.

D. Rubstrip and Tee Assembly, Cart

(1) Check every rubstrip and tee assembly for dents and nicks.

NOTE: RUBSTRIPS SHOWING 50% WEAR MUST BE REPLACE.

(2) Check cable of slide extractor for frays. Cable with frays are unacceptable and slideextractor mus be replace.

E. Workdecks and work counters

(1) Check workdecks and work counters for corrosion and flawless sealing.

F. Air Filters and Vents

WARNING: AIR FILTER MASK MUST BE WORN ALL TIMES DURING THISPROCEDURE.

(1) Check air filters for dirt and dust accumulation.

WARNING: NEVER WASH THE AIR FILTER. IT SHOULD BE REPLACE.

(2) Check air vents for dirt and dust accumulation. To clean the vents, do the step bystep procedures:

(a) Remove the vent by unfastening the screws.

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25-34-93 Aug 31/2003

(b) Use compressed air to blow out accumualted dirt and dust. If dirt still exist,replace the vent.

G. Mechanical

(1) Slide Extractor

(a) Check cable for frays. Replace slide extractor cable has frays.

(2) 1/4 Turn Retainer

(a) Check the retainer by rotating counterclockwise.

(b) There should be no looseness once the retainer was turned. If it is loose, use ascrew driver to tighten.

(3) Door Assembly

(a) Check doors for “OPEN” and “CLOSE” positions.

(b) Check hinges, springs, extrusions and door panel for damage.

(c) Check slam and slide latches for operational.

H. Electrical

(1) Check mechanical functions of switches, circuit breakers and fans.

(2) Check wires and electrical components for attachment, damage and overheatingsigns.

(3) Check all electrical connections for tightness and contact.

(4) Check all connections for cleanliness.

(5) Check plugs and receptacles for looseness. Also check for missing pins and contactsockets.

(6) Check terminal lugs for firm connection on wire ends.

Page 5004


Aug 31/200325-34-93 Page 5005

(7) Check connections on terminal boards and ground studs for corrosion.

(8) Check soldered and crimped connections for security.

(9) Check tension relief clamps on plugs and receptacles for security.

(10) Check wires and inserts for insulation resistance according to Section 1000, Testing and Fault Isolation of this manual.

(11) Perform dielectric test according to Section 1000, Testing and Fault Isolation of this manual.

(12) Check work light lenses, area light lenses, cap and control lamps for cleanliness, damage and presence.

(13) Check all bulbs and flourescent tubes in work lights, area lights and indicator lights.

J. Placards

(1) Check all placards for scratches. Unreadable placards must be replace.


25-34-93 Aug 31/2003Page 5006



Aug 31/200325-34-93

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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Aug 31/2003

(5) To install placards with pressure-sensitive adhesive, remove backIng 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


Aug 31/200325-34-93 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.

25-34-93


Aug 31/2003Page 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


Aug 31/200325-34-93 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.

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Aug 31/2003

(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


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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

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Aug 31/2003

(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 N122 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


Aug 31/200325-34-93

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 galley, inspect all parts for wear and/or damage which could result infailure of the galley 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


25-34-93 Aug 31/2003

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, P/N 501165-1) to assemble.

(b) Refer to IPL Figure 2 (Structure Assembly, P/N 102724-211) to assemble.

(c) Refer to IPL Figure 3 (Placard Installation, P/N 518165-11) to assemble.

(d) Refer to IPL Figure 4 (Electrical Installation, P/N 507165-11) to assemble.

(e) Refer to IPL Figure 5 (Electrical Assembly, P/N 508165-11)) to assemble.

(f) Refer to IPL Figure 6 (Plumbing Installation, P/N 510165-11) to assemble.

(g) Refer to IPL Figure 7 (Door Assembly, P/N 527165-11) to assemble.

(h) Refer to IPL Figure 8 (Drawer Installation, P/N 534165-11) to assemble.

(i) Refer to IPL Figure 9 (Waste Chute Assembly, P/N 143719-11) to assemble.

(j) Refer to IPL Figure 10 (Light Fixture Assembly, P/N 239051-21) to assemble.

Page 7002

Aug 31/200325-34-93


FITS AND CLEARANCES

1. General

The torque values (Refer to Table 8001) used are in accordance with the usual standardpractices.

Page 8001

Table 8001Torque Values

TENSION TORQUE (IN-LBS) 15-17 30-35 65-90 130-180 220-360 270-610 630-950

TENSION TORQUE (N-M) 1.7-1.9 3.4-4.0 7.3-10.2 14.7-20.4 24.8-40.7 41.8-68.9 71.2-107.3

THREAD SIZE 8-32 10-32 1/4-28 5/16-24 3/8-24 7/16-20 1/2-20

25-34-93 Aug 31/2003


Page 8002



Aug 31/200325-34-93

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 galley 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

25-34-93


Aug 31/2003

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


Aug 31/200325-34-93 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

V4001 AEROWORKS2727 S. CRODDY WAY.SUITE D.SANTA ANA, CA 92704

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

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

25-34-93


Aug 31/2003Page 10004

VENDOR LISTING CODE ADDRESS CODE ADDRESS

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

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 AEROWORKS.2727 S. CRODDY WAY,SUITE D.SANTA ANA, CA 92704.


Aug 31/200325-34-93

PART AIRLINE FIGURE ITEM TOTAL NUMBER STOCK NUMBER REQ

NUMERICAL INDEX

Page 10005-1

ACHC3-13 5 -275 1AN735C7 4 -205 1AN960-8L 2 -185 2AN960C10L 10 80 3AN960C416 4 -635 1BACC45FT14C7P 5 -270 1BACC63CE24A22P 5 -265 1BV03031B01-24 10 20 2BV03031D01-24 10 25 2C7A 5 150 2CBC6-33-1 5 -280 1FA4T5CWRS5004 10 15 2FH032-8-21 4 -475 1M22759-34-10-9 4 -285 1

4 -310 1MILW22759-34 4 -200 1

4 -410 14 -495 14 -660 15 -130 14 -245 1

MS14154-10 5 190 1MS14154-15 5 185 1MS18029-2S5 4 320 1MS18029-2S7 5 30 1MS20004-12 1 -150 2MS21042-08 5 -120 1MS21042-3 4 -230 1

4 -485 14 -530 14 -585 15 25 15 225 1

MS21042L06 9 -15 39 -50 3

MS21042L08 4 565 4MS21042L3 1 -195 3

4 -85 14 -270 14 -305 1


25-34-93 Aug 31/2003


NUMERICAL INDEX

Page 10005-2

MS21042L3 4 -430 14 -460 14 -615 1

MS21042L4 1 -175 2MS21042L6 1 -220 2

1 -235 2MS21043-04 10 35 8MS21043-06 10 60 2MS21043N3 10 85 1MS21069L4 4 -130 1MS21207-8-6 7 65 8MS21919WCH 4 5 17

4 30 15 5 1

MS21919WDG10 6 5 1MS21919WDG16 6 145 1MS21919WDG18 6 125 2MS21919WDG24 6 165 1MS21919WDG6 6 85 1

6 105 2MS21919WDG8 6 25 1

6 45 36 65 1

MS22759-34-10-9 4 -435 1MS24523-22 5 140 1MS24693C274 4 -630 1MS25036-108 5 -290 7MS25036-149 5 -285 6MS25226-4-3 5 75 1MS25281-F2 4 35 1MS27212-2-5 4 325 1MS27212-2-7 5 35 1MS27407-4 5 180 2MS3320-1 5 135 1MS3320-7-5 5 160 1MS35206-215 10 30 8

10 -45 2MS35206-230 10 55 2MS35265-12 7 25 2MS35335-64 6 240 1


Aug 31/200325-34-93


NUMERICAL INDEX

Page 10005-3

MS35338-138 4 355 15 65 1

MS35338-43 4 -260 14 -515 14 -605 15 210 110 75 1

MS35338-44 4 -120 2MS3560-3252 4 -125 2MS35650-302 4 -235 1

4 -525 14 -610 15 220 110 90 1

MS35650-304 4 360 14 -400 14 -645 15 70 1

MS35650-3252 4 340 25 50 2

MS51500B4-4S 6 290 16 325 2

MS51503B4S 6 265 1MS51504B4S 6 225 1MS51504B8-4S 6 200 1

6 230 1MS51510B4S 6 300 2MS51860-53SS 6 245 1MS51865-3 5 100 4MS51958-63 4 -180 1MS51958-66 4 -390 1NAS1149C0332R 4 -185 2

4 350 14 -395 34 -640 25 60 1

NAS1149C0432R 1 -135 44 -115 4

NAS1149F0332P 1 -60 31 -75 6


25-34-93 Aug 31/2003Page 10005-4


NUMERICAL INDEX

NAS1149F0332P 1 -90 21 -105 61 -120 21 -190 31 -285 51 -320 21 -345 24 -80 24 -265 24 -300 24 -425 14 -455 24 -600 3

NAS1149F0463P 1 -165 2NAS1149F0663P 1 -215 2

1 -230 2NAS1149FN616P 4 560 4NAS1149FN832P 4 -110 4

5 -255 26 -15 16 -35 16 -55 36 -75 16 -95 16 -115 26 -135 16 -155 16 -175 16 -220 36 -285 46 -345 46 -365 26 -490 36 -510 2

NAS1149G0332P 4 20 14 50 14 -220 24 -480 24 -510 24 -580 3


Aug 31/200325-34-93 Page 10005-5


NUMERICAL INDEX

NAS1149G0332P 5 20 15 205 2

NAS1149GN832P 4 -160 24 380 24 -550 25 95 45 -115 2

NAS1801-3-10 4 -450 14 -575 1

NAS1801-3-9 4 -75 14 -255 14 -295 1

NAS1801-4-15 4 -105 1NAS43DD3-32 4 25 1

4 55 1NAS514P1032-10 4 -215 1

5 15 1NAS514P1032-12 4 -505 1

5 200 110 70 1

NAS514P1032-14 2 -55 84 -595 1

NAS514P1032-6 2 2 255 20NAS514P1032-8 1 -260 12

2 -245 22 265 8

NAS514P440-6 4 335 25 45 2

NAS514P632-5 1 -375 29 -10 39 -45 3

NAS514P632-8 4 555 4NAS514P832-14 1 -360 2NAS514P832-5 7 15 4NAS514P832-6 1 -30 5

1 -295 45 90 45 -110 18 80 20

NAS514P832-7 2 15 4


25-34-93 Aug 31/2003Page 10005-6


NUMERICAL INDEX

NAS514P832-7 2 -100 42 -160 4

NAS517-2-19 8 85 6NAS602-10 6 -280 4

6 -485 3NAS602-12 4 -155 2

6 -30 16 -90 1

NAS602-16 6 -10 16 -110 2

NAS602-6 1 -55 31 -70 61 -85 21 -100 61 -115 21 -315 24 -100 44 375 24 -545 26 -215 3

NAS602-7 2 -30 62 -125 42 -140 82 -180 26 -340 4

NAS602-8 1 -365 15 -250 2

NAS603-14 4 15 14 45 1

NAS603-18 1 -185 3NAS603-6 1 -340 2

6 -505 2NAS603-7 1 -280 5

2 -115 20NAS604-10 1 -130 4NAS623-2-12 6 -70 1NAS623-2-14 6 -130 1

6 -150 1NAS623-2-18 6 -50 3

6 -170 1


Aug 31/200325-34-93 Page 10005-7


NUMERICAL INDEX

NAS623-2-32 6 -360 2S1A 6 330 1S4933959-531 5 165 1SL210-04-1 10 -110 2SS43F4 6 205 1

6 375 1SSCHS8-1-3 6 455 10377-00 6 335 110000-3 1 -210A REF10000-4 1 -225A REF10003-3 1 -245A 110003-4 1 -250A 110237-2 5 170 1102724-211 1 -5 1

2 -1 REF102724-75 2 -70 A/R102724-77 2 -20 A/R

2 -45 A/R103719-1035 2 135 1103719-1039 2 120 1103719-1047 1 350 1103724-105 1 -160 2103724-11 2 75 1103724-1179 2 95 1103724-13 2 10 1103724-21 1 290 1103724-33G 2 85 1103724-39 2 65 1103724-45 2 5 1103724-57 1 80 1103724-59 1 50 1103724-65 1 355 1103724-85G 2 80 1103724-87G 2 90 1103724-95 1 110 1103769-1087 1 310 1106 10 50 1130-0933-003 5 145 2131719-11 2 50 1134724-11 2 110 1


25-34-93 Aug 31/2003Page 10005-8


NUMERICAL INDEX

143719-1003 9 55 1143719-1009 9 40 1143719-11 2 155 1

9 -1 REF1691-0410 3 -10 4181-8836-09-553 5 155 2200011-101 4 -345 5

5 -55 7200011-111 4 500 1

5 -195 110 -65 1

200011-151 4 150 1200011-161 4 540 1200011-221 4 -370 1200011-31 5 -85 1200011-41 4 -330 1

5 -40 1200011-441 4 570 1200011-551 5 230 3200011-581 4 -40 1200011-621 4 625 1200011-631 4 385 1200011-641 4 470 1200011-661 4 210 3200011-681 4 175 4200011-71 5 -10 1200011-711 5 105 1200011-81 4 -10 17200033-51 2 40 1200049-141 4 590 1200049-161 4 65 2200049-171 4 290 7200049-181 4 445 3200049-221 4 250 3200049-351 4 420 1200049-441 4 95 1201011-13 2 -270 2201056-3 2 260 2201057-5 2 250 2202029-7 1 370 1


Aug 31/200325-34-93 Page 10005-9


NUMERICAL INDEX

209003-11 1 255 4209018-21 2 240 1210002-3 7 60 4210009-3 7 10 2212001-12 8 75 2213005-15 1 -200 1213005-91 1 180 1214N2036-1 1 330 1214N2037-1 1 335 1215015-3 7 5 2216001-3 1 210 2216001-4 1 225 2216022-3 1 245 1216022-4 1 250 1218001-3 8 10 1219011-3P3 4 -90 1

4 -140 14 -275 14 -465 14 -620 14 665 4

220001-11-0800 2 175 1223010-1220 1 95 2223010-2240 1 65 2228001-3 2 170 2230-05BR832-0 5 245 1231001-3 9 20 1231001-331 9 -5 1231001-5 9 30 1231001-7 9 35 1231010-9 2 130 1232002A-0852-1352 2 200 1235001-3 7 30 3

9 25 2236001-3 3 5 1236055-101 3 15 1236055-102 3 20 1236055-103 3 25 1236055-104 3 30 1236055-105 3 35 1


25-34-93 Aug 31/2003Page 10005-10


NUMERICAL INDEX

236055-106 3 40 1236066-101 3 45 1236066-102 3 50 1236066-103 3 55 1236066-104 3 60 1236066-105 3 65 1236066-106 3 70 1236070-3 3 75 1236090-3 3 80 1236096-55 3 85 1236096-59 3 90 1236096-9 3 95 1236139-415 3 180 1236224-29 3 100 1236324-15 10 10 1236341-115 3 105 1236341-117 3 110 2236341-119 3 115 6236341-125 3 120 1236341-127 3 125 1236341-145 3 130 1236341-147 3 135 1236341-149 3 185 1236341-155 3 140 1236341-157 3 145 2236341-99 3 175 1236355-3 5 175 1236754-53-24 3 150 1236822-14-30 3 155 2236822-43-95 3 160 1236822-50-110 3 165 2236822-9-20 3 170 1237002-61 2 25 3

2 145 2237004-3 4 60 4237005-3 4 145 1237006-13 4 -135 1237007-53 4 365 1237031-9 4 165 1239003-23 10 40 1


Aug 31/200325-34-93


NUMERICAL INDEX

Page 10005-11

239051-21 4 535 110 -1 REF

239052-13 10 5 1239052-17 10 -125 1239052-21 10 95 1239052-41 10 120 1239052-7 10 -100 1240017-41 6 355 1240038-13 6 255 1240038-9 6 250 1240043-11 6 210 1241004-8-95 6 435 1241018-61 6 400 1241018-71 6 415 1242002-21 6 275 1242011-3 10 -105 1242020-13-0045 6 445 1242020-13-0110 6 430 1242020-15-0120 6 395 1242020-19-0030 6 475 1242020-19-0035 6 420 1242020-19-0160 6 515 1242020-19-0190 6 410 1242020-3-0070 6 440 1242020-3-0080 6 465 1242020-7-0050 6 405 1242020-7-0070 6 390 1242032-11-0035 6 310 1242032-11-030 6 260 1242032-11-0450 6 315 1242032-21-0060 6 305 1242032-21-0090 6 295 1242032-21-0190 6 320 1242034-41-0360 6 195 1242057-3 6 235 1243020-51 6 470 1247010-31-0600 7 70 2247010-51-1225 2 235 1247010-51-1300 1 270 2247010-51-1644 2 225 1


25-34-93 Aug 31/2003


NUMERICAL INDEX

Page 10005-12

247010-71-0300 2 215 1247010-71-0630 2 220 1247010-71-0780 2 205 1247010-71-1650 2 210 1247010-71-1950 1 205 2247010-91-1300 1 265 4247010-91-1800 2 230 2247016-31-0300 1 325 1247017-21-1950 2 60 2247018-5 1 140 1247046-21-1319 1 275 1248003-5 1 -40 5

1 -305 42 -105 42 -150 42 -165 42 -195 1

248004-23 2 -35 62 -190 1

248514-3 1 -35 51 -300 4

251001-3 1 240 2251002-025 6 -495 3251002-075 6 -80 1251002-100 6 -60 3

6 -140 16 180 1

251002-225 6 -370 2251002-25 6 -40 1

6 -100 1251002-50 6 -20 1

6 -120 2251002-75 6 -160 1259001-229 6 380 12600LW 5 240 126551-3 10 -130 426551-5 5 235 12KILF15 6 270 1416-0201-27 1 125 1501165-1 1 -1 REF


Aug 31/200325-34-93


NUMERICAL INDEX

Page 10005-13

507165-11 1 -15 14 -1 REF

508165-11 4 670 15 -1 REF6 -1 REF

50845-2 4 -195 14 -415 14 -655 1

510165-11 1 -20 16 500 1

511165-21 6 425 1511165-3 6 385 1511165-31 6 460 1511165-9 6 450 1518165-1 3 -1 REF518165-11 1 -10 1521165-21 1 -380 1521165-31 1 -385 1527165-11 1 25 1

7 -1 REF527165-13 7 50 1527165-15 7 40 1527165-17 7 35 1527165-19 7 20 1527165-3 7 75 1527165-5 7 55 1527165-9 7 45 1534165-11 1 45 1

8 -1 REF535165-11 8 -5 1535165-21 8 70 1535165-3 8 90 1535165-31 8 60 1535165-33 8 15 1535165-34 8 20 1535165-35 8 25 1535165-36 8 30 1535165-41 8 65 1535165-43 8 35 1535165-45 8 40 1


25-34-93 Aug 31/2003


NUMERICAL INDEX

Page 10005-14

535165-47 8 45 1535165-49 8 50 15416K11 6 190 105416K15 6 185 12550165-11 5 260 15676000507 5 -300 15676000807 4 170 15676001307 5 -295 16052T3 8 55 260B50338-31 6 480 16400 4 -225 1

4 -520 15 215 1

65-5458-20 1 145 165-5458-21 1 -170 266-9776-1 1 -155 26C108 5 -125 16C109 4 -240 1

4 -280 14 -315 14 -440 14 -490 1

6F6XSS 6 350 177-54 5 80 18694KGI 10 -115 A/R90101A225 4 -190 1

4 -405 14 -650 1

99W10-01A1 10 -135 4


Aug 31/200325-34-93Page 10006-3

FIG.ITEM PART NUMBER

AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE

- ITEM NOT ILLUSTRATED

1 -1 501165-1 1 FINAL ASSY, GALLEY 1 REF-5 102724-211 2 STRUCTURE ASSY 1

(SEE IPL FIG. 2 FOR BREAKDOWN)-10 518165-11 2 PLACARD INSTL 1

(SEE IPL FIG. 3 FOR BREAKDOWN)-15 507165-11 2 ELECTRICAL INSTL 1

(SEE IPL FIG. 4 FOR BREAKDOWN)-20 510165-11 2 PLUMBING INSTL 1

(SEE IPL FIG. 6 FOR BREAKDOWN)25 527165-11 2 DOOR ASSY 1

(SEE IPL FIG. 7 FOR BREAKDOWN) ATTACHING PARTS

-30 NAS514P832-6 2 SCREW, FLAT HD, # 8-32 X .50 LG 5-35 248514-3 2 WASHER 5-40 248003-5 2 NUT, BLIND 5

***45 534165-11 2 ICE DRAWER INSTALLATION 1

(SEE IPL FIG. 8 FOR BREAKDOWN)50 103724-59 2 VENT SCREEN 1

ATTACHING PARTS-55 NAS602-6 2 SCREW, PAN HD, # .164-32 X .375 LG 3-60 NAS1149F0332P 2 WASHER, FLAT 3

***65 223010-2240 2 VENT SCREEN 2


***80 103724-57 2 VENT SCREEN 1


***95 223010-1220 2 VENT SCREEN 2


***110 103724-95 2 SHROUD, WORK LIGHT 1

IND


25-34-93 Aug 31/2003Page 10006-4


AIRLINEPART NO.

UNITSPER

ASSY

EFFCODE

NOMENCLATURE


IND

1 ATTACHING PARTS-115 NAS602-6 2 SCREW, PAN HD, # .164-32 X .375 LG 2-120 NAS1149F0332P 2 WASHER, FLAT 2

***125 416-0201-27 2 RAIL, COFFEE MAKER 1

(COSTUMER FURNISHED, DRIESSENINSTALLED) ATTACHING PARTS

-130 NAS604-10 2 SCREW, PAN HD, # .250-28 X .625 LG 4-135 NAS1149C0432R 2 WASHER, FLAT 4

***140 247018-5 2 BUMPON 1145 65-5458-20 2 HANDLE 1

ATTACHING PARTS-150 MS20004-12 2 BOLT, INT. WRENCHING 2-155 66-9776-1 2 COLLAR 2-160 103724-105 2 DOUBLER 2-165 NAS1149F0463P 2 WASHER, FLAT 2-170 65-5458-21 2 NUT, HANDLE 2-175 MS21042L4 2 NUT, SELF LOCKING 2

***180 213005-91 2 BRACKET, OVEN ALIGNMENT 1

ATTACHING PARTS-185 NAS603-18 2 SCREW, PAN HD, # .190-32 X 1.12 LG 3-190 NAS1149F0332P 2 WASHER, FLAT 3-195 MS21042L3 2 NUT, SELF LOCKING 3-200 213005-15 2 SPACER 1

***205 247010-71-1950 2 RUBSTRIP ASSY 2210 216001-3 2 RETAINER, 1/4 TURN 2

-210A 10000-3 2 RETAINER, 1/4 TURN (V4001) REF(OPTIONAL P/N FOR 216001-3) ATTACHING PARTS

-215 NAS1149F0663P 2 WASHER, FLAT 2-220 MS21042L6 2 NUT, SELF LOCKING 2

***225 216001-4 2 RETAINER, 1/4 TURN 2

-225A 10000-4 2 RETAINER, 1/4 TURN (V4001) REF(OPTIONAL P/N FOR 216001-4)


Aug 31/200325-34-93


AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE


IND

Page 10006-5

1 ATTACHING PARTS-230 NAS1149F0663P 2 WASHER, FLAT 2-235 MS21042L6 2 NUT, SELF LOCKING 2240 251001-3 2 SPACER, RETAINER 2

***245 216022-3 2 RETAINER, 1/4 TURN 1

-245A 10003-3 2 RETAINER, 1/4 TURN (V4001) 1(OPTIONAL P/N FOR 216022-3)

250 216022-4 2 RETAINER, 1/4 TURN 1-250A 10003-4 2 RETAINER, 1/4 TURN (V4001) 1

(OPTIONAL P/N FOR 216022-4)255 209003-11 2 STOP ASSY, CART 4

ATTACHING PARTS-260 NAS514P1032-8 2 SCREW, FLAT HD, # .190-32 X .500 LG 12

***265 247010-91-1300 2 RUBSTRIP ASSY 4270 247010-51-1300 2 RUBSTRIP ASSY 2275 247046-21-1319 2 BUMPER ASSY 1


***290 103724-21 2 DOOR, WATER FILTER 1

ATTACHING PARTS-295 NAS514P832-6 2 SCREW, FLAT HD, # .164-32 X .375 LG 4-300 248514-3 2 WASHER, CSK 4-305 248003-5 2 NUT, BLIND 4

***310 103769-1087 2 SHROUD, STOP 1


***325 247016-31-0300 2 RUBSTRIP ASSY 1330 214N2036-1 2 GRILL 1335 214N2037-1 2 PLENUM 1



25-34-93 Aug 31/2003Page 10006-6

UNITSPER

ASSY

EFFCODE

NOMENCLATUREFIG.ITEM PART NUMBER

AIRLINEPART NO.


IND

1 ***350 103719-1047 2 KICKSTRIP 1355 103724-65 2 GUIDE, WHEEL 1

ATTACHING PARTS-360 NAS514P832-14 2 SCREW, FLAT HD, # .164-32 X .875 LG 2-365 NAS602-8 2 SCREW, PAN HD, # .164-32 X .500 LG 1

***370 202029-7 2 PLATE, SHIM 1

ATTACHING PARTS-375 NAS514P632-5 2 SCREW, FLAT HD, # .138-32 X .312 LG 2

***-380 521165-21 2 INSTALLATION DRAWING 1

(REFER TO SECTION 13000, PAGE13003, INSTL ASSY)

-385 521165-31 2 INSTALLATION DRAWING 1(REFER TO SECTION 13000, PAGE13003, INSTL ASSY)


Aug 31/200325-34-93Page 10010-3


AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE


2 -1 102724-211 1 STRUCTURE ASSY, GALLEY 1 REF(SEE IPL FIG. 1 FOR NHA)

5 103724-45 2 PLATE 110 103724-13 2 COVER, ACCESS 1

ATTACHING PARTS15 NAS514P832-7 2 SCREW, FLAT HD, # 8-32 X .44 LG 4-20 102724-77 2 FOAM TAPE, SEAL A/R

***25 237002-61 2 RECEPTACLE ASSY 3

ATTACHING PARTS-30 NAS602-7 2 SCREW, PAN HD, # 8-32 X .44 LG 6-35 248004-23 2 INSERT, BLIND 6

***40 200033-51 2 COVER, ACCESS, HOT CUP 1

ATTACHING PARTS-45 102724-77 2 FOAM TAPE, SEAL A/R

***50 131719-11 2 SUMP 1

ATTACHING PARTS-55 NAS514P1032-14 2 SCREW, FLAT HD, # 10-32 X .88 LG 8

***60 247017-21-1950 2 RUBSTRIP 265 103724-39 2 RUBSTRIP 1

ATTACHING PARTS-70 102724-75 2 TAPE, FOAM A/R

***75 103724-11 2 BLOCK ASSY 180 103724-85G 2 SPLASH GUARD 185 103724-33G 2 SPLASH GUARD 190 103724-87G 2 SPLASH GUARD 195 103724-1179 2 CONNECTOR, SOCKET 1

ATTACHING PARTS-100 NAS514P832-7 2 SCREW FLAT HD, # 8-32 X .44 LG 4-105 248003-5 2 NUT, BLIND 4

***110 134724-11 2 WORK DECK, ASSY 1

ATTACHING PARTS-115 NAS603-7 2 SCREW, PAN HD, # 10-32 X .44 LG 20

***

IND


25-34-93 Aug 31/2003Page 10010-4


AIRLINEPART NO.

UNITSPER

ASSY

EFFCODE

NOMENCLATURE


IND

2 120 103719-1039 2 COVER, ACCESS 1 ATTACHING PARTS

-125 NAS602-7 2 SCREW, FLAT HD, # 8-32 X .88 LG 4 ***

130 231010-9 2 DEFLECTOR 1135 103719-1035 2 DEFLECTOR 1

ATTACHING PARTS-140 NAS602-7 2 SCREW, PAN HD, # 8-32 X .44 LG 8

***145 237002-61 2 RECEPTACLE ASSY 2

ATTACHING PARTS-150 248003-5 2 NUT, BLIND 4

***155 143719-11 2 WASTE CHUTE ASSY 1

(SEE IPL FIG. 9 FOR BREAKDOWN) ATTACHING PARTS

-160 NAS514P832-7 2 SCREW, FLAT HD, # 8-32 X .44 LG 4-165 248003-5 2 NUT, BLIND 4

***170 228001-3 2 STRIKER 2175 220001-11-0800 2 FLIGHT CABLE ASSY 1

ATTACHING PARTS-180 NAS602-7 2 SCREW, PAN HD, # 8-32 X .44 LG 2-185 AN960-8L 2 WASHER 2-190 248004-23 2 NUT, BLIND 1-195 248003-5 2 INSERT, BLIND 1

***200 232002A-0852-1352 2 COVER, ACCESS 1205 247010-71-0780 2 RUBSTRIP, .54" THK 1210 247010-71-1650 2 RUBSTRIP, .54" THK 1215 247010-71-0300 2 RUBSTRIP, .54" THK 1220 247010-71-0630 2 RUBSTRIP, .54" THK 1225 247010-51-1644 2 RUBSTRIP, .29" THK 1230 247010-91-1800 2 RUBSTRIP, .41" THK 2235 247010-51-1225 2 RUBSTRIP, .29" THK 1240 209018-21 2 STOP ASSY 1

ATTACHING PARTS-245 NAS514P1032-8 2 SCREW, FLAT HD, # 10-32 X .44 LG 2

***


Aug 31/200325-34-93


AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE


IND

2 250 201057-5 2 FITTING, FLOOR 2 ATTACHING PARTS

2 255 NAS514P1032-6 2 SCREW, FLAT HD, # 10-32 X 3/8 LG 20 ***

260 201056-3 2 CUP, FLOOR 2 ATTACHING PARTS

265 NAS514P1032-8 2 SCREW, FLAT HD, # 10-32 X .44 LG 8-270 201011-13 2 SPACER (FLOOR CUP FITTING) 2

***

Page 10010-5


25-34-93 Aug 31/2003Page 10010-6



Aug 31/200325-34-93Page 10015-3


AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE


3 -1 518165-1 1 PLACARD INSTL, GALLEY 1 REF(SEE IPL FIG.1 FOR NHA)

5 236001-3 2 PLACARD, IDENTIFICATION 1 ATTACHING PARTS

-10 1691-0410 2 RIVET, POP 4 ***

15 236055-101 2 PLACARD, COMPARTMENT ID 120 236055-102 2 PLACARD, COMPARTMENT ID 125 236055-103 2 PLACARD, COMPARTMENT ID 130 236055-104 2 PLACARD, COMPARTMENT ID 135 236055-105 2 PLACARD, COMPARTMENT ID 140 236055-106 2 PLACARD, COMPARTMENT ID 145 236066-101 2 PLACARD, COMPARTMENT ID 150 236066-102 2 PLACARD, COMPARTMENT ID 155 236066-103 2 PLACARD, COMPARTMENT ID 160 236066-104 2 PLACARD, COMPARTMENT ID 165 236066-105 2 PLACARD, COMPARTMENT ID 170 236066-106 2 PLACARD, COMPARTMENT ID 175 236070-3 2 PLACARD, WATER SPIGOT 180 236090-3 2 PLACARD, DRIESSEN NAMEPLATE… 185 236096-55 2 PLACARD, OVEN 190 236096-59 2 PLACARD, COFFEE MAKER 195 236096-9 2 PLACARD, HOT CUP 1100 236224-29 2 PLACARD, NO CIGARRETTE DISPOSAL 1105 236341-115 2 PLACARD, WASTE CONTAINER… 1110 236341-117 2 PLACARD, HALF SIZE STOWAGE… 2115 236341-119 2 PLACARD, SEAL WHEN REINSTALLED 6120 236341-125 2 PLACARD, ACCESS TO WATER… 1125 236341-127 2 PLACARD, EMERGENCY WATER… 1130 236341-145 2 PLACARD, ALL CART OR NO… 1135 236341-147 2 PLACARD, CLOSE WHEN NOT IN USE 1140 236341-155 2 PLACARD, ICE DRAWER 1145 236341-157 2 PLACARD, NO STOWAGE 2150 236754-53-24 2 PLACARD, MAX OVEN WEIGHT 1155 236822-14-30 2 PLACARD, MAX STOW WEIGHT 2160 236822-43-95 2 PLACARD, MAX STOW WEIGHT 1165 236822-50-110 2 PLACARD, MAX STOW WEIGHT 2170 236822-9-20 2 PLACARD, MAX STOW WEIGHT 1175 236341-99 2 PLACARD, CAUTION NOTICE 1

IND


25-34-93 Aug 31/2003Page 10015-4


AIRLINEPART NO.

UNITSPER

ASSY

EFFCODE

NOMENCLATURE


IND

3 180 236139-415 2 PLACARD, STOW HOT CUP IN COMPT. 1185 236341-149 2 PLACARD, CLOSE AND SECURE 1


Aug 31/200325-34-93Page 10025-3


AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE


4 -1 507165-11 1 ELECTRICAL INSTL, GALLEY 1 REF(SEE IPL FIG.1 FOR NHA)

5 MS21919WCH 2 CLAMP, LOOP 17 ATTACHING PARTS

-10 200011-81 2 CLAMP INSTL 1715 NAS603-14 3 SCREW, PAN HD, # 10-32 X .87 LG 120 NAS1149G0332P 3 WASHER, FLAT 125 NAS43DD3-32 3 SPACER, SLEEVE 1

***30 MS21919WCH 2 CLAMP, LOOP 135 MS25281-F2 2 CLAMP, LOOP 1

ATTACHING PARTS-40 200011-581 2 CLAMP INSTL 145 NAS603-14 3 SCREW, PAN HD, # 10-32 X .87 LG 150 NAS1149G0332P 3 WASHER, FLAT 155 NAS43DD3-32 3 SPACER, SLEEVE 1

***60 237004-3 2 COVER, RETAINER 465 200049-161 2 STRAP INSTL, GROUND 2-75 NAS1801-3-9 3 SCREW, HEX HD, # .190-32 X .563 LG 1-80 NAS1149F0332P 3 WASHER, FLAT 2-85 MS21042L3 3 NUT, SELF LOCKING 1-90 219011-3P3 3 GROUNDING STRIP 195 200049-441 2 STRAP INSTL, GROUND 1

-100 NAS602-6 3 SCREW, PAN HD, # .164-32 X .375 LG 4-105 NAS1801-4-15 3 SCREW, HEX HD, # .250-28 X .938 LG 1-110 NAS1149FN832P 3 WASHER, FLAT 4-115 NAS1149C0432R 3 WASHER, FLAT 4-120 MS35338-44 3 WASHER, LOCK SPRING 2-125 MS3560-3252 3 NUT, PLAIN HEX 2-130 MS21069L4 3 NUT PLATE, SELF LOCKING 1-135 237006-13 3 PLATE 1-140 219011-3P3 3 GROUNDING STRIP 1145 237005-3 2 RETAINER, ELECTRICAL PANEL 1

ATTACHING PARTS150 200011-151 2 BRACKET INSTL, RETAINER 1-155 NAS602-12 3 SCREW, PAN HD, # 8-32 X .750 LG 2-160 NAS1149GN832P 3 WASHER, FLAT 2

***

IND


25-34-93 Aug 31/2003Page 10025-4


AIRLINEPART NO.

UNITSPER

ASSY

EFFCODE

NOMENCLATURE


IND

4 165 237031-9 2 SKID, ELECTRICAL PANEL 1170 5676000807 2 CONDUIT 1175 200011-681 2 TUBE INSTL, GROUNDING 4-180 MS51958-63 3 SCREW, PAN HD, # 10-32 X .50 LG 1-185 NAS1149C0332R 3 WASHER, FLAT 2-190 90101A225 3 NUT, HEX SELF LOCKING 1-195 50845-2 3 LUG 1-200 MILW22759-34 3 WIRE 1-205 AN735C7 3 CLAMP, TUBE 1210 200011-661 2 COMPONENT INSTL, ELECTRICAL 3-215 NAS514P1032-10 3 SCREW, FLAT HD, # 10-32 X .62 LG 1-220 NAS1149G0332P 3 WASHER, FLAT 2-225 6400 3 WASHER, CSK 1-230 MS21042-3 3 NUT, SELF LOCKING 1-235 MS35650-302 3 NUT, HEX 1-240 6C109 3 LUG 1-245 MILW-22759-34 3 WIRE 1250 200049-221 2 STRAP INSTL, GROUND 3-255 NAS1801-3-9 3 SCREW, HEX HD, # .190-32 X .563 LG 1-260 MS35338-43 3 WASHER, LOCK SPRING 1-265 NAS1149F0332P 3 WASHER, FLAT 2-270 MS21042L3 3 NUT, SELF LOCKING 1-275 219011-3P3 3 GROUNDING STRIP 1-280 6C109 3 LUG 1-285 M22759-34-10-9 3 WIRE 1290 200049-171 2 STRAP INSTL, GROUND 7-295 NAS1801-3-9 3 SCREW, HEX HD, # .190-32 X .563 LG 1-300 NAS1149F0332P 3 WASHER, FLAT 2-305 MS21042L3 3 NUT, SELF LOCKING 1-310 M22759-34-10-9 3 WIRE 1-315 6C109 3 LUG 1320 MS18029-2S5 2 COVER, TERMINAL BOARD 1325 MS27212-2-5 2 BOARD, TERMINAL 1

ATTACHING PARTS-330 200011-41 2 BOARD INSTL, TERMINAL 1335 NAS514P440-6 3 SCREW, FLAT HD, # 4-40 X .50 LG 2340 MS35650-3252 3 NUT, HEX 2

***-345 200011-101 2 TERMINAL ASSY 5


Aug 31/200325-34-93Page 10025-5


AIRLINEPART NO.

UNITSPER

ASSY

EFFCODE

NOMENCLATURE


IND

4 350 NAS1149C0332R 3 WASHER, FLAT 1355 MS35338-138 3 WASHER, LOCK 1360 MS35650-304 3 NUT, PLAIN HEX 1365 237007-53 2 BRACKET, TERMINAL BOARD 1

ATTACHING PARTS-370 200011-221 2 BRACKET INSTL 1375 NAS602-6 3 SCREW, PAN HD, # 8-32 X .375 LG 2380 NAS1149GN832P 3 WASHER, FLAT 2

***385 200011-631 2 GROUND INSTL, WALLMOUNT 1-390 MS51958-66 3 SCREW, PAN HD, # 10-32 X .88 LG 1-395 NAS1149C0332R 3 WASHER, FLAT 3-400 MS35650-304 3 NUT, PLAIN HEX 1-405 90101A225 3 NUT, HEX SELF LOCKING 1-410 MILW22759-34 3 WIRE 1-415 50845-2 3 LUG 1420 200049-351 2 STRAP INSTL, GROUND 1-425 NAS1149F0332P 3 WASHER, FLAT 1-430 MS21042L3 3 NUT, SELF LOCKING 1-435 MS22759-34-10-9 3 WIRE 1-440 6C109 3 LUG 1445 200049-181 2 STRAP INSTL, GROUND 3-450 NAS1801-3-10 3 SCREW, HEX HD, # .190-32 X .625 LG 1-455 NAS1149F0332P 3 WASHER 2-460 MS21042L3 3 NUT, SELF LOCKING 1-465 219011-3P3 3 GROUNDING STRIP 1470 200011-641 2 COMPONENT INSTL, ELECTRICAL 1-475 FH032-8-21 3 STUD, ZINK 1-480 NAS1149G0332P 3 WASHER, FLAT 2-485 MS21042-3 3 NUT, SELF LOCKING 1-490 6C109 3 LUG 1-495 MILW22759-34 3 WIRE 1500 200011-111 2 PANEL GROUND, ELECTRICAL 1-505 NAS514P1032-12 3 SCREW, FLAT HD, # 10-32 X .75 LG 1-510 NAS1149G0332P 3 WASHER, FLAT 2-515 MS35338-43 3 WASHER, LOCK 1-520 6400 3 WASHER, CSK 1-525 MS35650-302 3 NUT, HEX 1-530 MS21042-3 3 NUT, SELF LOCKING 1


25-34-93 Aug 31/2003Page 10025-6


AIRLINEPART NO.

UNITSPER

ASSY

EFFCODE

NOMENCLATURE


IND

4 535 239051-21 2 WORKLIGHT 1(SEE IPL FIG.10 FOR BREAKDOWN) ATTACHING PARTS

540 200011-161 2 LIGHT ASSY, INSTL 1-545 NAS602-6 3 SCREW, PAN HD, # 8-32 X .375 LG 2-550 NAS1149GN832P 3 WASHER, FLAT 2

***555 NAS514P632-8 2 SCREW, FLAT HD, # .138-32 X .50 LG 4560 NAS1149FN616P 2 WASHER, FLAT 4565 MS21042L08 2 NUT, SELF LOCKING 4570 200011-441 2 GROUNDING INSTL, BRACKET 1-575 NAS1801-3-10 3 SCREW, HEX HD, # 10-32 X .62 LG 1-580 NAS1149G0332P 3 WASHER, FLAT 3-585 MS21042-3 3 NUT, SELF LOCK 1590 200049-141 2 STRAP INSTL, GROUND 1-595 NAS514P1032-14 3 SCREW, FLAT HD, # .190-32 X .875 LG 1-600 NAS1149F0332P 3 WASHER, FLAT 3-605 MS35338-43 3 WASHER, LOCK SPRING 1-610 MS35650-302 3 NUT, PLAIN HEX 1-615 MS21042L3 3 NUT, SELF LOCKING 1-620 219011-3P3 3 GROUNDING STRIP 1625 200011-621 2 GROUND INSTL, BRACKET 1-630 MS24693C274 3 SCREW, FLAT HD, # 10-32 X .75 LG 1-635 AN960C416 3 WASHER 1-640 NAS1149C0332R 3 WASHER, FLAT 2-645 MS35650-304 3 NUT, PLAIN HEX 1-650 90101A225 3 NUT, SELF LOCKING 1-655 50845-2 3 LUG 1-660 MILW22759-34 3 WIRE 1665 219011-3P3 2 GROUNDING STRIP 4670 508165 2 ELECTRICAL ASSY 1

(SEE IPL FIG. 5 FOR BREAKDOWN)


Aug 31/200325-34-93Page 10030-3


AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE


5 -1 508165-11 1 ELECTRICAL ASSY, GALLEY 1 REF(SEE IPL FIG.4 FOR NHA)

5 MS21919WCH 2 CLAMP, LOOP 1 ATTACHING PARTS

-10 200011-71 2 CLAMP INSTL 115 NAS514P1032-10 3 SCREW, FLAT HD, # 10-32 X .62 LG 120 NAS1149G0332P 3 WASHER, FLAT 125 MS21042-3 3 NUT, SELF LOCKING 1

***30 MS18029-2S7 2 COVER, TERMINAL BOARD 135 MS27212-2-7 2 BOARD, TERMINAL 1

ATTACHING PARTS-40 200011-41 2 BOARD INSTL, TERMINAL 145 NAS514P440-6 3 SCREW, FLAT HD, # 4-40 X .50 LG 250 MS35650-3252 3 NUT, HEX 2

***-55 200011-101 2 TERMINAL ASSY 760 NAS1149C0332R 3 WASHER, FLAT 165 MS35338-138 3 WASHER, LOCK 170 MS35650-304 3 NUT, PLAIN HEX 175 MS25226-4-3 2 LINK, TERMINAL CONNECTOR 180 77-54 2 BALLAST 1

ATTACHING PARTS-85 200011-31 2 BALLAST INSTL 190 NAS514P832-6 3 SCREW, FLAT HD, # 8-32 X .375 LG 495 NAS1149GN832P 3 WASHER, FLAT 4100 MS51865-3 3 NUT 4

***105 200011-711 2 ELEC. COMPONENT INSTL 1-110 NAS514P832-6 3 SCREW, FLAT HD, # 8-32 X .375 LG 1-115 NAS1149GN832P 3 WASHER, FLAT 2-120 MS21042-08 3 NUT, SELF LOCKING 1-125 6C108 3 LUG 1-130 MILW22759-34 3 WIRE 1135 MS3320-1 2 BREAKER, CIRCUIT 1140 MS24523-22 2 SWITCH, TOGGLE 1145 130-0933-003 2 LENS CAP, LIGHT 2150 C7A 2 BULB, LIGHT 2155 181-8836-09-553 2 LIGHT ASSY 2

IND


25-34-93 Aug 31/2003Page 10030-4


AIRLINEPART NO.

UNITSPER

ASSY

EFFCODE

NOMENCLATURE


IND

5 160 MS3320-7-5 2 BREAKER, CIRCUIT 1165 S4933959-531 2 WASHER 1170 10237-2 2 COLLAR 1175 236355-3 2 PLACARD 1180 MS27407-4 2 SWITCH, TOGGLE 2185 MS14154-15 2 BREAKER, CIRCUIT 1190 MS14154-10 2 BREAKER, CIRCUIT 1-195 200011-111 2 PANEL GROUND, ELECTRICAL 1200 NAS514P1032-12 3 SCREW, FLAT HD, # 10-32 X .75 LG 1205 NAS1149G0332P 3 WASHER, FLAT 2210 MS35338-43 3 WASHER, LOCK 1215 6400 3 WASHER, CSK 1220 MS35650-302 3 NUT, HEX 1225 MS21042-3 3 NUT, SELF LOCKING 1230 200011-551 2 INSTL, ELECTRICAL PANEL 3235 26551-5 3 STUD 1240 2600LW 3 RETAINER, RING 1245 230-05BR832-0 2 HANDLE 1

ATTACHING PARTS-250 NAS602-8 2 SCREW, PAN HD, # .164-32 X .50 LG 2-255 NAS1149FN832P 2 WASHER, FLAT 2

***260 550165-11 2 PANEL, ELECTRICAL 1-265 BACC63CE24A22P 2 CONNECTOR 1-270 BACC45FT14C7P 2 CONNECTOR 1-275 ACHC3-13 2 CONNECTOR, HOT CUP 1-280 CBC6-33-1 2 CONNECTOR, OVEN 1-285 MS25036-149 2 LUG, TERMINAL 6-290 MS25036-108 2 LUG, TERMINAL 7-295 5676001307 2 CONDUIT 1-300 5676000507 2 CONDUIT 1


Aug 31/200325-34-93Page 10035-3


AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE


6 -1 508165-11 1 PLUMBING ASSY, GALLEY 1 REF(SEE IPL FIG.1 FOR NHA)

5 MS21919WDG10 2 CLAMP, LOOP 1 ATTACHING PARTS

-10 NAS602-16 2 SCREW, PAN HD, # .164-32 X 1.00 LG 1-15 NAS1149FN832P 2 WASHER, FLAT 1-20 251002-50 2 SPACER, THREADED 1

***25 MS21919WDG8 2 CLAMP, LOOP 1

ATTACHING PARTS-30 NAS602-12 2 SCREW, PAN HD, # .164-32 X .750 LG 1-35 NAS1149FN832P 2 WASHER, FLAT 1-40 251002-25 2 SPACER, THREADED 1


ATTACHING PARTS-50 NAS623-2-18 2 SCREW, PAN HD, # .164-32 X 1.401 LG 3-55 NAS1149FN832P 2 WASHER, FLAT 3-60 251002-100 2 SPACER, THREADED 3




ATTACHING PARTS-90 NAS602-12 2 SCREW, PAN HD, # .164-32 X .750 LG 1-95 NAS1149FN832P 2 WASHER, FLAT 1-100 251002-25 2 SPACER, THREADED 1


ATTACHING PARTS-110 NAS602-16 2 SCREW, PAN HD, # .164-32 X 1.00 LG 2-115 NAS1149FN832P 2 WASHER, FLAT 2-120 251002-50 2 SPACER, THREADED 2


IND


25-34-93 Aug 31/2003Page 10035-4


AIRLINEPART NO.

UNITSPER

ASSY

EFFCODE

NOMENCLATURE


IND

6 ATTACHING PARTS-130 NAS623-2-14 2 SCREW, PAN HD, # .164-32 X 1.151 LG 1-135 NAS1149FN832P 2 WASHER, FLAT 1-140 251002-100 2 SPACER, THREADED 1




ATTACHING PARTS-170 NAS623-2-18 2 SCREW, PAN HD, # .164-32 X 1.401 LG 1-175 NAS1149FN832P 2 WASHER, FLAT 1180 251002-100 2 SPACER, THREADED 1

***185 5416K15 2 CLAMP, HOSE 12190 5416K11 2 CLAMP, HOSE 10195 242034-41-0360 2 FLEXHOSE ASSY 1200 MS51504B8-4S 2 ELBOW, 90 DEGR, MALE 1205 SS43F4 2 VALVE, SHUTOFF 1210 240043-11 2 BRACKET, SHUTOFF VALVE 1


***225 MS51504B4S 2 ELBOW, 90 DEGR, MALE 1230 MS51504B8-4S 2 ELBOW, 90 DEGR, MALE 1235 242057-3 2 SPIGOT 1240 MS35335-64 2 WASHER, LOCK FLAT 1245 MS51860-53SS 2 LOCKNUT, BULKHEAD 1250 240038-9 2 CUP, SPIGOT 1255 240038-13 2 BRACKET, GND 1260 242032-11-030 2 FLEXHOSE ASSY 1265 MS51503B4S 2 ADAPTER, STRGHT MALE 1270 2KILF15 2 SEAM QUICK DISCONNECT 1275 242002-21 2 COUPLING, WALLMOUNT 1

ATTACHING PARTS


Aug 31/200325-34-93Page 10035-5


AIRLINEPART NO.

UNITSPER

ASSY

EFFCODE

NOMENCLATURE


IND

6 -280 NAS602-10 2 SCREW, PAN HD, # .164-32 X .625 LG 4-285 NAS1149FN832P 2 WASHER, FLAT 4

***290 MS51500B4-4S 2 ADAPTER, STRGHT MALE 1295 242032-21-0090 2 FLEXHOSE ASSY 1300 MS51510B4S 2 TEE, TUBE 2305 242032-21-0060 2 FLEXHOSE ASSY 1310 242032-11-0035 2 FLEXHOSE ASSY 1315 242032-11-0450 2 FLEXHOSE ASSY 1320 242032-21-0190 2 FLEXHOSE ASSY 1325 MS51500B4-4S 2 ADAPTER, STRGHT MALE 2330 S1A 2 FILTER, WATER 1335 0377-00 2 BRACKET, WATER FILTER 1


***350 6F6XSS 2 COUPLING, ADAPTER 1355 240017-41 2 BRACKET, DRAIN VALVE 1


***375 SS43F4 2 VALVE, SHUTOFF 1380 259001-229 2 VENT HOSE 1385 511165-3 2 TUBE, TYGON 1390 242020-7-0070 2 TUBE, TEFLON 1395 242020-15-0120 2 TUBE, TYGON 1400 241018-61 2 MANIFOLD ASSY 1405 242020-7-0050 2 TUBE, TEFLON 1410 242020-19-0190 2 TUBE, TYGON 1415 241018-71 2 MANIFOLD ASSY 1420 242020-19-0035 2 TUBE, TYGON 1425 511165-21 2 MANIFOLD ASSY 1430 242020-13-0110 2 TUBE, TYGON 1435 241004-8-95 2 ELBOW 1440 242020-3-0070 2 TUBE, TEFLON 1445 242020-13-0045 2 TUBE, TYGON 1


25-34-93 Aug 31/2003Page 10035-6

6 450 511165-9 2 TUBE 1455 SSCHS8-1-3 2 VALVE, CHECK 1460 511165-31 2 MANIFOLD ASSY 1465 242020-3-0080 2 TUBE, TEFLON 1470 243020-51 2 SUMP ASSY 1475 242020-19-0030 2 TUBE, TYGON 1480 60B50338-31 2 STRAINER, DRAIN 1

(BOEING FURNISHED, DRIESSENINSTALLED) ATTACHING PARTS

-485 NAS602-10 2 SCREW, PAN HD, # .164-32 X .625 LG 3-490 NAS1149FN832P 2 WASHER, FLAT 3-495 251002-025 2 SPACER, THREADED 3

***500 511165-11 2 PAN ASSY 1


***515 242020-19-0160 2 TUBE, TYGON 1


AIRLINEPART NO.

UNITSPER

ASSY

EFFCODE

NOMENCLATURE


IND


Aug 31/200325-34-93Page 10045-3


AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE


7 -1 527165-11 1 DOOR ASSY, GALLEY 1 REF(SEE IPL FIG. 1 FOR NHA)

5 215015-3 2 LATCH 210 210009-3 2 PLATE, BACKING 2

ATTACHING PARTS15 NAS514P832-5 2 SCREW, FLAT HD, # 8-32 X 5/16 LG 4

***20 527165-19 2 PIN, HINGE 125 MS35265-12 2 SCREW, PAN HD, #.112-40 X .190 LG 230 235001-3 2 SPRING 335 527165-17 2 HINGE, HALF 1

(M/F 219002-5)40 527165-15 2 EXTRUSION, HINGE SIDE 1

(M/F 219006)45 527165-9 2 EXTRUSION, LATCH SIDE 1

(M/F 3090012)50 527165-13 2 EXTRUSION 1

(M/F 3090012)55 527165-5 2 EXTRUSION 1

(M/F 3090012)60 210002-3 2 BRACKET, CORNER 4

ATTACHING PARTS65 MS21207-8-6 2 SCREW, SELF TAP, # 8-18 X .38 LG 8

***70 247010-31-0600 2 RUBSTRIP ASSY 275 527165-3 2 PANEL 1

IND


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Aug 31/200325-34-93Page 10046-3


AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE


8 -1 534165-11 1 DRAWER INSTALLATION, GALLEY1 REF(SEE IPL FIG. 1 FOR NHA)

-5 535165-11 2 ICE DRAWER ASSEMBLY 110 218001-3 3 HANDLE, PULL 115 535165-33 3 EXTRUSION, DRAWER 1

(M/F 3090013)20 535165-34 3 EXTRUSION, DRAWER 1







(M/F 3090039)55 6052T3 3 TAPE, WARNING 260 535165-31 3 BONDED ASSEMBLY 165 535165-41 3 ICE DRAWER LINNER ASSEMBLY 170 535165-21 2 SUMP ASSEMBLY 175 212001-12 2 SLIDE, DRAWER 2

ATTACHING PARTS80 NAS514P832-6 2 SCREW, FLAT HD, # .164-32 X .375 LG 2085 NAS517-2-19 2 SCREW, FLAT HD, # .164-32 X 1.59 LG 690 535165-3 2 SPACER 1

***

IND


25-34-93 Aug 31/2003Page 10046-4



Aug 31/200325-34-93Page 10047-3


AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE


9 -1 143719-11 1 WASTE CHUTE ASSY REF(SEE IPL FIG. 2 FOR NHA)

-5 231001-331 2 FLAP, WASTE CHUTE 1 ATTACHING PARTS

-10 NAS514P632-5 2 SCREW, FLAT HD, # 6-32 X .31 LG 3-15 MS21042L06 2 NUT 3

***20 231001-3 3 FLAP 125 235001-3 3 SPRING 230 231001-5 3 HINGE 135 231001-7 3 HINGE 140 143719-1009 2 DEFLECTOR 1

ATTACHING PARTS-45 NAS514P632-5 2 SCREW, FLAT HD, # 6-32 X .31 LG 3-50 MS21042L06 2 NUT 3

***55 143719-1003 2 FRAME 1

IND


25-34-93 Aug 31/2003Page 10047-4



Aug 31/200325-34-93Page 10048-3


AIRLINEPART NO.

UNITSPERASSY

EFFCODE

NOMENCLATURE


10 -1 239051-21 1 LIGHT FIXTURE ASSY REF(SEE IPL FIG. 4 FOR NHA)

5 239052-13 2 COVER 110 236324-15 2 PLACARD 115 FA4T5CWRS5004 2 LAMP (V28107) 220 BV03031B01-24 2 HOLDER, LAMP (V17023) 225 BV03031D01-24 2 HOLDER, LAMP (V17023) 2

ATTACHING PARTS30 MS35206-215 2 SCREW 835 MS21043-04 2 NUT 8

***40 239003-23 2 HOUSING 1-45 MS35206-215 2 SCREW 250 106 2 TERMINAL STRIP (V76188) 1

ATTACHING PARTS55 MS35206-230 2 SCREW 260 MS21043-06 2 NUT 2

***-65 200011-111 2 ELEC PANEL, GND 170 NAS514P1032-12 3 SCREW, FLAT HD, # 10-32 X .75 LG 175 MS35338-43 3 WASHER, LOCK 180 AN960C10L 3 WASHER 385 MS21043N3 3 NUT, HEX SELF LOCK 190 MS35650-302 3 NUT, HEX SELF LOCK 195 239052-21 2 HOUSING ASSY 1

-100 239052-7 3 HOUSING, LIGHT 1-105 242011-3 3 VENT 1-110 SL210-04-1 3 CLIPNUT 2-115 8694KGI 3 FOAM, CLOSED SELL (V3A054) A/R120 239052-41 2 FRAME ASSY 1-125 239052-17 2 FRAME 1-130 26551-3 3 STUB (V08733) 4-135 99W10-01A1 3 RETAINER, WASHER (V08733) 4

IND


25-34-93 Aug 31/2003Page 10048-4



Aug 31/200325-34-93

1. General

The galley is an integrally-bonded structure which is fabricated from sandwich panels andaluminum 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 galley from the aircraftand removal of high-wear, easily damaged components of disassembly needed to accessthose items requiring repair and/or replacement. Individual panel repairs may beaccomplished using the repair procedures outlined in the REPAIR section, starting on page6001.

The galley should be disassembled only to the degree necessary to replace parts, carryout 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. 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 GALLEYASSEMBLY HAS BEEN REMOVED.

A. Galley 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.

CAUTION: EXERCISE EXTREME CARE WHEN REMOVING SCREWS ORBOLTS ATTACHING A PART TO THE SYNTHETIC PANELING.THREADED INSERTS, WHICH ARE INSTALLED IN THE PANELING

Page 12001

REMOVAL


25-34-93 Aug 31/2003

TO RECEIVE SCREWS OR BOLTS, ARE INSTALLED IN PANELINGWITH POTTING COMPOUND. UNNECESSARY DAMAGE TOINSERTS WILL REQUIRE REPLACEMENT WITH LARGER INSERTS.

(1) Remove Galley by following reverse instructions on figure 13001, pages 13003 thru13006.

Page 12002


Aug 31/200325-34-93

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 galley, inspect all parts for wear and/or damage which could result infailure of the galley 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. Installation

A. Galley 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


25-34-93 Aug 31/2003

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 floor fittings of the galley in between the following coordinates:

X= 270.75 (6877.05 mm), Y= 12.75 (323.85 mm) and X= 295.00 (7493.00 mm),Y=12.75 (323.85 mm).

(2) Follow installation instructions on figure 13001(see pages 13003 thru 13006).


Aug 31/200325-34-93

SERVICING

1. General

The galley must be serviced before it is checked or repaired. Servicing will restore thegalley'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


25-34-93 Aug 31/2003

3. Servicing While Disassembled

Perform these steps at any time the galley is disassembled, partial or complete overhaulof the galley 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

Page 14002


Aug 31/200325-34-93

SMALL PARTS CAN EASILY BE DAMAGING BY HOLDING THECOMPRESSED AIR JET NOZZLE TOO CLOSE. USE BRUSHESCAREFULLY ON DELICATE PARTS.

A. Door Assemblies

(1) Cleaning

(a) Remove stubborn dirt with a solution of 1.25 grams of Super Soilax detergent(or equivalent) per gallon of hot water.

(b) After cleaning completely, use hot water and a clean, soft cloth to wipe allsurfaces.

(c) Towel dry with a clean, lint-free cloth.

(2) Remove Corrosion

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

(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.

(3) Disinfect

(a) Wash in a solution of five (5) tablespoons of liquid disinfectant (Lysol orequivalent) to each gallon distilled.

(b) Rinse for five (5) minutes in running water.

(c) Blow dry with compressed air and/or wipe clean with a lint-free cloth.

B. Plumbing Installations

(1) Remove sump screens and remove any debris.

Page 14003


25-34-93 Aug 31/2003

(2) Check and clean drain strainers periodically for accumulated waste.

(3) Flush plumbing assemblies thoroughly using a solution consisting of five (5)tablespoons of liquid disinfectant per gallon of distilled water.

(4) After disinfecting, flush systems thoroughly for five (5) minutes with fresh, potablewater.

(5) Blow components dry with compressed air.

C. Electrical Installation

WARNING: OBSERVE ALL FIRE PRECAUTIONS WHEN FLAMMABLE AGENTSARE USED (SUCH AS ALIPHATIC NAPHTHA). ANY SUCHMATERIALS SHOULD ONLY BE USED WITH EXPLOSION-PROOFELECTRICAL EQUIPMENT IN A SPARK-FREE AND WELLVENTILLATED AREA.

CAUTION: DO NOT USE METAL TOOLS TO REMOVE FOREIGN SUBSTANCESFROM ELECTRICAL SOCKETS OR ANY ELECTRICAL CONTACTS.DAMAGE TO CONTACT PLATING WILL CAUSE CORROSION. ANYSOCKET WITH EVIDENCE OF CORRODED CONTACT SHALL BEREPLACED.

(1) Loosen dust and grit from electrical parts with a soft brush and compressed air.

(2) Clean electrical components with a clean, lint-free cloth or bristle brush andAliphatic Naphtha.

(3) Allow to air dry.

(4) Blow loosened dirt from all parts with moderately-compressed air (not to exceed25 psig).

(5) Wipe all accessible areas with a clean, lint-free cloth dampened with Rho-clene orsimilar cleaning agent.

(6) Allow parts to dry completely after using cleaner.

D. Structure Assembly

Page 14004


Aug 31/200325-34-93

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.

Page 14005


25-34-93 Aug 31/2003Page 14006



Aug 31/200325-34-93 Page 15001

1. Storage Instructions

A. The galley 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


25-34-93 Aug 31/2003


Page 15002

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