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Component Maintenance Publication: Outflow Valve Control Unit

This document is a Component Maintenance Publication for the Outflow Valve Control Unit, detailing technical data and maintenance procedures. It includes a list of effective data modules, change records, and highlights of modifications made in the latest issue dated June 5, 2019. The publication is subject to Canadian and U.S. export regulations and contains a comprehensive table of contents and list of abbreviations.

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100% found this document useful (1 vote)
125 views103 pages

Component Maintenance Publication: Outflow Valve Control Unit

This document is a Component Maintenance Publication for the Outflow Valve Control Unit, detailing technical data and maintenance procedures. It includes a list of effective data modules, change records, and highlights of modifications made in the latest issue dated June 5, 2019. The publication is subject to Canadian and U.S. export regulations and contains a comprehensive table of contents and list of abbreviations.

Uploaded by

k1merzlyakov
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
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Supplier code

(64547)
Initial Supplier code
(64547)

COMPONENT MAINTENANCE PUBLICATION


Outflow Valve Control Unit

Part Number
2119332-00
2119332-01

This document contains technical data and is subject to Canadian and


U.S. export regulations. If these commodities, technology, or software
were exported from Canada, no export permit is required. If these
commodities, technology, or software were exported from the United HON64547-64547-00003-00
States, they are in accordance with the export administration
regulations. Diversion contrary to Canadian or U.S. law is prohibited. Issue No : 003
ECCN: 9E991, NLR Eligible Date : 2019-06-05
Document D201201000070 21-34-06 Page TP-1
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Component Maintenance Publication
HON64547-64547-00003-00
2119332

List of effective data modules


The listed documents are included in issue 003, dated 2019-06-05, of this publication.

1. Descriptive information

The table gives the list of effective data modules with their status for this publication in relation to the previous
publication (status column):

- “N” indicates a new data module. This data module is an additional data module compared with the last issue
of this publication.

-“C” indicates a changed data module. This data module has some form of technical change compared with
the last issue of this publication.

-Empty status column indicates an unchanged data module. This data module does not change compared
with the last issue of this publication.

2. List of effective data modules

Data module code Issue Number Issue Date Status


Data module title
HONAERO-A-00-40-00-01A-021A-D 005 2019-01-01
Copyright - General
HON64547-A-21-34-06-01A-003A-C 003 2019-06-05 C
Change records and highlights -
Outflow Valve Control Unit
HONAERO-A-00-40-00-01A-018A-D 002 2019-04-05
Introduction - General
HON64547-A-21-34-06-01A-040A-C 001 2014-06-19
Description of how it is made and its
function - Outflow Valve Control Unit
HON64547-A-21-34-06-01A-033A-C 001 2014-06-19
Technical data (functional
breakdown) - Outflow Valve Control
Unit
HON64547-A-00-40-00-01A-0B0A-D 001 2014-09-23
Maintenance planning information -
General
HON64547-A-00-40-00-01A-330A-D 002 2019-06-05 C
Test preparation - General
HON64547-A-21-34-06-01A-330A-C 001 2014-06-19
Test preparation - Outflow Valve
Control Unit
HON64547-A-12-30-00-01A-310A-D 001 2014-09-23
Visual examination - General
HON64547-A-21-34-06-01A-310A-C 001 2014-06-19
Visual examination - Outflow Valve
Control Unit

LIST OF EFFECTIVE DATA MODULES


2019-06-05
21-34-06 Page LOEDM-1
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Component Maintenance Publication
HON64547-64547-00003-00
2119332

Data module code Issue Number Issue Date Status


Data module title
HON64547-A-21-34-06-01A-340A-C 002 2015-10-22
Function test - Outflow Valve Control
Unit
HON64547-A-21-34-06-01A-340B-C 001 2014-06-19
Function test - Outflow Valve Control
Unit
HON64547-A-21-34-06-01A-340C-C 002 2015-10-22
Function test - Outflow Valve Control
Unit
HON64547-A-21-34-06-01A-331A-C 001 2014-06-19
Connection of test equipment -
Outflow Valve Control Unit
HON64547-A-21-34-06-01A-342A-C 001 2014-06-19
Automatic test - Outflow Valve
Control Unit
HON64547-A-21-34-06-01A-332A-C 001 2014-06-19
Removal of test equipment - Outflow
Valve Control Unit
HON64547-A-00-40-00-01A-530A-D 001 2014-09-23
Disassemble procedure - General
HON64547-A-21-34-06-01A-530A-C 002 2015-10-22
Disassemble procedure - Outflow
Valve Control Unit
HON64547-A-00-40-00-01A-663A-D 001 2014-09-23
Standard repair procedure - General
HON64547-A-21-34-06-01A-663A-C 002 2015-10-22
Standard repair procedure - Outflow
Valve Control Unit
HON64547-A-00-40-00-01A-710A-D 001 2014-09-23
Assemble procedure - General
HON64547-A-21-34-06-01A-710A-C 002 2015-10-22
Assemble procedure - Outflow Valve
Control Unit
HON64547-A-00-40-00-01A-812A-D 001 2014-09-23
Shipping and storage - General -
General
HONAERO-A-00-40-00-01A-018B-D 002 2019-04-05
Introduction - General
HON64547-A-21-34-06-01A-941A-C 002 2015-10-22
Illustrated Parts Data - IPD - Outflow
Valve Control Unit

LIST OF EFFECTIVE DATA MODULES


2019-06-05
21-34-06 Page LOEDM-2
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Component Maintenance Publication
HON64547-64547-00003-00
2119332

HON64547-A-21-34-06-01A-003A-C (2019-06-05)

Change records and highlights


1 Make sure that the previous revisions have been incorporated.
2 Incorporated revisions must be recorded with the date of incorporation and a signature.

Issue Incorporated by (signature) Issue Incorporated by (signature)


Date Date
001 2014-06-19 Initial issue
002 2015-10-22
003 2019-06-05
004
005
006
007
008

End of HON64547-A-21-34-06-01A-003A-C

CHANGE RECORD
2019-06-05
21-34-06 Page CR-1
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Component Maintenance Publication
HON64547-64547-00003-00
2119332

Highlights
Data Module Change Page Number
HON64547-A-21-34-06-01A-003A-C MODIFIED CR-1
Change records and highlights — Outflow
Valve Control Unit
HON64547-A-21-34-06-01A-003A-C Updated to show the latest revision date. CR-1
Change records and highlights — Outflow
Valve Control Unit
HON64547-A-00-40-00-01A-330A-D MODIFIED TEST-1
Test preparation — General
HON64547-A-00-40-00-01A-330A-D Updated the Reason for Job Section to TEST-1
Test preparation — General refer to Test Requirement Document
(TRD) 16-65056948.

CHANGE RECORD
2019-06-05
21-34-06 Page HIGH-1
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Component Maintenance Publication
HON64547-64547-00003-00
2119332

List of abbreviations
Abbreviation Definition
AWG American Wire Gauge
CAGE Commercial And Government Entity
CAN Controller Area Network
COM Command Partition
CPIOM Core Input Output Processor
CSD Control Source Drawing
DC Direct Current
DPL Detailed Parts List
EMI Electro Magnetic Interface
ESDS Electrostatic Discharge Sensitive
GPO Government Printing Office
HCSD Honeywell Control Source Drawing
IEC International Electrotechnical Commission
IEEE Institute Of Electrical and Electronics Engineers
IMA Integrated Modular Avionics
IPD Illustrated Parts Data
ITA Interface Test Adapter
LRU Line Replaceable Unit
NI Numerical Index
OCU Outflow Valve Control Unit
OFV Outflow Valve
PBA Printed Board Assemblies
SI International System of Units
SIS Standalone Identification System
TPOS Test Programs and Operational Software
USMS United States Measurement System
UUT Unit Under Test
cRDC Common Remote Data Concentrator

LIST OF ABBREVIATIONS
2019-06-05
21-34-06 Page LOA-1
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Component Maintenance Publication
HON64547-64547-00003-00
2119332

Table of Contents
Section Page
List of effective data modules.............................................................................................................LOEDM-1
Change records and highlights .................................................................................................................CR-1
Highlights............................................................................................................................................ HIGH-1
List of abbreviations ............................................................................................................................... LOA-1
Table of Contents...................................................................................................................................TOC-1
List of Illustrations ................................................................................................................................... LOI-1
List of suppliers ................................................................................................................................ LOSUP-1
List of support equipment .....................................................................................................................LOSE-1
List of supplies.................................................................................................................................... LOSU-1
Copyright ........................................................................................................................................... COPY-1
Front matter and introduction.......................................................................................................... INTRO-1
How to Use this Manual ........................................................................................................ INTRO-1
Customer Support ................................................................................................................ INTRO-5
References .......................................................................................................................... INTRO-5
Functional and technical descriptions .............................................................................................. DESC-1
Description of Function................................................................................................................. DESC-1
General ................................................................................................................................ DESC-1
Description ........................................................................................................................... DESC-1
Operation ............................................................................................................................. DESC-1
Technical Description ................................................................................................................... DESC-3
Maintenance and servicing ............................................................................................................... SRVC-1
Servicing ..................................................................................................................................... SRVC-1
General ................................................................................................................................ SRVC-1
Examination, test, checks and fault isolation.................................................................................... TEST-1
Job Setup .............................................................................................................................. TEST-1
General Test Requirements..................................................................................................... TEST-2
Test Location ......................................................................................................................... TEST-2
Ambient Conditions ................................................................................................................ TEST-2
Test Conditions ...................................................................................................................... TEST-2
Job Setup .............................................................................................................................. TEST-3
General Check Procedures ..................................................................................................... TEST-3
Visual Inspection .................................................................................................................... TEST-3
Examination........................................................................................................................... TEST-3
Visually Examine the Unit........................................................................................................ TEST-5
Insulation Tests ...................................................................................................................... TEST-7
OCU Pin-to-Chassis Ground Insulation Test ............................................................................. TEST-7
OCU Pin to Pin Insulation Test................................................................................................. TEST-8
TVS Test.............................................................................................................................. TEST-13
Electrical Bonding and Grounding Test................................................................................... TEST-19
Acceptance Test Stand Setup................................................................................................ TEST-20
Ambient Test ........................................................................................................................ TEST-24
Setup .................................................................................................................................. TEST-24
Test Software Initialization..................................................................................................... TEST-24
Start of Test ......................................................................................................................... TEST-27
Removal of Test Equipment................................................................................................... TEST-28
Disconnect, remove and disassemble procedures .............................................................................. DIS-1
Job Setup ................................................................................................................................. DIS-1
Disassembly of the Outflow Valve Control Unit............................................................................. DIS-3
Job Setup ................................................................................................................................. DIS-3
Nameplates and Labels and Cover Assemblies ........................................................................... DIS-3
Access Cover Assembly ............................................................................................................ DIS-3

TABLE OF CONTENTS
2019-06-05
21-34-06 Page TOC-1
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Component Maintenance Publication
HON64547-64547-00003-00
2119332

Right Cover Assembly and Printed Board Assembly - Backup Motor Driver.................................... DIS-3
Printed Board Assembly - Command/Monitor .............................................................................. DIS-3
Printed Board Assembly - Electro Magnetic Interface ................................................................... DIS-4
Front Plate Assembly................................................................................................................. DIS-4
Repair instructions ......................................................................................................................... RPR-1
Job Setup ............................................................................................................................... RPR-1
References for Repair.............................................................................................................. RPR-1
Identification Plate ................................................................................................................... RPR-2
Caution Label.......................................................................................................................... RPR-2
Software Label ........................................................................................................................ RPR-2
Standalone Identification System Label..................................................................................... RPR-2
Information Plate ..................................................................................................................... RPR-3
Assemble, install and reconnect procedures ................................................................................... ASSY-1
Job Setup .............................................................................................................................. ASSY-1
Assembly of the Outflow Valve Control Unit .............................................................................. ASSY-2
Job Setup .............................................................................................................................. ASSY-2
Front Plate Assembly.............................................................................................................. ASSY-2
Printed Board Assembly - Electro Magnetic Interface ................................................................ ASSY-3
Printed Board Assembly - Command/Monitor ........................................................................... ASSY-3
Right Cover Assembly and Printed Board Assembly - Backup Motor Driver................................. ASSY-3
Access Cover Assembly ......................................................................................................... ASSY-4
Nameplates, Labels and Cover Assemblies.............................................................................. ASSY-4
Storage procedures and data ...................................................................................................... STORE-1
Job Setup ........................................................................................................................... STORE-1
Preservation and Packing .................................................................................................... STORE-1
Storage .............................................................................................................................. STORE-2
Transportation..................................................................................................................... STORE-2
Illustrated Parts Data ............................................................................................................................ IPD-1
IPD Introduction ............................................................................................................................... IPD-1
General .................................................................................................................................... IPD-1
Contents of the IPD ................................................................................................................... IPD-1
References ............................................................................................................................... IPD-4
Illustrated Parts Data........................................................................................................................ IPD-7

TABLE OF CONTENTS
2019-06-05
21-34-06 Page TOC-2
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Component Maintenance Publication
HON64547-64547-00003-00
2119332

List of Illustrations
Figure Page
Fig FM-1 Geometric Tolerance Symbols .................................................................................... INTRO-3
Fig FM-2 Weld Symbols ........................................................................................................... INTRO-4
Fig FM-3 ESDS and Moisture Sensitive Symbols ....................................................................... INTRO-5
Fig DESC-1 Outflow Valve Control Unit........................................................................................... DESC-2
Fig TEST-1 J1 Connector Polarization ............................................................................................ TEST-6
Fig TEST-2 Acceptance Test Station............................................................................................. TEST-22
Fig TEST-3 OCU to Acceptance Test Station Setup ....................................................................... TEST-23
Fig TEST-4 Desktop Icon ............................................................................................................. TEST-25
Fig TEST-5 Login Screens ........................................................................................................... TEST-25
Fig TEST-6 Screen after Login ..................................................................................................... TEST-26
Fig TEST-7 Test Software ............................................................................................................ TEST-26
Fig TEST-8 Serial Number ........................................................................................................... TEST-26
Fig TEST-9 Acceptance Test Station............................................................................................. TEST-29
Fig TEST-10 OCU to Acceptance Test Station Setup ....................................................................... TEST-30
Fig DIS-1 Outflow Valve Control Unit....................................................................................................DIS-5/6
Fig RPR-1 Outflow Valve Control Unit...................................................................................................RPR-5/6
Fig ASSY-1 Outflow Valve Control Unit................................................................................................ ASSY-5/6
Fig IPD-1 Description Indentures .................................................................................................... IPD-2
Fig IPD-2 Detailed Parts List Example............................................................................................. IPD-5
IPD Figure 1 Outflow Valve Control Unit................................................................................................ IPD-11/12

LIST OF ILLUSTRATIONS
2019-06-05
21-34-06 Page LOI-1
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Component Maintenance Publication
HON64547-64547-00003-00
2119332

List of suppliers
CAGE code Supplier
02WJ6 Fluke Corporation, 1430 75 St SW BLDG 4 , Everett, WA, 98203, USA
2D895 Agilent Technologies Inc., 9780 S. Meridian Blvd., Englewood, CO, 80112,
USA
53504 Valhalla Scientific, 12127 Kirkham Rd, POWAY , CA, 92064 , USA
64547 Honeywell International Inc. DBA Honeywell Div Aerospace-Tucson, 11100 N.
Oracle Rd , Tucson, AZ , 85737, USA
70210 Honeywell International Inc., DBA Honeywell Div Aerospace - Torrance, 2525
West 190Th St., Torrance, CA, 90504, USA
7D905 Genrad Inc, 17461 Derian Ave Ste 100 , IRVINE , CA, 92614 , USA
80009 Tektronix Inc., 14150 SW Karl Braun Dr., Beaverton, OR, 97077, USA
80164 Keithley Instruments, Inc., 28775 Aurora Rd., Solon, OH, 44139, USA
80205 National Aerospace Standards Committee Aerospace Industries Association
Of America Inc. Not For Rfq Or Solicitation Use, 1000 Wilson Blvd Suite 1700,
Arlington, VA, 22209, USA
90526 Clippard Instrument Laboratory Inc., 7390 Colerain Ave., Cincinnati, OH,
45239, USA
96906 Military Standards Promulgated By Military Departments Under Authority Of
Defense Standardization Manual 4120 3-M

LIST OF SUPPLIERS
2019-06-05
21-34-06 Page LOSUP-1
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Component Maintenance Publication
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2119332

List of support equipment


Part name Part number CAGE code
1 KW Pulse Source Meter 2430 80164
A350 CPCS Acceptance Test Station STE65050552-1 or -2 64547
A350 CPCS ATP Interface Test Adapter STE65050553-1 64547
A350 Interface Test Adapter STE65050520-1 64547
A350 ITA test cable STE65050992-7 64547
Approved ATA container Commercially Available
Calipers, to 6 in (152 mm) min, ±0.001 in Commercially Available
(±0.025 mm) accuracy
Cap, Protective Commercially Available
Container Commercially Available
Current Probe 80i-110S 02WJ6
Current Probe N2779A 2D895
Dial Indicator, to 1.0 in (25.4 mm) min, ±0.001 Commercially Available
in (±0.025 mm) accuracy
Digital Ohmmeter, ranges: .2 Ohms, 2 Ohms, 4100ATC 53504
20 Ohms, 200 Ohms, 2KOhms, 20KOhms
Keithley 2430 Source Meter SMU-2430 80164
Magnifying Glass, 5x power Commercially Available
Megohmmeter 1836 or equivalent 7D905
OCU Dielectric Test Box STE65054088-1 64547
OCU Insulation Test Box STE65053710-1 64547
Oscilloscope Tektronix TDS3054B 80009
Oven, capable of 350 °F (177 °C) Commercially Available
Pneumatic tubing S8818-7 70210
T-connector T-44-4-BLK 90526
Torque Wrench, 0 to 15 lbf.in (0 to 1.7 N.m) Commercially Available

LIST OF SUPPORT EQUIPMENT


2019-06-05
21-34-06 Page LOSE-1
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Component Maintenance Publication
HON64547-64547-00003-00
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List of supplies
Part name Part number CAGE code
Anti-Static Bag Commercially Available
Desiccant Commercially Available
Grease 369-017-9001 64547
Isopropyl Alcohol Commercially Available
Lint-Free Cloth Commercially Available
Material, Cushioning Commercially Available
Paper, pH neutral Commercially Available

LIST OF SUPPLIES
2019-06-05
21-34-06 Page LOSU-1
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Component Maintenance Publication
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2119332

HONAERO-A-00-40-00-01A-021A-D (2019-01-01)

Copyright
1 Proprietary Information
1.1 Honeywell - Confidential
1.1.1 COPYRIGHT BY HONEYWELL INTERNATIONAL INC. (“HONEYWELL”). ALL RIGHTS
RESERVED. THIS DOCUMENT AND ALL INFORMATION CONTAINED HEREIN ARE THE
CONFIDENTIAL AND PROPRIETARY INFORMATION OF HONEYWELL AND CONTAIN
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CONTAINED HEREIN MAY, IN WHOLE OR IN PART, BE USED, DUPLICATED, OR DISCLOSED
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1.2 Honeywell Materials License Agreement
1.2.1 This document and the information contained herein (“the Materials”) are the proprietary data of
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used for the purpose of the rights granted herein. The Material furnished hereunder may be subject
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1.2.12 Limitation of Liability - Honeywell makes no representations or warranties regarding the use or
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HONEYWELL HAS BEEN ADVISED OF ANY SUCH INFRINGEMENT. IN NO EVENT WILL


HONEYWELL BE LIABLE FOR ANY INCIDENTAL DAMAGES, CONSEQUENTIAL DAMAGES,
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OPERATION OF LAW, OR OTHERWISE.
1.2.13 Controlling Law - This License Agreement shall be governed and construed in accordance with the
laws of the State of New York without regard to the conflict of laws provisions thereof.
1.2.14 Severability - In the event any provision of this License Agreement is determined to be illegal, invalid,
or unenforceable, the validity and enforceability of the remaining provisions of this License
Agreement will not be affected and, in lieu of such illegal, invalid, or unenforceable provision, there
will be added as part of this License Agreement one or more provisions as similar in terms as may be
legal, valid and enforceable under controlling law.
1.2.15 14. Integration and Modification - This License Agreement and all attachments set forth the entire
agreement and understanding between the parties on the subject matter of the License Agreement
and merges all prior discussions and negotiations among them. This License Agreement may be
modified only by a duly-authorized representative of Honeywell.
1.3 Safety Advisory
1.3.1 WARNING: BEFORE THE MATERIALS CALLED OUT IN THIS PUBLICATION ARE USED, KNOW
THE HANDLING, STORAGE AND DISPOSAL PRECAUTIONS RECOMMENDED BY THE
MANUFACTURER OR SUPPLIER. FAILURE TO OBEY THE MANUFACTURERS OR SUPPLIERS
RECOMMENDATIONS CAN RESULT IN PERSONAL INJURY OR DISEASE.
1.3.2 This publication describes physical and chemical processes which can make it necessary to use
chemicals, solvents, paints, and other commercially available materials. The user of this publication
must get the Material Safety Data Sheets (OSHA Form 174 or equivalent) from the manufacturers or
suppliers of the materials to be used. The user must know the manufacturer/ supplier data and obey
the procedures, recommendations, warnings and cautions set forth for the safe use, handling,
storage, and disposal of the materials.
1.4 Warranty/Liability Advisory
1.4.1 WARNING: HONEYWELL ASSUMES NO RESPONSIBILITY FOR ANY HONEYWELL
EQUIPMENT WHICH IS NOT MAINTAINED AND/OR REPAIRED IN ACCORDANCE WITH
HONEYWELLS PUBLISHED INSTRUCTIONS AND/OR HONEYWELLS FAA/SFAR 36 REPAIR
AUTHORIZATION. NEITHER DOES HONEYWELL ASSUME RESPONSIBILITY FOR SPECIAL
TOOLS AND TEST EQUIPMENT FABRICATED BY COMPANIES OTHER THAN HONEYWELL.
1.4.2 WARNING: INCORRECTLY REPAIRED COMPONENTS CAN AFFECT AIRWORTHINESS OR
DECREASE THE LIFE OF THE COMPONENTS. INCORRECTLY FABRICATED SPECIAL
TOOLING OR TEST EQUIPMENT CAN RESULT IN DAMAGE TO THE PRODUCT COMPONENTS
OR GIVE UNSATISFACTORY RESULTS.
1.5 Copyright - Notice
1.5.1 Copyright 2019 Honeywell International Inc. All rights reserved.
1.5.2 Honeywell is a registered trademark of Honeywell International Inc. All other marks are owned by
their respective companies.

End of HONAERO-A-00-40-00-01A-021A-D

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Front matter and introduction

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Front matter and introduction


HONAERO-A-00-40-00-01A-018A-D (2019-04-05)

General — Introduction
1 How to Use this Manual
1.1 General Information
1.1.1 This publication gives maintenance instructions for the equipment shown on the Title page.
1.1.2 Refer to the Special Tools, Fixtures, and Equipment and Consumables tables in each section before
the start of maintenance or repair procedures.
1.1.3 An explanation on how to use the IPD (Illustrated Parts Data) is given in the Introduction to that
section.
1.1.4 Honeywell recommends that you do the tests in TESTING AND FAULT ISOLATION before you
disassemble the unit. These tests can show the condition of the unit or most possible cause of a
malfunction. If a malfunction occurs, repair as necessary.
1.1.5 Warnings, cautions, and notes in this manual give the data that follows:
– A WARNING gives a condition or tells personnel what part of an operation or maintenance
procedure, which if not obeyed, can cause injury or death
– A CAUTION gives a condition or tells personnel what part of an operation or maintenance
procedure, which if not obeyed, can cause damage to the equipment
– A NOTE gives data, not commands. The NOTE helps personnel when they do the related
instruction.
1.1.6 Warnings and cautions go before the applicable paragraph or step. Notes follow the applicable
paragraph or step.
1.2 Observance of Manual Instructions
1.2.1 The procedures used must be consistent with standard shop practices and be carefully examined to
make sure that all safety, efficiency, and operation procedures of the unit are obeyed.
1.2.2 All personnel who operate equipment and do maintenance specified in this manual must know and
obey the safety precautions.
1.3 Symbols
1.3.1 The symbols and special characters are in agreement with IEEE (Institute of Electrical and
Electronics Engineers) Publication 260 and IEC (International Electrotechnical Commission)
Publication 27. Special characters in text are spelled out.
1.3.2 The signal mnemonics, unit control designators, and test designators are shown in capital letters.
1.3.3 The signal names followed by an “*” show an active low signal.
1.3.4 Some figures in this manual incorporate standard geometric characteristic symbols. Refer to Fig FM-
1 for the geometric characteristic symbols.

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Fig FM-1 (Sheet 1 of 2) Geometric Tolerance Symbols

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Fig FM-1 (Sheet 2 of 2) Geometric Tolerance Symbols

1.3.5 Some figures in this manual incorporate standard weld symbols. Refer to Fig FM-2 for the weld
symbols.

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Fig FM-2 Weld Symbols

1.3.6 The symbols in Fig FM-3 show ESDS (Electrostatic Discharge Sensitive) and moisture sensitive
symbols. Handle the items susceptible to electrostatic discharge in accordance with MIL-HDBK-263.
Refer to MIL-STD-1686 for definition of the standards and conditions.

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Fig FM-3 ESDS and Moisture Sensitive Symbols

1.4 Units of Measure


Measurements, weights, temperatures, dimensions, and other values are expressed in the USMS
(United States Measurement System) followed by the appropriate SI (International System of Units)
metric units in parentheses. Some standard tools or parts such as drills, taps, bolts, nuts, etc. do not
have an equivalent.
1.5 Illustration
1.5.1 Some of the exploded view illustrations shown in the ILLUSTRATED PARTS LIST section are also
referenced in the DISASSEMBLY, CLEANING, INSPECTION/CHECK, REPAIR, ASSEMBLY, and/or
FITS AND CLEARANCES sections of this manual.
1.5.2 Illustrations that support the individual items are shown by the item nomenclature, and in
parenthesis, the item number followed by the basic figure number, i.e. washer (90, IPD Figure 1).
Item numbers refer to the same IPD figure until a different IPD figure is specified.
1.5.3 If a code symbol (Code _____), part number, or Service Bulletin Number (Pre SB _____ or Post SB
_____) is before the illustration title, it is applicable to a specific unit.
1.5.4 Illustrations with no specific designation are applicable to all units.
1.6 Standard Practices Manual
Standard cleaning, check, repair, and assembly procedures applicable to multiple models can be
found in a standard practices manual. Refer to the References paragraph below.
2 Customer Support
2.1 Honeywell Aerospace Online Technical Publications Website
2.1.1 Go to the Honeywell Online Technical Publications Website at (www.myaerospace.com).
– To download or see publications online
– To order a publication
– To tell Honeywell of a possible data error in a publication.
2.2 Global Customer Care Center
2.2.1 If you do not have access to the Honeywell Technical Publications Website, or if you need to speak to
personnel about non-Technical Publication matters, the Honeywell Aerospace Global Customer Care
Center gives 24/7 customer service to Air Transport & Regional, Business & General Aviation, and
Defense & Space customers around the globe.
– Telephone: 800-601-3099 (Toll Free U.S.A./Canada)
– Telephone: 602-365-3099 (International)
– Telephone: 00-800-601-30999 (Europe, Middle East, & Africa – Toll Free)
– Telephone: 420-234-625-500 (Europe, Middle East, & Africa – Direct).
3 References

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3.1 Honeywell/Vendor Publications


3.1.1 Honeywell publications that may be related to this manual are shown in the list that follows:
– Pub. No. A09-1100-001, Handling, Storage, and Shipping Procedures for Honeywell Avionics
Equipment Instruction Manual
– Pub. No. A09-1100-004, Standard Repair Procedures for Honeywell Avionics Equipment
Instruction Manual
– Pub. No. C44-9000-001, Catalog of TPOS (Test Programs and Operational Software)
3.2 Other Publications
3.2.1 These publications are standard references. Check for latest version of publication.
– The United States GPO (Government Printing Office) Style Manual 2000 (available at http://www.
gpoaccess.gov /stylemanual/browse.html)
– IEEE Std 260.1, Standard Letter Symbols for Units of Measurement (available from the American
National Standards Institute at http://www.ansi.org)
– ASME Y14.38, Abbreviations for Use on Drawings and Related Documents (available from the
American National Standards Institute at http://www.ansi.org)
– ASME Y14.5, Dimensioning and Tolerancing (available from the American National Standards
Institute at http://www.ansi.org)
– ANSI/IEEE Std 91, Graphic Symbols for Logic Functions (available from the American National
Standards Institute at http://www.ansi.org)
– CAGE codes and manufacturers' addresses are available at https://cage.dla.mil.
– IEEE 315/ANSI Y32.2, Graphic Symbols for Electrical and Electronics Diagrams (available from
the American National Standards Institute at http://www.ansi.org))
– MIL-HDBK-263, Electrostatic Discharge Control Handbook for Protection of Electrical and
Electronic Parts, Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices)
(Metric) (available from any military standards database)
– MIL-STD-1686, Electrostatic Discharge Control Program for Protection of Electrical and Electronic
Parts, Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices) (Metric)
(available from any military standards database).
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End of FRONT MATTER AND INTRODUCTION

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Functional and technical descriptions

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Description of Function
HON64547-A-21-34-06-01A-040A-C (2014-06-19)

Outflow Valve Control Unit — Description of how it is made and its function
1 General
1.1 This section includes the description and operation for the OCU (Outflow Valve Control Unit).
2 Description
2.1 The OCU, Fig DESC-1 has PBA (Printed Board Assemblies) as follows:
– Backup Motor Driver
– Command/Monitor
– Electro Magnetic Interface.
3 Operation
3.1 The OCU transmits data to and receives data from the aircraft subsystems via ARINC 429 through a
CPIOM (Core Input Output Processor) in the IMA (Integrated Modular Avionics). The COM
(Command partition) transmits motor speed/direction data to and receives motor speed/direction
data from the cross OCU via RS-422. A CAN (Controller Area Network) bus is used between the
COM and a cRDC (Common Remote Data Concentrator) for data downloading purposes. The COM
also receives valve position data from the OFV (Outflow Valve) and gives motor commutation signals
to the OFV.

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Fig DESC-1 Outflow Valve Control Unit


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End of DESCRIPTION OF FUNCTION

DESCRIPTION OF FUNCTION
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Technical Description
HON64547-A-21-34-06-01A-033A-C (2014-06-19)

Outflow Valve Control Unit — Technical data (functional breakdown)


1 Refer to Table DESC-1 for the primary specifications.

Table DESC-1 Leading Particulars

Characteristic Specification

Power 28 VDC
Length 14.26 in (362.2 mm) max
Width 2.43 in (61.72 mm)
Height 7.64 in (194.05 mm)
Weight 5.75 lbm (2.61 kg) max

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Maintenance and servicing

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Servicing
HON64547-A-00-40-00-01A-0B0A-D (2014-09-23)

General — Maintenance planning information


1 General
1.1 There are no maintenance planning procedures for this component.

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SERVICING
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Examination, test, checks and fault isolation


HON64547-A-00-40-00-01A-330A-D (2019-06-05)

General — Test preparation


Reason For The Job
To perform the following Test chapters of this manual with equivalent equipment, refer to Test
Requirement Document (TRD) 16-65056948 Rev A.

Preliminary Requirements
None

Procedure
1 Job Setup
CAUTION: USE ONLY HONEYWELL MATERIALS OR THEIR APPROVED EQUIVALENT
ALTERNATIVES. OTHER MATERIALS CAN CAUSE DAMAGE AND CAN STOP THE
WARRANTY.
CAUTION: DO NOT HIT THE LINE-REPLACEABLE UNIT (LRU) OR LET IT FALL. THE LRU CAN
BE DAMAGED.
CAUTION: DO THESE PROCEDURES IN A CLEAN ENVIRONMENT TO PREVENT DAMAGE TO
THE MECHANICAL COMPONENTS.
1.1 This chapter gives testing procedures for the equipment shown on the title page.
1.2 Obey the precautions.
1.3 The test procedures give instructions to make the test setup.
1.4 Do all the tests at laboratory ambient conditions unless the procedure gives other specified
conditions.
1.5 Examine the LRU (Line Replaceable Unit) for cracks, dents, or any scratches. Do not do tests on a
damaged unit.
1.6 Make sure that the LRU is clean before you start the tests.
1.7 Record all test data on the appropriate data sheet.
1.8 Do the tests in the sequence given in this manual.

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EXAMINATION, TEST, CHECKS AND FAULT ISOLATION


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HON64547-A-21-34-06-01A-330A-C (2014-06-19)

Outflow Valve Control Unit — Test preparation


Reason For The Job
Self explanatory.

Preliminary Requirements
None

Procedure
2 General Test Requirements
2.1 Test Location
2.1.1 Do the tests at any Honeywell-approved facility.
2.2 Ambient Conditions
2.2.1 Unless specified otherwise in an individual test procedure, do all tests with the test unit at the
laboratory ambient pressure and temperature existing at the time of the test.
2.3 Test Conditions
2.3.1 No special test conditions are necessary to do the tests. Do all tests under ambient conditions.

End of HON64547-A-21-34-06-01A-330A-C

HON64547-A-12-30-00-01A-310A-D (2014-09-23)

General — Visual examination


Reason For The Job
Self explanatory.

Preliminary Requirements
Support Equipment
Table TEST-1 Support Equipment

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Magnifying Glass, 5x power Commercially Available As required
Calipers, to 6 in (152 mm) min, ±0.001 in Commercially Available As required
(±0.025 mm) accuracy

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Dial Indicator, to 1.0 in (25.4 mm) min, Commercially Available As required


±0.001 in (±0.025 mm) accuracy

Procedure
3 Job Setup
3.1 This chapter gives check procedures for the equipment shown on the title page.
3.2 Obey the precautions.
CAUTION: DO THESE PROCEDURES IN A CLEAN ENVIRONMENT TO PREVENT DAMAGE TO
THE MECHANICAL COMPONENTS.
4 General Check Procedures
4.1 Visual Inspection
4.1.1 Use a magnifying glass to examine the parts.
4.1.2 Refer to the detailed check procedures if a part shows a condition that could have caused wear.
4.1.3 Dimensional checks are given for parts that wear.
4.1.4 If a visual check shows no damage or wear, but a dimensional check is necessary, special
instructions are given.
4.1.5 Examine the parts that are usually replaced at each scheduled inspection cycle. Damage to these
parts can show a malfunction of other components.
4.2 Examination
4.2.1 If the LRU has threaded parts, examine the threaded parts.
4.2.1.1 Examine all threaded parts for crossed, stripped or broken threads. Discard the part if threads are
damaged.
4.2.1.2 Examine for loose threaded inserts and the condition of the threads. Refer to REPAIR if the inserts
are loose or damaged.
4.2.2 If the LRU has seals, examine the seal surfaces.
4.2.2.1 Examine all seal surfaces for minor surface defects. Refer to REPAIR if the seal surfaces are
damaged.
4.2.2.2 Examine all flanges for minor surface defects. Refer to REPAIR if the flanges are damaged.
4.2.3 If the LRU has bearings, examine the bearing bores and diameters (use calipers).
4.2.3.1 Examine all bearing bores and diameters for corrosion, wear and scoring.
4.2.3.2 Radial scoring lines must not be more than 0.005 in (0.13 mm) in width or 0.005 in (0.13 mm) in
depth.
4.2.3.3 Radial scoring lines must not be more than 30 percent of the bearing surface.
4.2.3.4 Radial scoring lines must not go through the protective coating, dry-film lubricant or other finishes on
the bore or diameter.

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4.2.4 If the LRU has dry-film lubricated, plated, anodized or painted parts, examine the surfaces for wear.
Make sure that the wear does not go through to the base metal.
4.2.5 If the LRU has coil springs, examine the coil springs.
4.2.5.1 Examine the coil spring. Roll the spring across a smooth, flat surface. Make sure that the coils are
correctly aligned. Make sure that the coils are not twisted.
4.2.5.2 Examine for cracks, deformation and elongation.
4.2.6 Examine gear and spline teeth.
4.2.6.1 Look for spalling, fretting, surface flaking, chipping, splitting, rubbing, and corrosion. If one or more of
these defects are found, replace the part.
4.2.6.2 Examine the part for corner loading. If the wear pattern shows that less than three quarters of the
normal loading area is bearing the load, replace the part.
4.2.6.3 Examine the part for metal displacement. If there is damage, replace the part.
4.2.6.4 Examine the parts for signs of healed scuffing of the tooth involute surface.
Note: Healed scuffing is shown by a dim gray finish or burnished color.
4.2.6.4.1 If the damaged area is not more than 30 percent of the pattern width, the involute contour does not
look changed, and no spalling or fretting is found, accept the part.
4.2.6.4.2 If the damaged area is more than 30 percent of the pattern width, the involute contour looks changed,
or spalling or fretting is found, replace the part.
4.2.6.3 Examine the part for discoloration caused by too much heat. If discoloration is found, replace the part
unless another procedure says it is acceptable.
4.2.6.4 Examine the teeth for signs of unusual or heavy wear patterns. If you find worn areas, do a
dimensional check. Refer to detailed check procedures.
4.2.6.5 Examine the part for uneven wear on the axial length of the spline teeth. If you find worn areas,
continue as follows:
4.2.6.5.1 Use a dial indicator to measure the worn area on the spline shaft. Move the spline tooth along the
axis from an area that is not worn to a worn area.
4.2.6.5.2 The worn area on the spline tooth must not be more than 0.004 in (0.10 mm). If the two sides of the
spline tooth are worn, the sum of the two wear measurements must be used.

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Outflow Valve Control Unit — Visual examination


References
Table TEST-2 References

Data Module/Technical Publication Title


HON64547-A-00-40-00-01A-663A-D General — Standard repair procedure

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Reason For The Job


Self explanatory.

Preliminary Requirements
None

Procedure
5 Visually Examine the Unit
5.1 Visually inspect the unit as follows:
1 Any physical damage
2 Unit weight is 5.75 lbm (2.61 kg) maximum.
5.2 Refer to General — Standard repair procedure [HON64547-A-00-40-00-01A-663A-D] for any
standard repairs.

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Fig TEST-1 J1 Connector Polarization


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HON64547-A-21-34-06-01A-340A-C (2015-10-22)

Outflow Valve Control Unit — Function test


Reason For The Job
Self explanatory.

Preliminary Requirements
Support Equipment
Table TEST-3 Support Equipment

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
OCU Insulation Test Box Part Number: STE65053710-1 As required
CAGE: 64547
Megohmmeter Part Number: 1836 or equivalent As required
CAGE: 7D905
Digital Ohmmeter, ranges: .2 Ohms, 2 Part Number: 4100ATC As required
Ohms, 20 Ohms, 200 Ohms, 2KOhms, CAGE: 53504
20KOhms
A350 CPCS Acceptance Test Station Part Number: STE65050552-1 or -2 As required
CAGE: 64547
Oscilloscope Part Number: Tektronix TDS3054B As required
CAGE: 80009
A350 CPCS ATP Interface Test Adapter Part Number: STE65050553-1 As required
CAGE: 64547
1 KW Pulse Source Meter Part Number: 2430 As required
CAGE: 80164
OCU Dielectric Test Box Part Number: STE65054088-1 As required
CAGE: 64547

Procedure
6 Insulation Tests
6.1 OCU Pin-to-Chassis Ground Insulation Test
6.1.1 Make sure that the OCU is fully assembled before you start the test.
6.1.2 If the OCU insulation test box is not available, this test can be done with the OCU dielectric test box.
6.1.2.1 Remove jumpers.
6.1.2.2 Refer to Table TEST-4 to connect UUT (Unit Under Test) side (red).

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6.1.3 Use a OCU insulation test box to electrically connect all J1 terminal pins. Do not connect pins J1-
AC7, J1-AF8, J1-BE3, J1-BE5 and J1-A112.
Note: If you do not have a test connector that connects all the pins together, do this test with a pin-to-
chassis procedure.
6.1.4 Connect the positive lead of the megohmmeter to the J1 terminal pins.
6.1.5 Connect the negative lead of the megohmmeter to the OCU chassis front mounting foot.
6.1.6 Use the megohmmeter to apply a voltage of 45 VDC (Direct Current) (50 VDC maximum) and
measure the insulation resistance. The insulation resistance must be 10 Mohm minimum.
6.1.7 Do Step 6.1.3 to Step 6.1.6 again for all pins. Do not do the test for pins J1-AC7, J1-AF8, J1-BE3, J1-
BE5 and J1-A112.
6.1.8 Remove the OCU insulation test box.
6.1.9 Use a digital ohmmeter to measure the resistance between J1-AC7 and the OCU chassis mounting
foot. Do the test again for pins J1-AF8, J1-BE3 and J1-BE5. Each measurement must be less than 1
ohm.
6.1.10 Use a digital ohmmeter to measure the resistance between J1-A112 and the OCU chassis mounting
foot. The insulation resistance must be less than 10 mohm.
6.1.11 Make a record of the results.
6.2 OCU Pin to Pin Insulation Test
6.2.1 Make sure that the OCU is fully assembled before you start the test.
6.2.2 If the OCU insulation test box is unavailable, this test can be done with the OCU dielectric test box.
6.2.2.1 Remove existing jumpers.
6.2.2.2 Refer to Table TEST-4 to connect UUT side (red).
6.2.3 Select the first group from Table TEST-4 Group one on the OCU insulation test box and remove the
jumpers.
6.2.4 Use the OCU insulation test box electrically connect all other J1 terminal pins. If a test connector is
not available that ties all the pins together, this test may be performed on a pin to pin bases or with a
breakout box.
6.2.5 Connect the positive lead of the megohmmeter to the group in Step 6.2.3.
6.2.6 Connect the negative lead of the megohmmeter to the terminal pins in Step 6.2.4.
6.2.7 Use the megohmmeter to apply a voltage of 45 VDC, no higher than 50 VDC and measure the
insulation resistance. The insulation resistance must be 10 Mohm minimum.
6.2.8 Repeat Step 6.2.3 to Step 6.2.7 until all of the groups given in Table TEST-4 have been measured
with respect to each other.
6.2.9 Once the insulation resistance between all groups has been taken, measure the insulation resistance
between all barrier pins in Group 4 from Table TEST-4 with the same method.

EXAMINATION, TEST, CHECKS AND FAULT ISOLATION


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21-34-06 Page TEST-8
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Table TEST-4 OCU Electrically Isolated Groups

ARINC600 Connector
Cavity ROW Letter Pin Number Group
A 1
A 2
A 3
A 4
A 5
A 6
A 7
A 8
A 9
111
B 11
117
C 1
C 4
C 10
C 11 Group 1
A
D 10
D 11

E 3
E 4

E 5
E 6
E 8
E 10
E 11
119
113
F 3
F 4
F 5
F 6

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21-34-06 Page TEST-9
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2119332

Table TEST-4 OCU Electrically Isolated Groups (Continued)

ARINC600 Connector
Cavity ROW Letter Pin Number Group
F 10
F 11

G 10
G 11
H 1
H 3
H 6
H 7
H 8
H 9
H 10
H 11
J 11
121
115
K 2
K 5
K 6
K 8

K 9
K 11
59
C
55
E 1
A Group 2
E 2
F 1
F 2
A Group 3
F 7
E 7
A 10
A Group 4
B 1

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21-34-06 Page TEST-10
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2119332

Table TEST-4 OCU Electrically Isolated Groups (Continued)

ARINC600 Connector
Cavity ROW Letter Pin Number Group
B 4
B 7
B 10
D 1
D 4
D 7
D 9
E 9
F 9
G 1
G 3
G 6
G 7
G 8
H 2
52
C
57
A 1
A 2
A 9
A 10
A 11
117
B 1
B Group 5
B 2
B 11
111
C 1
C 9
C 10
D 9

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Table TEST-4 OCU Electrically Isolated Groups (Continued)

ARINC600 Connector
Cavity ROW Letter Pin Number Group
D 10
E 1
119
113
H 1
H 2
H 3
H 4
121
115
K 2
K 5
K 6
K 8
K 9
56
51
A 3
B Group 6
A 4
A 5
A 6
B Group 7
A 7
A 8
C 7
A G 9
F 8 Group 8
E 3
B
E 5

End of HON64547-A-21-34-06-01A-340A-C

EXAMINATION, TEST, CHECKS AND FAULT ISOLATION


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21-34-06 Page TEST-12
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2119332

HON64547-A-21-34-06-01A-340B-C (2014-06-19)

Outflow Valve Control Unit — Function test


Reason For The Job
Self explanatory.

Preliminary Requirements
Support Equipment
Table TEST-5 Support Equipment

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Keithley 2430 Source Meter Part Number: SMU-2430 As required
CAGE: 80164
A350 Interface Test Adapter Part Number: STE65050520-1 1
CAGE: 64547
A350 ITA test cable Part Number: STE65050992-7 1
CAGE: 64547
Oscilloscope Part Number: Tektronix TDS3054B As required
CAGE: 80009

Procedure
7 TVS Test
7.1 Remove all jumpers on the front of the ITA (Interface Test Adapter) for the OCU. Do not remove
jumper J1-A116. Keep jumper J1-A116 on the front of the ITA for all tests.
7.2 Start the source meter 2430.
7.3 Start the ITA.
7.4 Set the 28VDC power switch on the front of the test adapter to the OFF position.
7.5 Connect the OCU to the ITA test cable.
7.6 Connect the source meter 2430 to the first set of test points in Table 1 in the columns ITA from (+)
and ITA to (-).
Note: Use only the red ITA front panel test points.
7.7 Do the steps that follow to configure the source meter 2430 with the front panel pushbuttons.
7.7.1 In the SOURCE section push V.
7.7.2 In the MEAS section push V.
7.7.3 Push the EDIT button.

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7.7.4 Use the RANGE up/down buttons to set an applicable voltage range. Refer to the Voltage Pulse
Amplitude column of Table TEST-6.
7.7.5 Use the EDIT up/down and left/right buttons to enter the Vsrc value from the Voltage Pulse Amplitude
column of Table TEST-6.
7.7.6 Push the EDIT button to select Cmpl.
7.7.7 Use the RANGE up/down buttons to set an applicable Cmpl value. Refer to the Current Compensation
column of Table TEST-6.
7.7.8 Use the EDIT up/down and left/right buttons to enter the Cmpl value from the Current Compensation
column in Table TEST-6.
7.7.9 Push the ENTER button.
7.7.10 In the MEAS section push I.
7.7.11 Use the RANGE up/down buttons to set the range for A to the same range selected for Cmpl.
7.7.12 In the MEAS section push V.
7.7.13 Push the CONFIG button.
7.7.14 In the EDIT section push the right arrow button.
7.7.15 Push I in the Source Section on the front panel to select OUTPUT.
7.7.16 In the EDIT section, push the left/right buttons until SHAPE is selected.
7.7.17 Push the ENTER button.
7.7.18 In the EDIT section, push the right arrow button to select PULSE.
7.7.19 Push the ENTER button.
7.7.20 In the EDIT section, push the left/right buttons to select PULSE-WIDTH.
7.7.21 Push the ENTER button.
7.7.22 Use the EDIT up/down and left/right buttons to set the PULSE-WIDTH to the value in Table TEST-6.
7.7.23 Push the ENTER button.
7.7.24 Use the EDIT up/down and left/right buttons to enter the PULSE-WIDTH to the value in Table TEST-
6.
7.7.25 Push the ENTER button.
7.7.26 Push the EXIT button.
7.7.27 Push the SPEED button.
7.7.28 Use the EDIT up/down and left/right buttons to set NPLC = 0.004.
7.7.29 Push the ENTER button.
7.8 On the source meter 2430, push the TRIG button.
7.9 Make a record of the voltage measurement shown on the front panel of the source meter 2430.
Compare the measurement with the value on the data sheet to accept or reject the LRU.

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Note: When you measure the voltages from J1-C59 to J1-C55, J1-C51 to J1-A112, J1–AE10 to J1-
C55, J1-C55 to J1–A112 and J1-C56 to J1-C51, use an oscilloscope to measure the peak
voltage in Table TEST-6.
7.10 Repeat Step 7.5 thru Step 7.9 for the remainder of the measurements in Table TEST-6.
7.11 Disconnect the OCU from the ITA test cable.
7.12 Turn off the ITA.
7.13 Turn off the source meter 2430.
7.14 Install all jumpers on the front of the ITA for the OCU.
7.15 Record PASS/FAIL on the data sheet.

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© Honeywell International Inc. Do not copy without express permission of Honeywell.
Table TEST-6 TVS Test Points and Settings

Mini-
Diode Voltage Maxi-
Test- mum
Under OCU Pulse Current mum
UUT UUT To ing Pulse ITA From Volt-
Test Pow- Ampli- Compen- ITA To — Voltage
From + — Meth- Width + age
Desig- ered tude sation Read-
od Read-
nators (Vdc) ing
ing
D80/D91 J1-AG10 J1-C55 N Pulse -35 20 500 J1-AG9 J1-C55 -25 -15
D80/D23 J1-AH10 J1-C55 N Pulse -35 20 500 J1-AH9 J1-C55 -25 -15
D48 J1-AH8 J1-C55 N Pulse -15 250 500 J1-AK1 J1-C55 -14 -8
D121 J1-AH9 J1-C55 N Pulse -15 250 500 J1-AK3 J1-C55 -14 -8
D125 J1-AH6 J1-C55 N Pulse -18 50 500 J1-AF5 J1-C55 -16 -10
D140 J1-AH7 J1-C55 N Pulse -18 50 500 J1-AH5 J1-C55 -16 -10
D88/D95 J1-AJ11 J1-C55 N Pulse -15 375 225 J1-AJ10 J1-C55 -13.2 -10.2
D88/D87 J1-AK11 J1-C55 N Pulse -15 375 225 J1-AK10 J1-C55 -13.2 -10.2

21-34-06
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D82/D60 J1-AG11 J1-C55 N Pulse -15 375 225 J1-AG10 J1-C55 -13.2 -10.2
D82/D77 J1-AH11 J1-C55 N Pulse -15 375 225 J1-AH10 J1-C55 -13.2 -10.2
D28 J1-AC4 J1-AE10 N Pulse 100 100 500 J1-AG7 J1-AE9 70 90
HON64547-64547-00003-00

D31 J1-AE8 J1-AE10 N Pulse 100 100 500 J1-AG8 J1-AE9 70 90


D25 J1-AH3 J1-AE10 N Pulse 100 100 500 J1-AH8 J1-AE9 70 90
D44 J1-AE10 J1-C55 N Pulse 60 75 500 J1-AE9 J1-C55 30 50

© Honeywell International Inc. Do not copy without express permission of Honeywell.


Component Maintenance Publication

D33/D94 J1-AG10 J1-C55 N Pulse 55 50 500 J1-AG9 J1-C55 30 50


D33/D24 J1-AH10 J1-C55 N Pulse 55 50 500 J1-AH9 J1-C55 30 50
D48 J1-AH8 J1-C55 N Pulse 15 250 500 J1-AK1 J1-C55 8 14
D121 J1-AH9 J1-C55 N Pulse 15 250 500 J1-AK3 J1-C55 8 14
D125 J1-AH6 J1-C55 N Pulse 18 50 500 J1-AK3 J1-C55 10 16
D140 J1-AH7 J1-C55 N Pulse 18 50 500 J1-AH5 J1-C55 10 16

2019-06-05
EXAMINATION, TEST, CHECKS AND FAULT ISOLATION

Page TEST-16
Table TEST-6 TVS Test Points and Settings (Continued)

Mini-
Diode Voltage Maxi-
Test- mum
Under OCU Pulse Current mum
UUT UUT To ing Pulse ITA From Volt-
Test Pow- Ampli- Compen- ITA To — Voltage
From + — Meth- Width + age
Desig- ered tude sation Read-
od Read-
nators (Vdc) ing
ing
D93/D92 J1-AJ11 J1-C55 N Pulse 18 375 225 J1-AJ10 J1-C55 10.2 13.2
D93/D90 J1-AK11 J1-C55 N Pulse 18 375 225 J1-AK10 J1-C55 10.2 13.2
D69/D62 J1-AG11 J1-C55 N Pulse 18 375 225 J1-AG10 J1-C55 10.2 13.2
D69/D68 J1-AH11 J1-C55 N Pulse 18 375 225 J1-AH10 J1-C55 10.2 13.2
D2 J1-C59 J1-C55 N Pulse -100 500 500 J1-C59 J1-C55 -90 -63
D1 J1-C55 J1–A112 N Pulse 100 500 5 J1-C55 J1-A116 63 90
D1 J1-C55 J1–A112 N Pulse -100 500 5 J1-C55 J1-A116 -90 -63

21-34-06
D184 J1-AK8 J1-C55 N Pulse 50 10 500 J1-AF1 J1-C55 25 45
2119332

D184 J1-AK8 J1-C55 N Pulse -50 10 500 J1-AF1 J1-C55 -45 -25
D186 J1-AK5 J1-C55 N Pulse 50 10 500 J1-AH1 J1-C55 25 45
HON64547-64547-00003-00

D186 J1-AK5 J1-C55 N Pulse -50 10 500 J1-AH1 J1-C55 -45 -25
D183 J1-AK9 J1-C55 N Pulse 50 10 500 J1-AF3 J1-C55 25 45
D183 J1-AK9 J1-C55 N Pulse -50 10 500 J1-AF3 J1-C55 -45 -25

© Honeywell International Inc. Do not copy without express permission of Honeywell.


D185 J1-AK6 J1-C55 N Pulse 50 10 500 J1-AH3 J1-C55 25 45
Component Maintenance Publication

D185 J1-AK6 J1-C55 N Pulse -50 10 500 J1-AH3 J1-C55 -45 -25
D16/D18 J1-BC9 J1-C51 N Pulse -35 20 500 J1-BB8 J1-C51 -25 -15
D16/D57 J1-BC10 J1-C51 N Pulse -35 20 500 J1-BB9 J1-C51 -25 -15
D23 J1-BH1 J1-C51 N Pulse -18 50 500 J1-BF5 J1-C51 -16 -10
D63 J1-BH2 J1-C51 N Pulse -18 50 500 J1-BH5 J1-C51 -16 -10

2019-06-05
EXAMINATION, TEST, CHECKS AND FAULT ISOLATION

Page TEST-17
Table TEST-6 TVS Test Points and Settings (Continued)

Mini-
Diode Voltage Maxi-
Test- mum
Under OCU Pulse Current mum
UUT UUT To ing Pulse ITA From Volt-
Test Pow- Ampli- Compen- ITA To — Voltage
From + — Meth- Width + age
Desig- ered tude sation Read-
od Read-
nators (Vdc) ing
ing
D27 J1-BH4 J1-C51 N Pulse -15 250 1 J1-BK3 J1-C51 -14 -8
D29 J1-BH3 J1-C51 N Pulse -15 250 1 J1-BK1 J1-C51 –14 -8
D35 J1-C56 J1-C51 N Pulse -100 500 500 J1-C56 J1-C51 -90 -60
D3 J1-C51 J1–A112 N Pulse 100 500 5 J1-C51 J1-A116 60 90
D3 J1-C51 J1–A112 N Pulse -100 500 5 J1-C51 J1-A116 –90 -60
D12/D59 J1-BC9 J1-C51 N Pulse 55 50 500 J1-BB8 J1-C51 30 50
D12/D13 J1-BC10 J1-C51 N Pulse 55 50 500 J1-BB9 J1-C51 30 50

21-34-06
D23 J1-BH1 J1-C51 N Pulse 18 50 500 J1-BF5 J1-C51 10 16
2119332

D63 J1-BH2 J1-C51 N Pulse 18 50 500 J1-BH5 J1-C51 10 16


D27 J1-BH4 J1-C51 N Pulse 15 250 500 J1-BK3 J1-C51 8 14
HON64547-64547-00003-00

DD29 J1-BH3 J1-C51 N Pulse 15 250 500 J1-BK1 J1-C51 8 14


U86 J1-BK9 J1-C51 N Pulse 50 10 500 J1-BF3 J1-C51 25 45
U86 J1-BK9 J1-C51 N Pulse -50 10 500 J1-BF3 J1-C51 -45 -25

© Honeywell International Inc. Do not copy without express permission of Honeywell.


U85 J1-BK8 J1-C51 N Pulse 50 10 500 J1-BF1 J1-C51 25 45
Component Maintenance Publication

U85 J1-BK8 J1-C51 N Pulse -50 10 500 J1-BF1 J1-C51 -45 -25
U88 J1-BK6 J1-C51 N Pulse 50 10 500 J1-BH3 J1-C51 25 45
U88 J1-BK6 J1-C51 N Pulse -50 10 500 J1-BH3 J1-C51 -45 -25
U87 J1-BK5 J1-C51 N Pulse 50 10 500 J1-BH1 J1-C51 25 45
U87 J1-BK5 J1-C51 N Pulse -50 10 500 J1-BH1 J1-C51 -45 -25

2019-06-05
EXAMINATION, TEST, CHECKS AND FAULT ISOLATION

Page TEST-18
Component Maintenance Publication
HON64547-64547-00003-00
2119332

End of HON64547-A-21-34-06-01A-340B-C

HON64547-A-21-34-06-01A-340C-C (2015-10-22)

Outflow Valve Control Unit — Function test


Reason For The Job
Self explanatory.

Preliminary Requirements
Support Equipment
Table TEST-7 Support Equipment

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Digital Ohmmeter, ranges: .2 Ohms, 2 Part Number: 4100ATC 1
Ohms, 20 Ohms, 200 Ohms, 2KOhms, CAGE: 53504
20KOhms

Consumables, Materials and Expendables


Table TEST-8 Consumables, Materials and Expendables

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Isopropyl Alcohol Commercially Available As required

Procedure
8 Electrical Bonding and Grounding Test
8.1 Use isopropyl alcohol to clean the area of the chassis mounting foot that is not painted and the A
ARINC connector shell.
8.2 Use a digital ohmmeter to measure the bonding resistance between any point on the chassis and the
mounting foot (A) and ARINC 600 connector housing.
8.3 Measure the resistance between chassis ground pin (pin 112 connector A cavity A) and equipment
casing. The resistance must not be more than 10 mohm.
8.4 Measure the resistance between the 28 V RTN (pin 55 connector A cavity C) and Chassis ground.
The measured resistance must be more than 1 Mohm.

End of HON64547-A-21-34-06-01A-340C-C

EXAMINATION, TEST, CHECKS AND FAULT ISOLATION


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21-34-06 Page TEST-19
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HON64547-A-21-34-06-01A-331A-C (2014-06-19)

Outflow Valve Control Unit — Connection of test equipment


Reason For The Job
Self explanatory.

Preliminary Requirements
Support Equipment
Table TEST-9 Support Equipment

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Oven, capable of 350 °F (177 °C) Commercially Available As required
A350 CPCS Acceptance Test Station Part Number: STE65050552-1 or -2 As required
CAGE: 64547
A350 CPCS ATP Interface Test Adapter Part Number: STE65050553-1 As required
CAGE: 64547
A350 ITA test cable Part Number: STE65050992-7 As required
CAGE: 64547
T-connector Part Number: T-44-4-BLK As required
CAGE: 90526
A350 Interface Test Adapter Part Number: STE65050520-1 As required
CAGE: 64547
Oscilloscope Part Number: Tektronix TDS3054B As required
CAGE: 80009
Current Probe Part Number: N2779A As required
CAGE: 2D895
Pneumatic tubing Part Number: S8818-7 As required
CAGE: 70210

Procedure
9 Acceptance Test Stand Setup
CAUTION: THIS UNIT CONTAINS COMPONENTS THAT ARE ELECTROSTATIC DISCHARGE
SENSITIVE (ESDS). TO PREVENT DAMAGE, OBEY THE ESD SAFETY
PRECAUTIONS BEFORE YOU TOUCH THIS UNIT.
9.1 The test station is shown in Fig TEST-2.
9.2 For hot and cold tests only, install the OCU into an oven. For ambient tests, put the OCU on the test
bench.
9.3 Set the 28 VDC power switch on the interface test adapter to the OFF position.

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9.4 Connect the ITA test cable to the A connector on the OCU as shown in Fig TEST-3.
9.5 Use a T-connector to connect tubing between the pneumatic test port fitting of the test station and the
COM and MON pressure ports on the OCU. Refer to Fig TEST-3.
9.6 Supply power to the test station. Make sure the power switches for the compressor and vacuum
sources, and for the computer and monitor are all in the ON position.
9.7 Supply power to the test station power supplies.
9.8 Supply power to the Break Power Supply.
9.9 Supply power to the NI PXI-1045.
9.10 If necessary, supply power to the oven.

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Fig TEST-2 Acceptance Test Station

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21-34-06 Page TEST-22
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Fig TEST-3 OCU to Acceptance Test Station Setup


End of HON64547-A-21-34-06-01A-331A-C

HON64547-A-21-34-06-01A-342A-C (2014-06-19)

Outflow Valve Control Unit — Automatic test


Reason For The Job
Self explanatory.

EXAMINATION, TEST, CHECKS AND FAULT ISOLATION


2019-06-05
21-34-06 Page TEST-23
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2119332

Preliminary Requirements
Support Equipment
Table TEST-10 Support Equipment

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Oven, capable of 350 °F (177 °C) Commercially Available As required
A350 CPCS Acceptance Test Station Part Number: STE65050552-1 or -2 As required
CAGE: 64547
A350 CPCS ATP Interface Test Adapter Part Number: STE65050553-1 As required
CAGE: 64547
A350 ITA test cable Part Number: STE65050992-7 As required
CAGE: 64547
T-connector Part Number: T-44-4-BLK As required
CAGE: 90526
A350 Interface Test Adapter Part Number: STE65050520-1 As required
CAGE: 64547
Oscilloscope Part Number: Tektronix TDS3054B As required
CAGE: 80009
Current Probe Part Number: 80i-110S As required
CAGE: 02WJ6

Procedure
10 Ambient Test
Note: Do this test with the OCU at factory ambient temperature.
10.1 Setup
CAUTION: THIS UNIT CONTAINS COMPONENTS THAT ARE ELECTROSTATIC DISCHARGE
SENSITIVE (ESDS). TO PREVENT DAMAGE, OBEY THE ESD SAFETY
PRECAUTIONS BEFORE YOU TOUCH THIS UNIT.
10.1.1 Setup the test station. Refer to Outflow Valve Control Unit — Connection of test equipment
[HON64547-A-21-34-06-01A-331A-C].
10.1.2 Let the OCU become stabile for 60 min at factory ambient temperature.
10.1.3 Connect the OCU to the test station. Refer to Outflow Valve Control Unit — Connection of test
equipment [HON64547-A-21-34-06-01A-331A-C].
10.1.4 Set the 28 VDC power switch on the interface test adapter to the ON position.
10.2 Test Software Initialization
10.2.1 Open the desktop icon shown in Fig TEST-4 below (ATP_A350) to initialize the test software.

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Fig TEST-4 Desktop Icon

10.2.2 Follow the prompts on the screen to start test. Refer to Fig TEST-5 for the next two screens.

Fig TEST-5 Login Screens

10.2.3 Enter the USER name and Password and press Login. Refer to Fig TEST-6 for the next screen.

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Fig TEST-6 Screen after Login

10.2.4 On the following screen, make an entry of CI2119332 for the test software. Refer to Fig TEST-7.

Fig TEST-7 Test Software

10.2.5 Make an entry of the serial number as shown on the nameplate and press OK. Refer to Fig TEST-8.

Fig TEST-8 Serial Number

EXAMINATION, TEST, CHECKS AND FAULT ISOLATION


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10.2.6 Follow the remaining prompts to start testing.


10.3 Start of Test
10.3.1 Enter the following data in the appropriate fields:
– OCU Serial Number: (as shown on the nameplate)
– OCU Part Number: (6500031–6)
– OCU MOD RECORD: (as shown on the nameplate)
– OCU SERIES Number: (as shown on the nameplate)
– OCU Weight: (actual weight from weight test)
– OCU Bonding Resistance: (actual bonding resistance from test)
– Select: AMBIENT AT>>NORMAL AT
10.3.2 When the computer prompts “Is this a FINAL AT” press “Yes” if it is a FINAL AT or press “NO” if it is
not a FINAL AT.
10.3.3 Make sure the screen shows that the test is successful after the test is complete. Only a unit that
successfully passes all tests will be accepted. Copy results to the current removable storage media
that is included with the Data Pack.
10.3.4 Set the 28 VDC power switch on the interface test adapter to the OFF position.

End of HON64547-A-21-34-06-01A-342A-C

HON64547-A-21-34-06-01A-332A-C (2014-06-19)

Outflow Valve Control Unit — Removal of test equipment


Reason For The Job
Self explanatory.

Preliminary Requirements
Support Equipment
Table TEST-11 Support Equipment

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Oven, capable of 350 °F (177 °C) Commercially Available As required
A350 CPCS Acceptance Test Station Part Number: STE65050552-1 or -2 As required
CAGE: 64547
A350 CPCS ATP Interface Test Adapter Part Number: STE65050553-1 As required
CAGE: 64547
A350 ITA test cable Part Number: STE65050992-7 As required
CAGE: 64547

EXAMINATION, TEST, CHECKS AND FAULT ISOLATION


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T-connector Part Number: T-44-4-BLK As required


CAGE: 90526
A350 Interface Test Adapter Part Number: STE65050520-1 As required
CAGE: 64547
Oscilloscope Part Number: Tektronix TDS3054B As required
CAGE: 80009
Current Probe Part Number: N2779A As required
CAGE: 2D895
Pneumatic tubing Part Number: S8818-7 As required
CAGE: 70210

Procedure
11 Removal of Test Equipment
CAUTION: THIS UNIT CONTAINS COMPONENTS THAT ARE ELECTROSTATIC DISCHARGE
SENSITIVE (ESDS). TO PREVENT DAMAGE, OBEY THE ESD SAFETY
PRECAUTIONS BEFORE YOU TOUCH THIS UNIT.
11.1 The test station is shown in Fig TEST-9.
11.2 If necessary, remove power from the oven.
11.3 Remove power from the NI PXI-1045.
11.4 Remove power from the Break power supply.
11.5 Remove power from the test station power supplies.
11.6 Remove power from the test station. Make sure the power switches for the compressor and vacuum
sources, and for the computer and monitor are all in the OFF position.
11.7 Disconnect the tubing between the pneumatic test port fitting of the Acceptance Test Station and the
COM and MON pressure ports on the OCU. Remove the T-connector. Refer to Fig TEST-10.
11.8 Disconnect the ITA test cable from the “A” connector on the OCU. Refer to Fig TEST-10.
11.9 Set the 28VDC power switch on the interface test adapter to the OFF position.
11.10 Remove the OCU from the oven or the test bench.

EXAMINATION, TEST, CHECKS AND FAULT ISOLATION


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Fig TEST-9 Acceptance Test Station

EXAMINATION, TEST, CHECKS AND FAULT ISOLATION


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Fig TEST-10 OCU to Acceptance Test Station Setup


End of HON64547-A-21-34-06-01A-332A-C
End of EXAMINATION, TEST, CHECKS AND FAULT ISOLATION

EXAMINATION, TEST, CHECKS AND FAULT ISOLATION


2019-06-05
21-34-06 Page TEST-30
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Disconnect, remove and disassemble procedures


HON64547-A-00-40-00-01A-530A-D (2014-09-23)

General — Disassemble procedure


Reason For The Job
Self explanatory.

Preliminary Requirements
None

Procedure
1 Job Setup
CAUTION: USE ONLY HONEYWELL MATERIALS OR THEIR APPROVED EQUIVALENT
ALTERNATIVES. OTHER MATERIALS CAN CAUSE DAMAGE AND CAN STOP THE
WARRANTY.
CAUTION: DO THESE PROCEDURES IN A CLEAN ENVIRONMENT TO PREVENT DAMAGE TO
THE MECHANICAL COMPONENTS.
1.1 This chapter gives disassembly procedures for the equipment shown on the title page.
1.2 Obey the precautions.
1.3 The item numbers shown in the DPL (Detailed Parts List) are the same as the item numbers on the
exploded view illustration(s). To find a part number, find the part on the illustration and note the item
number. Find the item number in the parts list and read the correct part number. Item numbers refer
to the same figure until a different figure is specified.
1.4 Before disassembly, use TESTING AND FAULT ISOLATION to examine the condition of the unit or to
find the malfunction. Do this to prevent disassembly that is not necessary.
1.5 If applicable, as an aid for assembly, tag the items that are disconnected to show where the
connections were made.
1.6 Include data for special conditions of a connection such as the polarity and the position of the items.
1.7 If applicable, identify the tie points for the wire assembly to prevent damage to the wire insulation
during assembly.
1.8 Disassemble the LRU in a dry, clean, area with good lighting.
1.9 If applicable, remove all protective caps, plugs, and closures before you disassemble the LRU.
1.10 Do not disassemble staked, welded, riveted, soldered, or press-fit assemblies, or remove plates,
passage- hole plugs, or threaded inserts unless replacement or repair of these parts is necessary.

End of HON64547-A-00-40-00-01A-530A-D

DISCONNECT, REMOVE AND DISASSEMBLE PROCEDURES


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HON64547-A-21-34-06-01A-530A-C (2015-10-22)

Outflow Valve Control Unit — Disassemble procedure


References
Table DIS-1 References

Data Module/Technical Publication Title


HON64547-A-21-34-06-01A-310A-C Outflow Valve Control Unit — Visual
examination
HON64547-A-21-34-06-01A-663A-C Outflow Valve Control Unit — Standard repair
procedure

Reason For The Job


Self explanatory.

Preliminary Requirements
Support Equipment
Table DIS-2 Support Equipment

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Torque Wrench, 0 to 15 lbf.in (0 to 1.7 N. Commercially Available 1
m)

Consumables, Materials and Expendables


Table DIS-3 Consumables, Materials and Expendables

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Anti-Static Bag Commercially Available 1

Procedure
CAUTION: THIS UNIT CONTAINS COMPONENTS THAT ARE ELECTROSTATIC DISCHARGE
SENSITIVE (ESDS). TO PREVENT DAMAGE, OBEY THE ESD SAFETY
PRECAUTIONS BEFORE YOU TOUCH THIS UNIT.
CAUTION: ONLY TOUCH THE ASSEMBLIES WITH CLEAN TOOLS, FIXTURES OR GLOVES. NO
SKIN CONTACT IS PERMITTED. SELECT GLOVES AND FINGER COTS THAT
SUPPLY ELECTROSTATIC DISCHARGE PROTECTION.

DISCONNECT, REMOVE AND DISASSEMBLE PROCEDURES


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CAUTION: OBEY THE ELECTROSTATIC-DISCHARGE (ESD) SAFETY PRECAUTIONS


SPECIFIED IN THE MIL-STD-1686, CLASS 2 SPECIFICATION. IF YOU DO NOT OBEY
THESE SAFETY PRECAUTIONS, DAMAGE TO EQUIPMENT CAN OCCUR.
2 Disassembly of the Outflow Valve Control Unit
2.1 Job Setup
2.1.1 Do all disassembly procedures in a dry area that has sufficient light and does not have dust.
2.1.2 Do not disassemble any staked, welded, or press fit assemblies, unless a replacement or repair of
these parts is necessary.
2.1.3 Be careful to prevent damage to parts that you can use again.
2.2 Nameplates and Labels and Cover Assemblies
2.2.1 Do not remove the identification plate Fig DIS-1 (5), SIS (Standalone Identification System) label
(20), caution labels (35), software label (15) or information plates (25, 30) unless necessary after
VISUAL EXAMINATION Outflow Valve Control Unit — Visual examination [HON64547-A-21-34-06-
01A-310A-C]. Refer to REPAIR Outflow Valve Control Unit — Standard repair procedure
[HON64547-A-21-34-06-01A-663A-C] for the removal and installation procedures.
2.2.2 Remove the screw (45) from the front plate (255) that holds the chains from the SIS and Pressure
Port Cover Assemblies (40).
2.2.3 Loosen the four screws and remove the SIS and Pressure Port Cover Assemblies (40) from the front
plate (255).
2.3 Access Cover Assembly
2.3.1 Remove seven screws (150) from the side of the access cover assembly (155) and one screw (245)
from the top of the left cover assembly (210) and remove the access cover assembly (155).
2.4 Right Cover Assembly and Printed Board Assembly - Backup Motor Driver
2.4.1 Disconnect the J3 connector of the EMI (Electro Magnetic Interface) (80) from the PBA - Backup
Motor Driver (50) connector P1.
2.4.2 Remove four screws (245) from the top of the left cover assembly (210).
2.4.3 Remove seven screws (205) from the side of the right cover assembly (170) and remove the PBA -
Backup Motor Driver (50) with the right cover assembly (170).
2.4.4 Remove fourteen screws (55) and washers (60) from the PBA - Backup Motor Driver (50) and
remove the PBA - Backup Motor Driver (50) from the right cover assembly (170).
2.4.5 Put the PBA - Backup Motor Driver (50) in an anti-static bag.
2.5 Printed Board Assembly - Command/Monitor
2.5.1 Remove four screws (120) and washers (125) from the front plate (255).
2.5.2 Disconnect the J2 connector of the EMI (80) from the PBA - Command/Monitor (65) connector P5.
2.5.3 Remove fourteen screws (70) and washers (75) from the PBA - Command/Monitor (65) and remove
the PBA - Command/Monitor (65) from left cover assembly (210).
2.5.4 Remove three screws (100) and washers (105) and remove the CPCS OCU pressure sensor
manifold (95) from the PBA - Command/Monitor (65).

DISCONNECT, REMOVE AND DISASSEMBLE PROCEDURES


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2.5.5 Remove two O-rings (110) and two retaining rings (115) from the PBA - Command/Monitor (65).
2.5.6 If necessary, remove the two straight fittings (97) from the CPCS OCU pressure sensor manifold
(95).
2.5.7 Put protective covers on the CPCS OCU pressure sensor manifold (95) ports.
2.5.8 Put the CPCS OCU pressure sensor manifold (95) in an anti-static bag.
2.5.9 Put the PBA - Command/Monitor (65) in an anti-static bag.
2.6 Printed Board Assembly - Electro Magnetic Interface
2.6.1 Remove the six screws (85) to remove the PBA EMI (80) from the chassis frame (140).
2.6.2 Install six screws (85) to secure the connector PBA EMI (80) while not installed in the chassis frame
(140).
2.6.3 Put the PBA EMI (80) in an anti-static bag.
2.7 Front Plate Assembly
2.7.1 Remove the six screws (270) to remove the front plate (255) from the chassis frame (140).
2.7.2 Remove the two screws (280) to remove the handle bow (275) from the front plate (255).
2.7.3 Remove the two screws (290) to remove the support hook (285) from the front plate (255).

DISCONNECT, REMOVE AND DISASSEMBLE PROCEDURES


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Fig DIS-1 Outflow Valve Control Unit

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End of HON64547-A-21-34-06-01A-530A-C
End of DISCONNECT, REMOVE AND DISASSEMBLE PROCEDURES

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Intentionally Left Blank

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Repair instructions
HON64547-A-00-40-00-01A-663A-D (2014-09-23)

General — Standard repair procedure


Reason For The Job
Self explanatory.

Preliminary Requirements
None

Procedure
1 Job Setup
1.1 This chapter gives repair procedures for the equipment shown on the title page.
1.2 Obey the precautions.
1.3 Replace all damaged parts that cannot be repaired.
2 References for Repair
2.1 These references show where to find repair data that is located in other sections of this manual and
in other manuals. The data in other sections of this manual is necessary for repair of the LRU and its
primary subassemblies. The data in other manuals gives procedures that are not included in this
manual.
2.2 Refer to SCHEMATIC AND WIRING DIAGRAMS for reference drawings for the LRU and its primary
subassemblies if applicable. The drawings give data about:
– Buswires
– Consumable materials
– Component layout
– Component termination
– Cut runs
– Schematic diagrams.
2.3 Refer to SCHEMATIC AND WIRING DIAGRAMS for wire list tables and for harness, cable, and lead
assemblies if applicable. The tables give data about wire:
– Terminations
– Type
– Size (AWG (American Wire Gauge))
– Color.
2.4 Refer to ILLUSTRATED PARTS LIST for:
– Figure and item numbers
– Subassembly and component locations

REPAIR INSTRUCTIONS
2019-06-05
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– Correct part numbers


– Correct quantities.
2.5 Refer to Standard Practices Manuals 20–00–02 and 70–00–01. Standard repair procedures are shop
repairs that use the same procedures on many types of assemblies. Use the standard repair
procedures and approved local shop procedures.

End of HON64547-A-00-40-00-01A-663A-D

HON64547-A-21-34-06-01A-663A-C (2015-10-22)

Outflow Valve Control Unit — Standard repair procedure


Reason For The Job
Self explanatory.

Preliminary Requirements
None

Procedure
3 Identification Plate
3.1 Refer to Fig RPR-1.
3.2 Remove the damaged identification plate (5) from the front plate (255).
3.3 If necessary, make a copy of the information from the damaged identification plate (5) on the new
identification plate (5).
3.4 Clean the surface where the old nameplate was removed.
3.5 Install the new identification plate (5) in correct position on the front plate (255).
4 Caution Label
4.1 Remove the damaged caution label (35) from the access cover assembly (155).
4.2 Clean the surface where the old label was removed.
4.3 Install the new caution label (35) in correct position on the access cover assembly (155).
5 Software Label
5.1 Remove the damaged software label (15) from the front plate (255).
5.2 Clean the surface where the old software label (15) was removed.
5.3 Install the new software label (15) in correct position on the front plate (255).
6 Standalone Identification System Label
6.1 Remove the damaged SIS label (20) from the front plate (255).
6.2 Clean the surface where the old label was removed.

REPAIR INSTRUCTIONS
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6.3 Install the new SIS label (20) in correct position on the front plate (255).
7 Information Plate
7.1 Remove the damaged information plate (25) or (30) from the front plate (255).
7.2 Clean the surface where the old plate was removed.
7.3 Install the new information plate (25) or (30) in correct position on the front plate (255).

REPAIR INSTRUCTIONS
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Intentionally Left Blank

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2019-06-05
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Fig RPR-1 Outflow Valve Control Unit

REPAIR INSTRUCTIONS
2019-06-05
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End of HON64547-A-21-34-06-01A-663A-C
End of REPAIR INSTRUCTIONS

REPAIR INSTRUCTIONS
2019-06-05
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Intentionally Left Blank

REPAIR INSTRUCTIONS
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21-34-06 Page RPR-8
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Assemble, install and reconnect procedures


HON64547-A-00-40-00-01A-710A-D (2014-09-23)

General — Assemble procedure


Reason For The Job
Self explanatory.

Preliminary Requirements
None

Procedure
1 Job Setup
CAUTION: USE ONLY HONEYWELL MATERIALS OR THEIR APPROVED EQUIVALENT
ALTERNATIVES. OTHER MATERIALS CAN CAUSE DAMAGE AND CAN STOP THE
WARRANTY.
CAUTION: DO THESE PROCEDURES IN A CLEAN ENVIRONMENT TO PREVENT DAMAGE TO
THE MECHANICAL COMPONENTS.
1.1 This chapter gives assembly procedures for the equipment shown on the title page.
1.2 Obey the precautions.
1.3 The item numbers shown in the DPL are the same as the item numbers on the exploded view
illustration(s). To find a part number, find the part on the illustration and note the item number. Find
the item number in the parts list and read the correct part number. Item numbers refer to the same
figure until a different figure is specified.
1.4 If applicable, refer to the data written during disassembly for the location of the tie points and where
to connect the components and wires.

End of HON64547-A-00-40-00-01A-710A-D

HON64547-A-21-34-06-01A-710A-C (2015-10-22)

Outflow Valve Control Unit — Assemble procedure


Reason For The Job
Self explanatory.

ASSEMBLE, INSTALL AND RECONNECT PROCEDURES


2019-06-05
21-34-06 Page ASSY-1
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Preliminary Requirements
Support Equipment
Table ASSY-1 Support Equipment

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Torque Wrench, 0 to 15 lbf.in (0 to 1.7 N. Commercially Available 1
m)

Consumables, Materials and Expendables


Table ASSY-2 Consumables, Materials and Expendables

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Anti-Static Bag Commercially Available 1
Grease Supply: 369-017-9001 As required
CAGE: 64547

Procedure
CAUTION: THIS UNIT CONTAINS COMPONENTS THAT ARE ELECTROSTATIC DISCHARGE
SENSITIVE (ESDS). TO PREVENT DAMAGE, OBEY THE ESD SAFETY
PRECAUTIONS BEFORE YOU TOUCH THIS UNIT.
CAUTION: ONLY TOUCH THE ASSEMBLIES WITH CLEAN TOOLS, FIXTURES OR GLOVES. NO
SKIN CONTACT IS PERMITTED. SELECT GLOVES AND FINGER COTS THAT
SUPPLY ELECTROSTATIC DISCHARGE PROTECTION.
CAUTION: OBEY THE ELECTROSTATIC-DISCHARGE (ESD) SAFETY PRECAUTIONS
SPECIFIED IN THE MIL-STD-1686, CLASS 2 SPECIFICATION. IF YOU DO NOT OBEY
THESE SAFETY PRECAUTIONS, DAMAGE TO EQUIPMENT CAN OCCUR.
2 Assembly of the Outflow Valve Control Unit
2.1 Job Setup
2.1.1 Do all assembly procedures in a dry area that has sufficient light and is free from dust.
2.1.2 Do not assemble any staked, welded, or press fit assemblies, unless a replacement or repair of these
parts is necessary.
2.1.3 Be careful to prevent damage to parts that you can use again.
2.1.4 Refer to Fig ASSY-1.
2.2 Front Plate Assembly
2.2.1 Install the two screws (290) to attach the support hook (285) to the front plate (255).

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2.2.2 Install the two screws (280) to attach the handle bow (275) to the front plate (255).
2.2.3 Install the six screws (270) to attach the front plate (255) to the chassis frame (140).
2.3 Printed Board Assembly - Electro Magnetic Interface
2.3.1 Remove the PBA EMI (80) from the anti-static bag.
2.3.2 Remove six screws (85) from the connector (50).
2.3.3 Install the PBA EMI (80) in the chassis frame (140).
2.3.4 Install the six screws (85) to attach the PBA EMI (80) to the chassis frame (140).
2.3.5 Use a torque wrench to torque screws (85) from 8.0 to 10.0 lbf.in (0.903 to 1.12 N.m).
2.4 Printed Board Assembly - Command/Monitor
2.4.1 Remove the PBA - Command/Monitor (65) from the anti-static bag.
2.4.2 Remove the CPCS OCU pressure sensor manifold (95) from the anti-static bag.
2.4.3 Remove the protective covers from the CPCS OCU pressure sensor manifold (95) ports.
2.4.4 Put the two retaining rings (115) on the two pressure sensor ports on the PBA - Command/Monitor
(65).
Note: Push the retaining rings down to make sure they touch the circuit card assembly.
2.4.5 Apply a thin layer of grease on the two O-rings (110).
2.4.6 Put two O-rings (110) on the two retaining rings (115).
2.4.7 Install three screws (100) and washers (105) to attach the CPCS OCU pressure sensor manifold (95)
to PBA - Command/Monitor (65).
2.4.8 Use a torque wrench to torque three screws (100) from 3.0 to 5.0 lbf.in (0.33 to 0.56 N.m).
2.4.9 Apply a thin layer of grease to the packings on the two straight fittings (97).
2.4.10 Install two straight fittings (97) in the CPCS OCU pressure sensor manifold (95).
2.4.11 Use a torque wrench to torque two straight fittings (97) from 12.0 to 14.0 lbf.in (1.35 to 1.58 N.m).
2.4.12 Place the PBA - Command/Monitor (65) into the left cover assembly (210).
2.4.13 Install fourteen screws (70) and washers (75) to secure the PBA - Command/Monitor (65) to the left
cover assembly (210).
2.4.14 Use a torque wrench to torque fourteen screws (70) from 5.0 to 7.0 lbf.in (0.56 to 0.79 N.m).
2.4.15 Install four screws (120) and washers (125) to the front plate (255).
2.4.16 Install the screw (45) to the front plate (255) and secure the chains from the SIS and Pressure Port
Cover Assemblies (40).
2.4.17 Use the four screws on the SIS and Pressure Port Cover Assemblies (40) and tighten them to the
front plate (255).
2.4.18 Connect the J2 connector of the PBA-EMI (80) to the PBA - Command/Monitor (65) connector P5.
2.5 Right Cover Assembly and Printed Board Assembly - Backup Motor Driver

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2.5.1 Remove the PBA - Backup Motor Driver (50) from the anti-static bag.
2.5.2 Place the PBA - Backup Motor Driver (50) into the right cover assembly (170).
2.5.3 Install fourteen screws (55) and washers (60) to secure the PBA - Backup Motor Driver (50) to the
right cover assembly (170).
2.5.4 Use a torque wrench to torque fourteen screws (55) from 5.0 to 7.0 lbf.in (0.56 to 0.79 N.m).
2.5.5 Put the PBA - Backup Motor Driver (50) with the right cover assembly (170) in the frame chassis
(140).
2.5.6 Loosely install seven screws (205) in the right cover assembly (170) and four screws (245) in the top
of the left cover assembly (210).
2.5.7 Connect the J3 connector of the PBA - EMI (80) to the PBA - Backup Motor Driver (50) connector P1.
2.6 Access Cover Assembly
2.6.1 Put the access cover assembly (155) in position and loosely install one screw (245) in the top of the
left cover assembly (210) and seven screws (150) in the side of the access cover assembly (155).
2.6.2 Use a torque wrench to torque screws (150) and screw (245) from 8.0 to 10.0 lbf.in (0.903 to 1.12 N.
m).
2.7 Nameplates, Labels and Cover Assemblies
2.7.1 Attach the SIS and Pressure Port Cover Assemblies (40) to the front plate (255) with four screws.
2.7.2 Attach the chains from the SIS and Pressure Port Cover Assemblies (40) to the front plate (255) with
screw (45).
2.7.3 If necessary, attach the identification plate (5), refer to Fig ASSY-1, SIS label (20), caution labels
(35), software label (15) or information plates (25,30). Refer to REPAIR Outflow Valve Control Unit —
Standard repair procedure [HON64547-A-21-34-06-01A-663A-C] for the installation procedures.

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Fig ASSY-1 Outflow Valve Control Unit

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End of ASSEMBLE, INSTALL AND RECONNECT PROCEDURES

ASSEMBLE, INSTALL AND RECONNECT PROCEDURES


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Intentionally Left Blank

ASSEMBLE, INSTALL AND RECONNECT PROCEDURES


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Storage procedures and data


HON64547-A-00-40-00-01A-812A-D (2014-09-23)

General — Shipping and storage - General


Reason For The Job
Self explanatory.

Preliminary Requirements
Support Equipment
Table STORE-1 Support Equipment

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Cap, Protective Commercially Available As required
Container Commercially Available As required
Approved ATA container Commercially Available As required

Consumables, Materials and Expendables


Table STORE-2 Consumables, Materials and Expendables

Nomenclature Identification no. Qty


(Equivalent alternatives may be used)
Lint-Free Cloth Commercially Available As required
Material, Cushioning Commercially Available As required
Paper, pH neutral Commercially Available As required
Desiccant Commercially Available As required

Procedure
1 Job Setup
1.1 Use these procedures to prepare the part for storage or transportation. These procedures are to
make sure the part is protected from dust, moisture, and other contamination.
1.2 Obey the precautions.
2 Preservation and Packing
WARNING: BEFORE YOU USE A CHEMICAL, PAINT, SOLUTION, SEALANT, COOLANT, OR
OTHER SUCH CONSUMABLE MATERIAL, OBEY THE PRECAUTIONS GIVEN IN ITS

STORAGE PROCEDURES AND DATA


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MANUFACTURER'S MATERIAL-SAFETY DATA-SHEET (MSDS). THE CHEMICALS


OR THEIR FUMES CAN KILL YOU OR CAUSE INJURY. ALSO OBEY YOUR LOCAL
REGULATIONS. AS A GENERAL PRECAUTION, YOU CAN PUT ON PROTECTIVE
CLOTHING, SAFETY GOGGLES, AND/OR GLOVES BEFORE YOU USE THESE
MATERIALS.
CAUTION: USE ONLY HONEYWELL MATERIALS OR THEIR APPROVED EQUIVALENT
ALTERNATIVES. OTHER MATERIALS CAN CAUSE DAMAGE AND CAN STOP THE
WARRANTY.
2.1 Clean the external surfaces with a lint-free cloth.
2.2 Make sure all ports are covered with protective caps.
2.3 Wrap the part in pH neutral paper.
2.4 Put cushioning material at the sharp corners to prevent damage to the container. Put a desiccant in
the container with the part.
3 Storage
3.1 Keep the parts away from high temperatures, dust, moisture, and corrosive fumes.
3.2 Control the humidity to prevent water from collecting on the parts.
4 Transportation
CAUTION: USE ONLY HONEYWELL MATERIALS OR THEIR APPROVED EQUIVALENT
ALTERNATIVES. OTHER MATERIALS CAN CAUSE DAMAGE AND CAN STOP THE
WARRANTY.
4.1 When parts are sent to Honeywell for warranty repair, use the container, or equivalent.

End of HON64547-A-00-40-00-01A-812A-D
End of STORAGE PROCEDURES AND DATA
End of MAINTENANCE AND SERVICING

STORAGE PROCEDURES AND DATA


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Illustrated Parts Data

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IPD Introduction
HONAERO-A-00-40-00-01A-018B-D (2019-04-05)

General — Introduction
1 General
1.1 The IPD gives the parts that are used to make the applicable equipment. It also supplies the
necessary data to get replacement parts for repair and testing and fault isolation.
1.2 The DPL gives a breakdown, in disassembly sequence, of assemblies and detail parts of the unit.
1.3 The illustrations show where you can find each part and are an important aid in disassembly and
assembly.
1.4 The item numbers shown in the DPL are the same as the item numbers on the exploded view
illustration(s). To find a part number, find the part on the illustration and record the item number. Go to
the DPL to find the item number and related part number.
2 Contents of the IPD
2.1 Numerical Index
2.1.1 The NI (Numerical Index) is an alphanumeric list of all the part numbers shown in the part number
column of the DPL.
2.1.2 Also included in the index are the Honeywell part numbers that are equivalent to the manufacturer
part number. Optional manufacturer part numbers are not included in the index.
2.1.3 The FIG. ITEM column gives all of the locations of a part. If a part number is in more than one figure
item location, the part number is shown only one time in the Part Number column.
2.1.4 The TTL REQ column shows the total number of parts that are used at each figure item location.
2.1.5 The AIRLINE PART NO. column has space for customers to use.
2.2 Detailed Parts List
Note: Refer to Fig IPD-2 for an example of a DPL.
2.2.1 An item number is given to each part in the DPL and on the related illustration. The item numbers
show the general disassembly sequence.
2.2.2 To find a part number in the DPL, do the steps that follow.
2.2.2.1 If the part number is known, refer to the NI to find the figure and item numbers in the DPL.
2.2.2.2 If the part number is not known, locate the part on the illustration and record the item number. The
part number is shown opposite the item number in the DPL.
2.2.3 Revision bars in the left margin adjacent to an entry show added, changed, or deleted data (Refer to
Fig IPD-2, Item 25).
2.2.4 Fig/Item column (Item 1).
2.2.4.1 A part not shown on the illustration is identified in the DPL as non-illustrated by a dash (-) before the
item number (Item 26).
2.2.4.2 When two or more items that are visually alike are listed in sequence, only the first item is illustrated.
The illustration, however, is applicable to both items.
2.2.4.3 When the detailed parts of an assembly or installation are illustrated, they can be identified by a
bracket. The bracket identifies the next higher assembly or installation. If brackets are not used, the
detail parts are illustrated, but the next higher assembly or installation is not.
2.2.4.4 The parts that make up a select-from range group (i.e. calibration resistor assortments) have a non-
illustrated item number or a different figure.
2.2.5 Part No. column (Item 2).

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2.2.5.1 A part number that is prefixed usually indicates a type of part or method of procurement. Examples of
these prefixes are AN, MS, and NAS. These standard part numbers may be suffixed by numbers only
or numbers and letters. Suffix numbers usually indicate configuration or design difference. Suffix
letters usually indicate material, color, or finish differences.
2.2.5.2 All procurable components manufactured by Honeywell have a part number. The part number is
stamped, etched, or cast on the part at time of manufacture when size, space, or shape is available.
More manufacturing symbol(s), letter(s), or number(s) can be shown with the part number to identify
a manufacturing process, a design change, or for a proprietary repair. Do not use this data to order a
part. Use only the item part number and nomenclature as shown in the DPL.
2.2.5.3 The letter “S” prefix of a part number designates a Honeywell standard part number. These standard
part numbers have suffix letters and numbers.
2.2.5.4 Honeywell commercial standard numbers are used in the parts lists to identify off-the-shelf items
procured from another manufacturer. A commercial standard number can be a ten or eleven digit
number.
2.2.5.5 Nonprocurable part numbers are usually easy to identify and are primarily used for information
purposes. The part number NONPROCXXX is not procurable and should not be ordered.
2.2.5.5.1 The part number NONPROCXXX is primarily used to sub-divide components into a logical, easy to
use, subgroup. The subgroup is not procurable, but is used to identify a group of procurable
components.
2.2.6 Manuf. Code column (Item 3).
2.2.6.1 Vendors are shown with a code number. This code, from H4/H8 CAGE Codes, identifies where to get
that item (Item 27).
2.2.7 Description column (Item 4).
2.2.7.1 The indenture code shows the relationship of each item to its NHA (Next Higher Assembly).
2.2.7.1.1 Each item goes in the description column one indenture (one dot) to the right of the assembly to
which it belongs.
2.2.7.1.2 The items at the same indenture are all components of a single assembly or subassembly. Refer to
Fig IPD-1 for an example of the indenture code system.

Fig IPD-1 Description Indentures

2.2.7.2 Wherever possible, abbreviations will agree with the ASME Y14.38 specification. The non-standard
abbreviations that spell words are not used.
2.2.7.3 A Honeywell specification drawing number will be shown if applicable.
2.2.7.4 Refer to this list of possible explanation terms. These terms may be abbreviated.

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2.2.7.4.1 OPTIONAL shows that the part is an optional alternative to other parts in the same item number
variant group (Fig IPD-2, Item 7).
2.2.7.4.2 ALTERNATE shows that the part is an alternative to other parts in the same item number variant
group (Item 8).
2.2.7.4.3 SUPERSEDED BY shows that the part is replaced by the part number or item number shown and is
not interchangeable (Item 9).
2.2.7.4.4 SUPERSEDES shows that the part replaces the part number or item number shown and is not
interchangeable (Item 10).
2.2.7.4.5 REPLACED BY shows that the part is replaced by the part number or item number shown and is
interchangeable. Part can be used until the supply is gone (Item 11).
2.2.7.4.6 REPLACES shows that the part replaces the part number or item number shown and is
interchangeable (Item 12).
2.2.7.4.7 PRE SERVICE BULLETIN XXXX shows that the part is used if service bulletin XXXX was not done
(Item 13).
2.2.7.4.8 POST SERVICE BULLETIN XXXX shows that the part is used if service bulletin XXXX was done
(Item 14).
2.2.7.4.9 PRE SPARE PARTS BULLETIN XXXX shows that the part is used if spare parts bulletin XXXX was
not done (Item 15).
2.2.7.4.10 POST SPARE PARTS BULLETIN XXXX shows that the part is used if spare parts bulletin XXXX was
done (Item 16).
2.2.7.4.11 NONREPAIRABLE shows that the part cannot be repaired (Item 17).
2.2.7.4.12 NONPROCURABLE shows that the part or assembled parts cannot be purchased and no part
number exists for the assembly. The components of the assembled parts can be ordered unless
differently specified (Item 18).
2.2.7.4.13 ORDER NEXT HIGHER ASSEMBLY shows that the part number is part of a matched set and cannot
be ordered independently. The next higher assembly can be ordered (Item 19).
2.2.7.4.14 OVERLENGTH PART NUMBER shows a nonstandard or reference part number (Item 20).
2.2.7.4.15 DELETED shows the part is not available for use (Item 21).
2.2.7.4.16 SEE FIGURE FOR BREAKDOWN shows the part number details in a different figure (Item 22).
2.2.7.4.17 SEE FIGURE FOR NEXT HIGHER ASSEMBLY refers the part number to the next higher assembly
(Item 23)
2.2.7.4.18 USE WITH (ITEM or PART NUMBER) shows a part is used with a different part (Item 24).
2.2.7.4.19 REFER TO ATA or PUBLICATION NUMBER identifies the assemblies that have their own CMP
(Component Maintenance Publications).
2.2.7.4.20 CSD (Control Source Drawing) shows the Honeywell drawing number for the part in the PART
NUMBER column (Item 28).
2.2.7.4.21 HCSD (Honeywell Control Source Drawing) shows the Honeywell drawing number for the part in the
PART NUMBER column.
2.2.7.5 If applicable, refer to REPAIR INSTRUCTIONS for description of wire, sleeving, and lacing given in
this DPL.
2.2.8 Usable on code assy column (Item 5)
2.2.8.1 The effectivity code identifies the different configurations of the top assembly in each IPD figure.
2.2.8.2 If this column is empty, the part is used in all configurations of the top assembly for that IPD figure.
2.2.8.3 If this column has a letter code in it, the part is only used in the configuration of the top assembly that
has the same letter code (Item 31).

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2.2.8.4 If this column has more than one letter code, the part is used in each top assembly with the same
letter codes.
2.2.8.5 If a comma separates the column entry (A, C), the other codes do not apply. For example, a
component coded “A, C” is applicable for Codes A and C only and not applicable for Code B.
2.2.8.6 If a dash separates the column entry (A-C), the other codes do apply. For example, a component
coded “A-C” is applicable for Codes A, B, and C.
2.2.8.7 This column also shows “use with” and “component of” parts data. Use numbers when the effectivity
code is not available or cannot be satisfactorily used to show this type of data. This code shows a
relationship between parts in the same figure (Item 29).
2.2.9 Units per assembly / Unit of issue column (Item 6).
2.2.9.1 The units per assembly column shows the quantity of parts necessary in the assembly of one next
higher assembly. The letters AR in this column show “as required” items and refer to bulk items or
adjustable quantity items, such as shims or spacers. The letters RF are used to show an item that is
shown in another area with a quantity (Items 30, 31 and 32).
3 References
3.1 The list that follows identifies references that are related to this section:
– CAGE (Commercial and Government Entity) codes and manufacturers' addresses are available at
https://cage.dla.mil.

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Fig IPD-2 Detailed Parts List Example


End of HONAERO-A-00-40-00-01A-018B-D
End of IPD INTRODUCTION

IPD INTRODUCTION
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Intentionally Left Blank

IPD INTRODUCTION
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Numerical Index
AIRLINE FIG. TTL
PART NUMBER PART NO. ITEM REQ

1037408-1 1 015A 1
1037428-1 1 020A 1
2119332-00 1 -001A RF
2119332-01 1 -001B RF
333-902-9002 1 -200A 14
-235A 14
-265A 3
333-902-9004 1 -145A 17
-165A 1
-260A 2
-295A 7
53001923-6 1 090A 2
097A 2
53003440-1 1 110A 2
65000031-6 1 -010A 1
65000031-9 1 -010B 1
65052188-1 1 -130A 1
65052188-11 1 210A 1
65052188-13 1 155A 1
65052188-20 1 140A 1
65052188-21 1 255A 1
65052188-22 1 -175A 1
65052188-23 1 -215A 1
65052188-24 1 -160A 1
65052188-25 1 190A 1
65052188-3 1 -135A 1
65052188-31 1 -185A 1
225A 1
65052188-33 1 -180A 2
65052188-35 1 220A 2
65052188-7 1 -250A 1
65052188-9 1 170A 1
65052247-2 1 040A 2
65052324-6 1 025A 1
65052324-8 1 030A 1
65052873-1 1 065A 1
65052873-2 1 -065B 1
65054585-1 1 -050A 1
-050C 1
65054633-2 1 095A 1
65054690-1 1 080A 1
65054731-1 1 115A 2
65054988-2 1 -065C 1
65055585-1 1 -050B 1
AN961-4T 1 060A 14
075A 14
DP2119332-1 1 005A 1
M24308-26-1 1 120A 4

ILLUSTRATED PARTS DATA


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AIRLINE FIG. TTL


PART NUMBER PART NO. ITEM REQ

MS20426AD2-3 1 -195A 39
-230A 38
MS20426AD4-5 1 240A 13
MS24693C24 1 150A 7
205A 7
245A 5
MS24693C25 1 270A 6
MS39087-307AN 1 275A 1
NAS1189E06P6L 1 085A 6
NAS1189E06P8L 1 290A 2
NAS1189E3P8L 1 280A 2
NAS1190E04P5L 1 045A 1
055A 14
070A 14
100A 3
NAS620C4L 1 105A 3
125A 4
NAS622CT2 1 285A 1
S10009E25Y 1 035A 1

ILLUSTRATED PARTS DATA


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HON64547-A-21-34-06-01A-941A-C (2015-10-22)

Outflow Valve Control Unit — Illustrated Parts Data - IPD

ILLUSTRATED PARTS DATA


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Intentionally Left Blank

ILLUSTRATED PARTS DATA


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IPD Figure 1 Outflow Valve Control Unit

ILLUSTRATED PARTS DATA


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Units per
Fig / Manuf. Usable on assembly
Part No. Description
Item Code code assy / Unit of
Issue

01
-001A 2119332-00 64547 OUTLINE, OUTFLOW VALVE CONTROL A RF
UNIT
-001B 2119332-01 64547 OUTLINE, OUTFLOW VALVE CONTROL B RF
UNIT
005A DP2119332-1 64547 • PLATE, DATA 1

-010A 65000031-6 64547 • TOP ASSY CPCS OCU A 1


-010B 65000031-9 64547 • TOP ASSY CPCS OCU B 1
015A 1037408-1 64547 • • LABEL 1
020A 1037428-1 64547 • • LABEL 1
025A 65052324-6 64547 • • PLATE, INFORMATION 1

030A 65052324-8 64547 • • PLATE, INFORMATION 1

035A S10009E25Y 64547 • • LABEL CAUTION 1


040A 65052247-2 64547 • • COVER ASSY 2
045A NAS1190E04P5L 80205 • • SCREW 1
-050A 65054585-1 64547 • • PRINTED BOARD ASSEMBLY - A 1
OUTFLOW VALVE CONTROL UNIT,
BACKUP MOTOR DRIVER
-050B 65055585-1 64547 • • PRINTED BOARD ASSEMBLY - B 1
OUTFLOW VALVE CONTROL UNIT,
BACKUP MOTOR DRIVER
-050C 65054585-1 64547 • • PRINTED BOARD ASSEMBLY - B 1
OUTFLOW VALVE CONTROL UNIT,
BACKUP MOTOR DRIVER
(ALTN PN)

055A NAS1190E04P5L 80205 * * SCREW 14


060A AN961-4T 80205 * * WASHER 14
065A 65052873-1 64547 • • PRINTED BOARD ASSEMBLY- A 1
OUTFLOW VALVE CONTROL UNIT,
COMMAND/MONITOR
(ALTN PN)

-065B 65052873-2 64547 • • PRINTED BOARD ASSEMBLY- A 1


OUTFLOW VALVE CONTROL UNIT,
COMMAND/MONITOR
- Item Not Illustrated
ILLUSTRATED PARTS DATA
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Units per
Fig / Manuf. Usable on assembly
Part No. Description
Item Code code assy / Unit of
Issue

-065C 65054988-2 64547 • • PRINTED BOARD ASSEMBLY- B 1


OUTFLOW VALVE CONTROL UNIT,
COMMAND/MONITOR
070A NAS1190E04P5L 80205 * * SCREW 14
075A AN961-4T 80205 * * WASHER 14
080A 65054690-1 64547 • • PRINTED BOARD ASSEMBLY 1
ELECTRO-MAGNETIC INTERFACE
085A NAS1189E06P6L 80205 * * SCREW 6
090A 53001923-6 30634 • • FITTING 2
095A 65054633-2 64547 • • MANIFOLD 1
097A 53001923-6 30634 • • • FITTING 2
100A NAS1190E04P5L 80205 * * SCREW 3
105A NAS620C4L 80205 * * WASHER 3
110A 53003440-1 64547 * * O-RING 2
115A 65054731-1 64547 • • RING, RETAINING 2

120A M24308-26-1 64547 • • SCREW LOCK FEMALE 4


(ORDER PN M24308/26-1)

125A NAS620C4L 80205 • • WASHER 4


-130A 65052188-1 64547 • • CHASSIS, ASSEMBLY 1

-135A 65052188-3 64547 • • • ASSY, CHASSIS FRAME 1

140A 65052188-20 64547 • • • • CHASSIS, FRAME 1

-145A 333-902-9004 46384 • • • • FASTENER 17


150A MS24693C24 80205 • • • SCREW 7
(ORDER PN MS24693-C24)

155A 65052188-13 64547 • • • COVER, ACCESS ASSEMBLY 1

-160A 65052188-24 64547 • • • • COVER, ACCESS 1

-165A 333-902-9004 46384 • • • • FASTENER 1


170A 65052188-9 64547 • • • COVER, RIGHT ASSEMBLY 1

-175A 65052188-22 64547 • • • • COVER, RIGHT 1

-180A 65052188-33 64547 • • • • RAIL, PBA SUPPORT, MEDIUM 2


- Item Not Illustrated
ILLUSTRATED PARTS DATA
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Units per
Fig / Manuf. Usable on assembly
Part No. Description
Item Code code assy / Unit of
Issue

-185A 65052188-31 64547 • • • • RAIL, PBA SUPPORT, SHORT 1

190A 65052188-25 64547 • • • • PLATE, JOINER 1

-195A MS20426AD2-3 80205 * * * * RIVET, CTSK 39

-200A 333-902-9002 46384 • • • • FASTENER 14


205A MS24693C24 80205 • • • SCREW 7
(ORDER PN MS24693-C24)

210A 65052188-11 64547 • • • COVER, LEFT ASSEMBLY 1

-215A 65052188-23 64547 • • • • COVER, LEFT 1

220A 65052188-35 64547 • • • • RAIL, PBA SUPPORT, LONG 2

225A 65052188-31 64547 • • • • RAIL, PBA SUPPORT, SHORT 1

-230A MS20426AD2-3 80205 * * * * RIVET, CTSK 38

-235A 333-902-9002 46384 • • • • FASTENER 14


240A MS20426AD4-5 80205 • • • RIVET, CTSK 13

245A MS24693C24 80205 * * * SCREW 5


(ORDER PN MS24693-C24)

-250A 65052188-7 64547 • • • PLATE, FRONT ASSEMBLY 1

255A 65052188-21 64547 • • • • PLATE, FRONT 1

-260A 333-902-9004 46384 • • • • FASTENER 2


-265A 333-902-9002 46384 • • • • FASTENER 3
270A MS24693C25 80205 • • • SCREW 6
(ORDER PN MS24693-C25)

275A MS39087-307AN 96906 • • • HANDLE BOW 1


280A NAS1189E3P8L 80205 * * * SCREW, SELF-LOCKING 2

285A NAS622CT2 80205 • • • HOOK, SUPPORT, CRES 1

290A NAS1189E06P8L 80205 * * * SCREW SELF-LKG 2


-295A 333-902-9004 46384 • • • FASTENER 7

End of HON64547-A-21-34-06-01A-941A-C

- Item Not Illustrated


ILLUSTRATED PARTS DATA
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