CMM 29-11-69

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Honeywell International Inc. Yeovil, Somerset, BA20 2YD

United Kingdom CAGE: U1605 / U1585

Telephone: +1 (800) 601-3099 (U.S.A.) Telephone: +1 (602) 365-3099 (International)

LETTER OF TRANSMITTAL for

REVISION No. 5

COMPONENT MAINTENANCE MANUAL PUBLICATION No. 2771

HYDRAULIC FILTER MANIFOLD SYSTEM 1 AND 2 PART No. 2346H000-002, 2346H000-003, 2346H000-004

2346H000-005 and 2346H000-006 This revision obeys British Civil Airworthiness

Requirements, Section A, Chapter A5-3

Signed ... 31 Aug 2007

Date ... HONEYWELL AEROSPACE YEOVIL UK

NOTE: In this revision, vertical black lines or the letter ‘R’ in the left-hand margin identify changes, additions or deletions. Vertical black lines alongside the page number and date, however indicate that the text/illustration has not been revised but has merely been relocated. Non-technical changes, made only to improve readability, are not specifically identified.

REVISION HIGHLIGHTS

Action Reasons for

Remove Insert Revision

TP1; T2; ROR-1; LEP 1 to 4 inclusive; Intro 3 and 4; Pages 1001, 1002, 1015, 1016, 10017 and 10018.

Manual Revised to incorporate references to ACMM 29-10-01. RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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REVISION RECORD

Action Reason

Transfer previous revision information from the existing Record of Revisions page and record the incorporation of this revision on the Record of Revisions page.

Retain this Letter of Transmittal. This certifies compliance with

Section A, Chapter A5-3 of British Civil Airworthiness Requirements.

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Component Maintenance Manual

With Illustrated Parts List

HYDRAULIC FILTER MANIFOLD, SYSTEM 1 AND 2

PART No. 2346H000-002, 2346H000-003,

2346H000-004, 2346H000-005 AND 2346H000-006

Publication No. 2771

This manual obeys British Civil Airworthiness Requirements, Section A, Chapter A5-3

Signed ... 31 Aug 2007

Date ...

NOTE: This approval cannot be used for changes put in this manual which are not approved by the Equipment Manufacturer. Changes made by other authorities must each be approved by that authority and a record made on other record sheets.

This document contains technical data and is subject to U.S. and U.K. export regulations. These commodities, technology, or software were exported from the United States or United Kingdom in accordance with the

export administration regulations. Diversion contrary to U.S. or U.K. law is prohibited. RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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TITLE PAGE

Component Maintenance Manual

With Illustrated Parts List

HYDRAULIC FILTER MANIFOLD, SYSTEM 1 AND 2

PART No. 2346H000-002, 2346H000-003,

2346H000-004, 2346H000-005 AND 2346H000-006

Honeywell Aerospace Yeovil

COPYRIGHT: JUNE 2007 HONEYWELL AEROSPACE YEOVIL

EQUIPMENT DESIGNED AND MANUFACTURED BY HONEYWELL AEROSPACE YEOVIL IS PROTECTED BY BRITISH AND FOREIGN PATENTS. ALL BUSINESS IS GOVERNED BY THE COMPANY’S STANDARD CONDITIONS; COPIES AVAILABLE ON REQUEST. PRINTED AND PUBLISHED BY HONEYWELL AEROSPACE YEOVIL, SOMERSET, ENGLAND.

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Honeywell - Confidential

THIS COPYRIGHTED WORK AND ALL INFORMATION ARE THE PROPERTY OF HONEYWELL INTERNATIONAL INC., CONTAIN TRADE SECRETS AND MAY NOT, IN WHOLE OR IN PART, BE USED, DUPLICATED, OR DISCLOSED FOR ANY PURPOSE WITHOUT PRIOR WRITTEN PERMISSION OF HONEYWELL INTERNATIONAL INC. ALL RIGHTS RESERVED.

THIS DOCUMENT AND ALL INFORMATION AND EXPRESSION CONTAINED HEREIN ARE THE PROPERTY OF HONEYWELL INTERNATIONAL INC., ARE PROVIDED IN CONFIDENCE, AND MAY BE USED BY PERSONS REQUIRED BY FEDERAL AVIATION REGULATION PART 21.50 TO COMPLY WITH ANY OF THE TERMS OF THESE INSTRUCTIONS. EXCEPT AS SET FORTH ABOVE, NO PERSON MAY, IN WHOLE OR IN PART, USE, DUPLICATE OR DISCLOSE THIS INFORMATION FOR ANY PURPOSE WITHOUT THE PRIOR WRITTEN PERMISSION OF HONEYWELL INTERNATIONAL INC.

Copyright - Notice

Honeywell is a registered trademark of Honeywell International Inc. All other marks are owned by their respective companies.

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COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

RECORD OF REVISIONS

Keep this record in the front of this document. When a revision is received:

(1) Remove the superseded pages from this document and discard.

(2) Put the revised pages into this document.

(3) Record the revision number, issue date, insertion date and incorporator’s initials.

INSERTED INSERTED REV No. ISSUE DATE DATE BY REV No. ISSUE DATE DATE BY 0 Oct 1/2001 HAY 1 Aug 26/2003 2 Aug 1/2004 3 Mar 17/06 4 Dec 13/06 5 Jun 12/07

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

RECORD OF TEMPORARY REVISIONS

Keep this record in the front of this document. When a temporary revision is received:

(1) Put the temporary revision page(s) into this document.

(2) Record the temporary revision (TR) number, issue date, insertion date, incorporator’s initials and page number.

When a permanent revision is received:

(1) Remove the temporary revision page(s) and put the permanent revision into this document.

(2) Record the removal date and remover’s initials.

INSERTED REMOVED

TEMP REV No.

ISSUE

DATE DATE BY DATE BY PAGE No.

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

SERVICE BULLETIN LIST

Keep this record in the front of this document. This list provides the following:

(1) Service bulletin number, service bulletin revision number, service bulletin incorporation date and subject title.

(2) When a service bulletin does not have an effect on the CMM, the words “No Effect” are shown in the service bulletin incorporation date column.

SERVICE BULLETIN NUMBER SERVICE BULLETIN REVISION NUMBER SERVICE BULLETIN INCORPORATION DATE SUBJECT TITLE

29-29 1 Aug 1/2004 Replacement of Pressure Transducer

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

LIST OF EFFECTIVE PAGES

SUBJECT PAGE DATE

Title Page TP-1 * Jun 12/07

T-2 * Jun 12/07

Record of Revisions ROR-1 * Jun 12/07

Record of Temporary Revisions RTR-1 Aug 1/2004

Service Bulletin List SBL-1 Aug 1/2004

List of Effective Pages LEP-1 * Jun 12/07

LEP-2 * Jun 12/07

LEP-3 Dec 13/06

LEP-4 * Jun 12/07

Table of Contents TOC-1 Aug 1/2004

TOC-2 Aug 1/2004

Introduction Intro-1 Aug 1/2004

Intro-2 Aug 1/2004

Intro-3 * Jun 12/07

Intro-4 * Jun 12/07

Intro-5 Mar 17/06

Intro-6 Dec 13/06

Description and Operation 1 Aug 1/2004

2 Aug 1/2004 3 Aug 1/2004 4 Aug 1/2004 5 Aug 1/2004 6 Aug 1/2004 7 Aug 1/2004 8 Aug 1/2004 9 Aug 1/2004 10 Blank

Testing and Fault Isolation 1001 * Jun 12/07

1002 Aug 1/2004

1003 Aug 1/2004

* Indicates pages added or changed

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1004 Aug 1/2004 1005 Aug 1/2004 1006 Aug 1/2004 1007 Aug 1/2004 1008 Aug 1/2004 1009 Aug 1/2004 1010 Aug 1/2004 1011 Aug 1/2004 1012 Aug 1/2004 1013 Aug 1/2004 1014 Aug 1/2004 1015 * Jun 12/07 1016 Aug 1/2004 1017 Aug 1/2004 1018 Aug 1/2004 1019 Aug 1/2004 1020 Blank Disassembly 3001 Aug 1/2004 3002 Aug 1/2004 3003 Aug 1/2004 3004 Aug 1/2004 3005 Aug 1/2004 3006 Aug 1/2004 3007 Aug 1/2004 3008 Blank Cleaning 4001 Aug 1/2004 4002 Aug 1/2004 Check 5001 Aug 1/2004 5002 Aug 1/2004 Repair 6001 Aug 1/2004 6002 Mar 17/06

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

6003 Aug 1/2004 6004 Aug 1/2004 6005 Aug 1/2004 6006 Blank Assembly 7001 Mar 17/06 7002 Mar 17/06 7003 Aug 1/2004 7004 Aug 1/2004 7005 Aug 1/2004 7006 Aug 1/2004 7007 Aug 1/2004 7008 Aug 1/2004 7009 Aug 1/2004 7010 Aug 1/2004 7011 Aug 1/2004 7012 Aug 1/2004

Fits and Clearances 8001 Aug 1/2004

8002 Mar 17/06

Special Tools, Fixtures and Equipment 9001 Mar 17/06

9002 Aug 1/2004 9003 Aug 1/2004 9004 Aug 1/2004 9005 Mar 17/06 9006 Aug 1/2004 Storage 15001 Aug 1/2004 15002 Aug 1/2004 15003 Aug 1/2004 15004 Blank

Illustrated Parts List 10001 Aug 1/2004

10002 Aug 1/2004

10003 Aug 1/2004

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10004 Aug 1/2004 10005 Aug 1/2004 10006 Aug 1/2004 10007 Aug 1/2004 10008 Aug 1/2004 10009 Dec 13/06 10010 Dec 13/06 10011 Dec 13/06 10012 Dec 13/06 10013 Dec 13/06 10014 Dec 13/06 10015 Dec 13/06 10016 Dec 13/06 10017 * Jun 12/07 10018 * Jun 12/07

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

LIST OF ILLUSTRATIONS

SUBJECT PAGE

Introduction... Intro-1

Description and Operation... 1

Testing and Fault Isolation ... 1001

Schematics and Wiring Diagrams ... 2001 (Not applicable) Disassembly ... 3001

Cleaning ... 4001

Check ... 5001

Repair... 6001

Assembly... 7001

Fits and Clearances ... 8001

Special Tools, Fixtures and Equipment... 9001

Special Procedures ... 11001 (Not applicable) Removal ... 12001 (Not applicable) Installation ... 13001 (Not applicable) Servicing... 14001 (Not applicable) Storage... 15001

Rework ... 16001 (Not applicable) Illustrated Parts List... 10001

FIGURE TITLE PAGE 1 Hydraulic Filter Manifold, System 1 and 2 (Sheet 1 of 3) ... 5

1 Hydraulic Filter Manifold, System 1 and 2 (Sheet 2 of 3) ... 6

1 Hydraulic Filter Manifold, System 1 and 2 (Sheet 3 of 3) ... 7

2 Schematic Diagram (Sheet 1 of 1) ... 8

3 Pressure Switch Circuit Diagram (Sheet 1 of 1)... 9

4 Pressure Transducer Circuit Diagram (Sheet 1 of 1) ... 9

1001 Manifold Bleed Circuit (Sheet 1 of 1) ... 1016

1002 Return Bypass Valve and Shim (Sheet 1 of 1)... 1017

1003 Non-return Valve (2304H070) Test Circuit (Sheet 1 of 1) ... 1018

1004 Non-return Valve (2346H180) Test Circuit (Sheet 1 of 1) ... 1019

IPL Figure 1 Hydraulic Filter Manifold, System 1 and 2 (Sheet 1 of 3) ... 10006

IPL Figure 1 Hydraulic Filter Manifold, System 1 and 2 (Sheet 2 of 3) ... 10007

IPL Figure 1 Hydraulic Filter Manifold, System 1 and 2 (Sheet 3 of 3) ... 10008 RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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LIST OF TABLES

TABLE TITLE PAGE

Intro-1 List of Related Publications... Intro-3

1001 Test Equipment...1002

1002 Test Materials ...1004

1003 Fault Isolation...1014

3001 Special Tools and Equipment ...3001

4001 Cleaning Materials ...4001

6001 Approved Repairs ...6001

6002 Special Tools and Equipment for Repair ...6001

6003 Repair Materials...6002

7001 Replacement Parts ...7001

7002 Assembly Materials...7003

7003 Special Tools and Equipment for Assembly ...7003

8001 Run-down Torque Values ...8001

8002 Torque Values...8002

9001 Special Tools, Fixtures and Equipment ...9001

9002 Materials ...9005

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 INTRODUCTION

TASK-29-11-69-99F-801-A01

1. General

A. This CMM is prepared in accordance with Air Transport Association (ATA) iSpec 2200. In accordance with this specification, the CMM is divided into the Sections given in the Table of Contents.

B. Refer to the Table of Contents for the page locations of the Sections of this CMM. TASK-29-11-69-99F-802-A01

2. Manual Use

A. The instructions in this CMM are arranged so that the operator can overhaul the assembly removed from service and, by use of the recommended procedures, make the unit

serviceable.

B. All weights and measures given in this CMM are in SI units with the equivalent imperial units in parenthesis.

TASK-29-11-69-99F-803-A01

3. Maintenance Task Oriented Support System

A. A Maintenance Task Oriented Support System (MTOSS) is used for Electronic Data Processing of the Maintenance Data in this CMM.

NOTE: For more data on MTOSS, refer to CMM Section 2-5-3 in ATA iSpec 2200.

B. An MTOSS number has seven elements. The first five elements must be used for each Task and Subtask. The sixth and seventh elements are used when necessary. This CMM uses six of the seven elements. These elements are used as follows:

(1) Element No. 1, 2 and 3 are the Chapter, Section and Subject numbers (29-11-69 for this CMM).

(2) Element No. 4 shows the maintenance function of the Task or Subtask.

NOTE: For more data on maintenance function codes, refer to CMM Section 2-5-3 in ATA iSpec 2200.

(a) Maintenance function code 990 is expanded as follows in this CMM: 1 99A is used to identify tables

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3 99C is used to identify front matter for Page Blocks or Tasks 4 99D is used to identify access

5 99E is used to identify references

6 99F is used to identify general/introduction

(b) Maintenance function code 940 is expanded as follows in this CMM: 1 94A is used to identify consumables and materials

2 94B is used to identify tools, fixtures and equipment

(3) Element No. 5 is used to make the Task or Subtask number different from other Tasks or Subtasks which have the same first four elements:

(a) Tasks are numbered from 801 thru 999.

(b) Subtasks are numbered from 001 thru 800.

(4) Element No. 6 is a three position alpha-numeric code which identifies differences in configurations or procedures or standard practices, etc.

(a) Most Tasks in this CMM will use “A01” as the sixth element. This shows that the Task is used for all configurations with no differences.

(b) If the sixth element is “S01”, it shows that a Service Bulletin is related to the Task. (5) Element No. 7 is a three position alpha-numeric code for customer use.

TASK-29-11-69-99F-804-A01

4. Warnings and Cautions

A. WARNINGS given in this CMM identify potential hazards which could cause injury to personnel. Use the material manufacturers warnings if they are different from those given in this CMM.

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 TASK-29-11-69-99F-805-A01

5. Statement of Verification

The disassembly, assembly and testing and fault isolation procedures given in this CMM have been verified by simulation.

TASK-29-11-69-99F-806-A01 6. Part Identification

A. The identification of detail parts is by reference to the item numbers shown in the Illustrated Parts List (IPL).

B. Alpha variants of IPL item numbers are not shown in the text or on illustrations unless different procedures are necessary.

TASK-29-11-69-99F-807-A01 7. List of Publications

Related publications that are referred to in this CMM are shown in Table Intro-1 (Refer to Table Intro-1 “TABLE-29-11-69-99A-801-A01”).

TABLE-29-11-69-99A-801-A01

List of Related Publications—Table Intro-1

TASK-29-11-69-99F-808-A01

8. Abbreviations

The abbreviations that follow are used throughout this publication:

Document Publication No.

Chromate Conversion Coatings for Aluminium and Aluminium Alloys

NGPS 30

Ultrasonic Cleaning NGPS 151

Cleaning of Metal Surfaces NGPS 256

Pressure Transducer - Part No 2329H100 (IPL1-700) ACMM 29-10-01

List of Related Publications — Table Intro-1

ACMP AC Motor Pump

A Ampere

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AR As required

°C Degrees Celsius

dia Diameter

DOI Drawing office instruction

DPI Differential pressure indicator

EDP Engine Driven Pump

°F Degrees Fahrenheit

Fig Figure

g Gram

HAY Honeywell Aerospace Yeovil

in Inches

in Hg Inch mercury

IPL Illustrated Parts List

kg Kilogrammes

l/min Litres per minute

lb Pounds

lbf.in Pounds force inch(es) (for torque values)

mA MilliAmpere

ml/min Millilitre per minute

mm Millimetres

Mod Modification

MTOSS Maintenance Task Oriented Support System

NGPS Normalair-Garrett Process Specification

N.m Newton-metre(s)

No. Number

NRV Non-return valve

oz Ounce

para Paragraph

psi Pounds per square inch

psid Pounds per square inch differential

psig Pounds per square inch gauge

REV Revision

RF Reference

TR Temporary revision

US gpm United States gallons per minute

V Vendor

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 TASK-29-11-69-99F-809-A01

9. Process Specifications

A. Cross-references to Normalair-Garrett Process Specifications (NGPSs) can be made in this publication.

B. User/holding organizations that are approved by HAY can get access to NGPSs through the internet if they have a password.

C. Passwords are unique and will only be given to approved user/holding organizations. Passwords are available from:

Honeywell Aerospace Yeovil Product Support Engineering Mail Box 702

Bunford Lane Yeovil BA20 2YD UK

For the attention of S Imrie

NOTE: Before you apply, make sure that your organization does not already have a password.

D. All NGPSs are covered by HAY copyright. The use of the data must be strictly in accordance with the referenced agreement. Password security and confidentiality must not be

compromised.

TASK-29-11-69-99F-810-A01 10. Publications

Cross-references can be made in this publication to Honeywell Aerospace Publications. Copies of these publications are available from:

Honeywell Aerospace Yeovil Product Support Engineering Mail Box 702

Bunford Lane Yeovil BA20 2YD UK

Tel: +44 (0) 1935 446729 Fax: +44 (0) 1935 446581

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TASK-29-11-69-99F-811-A01

11. Technical Queries and Comments

All queries, comments or observations relating to the content of this CMM should be sent to the Technical Documentation Manager at the address above.

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 DESCRIPTION AND OPERATION

TASK-29-11-69-99C-801-A01

1. General

A. The system 1 and 2 hydraulic filter manifold is used to filter the supply hydraulic fluid from the aircraft pumps and ground power.

B. A general view of the system 1 and 2 hydraulic filter manifold is shown in Figure 1 (Refer to Figure 1 “GRAPHIC-29-11-69-99B-801-A01”).

C. A schematic diagram of the system 1 and 2 hydraulic filter manifold is shown in Figure 2 (Refer to Figure 2 “GRAPHIC-29-11-69-99B-802-A01”).

D. A circuit diagram of the pressure switch is shown in Figure 3 (Refer to Figure 3 “GRAPHIC-29-11-69-99B-803-A01”).

E. A circuit diagram of the pressure transducer is shown in Figure 4 (Refer to Figure 4 “GRAPHIC-29-11-69-99B-804-A01”).

TASK-29-11-69-870-801-A01 2. Description

A. The primary component of the hydraulic filter manifold is a high strength aluminium forging, to which the filters and the other components are attached.

B. There are three filters, pressure, return and case drain. The filter bowls are attached to the manifold by threads and are held when tightened by locking devices that engage with serrations on the filter bowl outer diameters. The locking devices prevent the filter bowls from becoming loose during operation. The filter bowls are made to be removed and replaced by hand, a knurled surface is used as an aid.

C. The pressure and return filter elements filter the hydraulic fluid to 5 microns absolute. The case drain filter element filters the hydraulic fluid to 15 microns absolute. When the filter elements become blocked, they cannot be cleaned or used again, they must be discarded. D. Each filter port in the manifold contains a shut-off valve. The shut-off valve is a spring loaded

mechanism which prevents leakage of the hydraulic fluid from the manifold when the filter bowl is removed to replace a filter element. During operation, the shut-off valve is held open by the filter element. When the filter bowl and the element are removed, the shut-off valve is closed by a spring.

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E. The condition of the filter elements is shown by three differential pressure indicators (DPI). The three DPIs are the same. Each DPI is attached to the manifold by four screws and a clamp ring and is sealed by ‘O’ ring seals and back-up rings. The DPI gives an indication of increasing differential pressure across the filter element because of an impending blockage. At a set pressure, a red ‘pop-up button’ is operated and shows that the related filter element must be replaced as soon as possible. Each DPI includes a thermal cut-out device. This prevents operation of the DPI at low temperatures when the viscosity of the hydraulic fluid is high.

F. A bypass relief valve is installed in the manifold and operates when the return filter element is blocked. This prevents there from being too much pressure in the return line.

G. The engine driven pump (EDP) pressure inlet contains a check valve. A pressure switch adjacent to the EDP pressure inlet gives an electronic indication when the pressure reaches 16548 kPa (2400 psi).

H. The AC motor pump (ACMP) pressure inlet contains a check valve. A pressure switch adjacent to the ACMP pressure inlet gives an electronic indication when the pressure reaches 16548 kPa (2400 psi).

I. A pressure transducer is installed in the manifold. This gives an electronic indication of the hydraulic fluid pressure at the pressure outlet.

J. A system pressure relief valve is installed in the manifold between the pressure line and the return line. If there is too much pressure in the pressure line, the relief valve operates and decreases the pressure through the return line.

K. The manifold also includes all the necessary unions for connection to the aircraft hydraulic system.

L. 2346H000-003 introduces filter kits that incorporate a new shut-off valve piston. M. 2346H000-004 introduces a new manifold with revised positions for Ground Service

Pressure Fitting and ACMP Pressure switch.

N. 2346H000-005 introduces a filter kit that includes a new pressure filter bowl.

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 TASK-29-11-69-870-802-A01

3. Operation

A. The hydraulic fluid in the aircraft pumps and ground power systems is filtered to 5 microns absolute by the pressure and return filters. The hydraulic fluid which goes through the case drain filter is filtered to 15 microns absolute. The condition of the filters is shown by the differential pressure indicators installed adjacent to the filters.

B. If there is too much pressure in the pressure line, the system pressure relief valve operates and the hydraulic fluid goes into the return line.

C. If the return filter element becomes blocked, the return bypass relief valve operates and the hydraulic fluid goes into the return line.

D. Non-return valves prevent flow in the opposite direction through the pressure lines. TASK-29-11-69-870-803-A01

4. Data

Hydraulic Fluid ... Phosphate Ester to AS1241 type IV and V Pressure Line Operating Pressure... 20685 kPag (3000 psig) nominal Return Line Operating Pressure ... 496 kPag (72 psig) nominal Case Drain Line Operating Pressure ... 1034 kPag (150 psig) nominal Fluid Operating Temperature...-40 to 135°C (-40 to 275°F) Mounting ... Four holes 8,18 to 8,35 mm (0.322 to 0.329 in) dia Pressure Switch Connectors...D38999/25YA35XN Pressure Transducer Connector...D38999/25YB98PN Voltage...18 to 29 VDC Current (at 29 VDC) ... 0.030 A maximum EDP Pressure Inlet Connection ... MS33514E12 ACMP Pressure Inlet Connection ... MS33514E06 Pressure Outlet Connection... MS33514E10 Ground Service Pressure Connection ... MS33514E6

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Return Inlet Connection ...MS33514E12 Reservoir Fill Connection...MS33514E4 Return Outlet Connection ...MS33514E10 Case Drain Inlet Connection...MS33514E6 Case Drain Outlet Connection ...MS33514E6 DPI Setting ... 414 to 552 kPad (60 to 80 psid) DPI Thermal Cut-out Setting... 10 to 27°C (50 to 80°F) Return Bypass Valve Open Setting ...621 kPad (90 psid) minimum Return Bypass Valve Closed Setting...448 kPad (65 psid) minimum System Relief Valve Open Setting... 23443 to 24133 kPad (3400 to 3500 psid) System Relief Valve Closed Setting ...22409 kPad (3250 psid) minimum Height ... (2346H000-002 and 2346H000-003) 331,9 mm (13.06 in) (2346H000-004, 2346H000-005 and 2346H000-006) 360,3 mm (14.18 in) Width ... (2346H000-002 and 2346H000-003) approx 180,2 mm (7.09 in) (2346H000-004, 2346H000-005 and 2346H000-006) approx 201,0 mm (7.91 in) Length... approx 249,0 mm (9.80 in)

Weight (2346H000-002, 2346H000-003 and 2346H000-004) 7,1 kg (15.65 lb)

(2346H000-005) 7,25 kg (15.98 lb) (2346H000-006) 7,4 kg (16.31 lb)

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

GRAPHIC-29-11-69-99B-801-A01

Hydraulic Filter Manifold, System 1 and 2 (Sheet 1 of 3) RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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GRAPHIC-29-11-69-99B-801-A01

Hydraulic Filter Manifold, System 1 and 2 (Sheet 2 of 3) Figure 1

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

GRAPHIC-29-11-69-99B-801-A01

Hydraulic Filter Manifold, System 1 and 2 (Sheet 3 of 3) RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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GRAPHIC-29-11-69-99B-802-A01

Schematic Diagram (Sheet 1 of 1) Figure 2

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

GRAPHIC-29-11-69-99B-803-A01

Pressure Switch Circuit Diagram (Sheet 1 of 1) Figure 3

GRAPHIC-29-11-69-99B-804-A01

Pressure Transducer Circuit Diagram (Sheet 1 of 1) RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 TESTING AND FAULT ISOLATION

TASK-29-11-69-99C-802-A01

1. General

A. Unless specified differently, do these tests in the sequence given and at these conditions: (1) Temperature: room ambient, 21 ± 10°C (70 ± 18°F).

(2) Atmospheric pressure: normal ground, 724 ± 51 mm Hg (28.5 ± 2.0 in Hg). (3) Relative humidity: 50 ± 30%.

WARNING: HYDRAULIC FLUID CAN BE DANGEROUS TO PERSONS. KEEP AWAY FROM SOURCES OF IGNITION. PREVENT SKIN CONTACT AND PUT ON EYE PROTECTION.

CAUTION: DURING REMOVAL OF THE FILTER BOWLS OR WHEN ANY FILTER BOWL IS REMOVED, THE HYDRAULIC MANIFOLD MUST NOT BE PRESSURIZED TO MORE THAN 690 kPa (100 psig). FAILURE TO OBSERVE THIS CAUTION CAN RESULT IN DAMAGE TO THE FILTER SHUT-OFF VALVE MECHANISM. B. The test fluid must be clean to NAS1638, Class 5 or better.

C. Unless specified differently, the temperature of the test fluid must be 30 ± 10°C (86 ± 18°F) during the tests.

D. If a tolerance is not given in the procedure, the tolerances that follow must be used: (1) Pressure: ± 5% or 3,4 kPag (0.5 psig). Use the largest tolerance.

(2) Temperature: ± 2.5°C (5°F).

(3) Flow: ± 0,38 l/min (0.1 US gpm) for flows of more than 7,61 l/min (2 US gpm) or ± 5% for flows of less than 7,61 l/min (2 US gpm).

E. If the results of a test are unsatisfactory, refer to Fault Isolation to find the possible cause and recommended procedure for correction.

F. During all tests, all connections must have blanks installed unless specified differently. G. All item numbers relate to IPL Figure 1.

H. Refer to ACMM 29-12-01 to test pressure transducer 2329H100 (IPL 1-700). RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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TASK-29-11-69-94B-801-A01

2. Test Equipment

The test equipment given in Table 1001 is necessary for the tests given in this Section (Refer to Table 1001 “TABLE-29-11-69-99A-802-A01”).

TABLE-29-11-69-99A-802-A01 Test Equipment—Table 1001 NOTE: Equivalent alternatives can be used for these items.

NOMENCLATURE PART No./TYPE USE

Flexible hoses - Figure 1001 (Refer to Figure 1001

“GRAPHIC-29-11-69-99B-805-A01”)

Shut-off valves (quantity 8) - Figure 1001 (Refer to Figure 1001

“GRAPHIC-29-11-69-99B-805-A01”) and Figure 1003 (Refer to Figure 1003 “GRAPHIC-29-11-69-99B-806-A01”)

Connection blanks - Figure 1001 (Refer to Figure 1001

“GRAPHIC-29-11-69-99B-805-A01”) Pressure gauge,

0 to 31028 kPa (0 to 4500 psi)

- Figure 1001 (Refer to Figure 1001

“GRAPHIC-29-11-69-99B-805-A01”)

Drip spouts (quantity 3) - Figure 1001 (Refer to Figure 1001

“GRAPHIC-29-11-69-99B-805-A01”) Pressure/return filter

element blank

5688K000 Pressure and return line tests

Case drain filter element blank

5689K000 Case drain line tests

Flowmeter, 0 to 75 l/min (0 to 20 US gpm)

- Main assembly flow tests

Differential pressure gauge, 0 to 2000 kPad (0 to 290 psid)

- Differential pressure measurement

Dynamic pressure supply, 0 to 31028 kPa (0 to 4500 psi) at flows up to 72 l/min (19 US gpm)

- Pressure supply for all tests

Hand pump supply

0 to 31028 kPa (0 to 4500 psi)

- Pressure supply for main assembly

leak tests

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

TASK-29-11-69-94A-801-A01 3. Materials

The materials necessary for testing are shown in Table 1002 (Refer to Table 1002 “TABLE-29-11-69-99A-803-A01”).

Filter, 3 micron. Installed in the pressure supply line, upstream of the manifold assembly

- Removal of contamination

Voltmeter - Pressure transducer test

Low resistance ohmmeter - Bonding test

Test fixture 5697K000 Figure 1003 (Refer to Figure 1003

“GRAPHIC-29-11-69-99B-806-A01”) Pressure gauge, 0 to

35000 kPa (0 to 5000 psi)

“GRAPHIC-29-11-69-99B-806-A01”) Pressure gauges, 0 to 750

kPa (0 to 100 psi) (quantity 2)

“GRAPHIC-29-11-69-99B-806-A01”)

Pressure gauge, 0 to 100 kPa (0 to 10 psi)

“GRAPHIC-29-11-69-99B-806-A01”) Flowmeter, 0 to 100 l/min

(0 to 20 US gpm)

“GRAPHIC-29-11-69-99B-806-A01”)

Test fixture TBD Differential pressure indicator tests

Test fixture 5747K000-001 Figure 1004 (Refer to Figure 1004

“GRAPHIC-29-11-69-99B-809-A01”) NOTE: Equivalent alternatives can be used for these items.

Test Equipment (Sheet 2 of 2)—Table 1001 RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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TABLE-29-11-69-99A-803-A01 Test Materials—Table 1002

TASK-29-11-69-700-801-A01

4. Main Assembly Test Procedure

SUBTASK-29-11-69-790-001-A01

A. Manifold Bleed and Filter Shut-off Valves Leakage

(1) Connect a pressure supply to the manifold and attach drip spouts as shown in Figure 1001 (Refer to Figure 1001 “GRAPHIC-29-11-69-99B-805-A01”).

(2) Apply a pressure of 690 kPag (100 psig) to the manifold, and bleed all air from the unit through the drip spouts.

(3) Decrease the pressure to zero and replace the drip spouts with the pressure supply. (4) Apply a pressure of 207 kPag (30 psig) to all six connections at the same time. (5) Remove all three filter bowls and filter elements as given in DISASSEMBLY. (6) Increase the pressure to 690 kPag (100 psig). Remove any fluid from the lower

surface of each filter housing head.

(7) During a 2 minute period make sure that there is no leakage from each shut-off valve head.

(8) Decrease the pressure to zero. Install the pressure filter element and bowl on the manifold as given in ASSEMBLY and remove the test equipment.

SUBTASK-29-11-69-790-002-A01

B. Return Bypass Valve

(1) Install a return filter element blank and the return filter bowl on the manifold. NOTE: Equivalent alternatives can be used for these items.

NOMENCLATURE PART No./TYPE SUPPLIER

Test fluid, phosphate ester hydraulic fluid

AS1241 Type IV Class I (Skydrol LD IV)

Commercially available

Cloth (must not contain lint) DEF1410 Commercially available

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 (2) Increase the pressure at the Return Inlet connection until the return bypass valve

opens. This is shown by a flow of more than 8 ml/min (0.002 US gpm) at the Return Outlet connection. The inlet pressure must be 621 to 759 kPag (90 to 110.1 psig) minimum. If the inlet pressure cannot be obtained, a shim (IPL Figure 1, item 745) can be installed on the Return Bypass Valve as shown in Figure 1002 (Refer to Figure 1002 “GRAPHIC-29-11-69-99B-808-A01”).

NOTE: The shim (IPL Figure 1, item 745) will increase the inlet pressure by 39,3 kPag (5.7 psig). The shim has layers of 0,076 mm (0.0029 in). The removal of a layer decreases the inlet pressure by 2,9 kPag (0.43 psig).

(3) Increase the pressure at the Return Inlet connection to get a flow of 68,1 l/min. (18 US gpm). The pressure drop between the Return Inlet connection and the Return Outlet connection must not be more than 1551 kPad (225 psid).

(4) Slowly decrease the pressure until the return bypass valve closes. This is shown by a flow of less than 4 ml/min (0.001 US gpm) at the Return Outlet connection. The inlet pressure must be 448 kPag (65 psig) minimum.

(5) If necessary, decrease the pressure to 448 kPag (65 psig). Make sure that the leakage from the Return Outlet connection, in the third minute of a three minute test, is not more than 4 ml/min (0.001 US gpm).

(6) Decrease the pressure to zero. Remove the test equipment and install the return and case drain filter elements and bowls as given in ASSEMBLY.

SUBTASK-29-11-69-780-001-A01

C. Proof Pressure Test

(1) Connect the pressure supply to the EDP Pressure Inlet, ACMP Pressure Inlet and Ground Service Pressure connections.

(2) Connect the hand pump supply to the Reservoir Fill connection.

(3) Increase the pressure at the EDP Pressure Inlet, ACMP Pressure Inlet and Ground Service Pressure connections to 20685 kPag (3000 psig).

(4) Increase the pressure at the Reservoir Fill connection to 20685 kpag (3000 psig). (5) Increase the pressure at the EDP Pressure Inlet, ACMP Pressure Inlet and Ground

Service Pressure connections to 31028 kPag (4500 psig). Make sure that the pressure at the Reservoir Fill connection does not increase to more than 20685 kPag (3000 psig).

(6) Keep the pressures applied for 3 minutes then decrease the pressure at the EDP Pressure Inlet, ACMP Pressure Inlet and Ground Service Pressure connections to 20685 kpag (3000 psig).

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(7) Decrease the pressure at the Reservoir Fill connection to zero then decrease the pressure at the EDP Pressure Inlet, ACMP Pressure Inlet and Ground Service Pressure connections to zero.

(8) Visually examine the unit for external leakage and deformation. There must be no external leakage or deformation.

(9) Disconnect the pressure supply and hand pump supply.

(10) Connect the pressure supply to the Case Drain Inlet connection.

(11) Increase the pressure at the Case Drain Inlet connection to 3448 kPag (500 psig). Keep the pressure applied for 3 minutes then decrease the pressure to zero. (12) Visually examine the unit for external leakage and deformation. There must be no

external leakage or deformation.

(13) Disconnect the test equipment from the unit. SUBTASK-29-11-69-790-003-A01

D. System Pressure Relief Valve

(1) Connect the pressure supply to the Ground Service Pressure connection.

(2) Increase the pressure at the Ground Service Pressure connection until the flow at the Return Outlet connection increases to more than 20 ml/min (0.005 US gpm). The pressure must not be more than 24822 kPag (3600 psig).

(3) Increase the pressure at the Ground Service Pressure connection until the flow at the Return Outlet connection is 37,9 l/min (10 US gpm).

(4) Decrease the pressure to 20685 kPag (3000 psig). Make sure that the leakage from the Return Outlet connection, in the third minute of a three minute test, is not more than 4 ml/min (0.001 US gpm).

(5) Decrease the pressure to zero and remove the test equipment. SUBTASK-29-11-69-780-002-A01

E. Pressure Switches

NOTE: These tests must be done on each pressure switch (500 and 590).

(1) Connect a drip spout to the Ground Service Pressure connection and bleed all pressure from the unit.

(2) Connect the pressure supply to the EDP Pressure Inlet and ACMP Pressure Inlet connections.

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 (3) With the system pressure at zero make sure there is continuity between pins 1 and 2

and pins 4 and 5. Also make sure there is no continuity between pins 2 and 3 and pins 5 and 6.

(4) Slowly increase pressure at the EDP Pressure Inlet and ACMP Pressure Inlet connections to 16548 kPag (2400 psig).

(5) Make sure there is continuity between pins 2 and 3 and pins 5 and 6. Also make sure there is no continuity between pins 1 and 2 and pins 4 and 5.

(6) Decrease the pressure to zero and bleed all pressure through the Ground Service Pressure connection.

(7) Disconnect the test equipment from the unit. SUBTASK-29-11-69-750-001-A01

F. Pressure Transducer

(1) Connect the pressure supply to the Ground Service Pressure connection. (2) Apply a voltage of 18 to 29 VDC to pins C and D of the pressure transducer. (3) Apply a pressure of 20685 kPag (3000 psig) to the Ground Service Pressure

connection.

(4) Use the voltmeter to measure the output across pins A and B of the pressure transducer. The voltage must be between 5.32 and 5.68 VDC.

(5) Decrease the pressure to zero and disconnect the test equipment. SUBTASK-29-11-69-750-002-A01

G. Bonding

(1) Measure the bonding resistance between the manifold mounting lug and the points that follow with the ohmmeter set to a test current of 100 ± 20 mA. The resistance must not be more than 1 ohm for each test:

(a) EDP Pressure Inlet connection.

(b) ACMP Pressure Inlet connection.

(c) Pressure Outlet connection.

(d) Ground Service Pressure connection.

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(2) Measure the bonding resistance between the manifold mounting lug and the points that follow with the ohmmeter set to a test current of 100 ± 20 mA. The resistance must not be more than 5 milliohms for each test:

(a) Pressure Transducer connector shell. (b) EDP Pressure Switch connector shell. (c) ACMP Pressure Switch connector shell. TASK-29-11-69-700-802-A01

5. Non-return Valve (2304H070) Test Procedure SUBTASK-29-11-69-99F-001-A01

A. General

(1) Do these tests on the non-return valve (540) at the conditions that follow: (a) Ambient temperature: 23 ± 10°C (73.4 ± 18°F).

(b) Atmospheric pressure: 718 ± 57 mm Hg (28.25 ± 2.25 in Hg). (c) Fluid temperature: 25 ± 5°C (77 ± 9°F).

(2) Install slave ‘O’ ring seals (560 and 580) and back-up rings (550 and 570) on the non-return valve (540) for these tests.

(3) If the results of a test are unsatisfactory, the non-return valve must be replaced. SUBTASK-29-11-69-780-003-A01

B. Proof Pressure Test

(1) Connect the non-return valve to the test circuit shown in Figure 1003 (Refer to Figure 1003 “GRAPHIC-29-11-69-99B-806-A01”).

(2) Close all shut-off valves. (3) Open shut-off valves B and D.

(4) Slowly increase the pressure to 31028 kPag (4500 psig). Keep the pressure applied for 3 minutes and make sure that there is no external leakage or damage caused to the non-return valve. Decrease the pressure to zero.

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 SUBTASK-29-11-69-780-004-A01

C. Pressure Drop Test

(1) Open shut-off valves A, B, D, G and H.

(2) Apply sufficient pressure to get a flow of 90,8 l/min (20 US gpm).

(3) Make sure that the pressure drop across the non-return valve is not more than 138 kPad (20 psid).

(4) Decrease the pressure to zero. (5) Close all shut-off valves. SUBTASK-29-11-69-790-004-A01

D. Leakage Test

(1) Open shut-off valves C and E.

(2) Increase the pressure to 34,5 kPag (5 psig), keep the pressure applied for 2 minutes then measure the leakage from the inlet port during the subsequent 1 minute. The leakage must not be more than 1 drop/minute.

(3) Increase the pressure to 20340 kPag (2950 psig), keep the pressure applied for 2 minutes then check for leakage during the subsequent 1 minute. There must be no leakage.

E. Cracking Test

(1) Open shut-off valves B, D and F.

(2) Slowly increase the pressure until the non-return valve opens. The non-return valve must open at a pressure of 13,8 to 55,2 kPag (2 to 8 psig).

(3) Decrease the pressure to zero. (4) Close all shut-off valves.

(5) Disconnect the non-return valve from the test circuit. RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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TASK-29-11-69-700-805-A01

6. Non-return Valve (2346H180) Test Procedure SUBTASK-29-11-69-99F-004-A01

A. General

(1) Do these tests on the non-return valve (540A) at the conditions that follow: (a) Ambient temperature: 23 ± 10°C (73.4 ± 18°F).

(b) Atmospheric pressure: 692.5 ± 82.5 mm Hg (27.25 ± 3.25 in Hg). (c) Fluid temperature: 25 ± 5°C (77 ± 9°F).

(2) Install slave ‘O’ ring seals (560A and 580A) and back-up rings (550A and 570A) on the non-return valve (540A) for these tests.

(3) If the results of a test are unsatisfactory, the non-return valve must be replaced. SUBTASK-29-11-69-780-010-A01

(1) Connect the non-return valve to the test circuit shown in Figure 1004 (Refer to Figure 1004 “GRAPHIC-29-11-69-99B-809-A01”).

(2) Close all shut-off valves. (3) Open shut-off valves B and D.

(4) Slowly increase the inlet pressure to 31028 kPag (4500 psig). Keep the pressure applied for 3 minutes and make sure that there is no external leakage or damage caused to the non-return valve. Decrease the pressure to zero.

(5) Close all shut-off valves. SUBTASK-29-11-69-780-011-A01

C. Pressure Drop Test

(1) Open shut-off valves A, B, D, G and H.

(2) Apply sufficient pressure to get a flow of 68,2 l/min (18 US gpm) through the non-return valve.

(3) Make sure that the pressure drop across the non-return valve is not more than 207 kPad (30 psid).

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 (4) Decrease the pressure to zero.

(5) Close all shut-off valves. SUBTASK-29-11-69-790-006-A01

D. Leakage Test

(1) Open shut-off valves C and E.

(2) Apply a pressure of 34,5 kPag (5 psig) to the outlet port. Keep the pressure applied for 2 minutes then measure the leakage from the inlet port during the subsequent 1 minute. The leakage must not be more than 1 drop/minute.

(3) Increase the pressure to 20340 kPag (2950 psig), keep the pressure applied for 2 minutes then check for leakage during the subsequent 1 minute. There must be no leakage.

E. Cracking Test

(1) Open shut-off valves B, D and F.

(2) Slowly increase the inlet pressure until the non-return valve opens. The non-return valve must open at a pressure of 13,8 to 55,2 kPag (2 to 8 psig).

(3) Decrease the pressure to zero. (4) Close all shut-off valves.

(5) Disconnect the non-return valve from the test circuit. TASK-29-11-69-700-803-A01

7. Check Valve Test Procedure

SUBTASK-29-11-69-99F-002-A01

A. General

(1) Do these tests on the check valve (610) at a temperature of 32 ± 11°C (90 ± 20°F). (2) If the results of a test are unsatisfactory, the check valve must be replaced.

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SUBTASK-29-11-69-780-006-A01

(1) Connect the pressure supply to the inlet and outlet connections of the check valve. (2) Slowly increase the pressure to 31028 kPag (4500 psig). Keep the pressure applied

for 1 minute and make sure that there is no external leakage or damage caused to the check valve. Decrease the pressure to zero.

(3) Disconnect the check valve from the test equipment.

(4) Manually operate the check valve to make sure that it moves correctly and smoothly. SUBTASK-29-11-69-790-005-A01

C. Leakage Test

(1) Connect the pressure supply to the outlet connection of the check valve.

(2) Increase the pressure to 34,5 kPag (5 psig), keep the pressure applied for 2 minutes then measure the internal leakage during the subsequent 1 minute. The leakage must not be more than 1 drop/minute.

(3) Increase the pressure to 6895 kPag (1000 psig), keep the pressure applied for 2 minutes then do a check for internal leakage during the subsequent 1 minute. There must be no leakage. Decrease the pressure to zero.

(4) Increase the pressure to 20685 kPag (3000 psig), keep the pressure applied for 2 minutes then do a check for internal leakage during the subsequent 1 minute. There must be no leakage. Decrease the pressure to zero.

(5) Disconnect the check valve from the test equipment. SUBTASK-29-11-69-780-007-A01

D. Cracking Pressure Test

(1) Connect the pressure supply to the inlet connection of the check valve.

(2) Connect a tee and a 0 to 100 kPag (0 to 10 psig) pressure gauge to the outlet connection.

(3) Slowly increase the pressure supply until there is a constant flow from the outlet connection. This shows that the valve has opened. The valve must open at a pressure of 517 to 690 kPag (75 to 100 psig).

(4) Decrease the pressure to zero and disconnect the check valve from the test equipment.

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E. Flow Test

(1) Connect the pressure supply to the outlet connection of the check valve with piezometer tubes that are the same size as the valve connections. Connect a flowmeter downstream of the valve.

(2) Slowly increase the pressure until you get a flow rate of 22,71 l/min (6 US gpm). Make sure that the pressure drop across the valve is not more than 965 kpad (140 psid). (3) Slowly increase the pressure until you get a flow rate of 37,85 l/min (10 US gpm). Make

sure that the pressure drop across the valve is not more than 1034 kPad (150 psid). (4) Decrease the pressure to zero and disconnect the check valve from the test

equipment. TASK-29-11-69-700-804-A01

8. Differential Pressure Indicator Test Procedure SUBTASK-29-11-69-99F-003-A01

A. General

(1) Do these tests on each differential pressure indicator (270, 340 and 410).

(2) Do these tests at ambient temperature and pressure, unless specified differently. (3) If the results of a test are unsatisfactory, the differential pressure indicator must be

replaced.

SUBTASK-29-11-69-780-008-A01

(1) Install the differential pressure indicator on the test fixture.

(2) Connect the pressure supply to the inlet and outlet connections of the test fixture. (3) Slowly increase the pressure to 31028 to 31200 kPag (4500 to 4525 psig). Keep the

pressure applied for 3 minutes then decrease the pressure to zero.

(4) Make sure that there is no external leakage or damage caused to the differential pressure indicator.

(5) Disconnect the pressure supply from the test fixture. RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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SUBTASK-29-11-69-780-009-A01 C. Indicator Operation Test

(1) Connect the pressure supply to the inlet connection of the test fixture. Keep the outlet connection of the test fixture open to atmosphere.

(2) Decrease the temperature of the test fluid to 8.3 to 9.4°C (47 to 49°F) and let the temperature become stable.

(3) Increase the inlet pressure to 552 to 586 kPag (80 to 85 psig). Make sure that the indicator button does not come out.

(4) Decrease the pressure to zero.

(5) Increase the temperature of the test fluid to 27.2 to 30°C (81 to 86°F) and let the temperature become stable.

(6) Increase the inlet pressure to 379 to 407 kPag (55 to 59 psig). Make sure that the indicator button does not come out.

(7) Slowly increase the pressure to 552 kpag (80 psig) and make sure that the indicator button comes out at a pressure of 414 to 552 kPad (60 to 80 psid).

(8) Decrease the pressure to zero. Make sure that the indicator button stays out. (9) Push the indicator button in then release it. The indicator button must stay in. (10) Disconnect the differential pressure indicator from the test equipment.

TASK-29-11-69-810-801-A01 9. Fault Isolation

Fault isolation procedures are given in Table 1003 (Refer to Table 1003 “TABLE-29-11-69-99A-804-A01”).

TABLE-29-11-69-99A-804-A01 Fault Isolation—Table 1003

PROBLEM POSSIBLE CAUSE RECOMMENDED PROCEDURE

Leakage from filter shut-off valves.

Damaged shut-off valve. Replace manifold.

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

Return bypass valve

operates out of limits or does not operate.

Damaged return bypass valve.

Replace return bypass valve.

Damaged seat in manifold. Replace manifold.

System pressure relief valve operates out of limits or does not operate.

Damaged system pressure relief valve.

Replace system pressure relief valve.

EDP pressure inlet non-return valve operates out of limits.

Damaged non-return valve. Replace non-return valve.

ACMP pressure inlet check valve operates out of limits.

Damaged non-return valve. Replace non-return valve.

Differential pressure indicator does not operate correctly.

Damaged differential pressure indicator.

Replace differential pressure indicator.

Pressure switch does not operate correctly.

Damaged pressure switch. Replace pressure switch.

Pressure transducer

operates out of limits or does not operate.

Damaged pressure transducer.

Test the pressure transducer to ACMM 29-12-01.

PROBLEM POSSIBLE CAUSE RECOMMENDED PROCEDURE

Fault Isolation (Sheet 2 of 2)—Table 1003 RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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GRAPHIC-29-11-69-99B-805-A01

Manifold Bleed Circuit (Sheet 1 of 1) Figure 1001

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

GRAPHIC-29-11-69-99B-808-A01

Return Bypass Valve and Shim (Sheet 1 of 1) Figure 1002

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GRAPHIC-29-11-69-99B-806-A01

Non-return Valve (2304H070) Test Circuit (Sheet 1 of 1) Figure 1003

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

GRAPHIC-29-11-69-99B-809-A01

Non-return Valve (2346H180) Test Circuit (Sheet 1 of 1) Figure 1004

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 DISASSEMBLY

TASK-29-11-69-99C-803-A01

1. General

A. Make sure that the area where you disassemble the hydraulic filter manifold and the tools you use to disassemble the hydraulic filter manifold are clean.

B. Do the main assembly tests given in TESTING AND FAULT ISOLATION before you

disassemble the hydraulic filter manifold to find the possible cause of malfunction. Disassemble the hydraulic filter manifold only to the level necessary to correct the malfunction.

C. Each removal SUBTASK of these disassembly procedures can be done independently but the unit must be drained first.

D. Put the components in clean containers in the sequence of removal to help assembly. E. Do not remove protective caps from components unless it is necessary for their removal. F. To prevent damage to lockwire holes, lockwire must be cut, not broken, when components

are released.

G. All item numbers in parenthesis relate to IPL Figure 1. TASK-29-11-69-94-B-805-A01

2. Special Tools, Fixtures and Equipment

The special tools and equipment given in Table 3001 are necessary for disassembly (Refer to Table 3001 “TABLE-29-11-69-99A-819-A01”).

TABLE-29-11-69-99A-819-A01

Special Tools and Equipment - Table 3001 NOTE: Equivalent alternatives can be used for these items.

Open end crowfoot wrench, 7/8 inch AF

STARTRITE E2030 Removal of pressure transducer

from the manifold assembly Special Tools and Equipment - Table 3001

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TASK-29-11-69-030-801-A01 3. Procedure (IPL Fig 1)

SUBTASK-29-11-69-630-001-A01 A. Drain Hydraulic Fluid

WARNING: HYDRAULIC FLUID CAN BE DANGEROUS TO PERSONS. KEEP AWAY FROM OPEN FLAMES OR SOURCES OF IGNITION. DO NOT GET THE HYDRAULIC FLUID ON YOUR SKIN OR IN YOUR EYES. PUT ON PROTECTIVE CLOTHES AND EYE PROTECTION.

(1) Remove the nine protective caps (820, 830, 840 and 850) from the hydraulic filter manifold.

(2) Drain as much hydraulic fluid as possible from the hydraulic filter manifold through the connections.

(3) Install the nine protective caps (820, 830, 840 and 850) back on the hydraulic filter manifold.

SUBTASK-29-11-69-010-001-A01 B. Removal of Filter Elements

WARNING: THE BOWL CAN CONTAIN HYDRAULIC FLUID. HYDRAULIC FLUID CAN BE DANGEROUS TO PERSONS. KEEP AWAY FROM OPEN FLAMES OR SOURCES OF IGNITION. DO NOT GET THE HYDRAULIC FLUID ON YOUR SKIN OR IN YOUR EYES. PUT ON PROTECTIVE CLOTHES AND EYE PROTECTION.

NOTE: The removal procedure for the three filter elements (60, 120 and 180) is the same. (1) Push and hold the locking lever (30, 90 or 150) and remove the bowl assembly (20, 80

or 140) with the filter element (60, 120 or 180).

(2) Remove the retaining ring (15, 75 or 135) of the bowl assembly (20, 80 or 140) and remove the filter element (60, 120 or 180). Discard the filter element. Install the retaining ring back (15, 75 or 135) in the bowl assembly.

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C. Removal of Pressure Shut-off Valve

WARNING: THE MANIFOLD ASSEMBLY CAN CONTAIN HYDRAULIC FLUID. HYDRAULIC FLUID CAN BE DANGEROUS TO PERSONS. KEEP AWAY FROM OPEN FLAMES OR SOURCES OF IGNITION. DO NOT GET THE HYDRAULIC FLUID ON YOUR SKIN OR IN YOUR EYES. PUT ON PROTECTIVE CLOTHES AND EYE PROTECTION.

(1) Remove the stop bolt (23), the shut-off stop (22), the shut-off valve piston (25), the spring (26) and the cup washer (28) from the manifold assembly (790).

(2) Remove the two ‘O’ ring seals (52) (2346H000-002) or one ‘O’ ring seal (52)

(2346H000-003, 2346H000-004, 2346H000-005 or 2346H000-006) from the shut-off valve piston (25). Discard the ‘O’ ring seal(s) (52).

(3) Remove the ‘O’ ring seal (54) from the shut-off valve piston (25). Discard the ‘O’ ring seal (54).

(4) Remove the back-up ring (56) and ‘O’ ring seal (58) from the manifold assembly (790). Discard the back-up ring (56) and ‘O’ ring seal (58).

SUBTASK-29-11-69-010-013-A01

D. Removal of Case Drain Shut-off Valve

(1) Remove the stop bolt (84), the shut-off stop (82), the shut-off valve piston (86) and the spring (88) from the manifold assembly (790).

(2) Remove the two ‘O’ ring seals (112) from the shut-off valve piston (86). Discard the ‘O’ ring seals (112).

(4) Remove the back-up ring (116) and ‘O’ ring seal (118) from the manifold assembly (790). Discard the back-up ring (116) and ‘O’ ring seal (118).

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SUBTASK-29-11-69-010-014-A01

E. Removal of the Return Shut-off Valve

(1) Remove the stop bolt (143), the shut-off stop (142), the shut-off valve piston (145), the spring (146) and the cup washer (148) from the manifold assembly (790).

(2) Remove the two ‘O’ ring seals (172) (2346H000-002) or one ‘O’ ring seal (172) (2346H000-003, 2346H000-004, 2346H000-005 or 2346H000-006) from the shut-off valve piston (145). Discard the ‘O’ ring seal(s) (172).

(4) Remove the ‘O’ ring seal (178) from the manifold assembly (790). Discard the ‘O’ ring seal (178).

SUBTASK-29-11-69-010-002-A01

F. Removal of Locking Levers

NOTE: The removal procedure for the three locking levers (30, 90 and 150) is the same. Remove the shoulder bolt (40, 100 or 160), locking lever (30, 90 or 150) and spring (50, 110 or 170) from the manifold assembly (790).

SUBTASK-29-11-69-010-003-A01 G. Removal of System Relief Valve

(1) Remove and discard the lockwire from the system relief valve (190). (2) Remove the system relief valve (190) from the manifold assembly (790).

(3) Remove the ‘O’ ring seal (200), back-up ring (210) and ‘O’ ring seal (220) from the system relief valve (190). Discard the ‘O’ ring seals and back-up ring.

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H. Removal of Unions

NOTE: The removal procedure for the seven unions (230, 250, 480, 520, 660, 680 and 720) is the same.

(1) Remove the union (230, 250, 480, 520, 660, 680 or 720) from the manifold assembly (790).

(2) Remove the ‘O’ ring seal (240, 260, 490, 530, 670, 690 or 730) from the union (230, 250, 480, 520, 660, 680 or 720). Discard the ‘O’ ring seal.

SUBTASK-29-11-69-010-005-A01

I. Removal of Differential Pressure Indicators

NOTE: The removal procedure for the three differential pressure indicators (270, 340 and 410) is the same.

(1) Remove the four screws (280, 350 or 420) and the clamp ring (290, 360 or 430) from the differential pressure indicator (270, 340 or 410).

(2) Remove the differential pressure indicator (270, 340 or 410) from the manifold assembly (790).

(3) Remove the ‘O’ ring seal (310, 380 or 450) from the differential pressure indicator (270, 340 or 410). Discard the ‘O’ ring seal.

(4) Remove the ‘O’ ring seal (320, 390 or 460) and back-up ring (330, 400 or 470) from the differential pressure indicator (270, 340 or 410). Discard the ‘O’ ring seal and back-up ring.

(5) If necessary, remove the protective cap (300, 370 or 440) from the differential pressure indicator (270, 340 or 410).

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SUBTASK-29-11-69-010-006-A01

J. Removal of Pressure Switches

NOTE: The removal procedure for the two pressure switches (500 and 590) is the same. (1) Remove and discard the lockwire from the pressure switch (500 or 590).

(2) Remove the pressure switch (500 or 590) from the manifold assembly (790).

(3) Remove the ‘O’ ring seal (510 or 600) from the pressure switch (500 or 590). Discard the ‘O’ ring seal.

SUBTASK-29-11-69-010-007-A01 K. Removal of Non-return Valve

(1) Remove the non-return valve (540 or 540A) from the manifold assembly (790). (2) Remove the back-up ring (550 or 550A), ‘O’ ring seal (560 and 560A) and back-up ring

(570 and 570A) from the non-return valve (540 or 540A). Discard the back-up rings and ‘O’ ring seal.

(3) Remove the ‘O’ ring seal (580 or 580A) from the non-return valve (540 or 540A). Discard the ‘O’ ring seal.

SUBTASK-29-11-69-010-008-A01

L. Removal of Check Valve

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 (2) Remove the back-up ring (620), ‘O’ ring seal (630) and back-up ring (640) from the

check valve (610). Discard the back-up rings and ‘O’ ring seal.

(3) Remove the ‘O’ ring seal (650) from the check valve (610). Discard the ‘O’ ring seal. SUBTASK-29-11-69-010-009-A01

M. Removal of Pressure Transducer

(1) Remove and discard the lockwire from the pressure transducer (700).

(2) Use the open end crowfoot wrench to remove the pressure transducer (700) from the manifold assembly (790).

(3) Remove the ‘O’ ring seal (710) from the pressure transducer (700). Discard the ‘O’ ring seal.

SUBTASK-29-11-69-010-010-A01

N. Removal of Bypass Valve

(1) Remove and discard the lockwire from the bypass valve (740). (2) Remove the bypass valve (740) from the manifold assembly (790).

(3) Remove the ‘O’ ring seal (750) and back-up ring (760) from the bypass valve (740). Discard the ‘O’ ring seal and back-up ring.

(4) If fitted, remove the shim (745) from the bypass valve (740). RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 CLEANING

TASK-29-11-69-99C-804-A01

1. General

A. Clean all of the parts before you do the check procedures. Prevent contamination of the parts after cleaning.

B. After cleaning, do not touch the parts with your hands. Put on PVC or polyethylene gloves to prevent contamination.

C. After cleaning and check, put the parts in sealed polyethylene bags until they are assembled. D. All item numbers in parenthesis relate to IPL Figure 1.

TASK-29-11-69-94A-802-A01 2. Materials

The materials necessary for cleaning are shown in Table 4001 (Refer to Table 4001 “TABLE-29-11-69-99A-805-A01”).

TABLE-29-11-69-99A-805-A01 Cleaning Materials—Table 4001 NOTE: Equivalent alternatives can be used for these items.

NOMENCLATURE PART No./TYPE SUPPLIER

Isopropyl alcohol - Commercially available

Cloth (must not contain lint) DEF1410 Commercially available

Aqueous cleaning solution (refer to NGPS 256 Method 1C for mixture)

- Commercially available

Alkaline cleaning solution (refer to NGPS 256 Method 2 for mixture)

Polyethylene bags - Commercially available

PVC or polyethylene gloves

Cleaning Materials —Table 4001 RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

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TASK-29-11-69-110-801-A01

3. Procedure

WARNING: CLEANING MATERIALS CAN BE DANGEROUS TO PERSONS. USE THE MATERIALS IN AN AREA WITH A GOOD FLOW OF AIR. KEEP THE

MATERIALS AWAY FROM OPEN FLAMES OR SOURCES OF IGNITION. DO NOT GET THE CLEANING MATERIALS ON YOUR SKIN OR IN YOUR EYES. PUT ON PROTECTIVE CLOTHES AND EYE PROTECTION.

CAUTION: CLEANING MATERIALS CAN MIX WITH SMALL QUANTITIES OF WATER FOUND IN HYDRAULIC SYSTEMS TO MAKE HYDROCHLORIC ACID. THIS CAN CAUSE CORROSION OF THE INTERNAL METAL SURFACES. MAKE SURE THAT THERE ARE NO CLEANING MATERIALS ON SURFACES AFTER CLEANING AND THAT ALL SURFACES ARE FULLY DRIED.

A. Clean the external surfaces of the components that follow with a cloth that is moist with isopropyl alcohol:

(1) System relief valve (190).

(2) Differential pressure indicators (270, 340 and 410). (3) Pressure switches (500 and 590).

(4) Non-return valve (540 or 540A).

(5) Check valve (610).

(6) Pressure transducer (700).

(7) Bypass valve (740).

(8) Manifold assembly (790, 790A or 790B).

B. Ultrasonically clean all other components of the hydraulic filter manifold as given in the aqueous cleaning method of NGPS 151.

WARNING: COMPRESSED AIR CAN CAUSE SMALL PARTICLES TO BE BLOWN INTO THE AIR. DO NOT USE A PRESSURE OF MORE THAN 172 kPag (25 psig). PUT ON EYE PROTECTION. DO NOT POINT THE NOZZLE OF THE

COMPRESSED AIR AT YOURSELF OR OTHER PERSONNEL. C. Dry all parts with a clean, dry cloth or with clean, dry compressed air.

CMM 29-11-69

Component Maintenance Manual

With Illustrated Parts List

HYDRAULIC FILTER MANIFOLD, SYSTEM 1 AND 2

PART No. 2346H000-002, 2346H000-003,

2346H000-004, 2346H000-005 AND 2346H000-006

Publication No. 2771

Component Maintenance Manual

With Illustrated Parts List

HYDRAULIC FILTER MANIFOLD, SYSTEM 1 AND 2

PART No. 2346H000-002, 2346H000-003,

2346H000-004, 2346H000-005 AND 2346H000-006

Honeywell Aerospace Yeovil

Honeywell - Confidential

Copyright - Notice

RECORD OF REVISIONS

RECORD OF TEMPORARY REVISIONS

SERVICE BULLETIN LIST

LIST OF EFFECTIVE PAGES

TABLE OF CONTENTS

LIST OF ILLUSTRATIONS

LIST OF TABLES