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Technologies, Inc.
!scott
Aviation
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COMPONENT
MAINTENANCE
MANUAL
-with-
ILLUSTRATED
PARTS LIST
(CMM with IPL)
ATA Chapter 35 - Oxygen
e
Multiple ETN's Apply
5500 and 5600 Series
Portable Cylinder Assemblies
Scott Aviation
A Scott Technologies Company
Tyco International
225 Erie Street
Lancaster NY 14086-9502
USA
Tel: 716-683-5100
Fax: 716-681-1089
Vendor Code: 53655
www.scottaviation.com
Original Issue Date: 20040415
© Copyright Scott Technologies. Inc. 2004 All Rights Reserved
•
35-32-18
IlIformatJon contained in Ihis mallllal is
for tile sok: use of performing wor k on
l\mcrtC3n Eagle ain:nfl and/or components.
TITLE PAGE
PAGE T-1/2
20040415
•
.
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1:qCD /scott
Technologies. Inc.
jSCDtt
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & U'L
SERVICE
BULLETIN
LIST
Keep this record in the front of this Component Maintenance Manual (CMM). When you receive service bulletins
or service information letters for this CMM write the service bulletin or service information letter number and the
date issued in the table below.
SERVICE BULLETIN
SERVICE BULLETIN
or
or
SERVICE
INFORMATION LEDER
ISSUE
DATE
DATE
INCORPORATED
Sll-35-21
20030212
20040415
SERVICE
INFORMATION LEITER
ISSUE
DATE
DATE
INCORPORATED
•
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BULLETIN
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SCO/l
Techn%gies.
Scott
Aviation
CMM & IPL
Co
LIST OF EFFECTIVE
Subject
Page
Date
PAGES
Subject
TitlePage
Record ofRevisions
Record ofTemporary
Revisions
ServiceBulletinList
Listor EffectivePages
T-1/2
RR-112
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Description& Operation
(Continued)
RTR-1/2
SBL-112
lEP-1
lEP·2
LEP-3
LEP-4
TC-1
TC-2
TC-3
TC-4
Te-5
TC-6
INTRO-1
INTRO-2
INTRO-3
INTRO-4
INTRO-5/6
1
2
3
4
5
6
7
8
9
10
11
12
13
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15
16
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Testing& FaullIsolation
Introduction
Description& Operation
17
18
19
20
•
I
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
Table ofContents
•
Inc.
Schematics & Wiring
Diagrams
Disassembly
Cleaning
Page
Date
21
22
1001
1002
1003
1004
1005
1006
1007
1008
1009
1010
1011
1012
1013
1014
1015
1016
1017
1018
1019
1020
1021
1022
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CM'" & /PL
~
SUbject
Page
Date
SUbject
Page
Date
Cleaning (Continued)
4005
4006
5001
5002
5003
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6003
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6006
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Assembly (Continued)
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7029
7030
7031
7032
8001/8002
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9002
9003
9004
9005
9006
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10002
10003
10004
10005
10006
10007
10008
10009
10010
10011
10012
10013
10014
10015
10016
10017
10018
10019
10020
10021
10022
10023
10024
10025
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Check
Repair
6007/6008
7001
7002
7003
7004
7005
7006
7007
7008
7009
7010
7011
7012
7013
7014
7015
7016
7017
7018
7019
7020
7021
7022
Assembly
7023
7024
7025
7026
EFFECTIVITY:
ALL
7033170034
Fits & Clearances
Special Tools, Fixtures,
Equipment, & Consumables
Illustrated Parts List
LIST OF EFFECTIVE
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Technologies. Inc.
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY • CMM & IPL
("
SUbject
Illustrated Parts List
(Continued)
•
•
I
Page
Date
10027
10028
10029
10030
10031
10032
10033
10034
10035
10036
10037
10038
10039
10040
10041
10042
10043
10044
10045
10046
10047
10048
10049
10050
10051
10052
10053
10054
10055
10056
10057
10058
10059
10060
10061
10062
10063
10064
10065
10066
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Subiect
Illustrated Parts List
(Continued)
Page
Date
10067
10068
10069
10070
10071
10072
10073
10074
10075
10076
10077
10078
10079
10080
10081
10082
10083
10084
10085
10086
10087
10088
10089
10090
10091
10092
10093
10094
10095
10096
10097
10098
10099
10100
10101
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Inc.
I
Scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
Subject
Illustrated Parts list
(Continued)
EFFECTIVITY:
ALL
.....
CMM & IPL
Page
Date
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10108
10109
10110
10111
10112
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10114
10115
10116
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10118
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10122
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~
Subject
Page
Illustrated Parts list
(Continued)
Special Procedures
Removal
Installation
Servicing
10129
. 10130
10131
10132
10133
10134
10135
10136
. 10137
10138
10139
10140
10141
10142
11001/11002
12001/12002
. 13001/13002
14001/14002
Storage
15001
15002
Rework
16001/16002
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LIST OF EFFECTIVE PAGES
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t'lco/SCOtl
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEAfBLY • CMM & IPL
TABLE OF CONTENTS
PAGE
SUB..IECT
INTRODUCTION
--
1. Scope
2. Warning, Cautions, and Notes
3. Product Support Services
4. Abbreviations
5. Verification
.
.
.
.
..
,
DESCRIPTION & OPERATION _1. General
,
2. Leading Particulars
A. 5500 Series PCA
"
B. 5600 Series PCA
"
3. Part Number Identification
4. Part Number Guidelines
"
5. Purpose of Equipment
6. Typical Installation
7. Operation
A. Respirator Regulator
B. Cylinder
C. Regulator Assembly
D. Harness Assemblies and Mask Assemblies in
Fastener-Mounted Storage Bags
E. Outlet Assembly
F. RegUlator SUbassemblies
B. Optional PCA Mounting Bracket Set
•
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_
EFFECTIVITY:
ALL
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TESTING & FAULT ISOLATION
1. General.................................................................................................
2. Reference Documents
3. Special Tools, Fixtures, and Test EqUipment
4. Consumable Test Materials
5. Relief Valve Assembly Test
A. Leakage
B. Flow
C. Pressure to Close
6. Outlet Assembly Test
A. Full Flow (non-metered) Outlet Assemblies
B. Leak Test of Test Setup
C. Constant Flow (metered) "Precision" Type OuUet Assemblies
D. Constant Flow (metered) "Adjustable" Type Outlet Assemblies
7. Respirator Regulator Tests ..
A. Demand Valve Assembly Leakage
B. Inward Leakage Test
C. Outward Leakage Test
D. Flow Test
8. RegUlator Assembly Output Pressure Test
9. Gauge Accuracy Test
10. Valve Torque Test
INTRO-1
INTRO-1
INTRO-2
INTRO-3
INTRO-3
INTRO-5
,
1
1
1
5
B
12
13
13
14
14
15
15
17
17
19
21
1001
1001
1002
1002
1004
1005
1005
1005
1005
1005
1006
1007
1007
1008
1009
1009
1010
1010
1011
1013
1015
1016
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-tyca!scott
/scott
.".
Technologies.
Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & #PL
SUBJECT
PAGE
11. PCA Final Test
1017
1017
1018
1018
A. External Leakage
B. Functional Test
12. Fault Isolation
SCHEMATICS AND WIRING DIAGRAMS
2001
DISASSEMBLY
1. General
2. Special Tools, Fixtures, and Equipment
3. General PCA Disassembly
A. 5600 Series Only
B. 5500 & 5600 Series
C. 5500 Series Only
4. Respirator Regulator Assembly Disassembly
A. Cover Assembly Removal, and Disassembly
B. Diaphragm Removal
C. Deflector and Demand Valve Assembly Removal and
Disassembly
,
D. General Disassembly
5. Regulator Port Device Removal and Disassembly
A. Gauge
B. Relief Valve Assembly
C. Charging Valve
D. Safety Plug Assembly or Safety Outlet Assembly
E. On/OffValve
F. SPN 800503·00,5009-00,or 5009 Series Outlet Assembly
G. 5041-00 and 5041 Series Outlet Assembly
H. 5507-00 and 5507 Series Outlet Assembly
J. SPN 10003566 Oxygen Coupling or SPN 802856-01
Outlet Assembly
K. SPN 5052-00 Outlet Assembly
L. SPN 36728-01 Outlet Assembly
M. SPN 10006017 Outlet Assembly
N. SPN 8572-02 Outlet Assembly
P. SPN 802863-02 Outlet Assembly
"
6. General Regulator Disassembly
A. 5500 & 5600 series
B. 5500 Series Only
CLEANING
1. General
2. Safety
3. Reference Documents
4. Special Tools, Fixtures, and Equipment
5. Consumable Cleaning Materials
6. Cylinder Cleaning
A. External Cleaning
B. Generallntemal Cleaning
C. Steel Cylinder Internal Cleaning
EFFECTIVITY:
ALL
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..
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3002
3002
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3005
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3006
3006
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20040415
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tl./co/scott
/SCDtt
Technologies. Inc. AviatiDn
~ 550015600 SERIES PORTABLE CYLINDER ASSEMBLY - CMM & ,PL
SUBJECT
PAGE
D. Composite Cylinder Internal Cleaning
7. PAX Mask Assemblies
8. Metallic Parts ...... "................................................................................
9. Non-Metallic Parts
10. Miscellaneous Parts
4005
4005
4006
4006
4006
CHECK
1. General.................................................................................................
2. Reference Documents
3. Special Tools, Fixtures, and Equipment
4. PCA and PCA Components
A. General.....
B. Gauge
C. Plates, Decals, Placards, and Labels
D. Harness Assemblies
".........................
E. Pass Oxygen Mask Assemblies
5. Cylinder Assembly
A. Composite Cylinder
B. DOT-3HT-1B50 Steel Cylinder
C. DOT-3AA-1800SteeICylinder
"..............................................
6. Optional PCA Mounting Bracket Set
•
•
REPAIR
----1. General
2. Reference Documents
3. Special Tools, Fixtures, and Equipment
4. Consumable Repair Materials
5. Repair
6. Steel Cylinder Phosphate Coating
A. Surface Preparation
B. Phosphate Coating
7. Steel Cylinder Paint Application
A. Surface Preparation
B. Primer Application
C. Paint Application
8. Composite Cylinder Paint Application
A. Surface Preparation
B. Paint Application
9. Optional PCA Mounting Bracket Set
_
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..
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..
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..
.
.
ASSEMBLY
1. General..
2. Reference Documents
".........................
3. Special Tools, Fixtures, and Equipment
".........................
4. Consumable Assembly Materials
".........................
5. Pre-Assembly Information
6. Outlet Assemblies
A. Constant Flow (metered) Type Outlet Assemblies
B. Full Flow (non-metered) Type Outlet Assemblies
EFFECTIVITY:
ALL
5001
5001
5002
5003
5003
5003
5003
5003
5003
5003
5004
5005
5005
5006
5006
6001
6001
6001
6001
6002
6003
6003
6004
6004
6005
6005
6005
6005
6006
6006
6006
6007
7001
7001
7001
7002
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7007
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/scott
Technologies, Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
.-
CMM & IPL
1
SUBJECT
PAGE
7. Respirator Regulator
A. General Assembly
B. Demand Valve Assembly
C. Demand Valve Assembly Leak Test
D. Deflector
E. Diaphragm
F. Cover Assembly
,
8. Regulator Assembly
A. General Assembly
,
B. Safety Plug
C. Safety Outlet Assembly
D. Charging Valve
E. On/Off Valve
F. Gauge
G. Testing
H. Final Assembly
9. PCA Assembly
A. Regulator Assembly
B. Regulator Assembly
C. Relief Valve Assembly
D. Harness
E. Respirator Regulator Assembly
F. OuUetAssemblies
G. Decal, Plate, Placard, and Label
10. PCA Charging Procedure
A. PCA Charging Setup
B. Charge the PCA
C. Disconnect the PCA
D. Testing
11. Final PCA Assembly
A. PIN 801660-00 Harness Assembly
B. PIN 801658-00 Harness Assembly
C. PIN 801662-00 Harness Assembly
D. PIN 801660-03, -05 Harness Assemblies
E. PIN's 801807-01, -02, -03 Mask Storage Bag and
Harness Assembly
F. PIN's 801808-01 -02, -03, -05 Mask Storage Bag and
Harness Assembly
G. PIN's 803177-01. -02,-03 Mask Storage Bag and
Harness Assembly
H. PIN 805436-01 Mask Storage Bag and Harness Assembly
..
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7009
7009
7009
7010
7010
7010
7011
7014
7014
7014
7014
7015
7015
7016
7016
7016
7017
7017
7017
7017
7018
7018
7018
7020
7022
7022
7022
7022
7022
7024
7024
7024
7024
7026
..
7027
.
7027
..
..
7030
7032
•
•
r
FITS AND CLEARANCES
_
SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES _
1. Special Tools, Fixtures, and Equipment
2. Consumable Materials
3. Illustrations, Special Tools, and Fixtures
ILLUSTRATED PARTS LIST
EFFECTIVITY: All
_
8001
.
.
.
9001
9001
9004
9006
10001
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tileD/scott
Technologies.
Inc.
/scott
Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
PAGE
SUBJECT
1. Introduction
"
A. How to Use This Section
B. Numerical Index
C. Description of the Illustrated Parts list Entries
Table 1 - PCA Connguration Matrix
D. Vendor Codes
2. Overhaul Kits
A. Obtaining Overhaul Kits
B. 5500 series PCA Overhaul Kit
C. 5600 Series PCA Overhaul Kit
3. Numerical Index
4. Detailed Parts list
Figure 1 - 5500 & 5600 Series Portable Cylinder Assembly
Figure 1A - 5500A Sub Series PCA
Figure 1B - 5500B Sub Series PCA
Figure 1C - 5500C Sub Series PCA
Figure 1D - 5500D Sub Series PCA
Figure 1E - 5500F, G, J, l, M, P, AND S Sub Series PCA
Figure 1F - 5500N and 55000 Sub Series PCA
Figure 1G - 5500T Sub Series PCA
,
Figure 1 H - 5600-1 and 5600-2 Sub Series PCA
Fjgure 1J - 5600-8 and 5600-9 Sub Series PCA
Figure 2 - 5500 and 5600 Series PCA
Harness Assembly with Mask and Storage Bag
Figure 3 - PIN's 6379-2C, -20 and 800649-00, -01
Respirator Regulator Assembly
Figure 4 - PIN 5041-00 and 5041 Series Outlet Assembly
Figure 5 - PIN 5009-00 and 5009 Series and 800503-00
Outlet Assemblies
Figure 6 - PIN 8572-00 Outlet Assembly
Figure 7 - PIN 5507-00 and 5507 Series OuUetAssembly
Figure 8 - PIN 5052-00 Outlet Assembly
Figure 9 - PIN 5510 series and 803199-04
Regulator Assembly
Figure 10 - PIN 802863-02 Outlet Assembly
Figure 11 -PIN 802856-01 Outlet Assembly
Figure 12 -PIN's 2661-03. -04 and 802821-01
Pressure Gauge Assembly
Figure 13 - PIN 36728-01 Outlet Assembly
•
.
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.
..
10112
10116
..
..
..
.
10120
10125
10126
10130
..
..
.
10132
10136
10138
.
.
10140
10142
__
11001
REMOVAl
_
12001
SERVICING
•
10001
10001
10001
10001
10002
10008
10009
10009
10009
10010
10011
10035
10036
10040
10052
10060
10072
10078
10086
10090
10092
10102
SPEC~PROCEDURES
INSTALLATION
EFFECTIVITY:
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/scott
..
".
Aviation
55Da'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
SUBJECT
CMM & IPL
PAGE
STORAGE
1. General
2. Storage
3. Transportation
A. Reference Documents
B. Packaging
15001
15001
15001
15001
15001
15002
REWORK
16001
•
•
EFFECTIVITY:
ALL
35-32-18
Page TC-6
20040415
•
35-32-18
A/C Type: SAAB
Eng.Code:
Manual: 35-32-18
ATA Chapt: 35
ENGINEERING TECHNICAL NOTICE LOG
ETN #
Rev.
G1-25-053
G1-35-009
G1-35-010
1
R1
PAGE REF.
DATE INSERTED DATE REMOVED
10/26/2007
10/26/2007
10/26/2007
INITIALS
COMMENTS
•
.
....
'tqeD / Technolog;es,
Scott
Inc.
/ Scoff
Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & fPL
~
INTRODUCTION
TASK 35-32-18-99F-801
1. Scope
This manual establishes the user maintenance, overhaul, and service procedures for servicing the
5500 Series and 5600 Series Portable Cylinder Assemblies (PCA) described herein. Configurations of the
5500 and 5600 Series PCA's that are covered by this CMM include but are not limited to the following:
•
•
SCOTT PIN
5500-A 1A-AB23A
5500-A 1A-A 15A
5500-A 1A-BB23A
5500-A 1A-BB25A
5500-A 1A-BC30A
5500-A 1A-BE20A
5500-A 1A-BE20B
5500-A 1A-BF10A
5500-A1A-BF20B
5500-A 1A-BF23A
5500-A1A-BF23B
5500-A1A-BF23D
5500-A1A-BF25A
5500-A1A-BF25B
5500-A1A-BF30A
5500-A1A-B15A
5500-A 1A-B20A
5500-A1A-e30B
5500-A 1A-E20A
5500-A 1A-E20B
5500-A 1A-F20A
5500-A 1A-F20B
5500-A 1A-F20D
5500-A 1A-F23A
5500-A 1A-F25A
5500-A1A-F25AN
5500-A1A-XOK
5500-A1A-VYOE
5500-A 1B-F23A
5500-A 1M-M 15B
5500-A 1N-BF23A
5500-A 10-B30AO
5500-A 10-B300
5500-A 10-B300A
5500-A 1R-EE25A
5500-A 1S-B20A
5500-A 1S-CC30A
5500-A 1T-BF20B
5500-A 1U-BF23A
5500-A 1U-BF25A
5500-A 1U-EE25A
5500-A 1U-F30AN
EFFECTIVITY:
ALL
SCOTT PIN
5500-A1V-BF20B
5500-A1V-BF23B
5500-A 1V-BF25B
5500-A 1V-F20BM
5500-A 1W-BF23A
5500-A 1W-BF25A
5500-A 1W-BF30A
5500-A1X-BF20B
5500-A1X-FF23A
5500-A W -BF20B
5500-A3A-BF23A
5500-ASA-BG20B
5500-A6A-BF23A
5500-A6A-BF238
5500-A6A-BG20B
5500-A6A-F20B
5500-A6P-FF23A
5500-A6S-B30A
5500-A6U-E30A
5500-A6W-BB 15A
5500-A6W-BB23A
5500-A6W-BB25A
5500-A6W-FF23A
5500-A6W-F30AP
5500-A9A-B30A
5500-A9S-AC25A
5500-A9S-BF30A
5500-A9S-G30A
5500-A9W-EE25A
5500-A9X-F23A
5500-B1A-BE20B
5500-B 1A-B F20A
5500-B 1A-B F20B
5500-B1A-BF20D
5500-B 1A-BF23A
5500-B1A-BF23B
5500-B 1A-B F25A
5500-B1A-B30A
5500-B 1A-CF23A
5500-B 1A-CF25A
5500-B1A-FF20A
5500-B1 A-F20D
SCOTT PIN
5500-B1A-F23A
5500-B1A-F30A
5500-B1A-YYOE
5500-B1A-YOP
5500-B 1S-B20A
5500-B1 S-B20AP
5500-B1 U-BF23A
5500-B1V-BE20B
5500-B1V-BF20B
5500-B1W-BF10A
5500-B 1W-BF20A
5500-B 1X-VYOE
5500-B1X-YOE
5500-B3B-F25A
5500-B6C-BF25A
5500-B6U-BF25A
5500-B6U-F30AN
5500-C1A-BB20B
5500-C1A-BF20A
5500-C1A-BF20B
5500-C1A-BF20D
5500-C1A-BF23A
5500-C1A-BF23B
5500-C1A-BF23D
5500-C1 A-BF30A
5500-C1 A-BG23A
5500-C1 A-B23A
5500-C1 A-EG23A
5500-C1 A-EY20BM
5500-C1A-E20BN
5500-C1 A-E23AN
5500-C1A-FF20A
5500-C1A-FF23A
5500-C1A-FG23A
5500-C1A-FH23A
5500-C1A-FY30BN
5500-C1A-F20B
5500-C1A-F23A
5500-C1A-F23AP
5500-C1A-F25A
5500-C1A-XOK
5500-C1A-VYOE
SCOTT PIN
5500-C1A- VYOEE
5500-C1A- VYON
5500-C1 A-YOE
5500-C1 A-YOEE
5500-C1A- YON
5500-C1B-BF23D
5500-C18-E25A
5500-C1 N-BF23A
5500-C1 S-BF20A
5500-C 1S-BY20AE
5500-C1 S-B20AE
5500-C 1S-B20AP
5500-C 1S-F23A
5500-CH-BF20B
5500-CH -F20BM
5500-C 1U-BF23A
5500-e1 U-BF25A
5500-e1 U·BF30A
5500-C1 U-B23AN
5500-C1 U-B25A
5500-C1 U-FF23A
5500-C1 U-F20AN
5500-C1 U-F23A
5500-C1 U-F30AN
5500-e1V-FG20B
5500-e1V-FY30AN
5500-e1V-FY30BN
5500-e1V-F20BM
5500-e1V-F30AN
5500-eW-F30BN
5500-e1W-BF15A
5500-e1 W-BF23A
5500-e1 W-BF30A
5500-e1X-BF20B
5500-e 1X-YON
5500-eW-BF20B
5500-e6A-BF1SA
5500-e6A-BF20B
5500-eSA-BF23A
5500-e6A-BF23B
5500-C6A-BF230
550Q-C6A-BF25A
35-32-18
SCOTT PIN
550o-C6A-BG30B
550o-C6A-EF20A
550o-C6A-F20A
550o-C6A-F20AR
550o-C6A-F23AE
550o-C6A-F30A
550o-C6A-F30AE
550o-C6A-F30AN
550o-C6A-G30AN
550o-C6A- VYON
5500-C6A- YON
5500-C6E-BF23D
5500-C6R-BF23D
5500-C6T -G20B
5500-C6U-BF30A
5500-C6U-F23AP
5500-C6U-F30AN
5500-C6W-FF23A
5500-C6X-BF230
5500-C9A-BF20A
5500-C9A-BF20B
5500-C9A-FF10A
5500-C9S-F30A
5500-C9U-F30AN
5500-C9U-H20A
5500-C9W-FF10A
5500-C9W-YOE
5500-C9X-BB20A
5500-D1A-BF23A
5500-D1A-E20A
5500-D1A-E25A
5500-D1A-F23A
5500-D1A-VYOE
5500-0 1A-YYOP
5500-D1A-YOE
5500-D1A-YON
5500-01 P-CC20A
5500-D1W-BB15A
5500-D1X-YOE
5500-01X-YON
5500-D6A- VYOE
550o-D6A- YVON
INTRODUCTION
Page INTRO-1
20040415
"tqCD /
SCott
TechnoJogies. Inc.
I
,-
Scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
4
CMM & IPL
"1
1. Scope (Continued)
SCOTT PIN
5500-06A-YOE
5500-06P-B F25A
5500-D6X-HH30A
5500-F1 X-FH20A
5500-F6A-BB30A
5500-G1 A-B23A
5500-G1 A-F20A
5500-G1W-EE30A
5500-J1A-ABE20B
5500-J1 A-BBF20A
5500-J1A-BBF20B
5500-J 1A-BBF23A
5500-J1A-BEG20B
5500-J 1A-BFL23A
5500-L 1W-BBF23A
5500-L6C-BBF23A
5500-L6C-BBF25A
5500-L6U-BBF25A
5500-L6W-BBF25A
5500-L6W-BEF23A
5500-L6W-FF23AP
5500-M1A-BBB20B
5500-M1A-BH23A
5500-M1A-BH23AN
5500-M1A-FFF25A
5500-M1 A-LLL30A
5500-M1 A-XOK
5500-M1W-BF23AM
5500-M6W-BBF10A
SCOTT PIN
550D-M6W-FF23AN
550D-M6W-FF23AP
5500-P6U-EEE20A
5500-S6X- YVOE
5500-S6X- YVON
5500-S9X- VYYOE
5500-S9X-YVOE
5500-N6S-BF10A
5500-Q6X-BF10A
5500-Q6X-BF23A
5500-Q6X- YYOE
5500- T2A-CC30B
5600-1 B1A-E20B
5600-1 B1A-F23A
5600-1 C1A-B20A
5600-1 C1A-B20B
5600-1 C1A-B23A
5600-1 C1A-E20A
5600-1 C1A-E20B
5600-1 C1A-E20D
5600-1 C1A-E23A
5600-1 C1A-E23B
5600-1 C1A-F20A
5600-1C1A-F20B
5600-1C1A-F23A
5600-1C1A-F23B
5600-1 C1A-F25A
5600-1C1A-XOK
SCOTT PIN
5600-1C1A-XOM
5600-1 C1A- YOM
5600-1C1B-XOK
5600-1C1B-XOM
5600-1 C1B-YOM
5600-1 C6A-E20A
5600-1 C6A-F23A
5600-1 C6A-F23B
5600-1 C6A-XOK
5600-101 A-F23A
5600-101 A-F30A
5600-106A-E20A
5600-1G1A-F20A
5600-1M1A-F20BM
5600-2A 1A-B23B
5600-2A1A-F23A
560D-2B1A-E20A
5600-2B1 A-F20A
560D-2B1 A-YOE
5600-2C1A-B20B
5600-2C1 A-C20A
560D-2C1 A-E20A
560D-2C1 A-E20B
560D-2C1 A-E20C
560D-2C1A-E20D
560Q-2C1A-E23A
560Q-2C1A-E238
560Q-2C1A-F20A
SCOTT PIN
5600-2C1A-F30A
5600-2C1 A-G25A
5600-2C1A-XOK
5600-2C1A-XOM
5600-2C1 A-YOM
5600-2C1 A-YON
5600-2C1 B-XOK
5600-2C5A-E20B
5600-2C6A-B23A
5600-2C6A-F23A
5600-2C6A-XOK
5600-2C9F-XOK
5600-201A-XOK
5600-201 B-XOK
56oo-2G1A-B20B
56oo-2J1 A-BF23A
5600-2M 1A-BF23A
56oo-2M 1A-BG23A
56oo-8B6A-XOK
56oo-8B9A-XOK
56oo-8C1 A-F23A
56OO-8C1A-XOK
56oo-8C1B-F23A
56oo-8C6A-F23A
56oo-8C6A-XOK
5600-801 A-XOK
5600-801 A-YON
56oo-8G2A-XOK
SCOTT PIN
5600-8G6A-XOK
5600-9C 1A-F20A
5600-9C 1A-F20B
5600-9C 1A-F23A
5600-9C 1A-XOK
5600-9C 1A-YOE
5600-9C 1A-YON
5600-9C6A-XOK
5600-9C6A- YOK
5600-9C9A-F10A
5600-9D1A-E20B
5600-901A-E30A
5600-901 A-F23A
5600-901 A-G30A
5600-901A-XOK
5600-9D1 A-YON
5600-901 B-XOK
5600-909A-XOK
5600-9G1A-XOK
56oo-9J6A-F30AN
5600-9M1A-HH20A
5600-9M6A-BF30A
5600-9M6A-FF30A
5600-9M6A-F30AE
560Q-9M6A-F30AN
5600-9M9F-F30AN
5600-9P1A-YOEN
5600-9P6A-F30AN
•
•
This manual provides the following information:
A. Warnings, Cautions, and Notes to be followed while performing service on the 5500 and 5600 Series
PCA.
B. The proper sequence of operations to be performed on the defined equipment.
C. Specifications and a list of the tools, equipment, and materials for maintenance, check, test, and repair
of the 5500 and 5600 Series PCA.
2. Warnings, Cautions. and Notes
The Warnings, Cautions and Notes call attention to important information.
A. Warnings
Warnings call attention to the use of materials, processes, methods, procedures or limits which must be
followed exactly to avoid personal injury or death.
B. Cautions
Cautions call attention to methods and procedures which must be followed to avoid damage to the
equipment.
EFFECTIVITY: ALL
35-32-18
INTRODUCTION
Page INTRO-2
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•
•
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•
tqca/scott
TechnoJogies.
Inc.
jSCDtt
A tliation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
.....
2. Warnings, Cautions, and Notes (Continued)
C. Notes
Notes call attention to methods that make the job easier.
WARNING:
ANY SERVICE OR OVERHAUL PERFORMED ON THE 5500 AND 5600 SERIES PCA
SHALL BE DONE ONLY BY THOSE FACILITIES EXPERIENCED IN, OR BY PERSONNEL
KNOWLEDGEABLE IN, AVIATION OXYGEN EQUIPMENT. IF NONE ARE KNOWN,
CONTACT SCOTT AVIATION OR ITS DISTRIBUTORS FOR NAMES OF AUTHORIZED
SERVICE CENTERS. IMPROPER USE OR IMPROPER MAINTENANCE OF THIS
EQUIPMENT MAY RESULT IN SERIOUS PERSONAL INJURY OR DEATH.
ALL PROCEDURES DESCRIBED IN THIS MANUAL MUST BE PERFORMED IN AN AREA
FREE OF OIL, GREASE, FLAMMABLE SOLVENTS OR OTHER COMBUSTIBLE
.
MATERIALS. COMBUSTIBLE MATERIALS THAT IGNITE WHEN EXPOSED TO OXYGEN
MAY RESULT IN SERIOUS PERSONAL INJURY OR DEATH.
DO NOT ALLOW OIL, GREASE, FLAMMABLE SOLVENTS OR OTHER COMBUSTIBLE
MATERIALS TO COME IN CONTACT WITH PARTS THAT WILL BE EXPOSED TO
PRESSURIZED OXYGEN. DUST, LINT, AND FINE METAL PARTICLES ARE ALSO
POTENTIAL COMBUSTIBLES THAT CAN IGNITE, AND RESULT IN EXPLOSION OR
FIRE, WHEN EXPOSED TO PRESSURIZED OXYGEN.
REFER TO AND FOLLOW ALL APPLICABLE MANUFACTURER'S OR SUPPLIER'S
MATERIAL SAFETY DATA SHEETS (MSDS) BEFORE USING PRODUCTS SPECIFIED IN
THIS MANUAL OR SERIOUS PERSONAL INJURY MAY OCCUR.
•
FAILURE TO USE TOOLS THAT ARE FREE FROM CONTAMINANTS OR ARE NOT
SUITABLE FOR USE ON OXYGEN LIFE SUPPORT EQUIPMENT, MAY RESULT IN FIRE,
EXPLOSION, OR PERSONAL INJURY DURING SUBSEQUENT USE OF THE 5500 AND
5600 SERIES PCA.
3. Product Support Services
Product support services for the equipment covered by this document are provided by Scott Aviation. The
services include repair and overhaul, replacement parts, and technical documentation.
Scott Aviation
225 Erie Street
Lancaster, NY 14086-9502
USA
Tel: 716-683-5100
Fax: 716-681-1089
Company Code: 53655
Web Site: www.scottaviation.com
4. Abbreviations
The following is a list of abbreviations found in this manual.
ABBREVIATION
AI
ALT
AR
ANPT
BKDN
Br
•
°C
EFFECTIVITY:
ALL
DEFINITION OF ITEM
Aluminum
Alternate
As Required
Aeronautical National Taper Pipe Thread
Breakdown
Brass
Degrees Celsius
35-32-18
INTRODUCTION
Page INTRO-3
20040415
�qCD /
Scott
Technologies. Inc.
!
550015600 SER/ES PORTABLE CYLINDER ASSEMBLY·
4. Abbreviations
of
FAA
FAR
FED STD
Fig or FIG
ft
ft2
gm
Hg
ID
Le.
in.
in·lb
IPL
kg
kPa
Ibs
LNG
Ipm
m
MAX
mg
min
MIN
ml
mm
MPa
MSDS
ALL
4
CMM & IPL
~
(Continued)
ABBREVIATION
CAD
cc
ccm
CFR
CGA
CID
em
cm.:!
CMM
CONFIG
CRA
CRES
cu ft
CYL
DET
DIA
DOT
EFF
e.g.
EFFECTiVITY:
..
Scott
Aviation
DEFINITION OF ITEM
Cadmium
cubic centimeter
cc per minute
Code of Federal Regulations
Compressed Gas Association
Commercial Item Description
centimeter
square centimeter
Component Maintenance Manual
Configuration
Cylinder and Regulator Assembly
Corrosion Resistant Steel
cubic feet
Cylinder
Detailed
Diameter
Department of Transportation
Effectivity
example given
Degrees Fahrenheit
Federal Aviation Administration (USA)
Federal Aviation Regulations (USA)
Federal Standard
Figure
feet
square feet
grams
Mercury
Identification or Inside Diameter
that is
inch
inch-pound
Illustrated Parts List
kilogram
kiloPascal
pounds
Long
liters per minute
meter
Maximum
milligram
minute
Minimum
milliliter
mIllimeter
MegaPascal
Material Safety Data Sheet
35-32-18
•
•
INTRODUCTION
Page INTRQ-4
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1:l/CCI/scott
Technologies,
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/scott
Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
4. Abbreviations
(Continued)
ABBREVIATION
N
NIA
NHA
N·m
No. or NO.
NP
NTPO
00
OPT
PARA
PAX
PCA
PIN
psia
psig
PTFE
REG
REPlD
REPlS
SB
SPN
SUPSO
SUPSOS
TC
THO
THK
thru
TOT
TYP orTyp
UNF
U.S.orUS
USA
VAC
WI or wi
WC
WIO orw/o
wt orwt
•
CMM & ,PL
DEFINITION OF ITEM
Newton
Not Applicable
Next Higher Assembly
newton-meter
Number
Not Procurable
Normal Temperature and Pressure Dry
[760 mm Hg, 70°F (21.1 0C)]
Outside Diameter
Optional
Paragraph
Passenger
Portable Cylinder Assembly
Part Number
pounds per square inch absolute
pounds per square inch gauge
polytetrafluoroethylene
Regulator
Replaced
Replaces
Service Bulletin
Scott Part Number
Superseded
Supersedes
Transport Canada
Thread
Thick
through
Total
Typical
United National Fine (Thread)
United States
United States of America
Vacuum
With
Water Column
Without
Weight
5. Verification
Section
Testing and Fault Isolation
Disassembly
Assembly
•
EFFECTIVITY: ALL
October 14, 1982
October 14, 1982
October 14, 1982
35-32-18
INTRODUCTION
Page INTRO-5/B
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1:LfCDJSCOtl
Technologies,Inc.
..
/scott
A lIiation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
DESCRIPTION AND OPERATION
TASK 35-32-18-870-801
1. General
This section describes the components and operation of the 5500 Series and 5600 Series Portable
Cylinder Assemblies (PCA). Information about part numbers, and how to order Portable Cylinder
Assemblies is also presented in this section. Refer to Figure 1 for an illustration of a typical PCA.
NOTE:
Unless otherwise noted, any use of an item number in this section includes all alpha variants and
dashed variants (i.e., items not shown) of that number. For example, item (500) includes 500,
-500, -SOOAthru -5000, unless otherwise noted.
Harness Assembly
~
Regulator Assembly
...
•
/
Cylinder
Outlet Assembly
Demand Respirator Regulator
(Present on 5600 Series Only)
5500 & 5600 Series Portable Cylinder Assembly
(5600 Series PCA Pictured)
Figure 1
TASK 35-32-18-870-802
2. Leading Particulars
Subtask 35-32-18-870-001
A. 5500 Series PCA
The leading particulars for the 5500 Series PCA are shown in Tables 1 and 2. Leading particulars and
weight data are subject to change without notice .
•
EFFECTIVITY: ALL
35-32-18
Page 1
20040415
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Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
2. Leading Particulars (Continued)
•
A. 5500 Series PCA (Continued)
Table 1
5500 Series PCA Leading Particulars
peA Envelope Dimensions
CYLINDER & REGULATOR ASSEMBLY
OUTLET ASSEMBLY
Dimensions
in. (cm)
Callout Code
(Refer to Fig. 2)
A
(Typ)
Dimensions
in. (em)
B
(Max)
C
(Max)
D
(Typ)
E
(Typ)
Callout Code
(Refer to Fig. 2)
F
(Typ)
A,J
3.6 (9.1)
9.3 (23.6)
13.0 (33.0)
2.5 (6.4)
2.3 (5.8)
A
2.50 (6.35)
B,L
3.6 (9.1)
13.4 (34.0)
17.3 (43.9)
2.5 (6.4)
2.3 (5.8)
B
2.69 (6.81)
C,M
3.6 (9.1)
18.9 (48.0)
22.6 (57.4)
2.5 (6.4)
2.3(5.8)
C
3.10 (7.90)
D,N,P
5.3 (13.5)
18.3 (46.5)
22.6 (57.4)
2.6 (6.6)
3.1 (7.9)
F,a
6.8 (17.3)
19.3 (49.0)
See Note
See Note
2.56 (6.50)
2.03 (5.16)
G
6.8 (17.3)
23.5 (59.7)
23.4 (59.4)
27.6 (70.1)
0
E
See Note
See Note
K
0.81 (2.06)
S
T
9.0 (22.9)
29.8 (75.7)
33.7 (85.6)
4.0 (10.2)
2.5(6.4)
5.0 (12.7)
L
2.50 (6.35)
2.3 (5.8)
M
2.00 (5.08)
N
2.25 (5.72)
2.25 (5.72)
2.81 (7.14)
2.22 (5.64)
3.6 (9.1)
18.8 (47.8)
22.8 (57.9)
NOTE: For this dimension, contact Scott Aviation Customer Service.
P
R
S
~----B--------..l
14--------
C ------~
PCAWeight..
High Pressure Relief
US DOT-3AA-1800 Steel Cylinder
US DOT-3HT-1850 Steel Cylinder
US DOT-E-8162-1850 Composite Cylinder
Operating Pressure Range
Operating Temperature Range
Clamp Weight
WWD-120 (SPN 13160..(0)
WWD-176 (SPN 13161..(0)
WWD-224 (SPN 13162.{J0)
EFFECTIVITY: ALL
•
.
Rerer 10 Table 2
.
.
.
.
..
.
.
.
2650 - 2900 psig (18.27 - 20.00 MPa) and 160 -165°F (71.1 - 73.9°C)
2650·2900 psig (18.27 - 20.00 MPa) and 160 -165°F (71.1- 73.9°C)
2500 - 2775 psig (17.24 -19.13 MPa)
150 - 1850 psig (1.03 -12.76 MPa)
-60 to +160°F (-51 to We)
0.0691bs (31.2 gm) each (used wI 4.25, 7.15 and 11 cu ft cylinders)
0.087 Ibs (39.6 gm) each (used wi 22 cu fl cylinders)
0.1141bs (51.6 gm) each (used wI 29, 39, 49 cu ft cylinders)
35-32-18
Page 2
20040415
•
•
t"CO/
..
....,
scott
!scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
2. Leading Particulars (Continued)
A. 5500 Series PCA (Continued)
Table 1 (Continued)
5500 Series PCA Leading Particulars
Regulator Assembly
Available Configurations
2 Outlet Ports ............................................................
3 Outlet Ports ............................................................
Material of Construction
Aluminum ..................................................................
Brass .........................................................................
Weight .........................................................................
Output Pressure ..........................................................
lock-up Pressure ........................................................
(Outlet Pressure At Zero Flow)
low Pressure Relief
Free Flow Rate (nominal) .........................................
Opening Pressure .....................................................
Reseating Pressure ..................................................
•
Cylinder
Material of Construction
US DOT·3M·1800 ....................................................
US DOT-3HT-1850 ....................................................
US DOT-E-8162·1B50 ...............................................
Thread Size
SPN 6084-01, ·02, -03, ·20 Steel Cylinders ..............
SPN 6084..(l4, ·05, ..(lB,-07, -34 Steel Cylinders .......
SPN 21507·06 Composite Cylinder ...........................
US DOT Approval Type
Steel ...........................................................................
Composite ..................................................................
Maximum Gas Storage Pressure
US OOT·3M·1BOO Steel Cylinder .............................
US OOT·3HT·1B50 Steel Cylinder .............................
US DOT·E·8162·1850 Composite Cylinder ...............
Service life .................................................................
Weight .........................................................................
SPN's 5510-00, -03, ·04, ·07, ·10, ·13, ·14,-17, -20 and 803199-04
SPN's 5510-05, -09, -15, ·19
SPN's 5510-00, -03, ·04, -05, ·07, ·09
(After Apr 1182,aluminum regulators were not Pfocurable)
SPN's 5510·10, ·13, ·14, ·15, ·17, -19, -20 and 803199-04
Refer to Table 2
55 ±2 psig (0.38 ±O.Ol MPa)
75 psig (0.52 MPa) maximum
300 lpm NTPD at 135 psig (0.93 MPa)
More than 90 psig (0.62 MPa)
less Ihan or equal to 90 psig (0.62 MPa)
Steel
Steel
Fiber·Wrapped Aluminum
0.500· 14 ANPT
1.00 • 11.5 ANPT
0.750 • 16UNF·2B
DOT-3M-1BOO or DOT·3HT·1B50
DOT-E-B162-1850
1800 psig (12.41 MPa) a170°F (21°C)
1850 psig (12.76 MPa) at 70°F (21°C)
1850 psig (12.76 MPa) at 70°F (21°C)
Refer to the CHECK section
Refer to Table 2
Accessories
Masks (Typical)
COfistant Flow Type
DUO-SEAL ® Mask ................................................
DUO-SEAL ® Mask wI
flow indicator and microphone ...............................
SKY MASK® wI indicator .......................................
Disposable Mask ....................................................
PAX Mask ...............................................................
PCA Mounting Bracket Set .........................................
•
EFFECTIVITY: 5500 SERIES
SPN 28312 Series
SPN 28316 Series
SPN 28314 Series
SPN 28301 Series
SPN 289-601 Series (Refer 10CMM 35-22-26)
SPN 289-701 Series (Refer to CMM 35·22-27)
SPN 289-801 Series (Refer to CMM 35·22·28)
SPN's 36758-11 and 36758-12 (Refer to Paragraph 8.)
35-32-18
Page 3
20040415
-tileD/scott
Technologies, Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
2. Leading Particulars (Continued)
A. 5500 Series PCA (Continued)
Table 2
5500 Series peA Weight Data
CYLINDER
AND REGULATOR
ASSY
HARNESS
Cyl PIN
(Capacity in
cu II/liters)
CylWeight
Empty
Ibs.(gm)
Regulator PIN
(Material)
(Note 1)
Charged Weight
(Cyl & Reg Only)
Ibs(gm}
6084.Q1
(4.25/120)
3.00 (1361)
5510..()0 (Aluminum)
5510-10 (Brass)
6084.Q2
(7.15/202)
6084-20 (Note 2)
(11/311)
6084-04
{22/623}
6084-\l6
(38.411.087)
6084-07
(48.3/1.368)
ASSY
Weight
Ibs(gm)
Part No.
Weight
Ibs(gm)
4.88 (2214)
5.76 (2613)
801660.Q0
0.09 (40.8)
5OO95eries
0.05 (22.7)
80165B-\l0
0.46 (208.7)
5041 Series
0.09 (40.8)
4.19 (1901)
5510-00 (Aluminum)
5510-10 (Brass)
6.31 (2862)
7.19 (3261)
801662.Q0
0.34 (154.2)
5052·00
0.20 (90.7)
801660-01
0.10 (45.4)
5507 Series
0.08 (36.2)
6.18 (2803)
5510·00 (Aluminum)
5510·10 (Brass)
8.62 (3910)
9.50 (4309)
801660-\l3
0.14 (63.5)
8572-02
0.07 (31.8)
801660-05
0.12 (54.4)
6818-01
0.01 (4.5)
10.90 (4944)
5510-03 (Aluminum)
5510·13 (Brass)
14.44 (6550)
15.32 (6949)
801663-00
0.03 {13.6}
800503-00
0.05 {22.7}
803177-03
0.50 (226.8)
802856·01
0.06 (27.2)
5510-03 (Aluminum)
805436-01
0.69 (313.01
5510-13 (Brass)
21.04 (9544)
21.92 (9943)
801808-05
0.90 (408.2)
36728-01
(Nole3)
0.06 (27.2)
23.37 (10 601)
5510-03 (Aluminum)
5510-13 (Brass)
28.84 (13 082)
29.72 (13481)
801807-01
0.91 (412.8)
802863·02
0.10 (45.4)
801808-01
0.66 (299.4)
10006017
0.06 (21.2)
3.00 (1361)
5510-05 (A1urriflum)
5510-15 (Brass)
4.88 (2214)
5.76 (2613)
10006298
0.07 (31.8)
4.19 (1901)
5510-05 (A1urrinum)
5510-15 (Brass)
17.80 (8074)
801807-02
0.94 (426.4)
0.91 (412.6)
6.31 (2862)
7.19 (3261)
801806-02
0.69 (313.0)
601808-03
0.67 (304.0)
6.18 (2803)
5510-05 (A1urrinum)
5510-15 (Brass)
8.62 (3910)
9.50 (4309)
603177-01
0.50 (226.8)
603177-02
0.50 (226.8)
6084-Q4
(22/623)
10.90 (4944)
5510-07 (Aluminum)
5510-17 (Brass)
14.44 (6550)
15.32 (6949)
6084-Q4
(22/623)
10.90 (4944)
5510-09 (Aluminum)
5510-19 (Brass)
14.44 (6550)
15.32 (6949)
17.80 (6074)
5510-17 (Brass)
21.92 (9943)
6.18 (2803)
5510-20 (Brass)
9.50 (4309)
6084·34
(115/3.256)
34.00 (15 422)
5510·19 (Brass)
45.90 (20 820)
21507·06
(11/311)
2.40 (1089)
803199-Q4 (Brass)
5.42 (2459)
6084..()2
(7.15/202)
6084-20 (Note 2)
(11f311)
6084-06
(38.4/1.087)
6084-20 (Nole 2)
(11/311)
ASSY
ParlNo.
801607-03
6084..()1
(4.25/120)
OUTLET
•
Note 1: After Apr 1f82 aluminum regulator assemblies
listed in this column were not procurable.
Note 2: Cylinder PIN 6084·20 replaces cylinder PIN 6084-03.
Note 3: Outlet SPN 36728-01 replaces outlet SPN DPB153. After Jan 01101 SPN DPB153 was not procurable.
EFFECTIVITY:
ALL
35-32-18
Page 4
20040415
•
•
..
-fllea/scott
Technologies. Inc.
jSCDtt
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
2. Leading Particulars (Continued)
Subtask 35-32-18-870-002
B. 5600 Series PCA
The leading particulars for the 5600 Series PCA are shown in Tables 3 and 4. Leading particulars and
weight data are subject to change without notice.
Table 3
5600 Series PCA Leading Particulars
PCA Envelope Dimensions
OUTLET ASSEMBLY
CYliNDER AND REGULATOR ASSEMBLY
Callout
Code
(Refer 10
Fig. 3)
A,J
B
C,M
D,P
•
G
DIMENSIONS (See Below)
in. (em)
E
A
(Typ)
B
(Max)
C
(Max)
D
(Typ)
(Typ)
G
(Max)
(Max)
J
(Max)
3.6
(9.1)
3.6
(9.1)
3.6
(9.1)
5.3
(13.5)
6.8
(17.3)
9.3
123.6)
13.4
(34.0)
18.9
(48.0)
18.3
(46.5)
23.5
(59.7)
13.0
(33.0)
17.1
(43.4)
22.6
(57.4)
22.6
(57.4)
27.6
(70.11
1.8
14.6)
2.5
(6.4)
2.5
(6.4)
2.6
(6.6)
See
Note
2.3
(5.B)
2.3
(5.B)
2.3
(5.8)
3.1
(7.9)
3.9
(9.91
4.7
(11.9)
4.7
(11.9)
4.7
(11.9)
5.5
(14.0)
6.3
(16.0)
3.4
18.6)
3.4
(8.6)
3.4
(8.6)
3.4
(8.6)
3.4
(B.6)
6.8
(17.3)
11.0
(27.9)
15.B
(40.1)
14.7
(37.3)
19.2
(48.8)
H
Callout
Code
(Refer to
Fig. 3)
NOTE: For this dimension, contact Scott Aviation Cuslomer Service.
A
B
C
D
E
K
M
N
1+----
DIMENSIONS
(See Below)
in. (em)
F
(Typ)
2.50
(6.35)
2.69
(6.83)
3.10
17.90)
2.56
(6.50)
2.03
(5.16)
0.81
(2.06)
2.00
/5.0Bl
2.25
(5.72)
B ----.I
-j
G
•
PCAWeight
High Pressure Relief
Operating Pressure Range
Operating Temperature Range
Clamp Weight
WWD-120 (SPN 13160-00)
WWD-176 (SPN 13161-00)
WWD-224 (SPN 13162-00)
EFFECTIVITY:
.
.
.
.
Refer to Table 4
2650 - 2900 psig (18.27 - 20.00 MPa) and 160 - 165°F (71.1 • 73.9°C)
150 ·1800 psig (1.03 -12.41 MPa)
-60 to +160°F (-51 to 71°C)
.
.
.
0.069Ibs (31.2 gm) each (used w/4.25, 7.15 and 11 eu It cylinders)
0.087Ibs (39.6 gm) each (used w/22 cu It cylinders)
0.114 Ibs (51.6 gm) each (used w/39. 49 cu It cylinders)
5600 SERIES
35-32-18
PageS
20040415
1:'1Co/scott
Technologies, Inc.
!scott
Aviation
55OG'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
2. Leading Particulars (Continued)
B. 5600 Series PCA (Continued)
Table 3 (Continued)
5600 Series PCA Leading Particulars
Regulator Assembly
Available Configurations
2 Outlet Ports .............................................................
3 Outlet Ports .............................................................
Material of Construction
AlumInum ...................................................................
Brass ..........................................................................
Weight ..........................................................................
Output Pressure ...........................................................
Lock-up Pressure .........................................................
(Outlet Pressure at Zero Flow)
Low Pressure Reltef
Free Flowrate (nominal) ............................................
Opening Pressure ................................ _.....................
Reseating Pressure ...................................................
Cylinder
Material of Construction ...............................................
Thread Size
SPN 6084-01, -02, -20 Cylinders ................................
SPN 6084-04, -06, -07 Cylinders ................................
US DOT .4.pprovalType ........._.....................................
Maximum Gas Storage Pressure .................................
Service ute ..................................................................
Weight ..........................................................................
Respirator Regulator Assembly
Configurations
Demand Type ............................................................
DemandlPressure-Demand Type ..............................
Inlet Pressure Range ...................................................
OulietFlow
Demand Type ............................................................
Demand, Pressure-Demand Type .............................
Accessories
Mask (Typical)
Demand, DemandlPressure-Demand
SCOTTORAMIC® Mask ..........................................
Constant Flow Mask
DUo-SEAL® Mask ..................................................
DUo-SEAL® Mask wi
flow indicator and microphone ................................
SKY MASK® Mask wi indicator ...............................
Disposable Mask......................................................
PPlXMask ...............................................................
Bracket AssemblY .......................................................
EFFECiIVITY: ALL
SPN's 5510-00, -03, -DB, -10, -13, -18
SPN's 5510-05, -15, -19
SPN's 5510-00, -03, {)S, -08
(After Apr 1/82, aluminum regulators were not procurable)
SPN's 5510-10, -13, -15, -18, -19
Refer to Table 4
55 ±2 psig (0.38 ±O.01 MPa)
15 psig (0.52 MPa) maximum
300 lpm NTPD at 135 psig (0.93 MPa)
More than 90 psig (0.62 MPa)
Less than or equal to 90 psig (0.62 MPa)
Steel
0.500 - 14 ANPT
1.00 -11.5 ANPT
DOT JAA-1800
1800 psig (12.41 MPa) at70°F (21°C)
Refer to tile CHECK section
Refer to Table 4
•
SPN's 6379-2C and 6379-20
SPN's 800649-00 and 800649-01
35 - 60 psig (0.24 - 0.41 MPa)
20 -100 lpm NTPD al35 - 60 psig (0.24 - 0.41 MPa)
20 -100 Ipm NTPD a135 - 60 psig (0.24 - 0.41 MPa)
SPN's 10100 and 10800 Series (Refer to CMM 35-10-71)
SPN 28312 Series
SPN 28316 Series
SPN 28314 Series
SPN 28301 Series
SPN 289-601 Series (Refer to CMM 35-21-87)
SPN 289-701 Series (Refer to CMM 35-21-88)
SPN 289-801 Series (Refer to CMM 35-22-07)
SPN's 36758-11 and 36758-12 (Refer to paragraph 8.)
35-32-18
Page 6
20040415
•
•
~
1:'1ca/scolt
/SCDtt
Technologies. Inc. Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY • CMM & lPi
2. Leading Particulars (Continued)
B. 5600 Series PCA (Continued)
Table 4
5600 Series PCA Weight Data
RESPIRATOR
REGULATOR ASSY
Part No.
Weight
Ibs(gm)
6379-2C
0.64(290)
6379-20
0.55 (249)
800649-00 0.70 (318)
800649-01 0.67 (304)
•
CYLINDER AND REGULATOR ASSY
Charged
Weight
Weight
(Cyl & Reg
Empty
Reg PIN
CylPIN
Only)
(Capacity in Cylinder
(Material)
Ibs(gm)
(Note 1)
Ibs(gm)
cu It /liters)
HARNESS ASSY
OUTLET ASSY
Part No.
Weight
Ibs(gm)
Part No.
Weight
lbs (gm)
5510-00 (AI)
4.89 (2218)
801660-00
0.09(40.8)
5009 Series
0.05 (22.7)
5510-10 (Br)
5.77 (2617)
801658-00
0.46 (208.7)
5041 Series
0.09 (40.8)
5510-00 (AI)
6.32 (2867)
801662·00
0.34 (154.2)
5052·00
0.20 (90.7)
551Q..l0 (Br)
7.20 (3266)
801660-01
0.10 (45.3)
5507 Series
0.08 (36.3)
551Q..03 (AI)
8.64 (3919)
801660-03
0.14 (63.5)
8572-02
0.07 (31.8)
551Q..l0 (Br)
9.52 (4318)
801660-05
0.12 (54.4)
6818-01
0.01 (4.5)
551Q..03 (AI)
14.61 (6627)
802856-01
0.06 (27.2)
551Q..13 (Br)
15.49 (7026)
36728-01
(Note 2)
0.06 (27.2)
23.37
(10.601)
551Q..03 (AI)
28.99 (13,150)
5510-13 (Br)
29.87 (13,549)
6084-01
(4.251120)
3.00
(1361)
5510-05 (AI)
4.67 (2120)
5510·15 (Br)
5.57 (2528)
6084-20
(111311)
5.25
(2381)
5510-05 (AI)
8.64 (3919)
5510-15 (Br)
9.52 (4318)
6084-04
(221623)
10.90
(4944)
5510-19 (Br)
15.49 (7026)
6084-01
(4.25/120)
3.00
(1361)
6084-02
(7.15/202)
4.19
(1901)
6084·20
(11/311)
5.25
(2381)
6084·04
(221623)
10.90
(4944)
6084-07
(48.3/1.368)
Note 1: After Apr 1/82 aluminum regUlator assemblies listed in this column were not procurable.
Note 2: After Jan 01/01, ouUet SPN 36728-01 replaced outlet SPN OPB153 .
•
EFFECTIVITY:
5600 SERIES
35-32-18
Page?
20040415
'tl.lca/scott
Technologies. Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
TASK .35-32-18-870-803
3. Part Number Identification
J1!;"'I.II...-
Refer to Figure 2 or Figure 3 to identify part numbers of 5500 Series or 5600 Series peA's.
5500-000-000
Basic Series
----=:r---
I
CYLINDER AND REGULA TOR ASSY
.
Refer to Sheet 2
CYLINDER FINISH
HARNESS ASSY
Regulator Assy PIN
Callout
Code
Cylinder PIN
(Note 1)
Aluminum Body
(Note 2)
Brass Bodv
Finish
(Note 3)
Callout
Code
A
6084-01
5510..QO
5510-10
1
8
5510..QO
5510-10
2
C
6084-02
6084-20
(Nole6)
Gray-Green
(24159)
Green (14187)
5510..QO
5510-10
3
Blue (15102)
0
6084-04
5510-03
5510-13
5
F
G
6084-06
6084-07
5510-03
5510-03
5510-05
(NoIe4)
5510-05
(Nole4)
5510-05
(Note 4)
5510-07
5510-09
(Nole4)
5510-13
5510-13
5510-15
(Nole4)
5510-15
(Nole4)
5510-15
(Nole 4)
5510-17
5510-19
(Nole 4)
5510-17
5510-19
(Notes 4 &5)
803199-04
6
9
6084-01
J
I
6084-02
L
6084-20
(Nole 6)
6084-04
M
N
P
6084-04
Q
6084-06
§
6084-34
T
21507-06
Callout
Code
Green (14187) &
Yellow (13538)
Green (24062)
Green (24062)
Harness PIN
A
801660-00
B
801658-00
C
801662-00
0
801660-01
E
F
801660-03
801660-05
G
801663-00
M
803177-03
N
805436-01
P
801808-05
Q
801807-01
R
801808-01
S
801807-02
T
801807-03
801808-02
801808-03
803177-01
No Harness
803177-02
U
V
W
X
y
•
Note 1: Cylinder PIN's 6084-01 -02, and -20 have 0.500 - 14 ANPT threads.
Cylinder PIN's 6084-04, -06, -07, -34 have 1.00 - 11.5 ANPT threads.
Cylinder PIN 21507 -Q6 has 0.750 - 16UNF-2A threads.
Note 2: After Apr 1/82 the regulators shown in this column were not procurable.
Note 3: Cylinder finish (paint) number (shown in parentheses) in this column is per specification FED STQ.595.
Note 4: These regulators are used when 3 outlet assembly ports are required.
Note 5: PCA SN 134269 and subsequent use regulator PIN 5510-19 (three outlet assembly ports).
PCA SN's before 134269 for Callout Code 'S' used regulator PIN 5510-17 (two outlet assembly ports).
Note 6: Cylinder PIN 6084·20 replaces cylinder PIN 6084-03.
5500 Series peA Matrix
Figure 2 (Sheet 1 of 2)
EFFECTIVITY:
ALL
35-32-18
PageS
20040415
•
•
~
1:I./CO/SCOtl
/scott
Technologies. Inc. Aviation
eMM & ,PL
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
3. Part Number Identification (Continued)
5500-000-000
I
Refer to Sheet 1
I
OUTlET FLOW RATE SETTING
(Note 8)
•
\
I
OUTlET STYLE
(Notes 10 and 12)
CABIN AlTITUDE SETTING
Callout
Code
Row
lpm atNTPD
(Note 9)
Callout
Code
A
0.5
0
B
2.0
5
C
2.5
E
Outlet
Type
Callout
Code
Outlet
PIN
A
5009 Series
Constant Flow (Metered)
5,000 (1524)
B
5041 Series
Constant Flow (Metered)
10
10,000 (3048)
C
3.0
15
15,000 (4572)
0
5507 Series
Constant Flow (Metered)
F
4.0
20
20,000 (6096)
E
8572-02
Full Flow (Non-Metered)
G
7.0
23
23,000 (7010)
K
6818-01
H
8.0
25
25,000 (7620)
L
800503-00
(Note 14)
Full Flow (Non-Metered)
L
4.5
30
30,000 (9144)
M
802856-01
Full Flow (Non-Metered)
X
0
N
36728.(J 1
Full Flow (Non-Metered)
(Replaces DPB153)
y
FULL
P
802863·02
Full Flow (Non-Metered)
(Cessna Type)
R
10006017
Full Flow (Non-Metered)
(Lockheed Type)
S
10008298
Full Flow (Non-Metered)
Altitude
feet (meters)
0(0)
(Note 11)
5052-00
(Note 13)
Constant Flow (Metered)
.
Plug
8: There may be 1, 2 or 3 Outlet Flow Rate Setting Callout Codes in the PIN.
9: Flow at 14.7 psia (760 mm Hg) at 32°F (O°C).
10: Outlet Style Callout Codes E, L, M, N, P, R and S identify full flow (non-metered) outlets.
11: Altitude Setting Callout Code 0 identWies full flow (non-metered) outlets (Outlet Style Callout Codes E, L, M, N, P, R or 5).
t2: There may be 1 or 2 Outlet Style Callout Codes in the PIN, however only one configuration of constant flow
(metered) Outlet Style (Callout Code A, B, or D) is allowed on a PCA.
Note 13: After Oct 01181 this outlet was not prororable.
Note 14: After Jun 22/95 this outlet was not procurable.
Note
Note
Note
Note
Note
5500 Series PCA Matrix
Figure 2 (Sheet 2 of 2)
•
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Technologies. Inc. Aviation
550Cl'5600SERifS PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
3. Part Number Identification (Continued)
-=rrD---~
5600-0000-000
Basic Series
I
-cII...-
Refer to Sheet 2
I
I
RESPIRATOR
REGULATOR ASSY
CYLINDER AND REGULATOR ASSY
CYLINDER FINISH
HARNESS ASSY
Regulator Assy PIN
Callout
Code
Reg PIN
(Type)
Callout
Code
Cylinder PIN
(Note1)
Aluminum Body
(Note 2)
Brass Body
Finish
(Note 3)
Callout
Code
Harness
PIN
1
6379-2C
(Demand)
A
6084-01
5510-00
5510-10
1
Gray-Green (24159)
A
801660.()()
2
6379·20
(Demand)
B
6084-02
5510-00
5510-10
2
Green (14187)
and
While (17875)
B
801658.()()
8
800649-00
(Demandl
Press·Demand)
C
6084·20
5510·03
5510·10
3
Blue (15102)
C
801662'()()
9
800649-01
(Demandl
Press-Demand)
D
6084-04
5510-03
5510-13
5
Green (14187)
and
Yellow (13538)
D
801660-01
G
6084-07
5510-03
5510-13
G
Green (24062)
E
801660-03
J
6084-01
5510-05 (Note 4)
5510-15 (Nole4)
J
Green (24062)
F
801660-05
M
6084-20
5510-05 (Note 4)
5510-15 (Note 4)
P
6084-04
callout
Code
•
5510-19 (Note 4)
Note 1: Cylinder PIN's 6084-01, -02 and -20 have 0.500 -14 ANPT threads.
Cylinder PIN's 6084-04, and -07 have 1.00 - 11.5 ANPT threads.
Note 2: After Apr 1/82 the regulators shown in this column were not procurable.
Note 3: Cylinder finish (paint) number (shown in parentheses) in this column is per specification FED STD-595.
Note 4: These regulators are used when two outlet assembly ports (in addition to the respirator regulator port) are required.
5600 Series peA Matrix
Figure 3 (Sheet 1 of 2)
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Technologies.
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Aviation
5500'5ti00 SERIES PORTABLE CYLINDER ASSEMBLY·
eMM & IPL
3. Part Number Identification (Continued)
5600-0000-000
I
Refer to Sheet 1
I
OUTLET FLOW RATE SETTING
(Note 5)
Callout Code
•
Flow
IpmalNTPD
(Note 6)
I
OUTlET STYLE
(Note 8)
CABIN ALTllUDE SETTING
Altitude
feet (meters)
CalioulCode
Callout Code
Outlet PIN
Outlet
Type
A
0.5
0
0(0)
(Note 7)
A
5009 Series
Constant
Flow (Metered)
B
2.0
5
5,000 (1524)
B
5041 Series
Constant
Flow (Metered)
C
2.5
10
10,000 (3048)
D
5507 Series
Constant
Flow (Metered)
D
2.7
15
15,000 (4572)
E
8572-02
E
3.0
20
20,000 (6096)
K
6816-01
F
4.0
23
23,000 (7010)
M
802856-01
Full Flow (Non-Metered)
G
7.0
25
25,000 (7620)
N
36728-01
Full Flow (Non-Metered)
(Replaces DPB153)
H
8.0
30
30,000 (9144)
K
0.7
L
4.5
X
0
Y
Full
Note 5:
Note 6:
Note 7:
Note 8:
,
Full Flow (Non-Metered)
Plug
There may be 1 or 2 Outlet Flow Rate setting Callout Codes in the PIN.
Flow at 14.7 psia (760 mm Hg) a132°F (OOC).
A11iludeSelling Callout Code 0 identifies lull flow (non-metered) outlets (OuUetStyle callout Codes E, Mar N).
There may be 1 or 2 Outlet Style callout Codes in the PIN; however, only one configuration of constant flow
(metered) Outlet Style (Callout Code A, B, or 0) is allowed on a PCA.
5600 Series PCA Matrix
Figure 3 (Sheet 2 of 2)
•
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5600 SERIES
35~32-18
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Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
eMM & IPL.
3. Part Number Identification (Continued)
Part numbers for the 5500 and 5600 Series PCA are made up of a basic series number and callout codes
for respirator regulator assembly (5600 Series only), cylinder and regUlator assembly, cylinder finish,
harness assembly, outlet flow rate setting, outlet altitude setting and outlet style.
•
The basic series number identifies a specific peA (either 5500 or 5600).
•
The respirator regulator assembly callout code (5600 Series peA only) identifies a respirator regUlator
assembly part number.
•
The cylinder and regulator assembly callout code identifies a cylinder part number and regUlator
assembly (aluminum or brass construction) part number.
-
The cylinder finish callout code identifies cylinder paint color.
The harness assembly callout code identifies the part number of the harness assembly that attaches to
the PCA. Some harness assemblies may include one or more passenger mask assemblies and mask
stowage bags.
•
The outlet flow rate setting callout code identifies the designated flow of oxygen from a constant flow
(metered) or full flow (non-metered) outlet type.
•
The outlet altitude setting callout code identifies the designated cabin altitude of the outlet assembly.
•
The outlet style callout code identifies the outlet assembly part number and outlet type.
TASK 35-32-18-870-804
4. Part Number Guidelines
\
Provided below are important guidelines to identify part numbers for 5500 Series or 5600 Series PCA's and
some examples of PCA configurations.
A. Outlet flow rate settings may be represented by one, two, or three callout codes. The 5500 Series PCA
may have as many as three outlet flow rate setting callout codes; however, the 5600 Series PCA may
only have a maximum of two outlet flow rate setting callout codes. When more than one constant flow
(metered) type outlet is specified, all outlets must be of the same style (outlet flow callout). An outlet flow
callout other than "Full" are for constant flow (metered) type outlet assemblies. An outlet flow callout of
"Full" is specified if the PCA is configured with only full flow (non-metered) type outlet assemblies or a
flow callout of "0" for a PCA configured with a plug.
•
B. Outlet altitude setting is represented by only one callout code. A PCA configured with either a full flow
(non-metered) type outlet assembly or a plug must have an altitude setting callout code of "0'. All other
outlet types have an altitude setting callout code greater than "0".
C. Outlet styles may have one or two callout codes. Three outlet types, a constant flow (metered), full flow
(non-metered) or plug can be used on a 5500 Series or 5600 Series PCA. Outlet assemblies attached
to the PCA can only have one outlet part number for a constant flow (metered) outlet type (e.g., 5009
Series) or a full flow (non-metered) outlet type (e.g., 36728-01).
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Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & fPL
4. Part Number Guidelines (Continued)
D. Provided below are examples of some PCA configurations.
• PIN 5500-Q1X-BB25A is a 5500 Series PCA with a PIN 6084-06 cylinder, PIN 5510-17 regulator
assembly, number 24159 gray-green cylinder finish, no harness assembly, and two PIN 5009-2-25
constant flow (metered) type outlet assemblies designated for a cabin altitude of 25,000 ft (7620 m).
• PIN 5500-P1A-YYYON is a 5500 Series PCA with a PIN 6084-04 cylinder, either a PIN 5510-09
aluminum regulator assembly or PIN 5510-19 brass regulator assembly, number 24159 gray-green
cylinder finish, PIN 801660-00 harness assembly, and three PIN 36728-01 full flow (non~metered) type
outlet assemblies.
• PIN 5500-J6C-BF23BN is a 5500 Series PCAwith a PIN 6084-01 cylinder, either a PIN 5510-05
aluminum regulator assembly or a PIN 5510-15 brass regulator assembly, number 24062 green
cylinder finish. PIN 801662-00 harness assembly. one PIN 5041-2-23 constant flow (metered) type
outlet assembly, one PIN 5041-4-23 constant flow (metered) type outlet assembly and one
PIN 36728-01 full flow (non-metered) type outlet assembly. The constant flow (metered) outlet
assemblies are designated for a cabin altitude of 23,000 ft (7010 m).
• PIN 5600-1 M3A-F20BM is a 5600 Series PCA with a PIN 6379-2C demand type respirator regulator
assembly, PIN 6084-20 cylinder, either a PIN 5510-05 aluminum regulator assembly or a
PIN 5510-15 brass regulator assembly, number 15102 blue cylinder finish, PIN 801660-00 harness
assembly, one PIN 5041-4-20 constant flow (metered) type outlet assembly, and one PIN 802856-01
full flow (non-metered) type outlet assembly. The constant flow (metered) outlet assembly is
designated for a cabin altitude of 20,000 ft (6100 m).
•
• PIN 5600-9L 1B-E23A is a 5600 Series PCA with a PIN 800649-01 demand/pressure-demand type
respirator regulator assembly, PIN 6084-02 cylinder, either a PIN 5510-05 aluminum regulator
assembly or a PIN 5510-15 brass regulator assembly, number 21459 gray-green cylinder finish,
PIN 801658-00 harness assembly, and one PIN 5009-3-23 constant flow (metered) type outlet
assembly designated for a cabin altitude of 23,000 ft (7010 m).
TASK 35-32-18-870-805
5. Purpose of Equipment
The 5500 Series PCA is a portable oxygen source that contains high-pressure aviation grade oxygen
(per Military Specification MIL-PRF-27210, Type I) for high altitude breathing or therapeutic use.
The 5600 Series PCA is a dual purpose portable oxygen source that contains high-pressure aviation grade
oxygen (per Military Specification MIL-PRF-27210. Type I) for high altitude breathing or therapeutic use. In
addition to providing a constant flow of supplemental oxygen, like the 5500 Series PCA, the 5600 Series
PCA also provides demand or pressure-demand flow capabilities. The 5600 Series PCA, when used with a
demand or demand/pressure-demand type SCOTTORAMIC® Mask, will provide protection from hazardous
smoke or fumes.
TASK 35-32-18-870-806
6. Typical Installation
All 5500 and 5600 Series PCA's may be configured with a sling-type carrying strap (harness) that attaches
to the PCA. PCA's may be stored in convenient and accessible locations on the aircraft. When the PCA
must be secured in an aircraft, optional lower (SPN 36758-11) and upper (SPN 36758-12) Portable
Cylinder Bracket Assemblies are available. Refer to Paragraph 8 for more information on optional Portable
Cylinder Bracket Assemblies.
The number of PCA's required on an aircraft is determined by applicable FAR's, number of passengers,
and the general flight profile of the aircraft .
•
EFFECTIVITY:
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/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CAtM & IPL
TASK 35-32-18-870-807
7. Operation
The 5500 Series and 5600 Series PCA's are made up of a respirator regulator assembly (5600 Series
only), high-pressure cylinder, regulator assembly, hamess assembly, outlet assemblies and, on some
configurations, mask assemblies stored in harness-mounted storage bags.
Subtask 35-32-18-870-003
A. Respirator Regulator
The 5600 Series PCA is configured with either a demand or demand/pressure-demand type respirator
regulator. The respirator regulator (Figure 4) is attached to the peA regulator assembly (-1.IPL Figure
9) outlet port as shown.
2
LEGEND
1. Diaphragm
2. Demand Valve Assembly
3. Screen
4. Regulator Assembly
5. Cylinder
6. Outlet Port (To Demand Mask)
7. Slide Button
8. Case Cover (Demand Type)
9. Case Cover (Oem/Press-Oem Type)
10. Plate and Lever Assy
11. Body
•
Respirator Regulator Assembly
(Demand Type Shown)
Figure 4
WARNING:
THE SCOTT 10100 SERIES SCOTTORAMIC@ MASK ASSEMBLY MUST ONLY BE
USED WITH A PIN 5600-1 SERIES OR PIN 5600-2 SERIES PCA OR THE PCA MAY
NOT PROVIDE OXYGEN FOR THE FULL RATED DURATION CAUSING SERIOUS
PERSONAL INJURY OR DEATH.
The demand type respirator regulator assembly allows oxygen to flow. on demand, to a demand style
mask assembly (e.g., 10100 Series SCOTTORAMIC). Inhalation of oxygen from the demand style mask
assembly removes oxygen from the body (11) of the respirator regulator through outlet port (6).
Removing oxygen from the body (11) causes a pressure drop allowing atmospheric pressure, acting on
the outside of the diaphragm (1), to move the diaphragm inward against the stem of demand valve
assembly (2). The action of the diaphragm opens the demand valve assembly and oxygen flows from
the cylinder (5) through the regulator assembly (4) porting and enters the respirator regUlator assembly
body. again raising the pressure in the body. Increased pressure within the body moves the diaphragm
away from the demand valve assembly and stops the flow of oxygen.
EFFECTIVITY:
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Scott
Inc.
/ Scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBL Y • CMIA & IPL
7. Operation (Continued)
A. Respirator Regulator (Continued)
The demand/pressure-demand style respirator regulator assembly is similar to the demand style
respirator regulator assembly except that a slide button (7) on case cover (9) allows the user to select
demand for donning the mask and pressure-demand mode when using the unit. In the pressuredemand mode the diaphragm is moved inward slightly by the action of a spring loaded plate and lever
assembly (10). The action of the plate and lever assembly creates a slight positive pressure within the
pressure-demand mask assembly (e.g., 10800 Series SCOTTORAMIC) before the demand valve
assembly stops the oxygen flow.
The 10800 Series SCOTTORAMIC Mask Assembly, equipped with compensated exhalation valve, is
designed to be used with the pressure-demand respirator regulator assembly only. The 10100 Series
SCOTTORAMIC Mask Assembly is designed for use only with the demand respirator regulator
assembly.
Subtask 35-32-18-870-004
B. Cylinder
The cylinder is a US Department of Transportation (DOT) & Transport Canada (TC) rated pressure
vessel that holds oxygen gas at a nominal working pressure of 1800 to 1850 psig (12.4 - 12.8
MPa). The cylinder is made of steel or of seamless aluminum that is wrapped with Kevlar* fiber.
Information on the cylinder service life and the hydrostatic test frequency requirements can be found in
the CHECK section Table 5003. Cylinder Inspection Frequency.
Subtask 35-32-18-870-005
C. Regulator Assembly
•
The single inlet regulator assembly is a multiple outlet device that lowers inlet pressure from the cylinder
to the outlet assemblies and to a respirator regulator assembly (5600 Series PCA only). The regulator
assembly has an on/off valve, high-pressure gauge, relief valve assembly, safety outlet assembly,
charging valve assembly and various styles of outlet assemblies attached. A regulator assembly may
have a plug installed as an alternative to an outlet assembly.
Refer to Figure 5 for a cross-sectional view of a regulator assembly shown in the open rON") position.
With the regulator assembly installed in the cylinder, and the handle (15) of the on/off valve in the open
position (fully counterclockwise), the head assembly (14) is not seated on the high-pressure oxygen
inlet orifice (13), allowing oxygen to be supplied to the respirator regulator assembly (5600 Series PCA
only) or the outlet assemblies aUached to the regulator assembly. Also, with the on/off valve in the open
position the cylinder can be recharged.
When the handle (15) is in the open position, high-pressure oxygen stored in the cylinder passes into
the inlet orifice (13). High-pressure oxygen and the spring (4) push the thrust pin (7) upward against the
seat assembly (6) preventing flow through the regulator assembly while the opposite end of the thrust
pin (7) acts against a thrust plate (8) and diaphragm (9). One side of the diaphragm is acted upon by an
adjusting spring (10) and the other side by the regulator assembly outlet pressure. The adjusting spring
pushes the diaphragm and thrust plate downward moving the thrust pin away from the seat assembly.
Increasing regulator assembly outlet pressure then moves the diaphragm upward, pushing against the
adjusting spring downward force. Oxygen will flow through the regulator assembly when the force of the
adjusting spring exceeds the regulator assembly outlet pressure acting on the diaphragm and other
forces tending to move the thrust pin against the seat assembly.
When the regulator assembly outlet pressure balances the adjusting spring (10) force, the thrust pin is
moved toward the seat assembly by high-pressure oxygen and spring (4) until a condition of equilibrium
is established and the regulator assembly outlet pressure is maintained. The adjusting spring is preset
to maintain a regulator assembly outlet pressure of apprOXimately 55 psi (0.37 MPa).
•
* Kevlar is a Registered Trademark of E. I. du Pont de Nemours & Co .
EFFECTIVITY:
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/scott
j
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
7. Operation (Continued)
•
C. Regulator Assembly (Continued)
11
10
9
8
7
6
5
17
4
2
•
3
LEGEND
1. Cylinder
2. Safety Plug
3. Safety Disc
4. Spring
5. Thrust Guide Pin
6. Seat Assembly
7. Thrust Pin
8. Thrust Plate
9. Diaphragm
10.
11.
12.
13.
14.
15.
16.
17.
Adjusting Spring
Setscrew
Case
Inlet Orifice
Head Assembly
Handle
Tube
Relief Valve Assembly
RegUlator Assembly
(Cross Sectional View, 5510 Series Regulator Shown)
Figure 5
EFFECTIVITY:
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Technologies.
Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
7. Operation (Continued)
Subtask 35-32-18-870-006
D. Harness Assemblies and Mask Assemblies in Fastener-Mounted Storage Bags.
Most 5500 and 5600 Series PCA's use a harness assembly that is attached to the cylinder with a clamp
near the bottom and a loop around the regulator assembly, allowing the unit to be carried by the
user. Other harness configurations are available and are typically attached to the cylinder using clamps
at the top and bottom of the cylinder.
Typically, PAX mask assemblies are used with fastener-mounted storage bags attached to the cylinder.
Subtask 35-32-18-870-007
E. Outlet Assembly
Ten different outlet style assemblies (300-370, IPL Figures 1A-1J, as applicable) and one outlet port
plug (-395, 396, 397, IPL Figures 1A-1 E, 1H, 1J, as applicable) are available for use on the 5500 and
5600 Series PCA. Some outlet assemblies control the flow rate of oxygen from the regulator
assembly. Each outlet has an internal check valve that permits oxygen flow from the regulator only
when a mating connector is attached to the outlet. Refer to Figure 6 for an illustration of available outlet
assemblies and their mating connectors. Other mating connectors (not illustrated in Figure 6) are
available for use with the outlet assemblies shown.
•
The outlet assembly and mating connector configurations allow a variety of constant flow mask
assemblies to be attached to the 5500 and 5600 Series PCA outlet assemblies. Refer to Table 1 for
accessory mask assemblies for a 5500 Series PCA and Table 3 for accessory mask assemblies for a
5600 Series PCA.
5500 and 5600 Series PCA's use two different types of outlet assemblies, a full flow (non-metered) type
and constant flow (metered) type.
(1) The full flow type outlet assembly contains only a check valve and does not restrict oxygen flow
from the regulator assembly when the check valve is unseated. The full flow outlet assembly is used
to provide an unrestricted flow of oxygen at regulated pressure to a downstream component,
typically a mask-mounted regulator.
(2) The constant flow type outlet assembly, like the full flow type, also contains a check valve which
only allows oxygen flow when unseated. Prior to November 1994, glass wool contained in the outlet
assembly was used to adjust oxygen flow at regulated pressure. Constant flow type outlet
assemblies containing glass wool media are referred to as "adjustable" outlets and are no longer
procurable.
Beginning in November 1994 the 5009-00,5041-00. and 5507-00 constant flow type "adjustable"
outlet assemblies had product improvements which incorporated fewer parts and eliminated the
task of adjusting the flow rate during testing. Constant flow type outlet assemblies manufactured
after November 1994, having a precision-drilled orifice that controls oxygen flow rate, are referred to
as "precision" outlets. The precision outlet has replaced the adjustable outlet and has not changed
in either fit or function.
Constant flow (metered) "precision" outlet assemblies have flow rate and cabin altitude settings
stamped into the exterior of the outlet body. In addition to the flow rate and altitude settings stamps,
the precision outlets (manufactured after November 1994) have special markings on the outlet body
to help identify the outlet. Refer to Figure 7 for details of the special markings stamped into the
"precision" outlet body .
•
EFFECTIVITY:
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Technologies. Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
7. Operation
E.
CMM & IPL
"J
(Continued)
Outlet Assembly
•
(Continued)
Outlet Assembly
SPN 800503-00
(Not Procurable)
~.-
~
.
ro_sec:ll:-llliewl
SPN 5009 Series
Mating Connector
~
....
~
...
:
."
:lZ.
"
,__
~.~
~
,.......~
".
SPN 5041 Series
SPN 5052 series
(Not Procurable)
SPN 5065-10
,
SPN 29559-00
SPN 5067-08
~
IO .... Secl,..,ol~1
SPN 5507 Series
~h----c--~
SPN 14807-00
•
~~
SPN 80285~01
:~'1Th
"..-uv
SPN 802857-01
~
SPN 36728-01
(EROS Type)
SPN 10007498
SPN 10006017
Lockheed Type
(PIN LAC672163-103)
SPN 802863-02
SPN 802627-01
Outlet Assembly
ALL
SPN 36857~1
SPN 10008298
SPN8572-02
EFFECTIVITY:
c§j '-'--r$fE~~
~----c:IJ:j
and Mating Connector
Figure 6
SPN 8570 Series
Combinations
35-32-18
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Technologies. Inc. Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & 'PL
7. Operation (Continued)
Typical Location of
Flow Rate and
Altitude Settings
Typical Location of
Flow Rate and
Altitude Settings
5009, 5041, and 5507 Series "Precision" Outlet Assembly Markings
Figure 7
•
Subtask 35-32-18-870-008
F. Regulator Subassemblies
The following subassemblies attach to the regulator assembly.
(1) Charging valve assembly
Refer to Figure 8.
The charging valve assembly is used to fill the cylinder with high-pressure oxygen. Because the
charging valve assembly is located in the low-pressure section of the regulator assembly, the
on/off valve (10 and -11, IPL Fig. 9) must be open to allow oxygen to flow into the cylinder. Highpressure oxygen applied to the charging valve assembly inlet (1) forces valve core (2) away from
the seat in the charging valve assembly body, and flows through porting into the oxygen cylinder.
When high-pressure oxygen is removed from the charging valve assembly, the valve core moves
toward the seat in the charging valve assembly body and stops the flow of oxygen.
A filler cap (160, IPL Fig. 9) prevents contamination of the valve inlet and also provides a secondary
seal .
•
EFFECTIVITY:
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Technologies. Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
7.
•
CMM & IPL
Operation (Continued)
F. Regulator Subassemblies (Continued)
2
1-----+1~
LEGEND
1. InJet
2. Valve Core
3. Filter
3
Charging Valve Assembly
Figure 8
(2) Relief Valve Assembly
Refer to Figure 9.
The relief valve assembly. installed in the low-pressure section of the regulator assembly, protects
the outlets from over-pressure. The relief valve assembly will open and close as needed and is
continuously available for over-pressure conditions.
Pressure greater than 90 psig (0.62 MPa), at regulator assembly outlet, will force the poppet
assembly (1) away from the seat (6) in the body (2) of the relief valve assembly anowing oxygen to
be vented through an opening in the relief valve assembly body. When pressure at the regulator
assembly outlet is equal to or less than 90 psig (0.62 MPa) a spring (3) forces the poppet against
the seat and stops the flow of oxygen.
•
4
5
LEGEND
1. Poppet Assembly
3
1
2. Body
3.
4.
5.
6.
Spring
Adjusting Screw
Potting Compound
Seat
Relief Valve Assembly
Figure 9
EFFECTIVITY:
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35-32-18
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jSCDtt
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY • CMAt & IPL
TASK 35-32-18-870-808
8.
Optional peA Mounting Bracket Set
Bracket assemblies, sold and shipped separately as optional accessories. may be used to secure certain
PCA configurations within an aircraft.
A bracket set is made up of one lower bracket and one upper bracket. The lower bracket (SPN 36758-01
or SPN 36758-11) supports the base of the cylinder and the upper bracket (SPN 36758-02 or
SPN 36758-12), equipped with a quick release clamp. secures the cylinder at the neck.
NOTE: A bracket set may be used only with cylinders having a nominal volume equal to or less than
11 cu ft (311 liters).
A bracket set is used only on PCA configurations having cylinder part numbers 6084-01. -02, -03, -20 or
21507-06. Using IPL Figures 1A thru 1C. 1E. and 1G (5500 Series PCA) or 1H and 1J (5600 Series PCA).
determine the cylinder part number used with a particular PCA configuration.
Lower bracket (SPN 36758-01) and upper bracket (SPN 36758-02) are not procurable and have been
replaced by SPN 36758-11 and SPN 36758-12 respectively. If replacement parts for either SPN 36758-01
or SPN 36758-02 are required, a complete replacement bracket set (SPN 36758-11 and SPN 36758-12)
must be ordered. Upper and lower brackets are available from Scott Aviation or your Scott Authorized
Aviation Products Distributor.
Refer to Table 5 and Figure 10 for nominal dimensions of upper and lower brackets used to secure a PCA in
an aircraft .
•
•
EFFECTIVITY:
ALL
35-32-18
Page 21
20040415
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1:qco!scott
/scott
Technologies.
Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
)
CMM & IPL
8. Optional peA Mounting Bracket Set {Continued}
•
Table 5
Optional PCA Bracket Set Information
NOMINAL DIMENSIONS
(REFER TO FIGURE 10)
in, (em)
LOWER BRACKET ASSEMBLY
PIN 36758-11
UPPER BRACKET ASSEMBLY
PIN 36758-12
A
DIA
B
3.40
(8.63)
2.31
2.00
0.85
0.72
0.21
0.21
1.75
3.00
2.31
(5.87)
(5.08)
(2.16)
(1.82)
(O.52)
(0.52)
(4.45)
(7.62)
(5.87)
0
C
E
G
DIA
F
H
-t
I:
B
K
J
I
~
K
Top View
~
Lower Bracket
•
Upper Bracket
Side View
Optional PCA Bracket Set
PIN 36758-11 and PIN 36758-12
Figure 10
EFFECTIVITY: ALL
35-32-18
Page 22
20040415
•
•
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f:'1ca/scolt
/scott
Technologies,Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & WL
TESTING AND FAULT ISOLATION
TASK 35-32-18-700-801
1. General
This section contains the testing and fault isolation procedures used to evaluate performance ofthe 5500
and 5600 Series Portable Cylinder Assembly (PCA). Should the PCA need repair or replacement parts
installed, the PCA must pass the appropriate test requirements before the unit is available for use. All tests
in this section must be performed on a PCA that has been overhauled.
Should a failure occur during test procedures, refer to the TrOUbleshooting Chart (Table 1008) for fault
isolation techniques.
Unless noted otherwise, the tests contained in this section apply to all 5500 and 5600 Series PCA. Tests
should be accomplished in a shop proper for repair of high pressure aviation oxygen equipment with an
environment maintained within the limits specified below.
Temperature: 59 - 95°F (15 - 35°C)
Relative Humidity: 5 - 95 Percent
Also, unless noted otherwise, Flowmeters (Table 1002) are open to the atmosphere at the outlet side
(eXhaust), and a Draft Gauge (Table 1002) specified in a test setup must be connected as follows.
-
•
For suction pressure (negative pressure) measurements the test setup connection must be placed on
the port of the Draft Gauge labeled "low" or "suction." The other port (labeled "hr or "pressure") will be
open to the atmosphere .
- For pressure (positive pressure) measurements the test setup connection must be placed on the port
of the Draft Gauge labeled "hi" or "pressure." The other port (labeled "low" or "suction") will be open to
the atmosphere.
Refer to the CHECK section for cylinder hydrostatic test requirements.
Refer to the ILLUSTRATED PARTS LISTS section of this manual for the item numbers given in
parentheses.
NOTE:
Unless otherwise noted, any use of an item number in this section includes all alpha variants and
dashed variants (i.e., items not shown) of that number. For example, item (500) includes SOD,
-500, -500A thru -500D, unless otherwise noted.
WARNING:
DO NOT, UNDER ANY CIRCUMSTANCES, USE OIL PUMPED GAS AS THIS WILL
CAUSE CONTAMINATION OF THE PCA AND THE TEST EQUIPMENT. OIL, EVEN IN
MINUTE QUANTITY, COMING IN CONTACT WITH OXYGEN MAY CAUSE AN
EXPLOSION OR FIRE RESULTING IN SERIOUS PERSONAL INJURY OR DEATH.
FAILURE TO FULLY DISCHARGE THE OXYGEN FROM THE 5500 OR 5600 SERIES PCA,
COMPONENT PARTS OR TEST SETUP PRIOR TO DISASSEMBLY OF ANY PART MAY
CAUSE SERIOUS PERSONAL INJURY OR DEATH.
REFER TO AND FOLLOW APPLICABLE MANUFACTURER'S OR SUPPLIER'S
MATERIAL SAFETY DATA SHEETS (MSDS) BEFORE USING CONSUMABLE TEST
MATERIALS SPECIFIED IN THIS SECTION OR SERIOUS PERSONAL INJURY MAY
OCCUR .
•
EFFECTIVITY: ALL
35-32-18
Page 1001
20040415
t'lco/scott
/scott
Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY •
eMAt a IPL
~,'
TASK 35-32-18-99E-801
2. Reference
•
Documents
A list of applicable
reference
documents
is given in Table 1001.
Table 1001
Reference Documents
DOCUMENT NUMBER
DOCUMENT NAME
MIL-PRF-25567
Military Specification
Leak Detection Compound,
Systems
MIL-PRF-27210
ORDERING INFORMATION
Oxygen
Military Specification
Oxygen, Aviator's Breathing,
Gas
Federal Specification
Nitrogen, Technical
A-A-59503
A-A-58092
Standardization
Documents Order Desk
Building 40, 700 Robbins Avenue
Philadelphia, PA
19111-5094 USA
Liquid and
General Services Administration
1800 F Street
Washington, DC 20405 USA
Commercial Item Description
Tape Antiseize, Polvtetrafluoroethylene
TASK 35-32-18-948-801
3. Special Tools. Fixtures, and Test Equipment
Speylal tools, fixtures, and test equipment required are given in Table 1002. Special tools, fixtures, and test
equipment must be cleaned for oxygen service before use. Unless otherwise noted, one of each item listed
is required. Equivalents may be substituted.
Table 1002
Special Tools, Fixtures, and Test Equipment
PART NUMBER
(or DESCRIPTION)
MANUFACTURER
(VENDOR CODE)
Pressure Gauge
(minimum accuracy ±0.25% full scale)
0-100 psig (0 - 0.69 MPa)
0- 200 psig (0 - 1.38 MPa)
o . 2000 psig (0 - 13.8 MPa)
1404 Series
Ametek (US Gauge)
Sellersville, PA 18960-2625
USA (V61349)
Vent Valve
0.250 in. - 18 ANPT Threads
P4T Series
B-4P4T4
Whitey Co.
Highland Heights, OH 44134-1533
USA (V12623)
Test Regulator
0- 2500 psig (0 -17.2 MPa)
Outlet Pressure
44-1110 Series
44-1114-24
0-250 psig (0 -1.72 MPa)
Outlet Pressure
26-1600 Series
26-1612-24
NOMENCLATURE
EFFECTIVITY:
ALL
•
Tescom Corp.
Elk River, MN 55330-2445
USA (V5H642)
35-32-18
Page 1002
20040415
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•
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tl./ca/scott
jSCDtt
Technologies. Inc. Aviation
550015500 SERIES PORTABLE CYLINDER ASSEMBLY·
3. Special
Tools,
Fixtures.
and Test Equipment
Special
•
•
Tools,
CMM & IPi
(Continued)
Table 1002
Fixtures, and Test Equipment
NOMENCLA lURE
PART NUMBER
(or DESCRIPTION)
MANUFACTURER
(VENDOR CODE)
Flowmeter (minimum accuracy ±2% full scale)
5.0 - 50 cem
13.6 -136 cem
0.62 - 6.20 Ipm
12.6 -1261pm
1110 Series
111 OCC21ABGAA
1110CC11BBGAA
111OCC7'1DBGAA
1110CJ42CBGAA
Emerson Electric Co.
Brooks Instruments Division
Hatfield, PA 19440-3052
USA (V91556)
Mating Connector for
800503-00, 5009-00, 5009 Series Outlet Assy
5041-00.5041 Series OutletAssy
5507-00, 5077 Series Outlet Assy
5052-00 Outlet Assy
10003566,802856-01 Outlet Assy
36728-01, DPB153 OutletAssy
10008298 Outlet Assy
10006017 Outlet Assy
802863-02 Outlet Assy
8572-02 Outlet Assy
5065-10
29559-00
14807-00
5067-08
802857-01
36857-01
10007498
LAC672163-103(Lockheed)
802627-01
8570 Series
Scott Aviation
Lancaster, NY 14086-9502
USA (V53655)
Shut Off Valve (2 required)
1 Series
B-1VF4
Whitey Co.
Highland Heights. OH 44134-1533
USA (V12623)
Flow Control Valve
18 Series
B-18RF8
Whitey Co.
Highland Heights, OH 44134-1533
USA (V12623)
Needle Valve
1 Series
B-1RF4
Whitey Co.
Highland Heights, OH 44134-1533
USA (V12623)
Regulator Test Adapter
0.500 -14 ANPT x 0.250 -18 ANPT Threads
1.00 -11.5 ANPT x 0.250 -18 ANPT Threads
0.750 -16UNF2A x 0.250 -18 ANPT Threads
803213-S58-12
803213-S58-10
803213-558-1
Scott Aviation
lancaster, NY 14086-9502
USA (V53655)
Graduated Cylinder
5 ce Capacity
A2-15
Na~onal Glass and Plastics Co.
Vineland, NJ 08360 USA (VOUUR4)
low Pressure Regulator
Vac to 2 psig (Vac to 14 kPa)
(Vac to 55 in. WC)
16 Series
16112J
Note: REG reqUires both VAC
and PRESS to operate.
Maximum inlet pressure is 250
psig (1.72 MPa).
Fairchild Industrial Products Co.
Winston-Salem. NC 27103-6708
USA (V07282)
Respirator RegUlator Mating Connector
Screw Type - Used with respirator regulator assy
PIN 6379-2C (on 5600-1 Series PCA) or
PIN 800649-00 (on 5600-8 Series peA)
EFFECTIVITY;
ALL
6210-00
Scott Aviation
lancaster, NY 14086-9502
USA (V53655)
35-32-18
Page 1003
20040415
"fLieo/scott
Technologies. Inc.
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
3. Special
Tools.
Fixtures,
,
/scott
Aviation
CMM & IPt
and Test Equipment
Special
•
(Continued)
•
Table 1002 (Continued)
Tools, Fixtures, and Test Equipment
NOMENCLATURE
Respirator Regulator Mating Connector
AN Type - Used with respirator regulator assy
PIN 6379-20 (on 5600-2 Series PCA) or
PART NUMBER
(or DESCRIPTION)
MANUFACTURER
(VENDOR CODE)
13822-00
Scott Aviation
Lancaster, NY 14086-9502
USA (V5365S)
PIN 800649-01 (on 5600-9 Series PCA)
Draft Gauge
(minimum accuracy ±2% full scale)
-5.0 to +5.0 in. WC (-12.7 to +12.7 em WC)
Differential Pressure
o to 15 in. WC (0 - 38 em WC)
2000 Series Magnehelic'
Dwyer Instruments Inc.
Michigan City, IN 46360-0373
USA (V85274)
2310-A-321
2015-A-321
• Magnehelie is a Registered Trademark of Dwyer Instruments Inc.
TASK
35-32-18-94A-801
4. Consumable
Test Materials
A list of consumable
test materials is given in Table
rates specified are for oxygen test gas at NTPD.
1003. Equivalent
materials
may be substituted.
All flow
•
Table 1003
Consumable
Test Materials
MANUFACTURER
(VENDOR CODE)
MATERIAL
DESCRIPTION
Test Gas
1850 psig (12.76 MPa) min press
Oxygen
MIL-PRF-27210, Type I
(Refer to NOTE 1 and NOTE 2)
Local Vendor
Thread sealing Tape
0.250 in. (0.635 em) wide
PTFE Ribbon Tape
CID A-A-58092, size 1
SPN 50011-00
Local Vendor
Leak Test Solution
Sherlock Leak Detector
MIL·PRF-25567, Type 1
Winton Products Co. Inc.
Charlotte, NC 28236
USA (V23316)
Rust Inhibiting Leak Test Solution
5 cc Sodium Chromate per gallon of water.
Allied Chemical Corp.
Morristown, NJ 07960
USA (V70308)
NOTE 1: Oxygen (MIL-PRF-27210, Type I) is the test gas specified in the test procedures in this section of the manual. If water
pumped nitrogen or water pumped air (specified in Note 2) is used for the test gas, the applicable test paramelers must
have the appropriate density correction factors calculated and used, and the test equipment must be calibrated for the
test gas. (A copy of specification Mll-PRF-27210 is available from: Standardization Documents Order Desk, Building 40,
700 Robbins Avenue, Philadelphia, PA 19111-5094 USA)
NOTE 2: Water pumped nitrogen per Federal Specification A-A-59503, Type I, Class I, Grade B. (A copy of Federal Specification
A-A-59503 is available from: General Services Administration, 1800F Street, Washington, DC 20405 USA)
Water pumped air, equivalent in purity to: MIL-PRF-27210. Type I
EFFECTIVITY: All
35-32-18
Page 1004
20040415
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•
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1:L/CD/scott
Technologies.
Inc.
!scott
Aviation
55OCV5600SERIES PORTABLE CYLINDER ASSEIdBLY • eM" & IP!
...
TASK 35-32-18-700-802
5. Relief Valve Assembly (320 thru 340, IPL Fig. 9) Test
Refer to Figure 1001, Table 1002 and Table 1003.
A relief valve which does not pass the following test must be replaced.
Subtask 35-32-18-790-001
A. Leakage
Close the Vent Valve and slowly apply a pressure of 90 psig (0.62 MPa) to the relief valve
assembly. There must be zero leakage from the relief valve assembly. No bubbles in the Rust Inhibiting
Leak Test Solution at the relief valve assembly outlet is an indication of zero leakage.
Subtask 35-32-18-720-001
B. Flow
Remove the relief valve assembly from the Rust Inhibiting Leak Test Solution and apply 135 psig
(0.93 MPa) to the relief valve assembly. The relief valve assembly must allow oxygen to flow through
the outlet opening.
Subtask 35-32~18-790-002
C. Pressure to Close
•
Lower the inlet pressure to 89 psig (0.61 MPa); the relief valve assembly must reseal. Immerse the relief
valve assembly in Rust Inhibiting Leak Test Solutlon. There must be zero leakage from the relief valve
assembly.
Reduce oxygen supply pressure to 0 psig (O MPa) and remove the relief valve assembly from the test
setup. Dry relief valve assembly in clean, dry air.
Pressure Gauge
0-200 psig (0-1.38 MPa)
Test Regulator
~
0-250 psig (0-1.72 MPa) _ ~
TestGaS~
~
CfJ
~
Relief Valve Assembly Test Setup
Figure 1001
TASK 35-32-18-700-803
6. Outlet Assembly Test (300-370, as applicable. IPL Figures 1A thru 1J)
Test applies to all outlet assemblies unless noted otherwise.
•
Refer to paragraph 7.E.(2) in the DESCRIPTION AND OPERATION section to determine if a constant flow
(metered) outlet assembly is an "adjustable" type (300. 310,320,370, IPL Figures 1A thru 1J, as
applicable) or "precision" type (305, 315, 325, IPL Figures 1A thru 1J, as applicable) .
EFFECTIVITY: ALL
35-32-18
Page 1005
20040415
1:'1c:o/scott
/SCOft
Technologies,Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
ClAM & IPL
Refer to Figure 1002, Table 1002 and Table 1003.
•
6. Outlet Assembly Test (Continued)
Subtask 35-32-18-790-003
A. Full Flow (non-metered) Outlet Assemblies (330 thru 355, as applicable, IPL Figures 1A thru 1J)
CAUTION:
FAILURE TO DISCONNECT THE FLOWMETER WHILE TESTING A FULL-FLOW
OUTLET ASSEMBLY MAY DAMAGE THE FLOWMETER BECAUSE OF THE HIGH
FLOW RATE OR PRESSURE POSSIBLE.
(1) Disconnect the Flowmeter from the test setup.
(2) Plug the outlet side of the applicable Mating Connector.
(3) Apply Leak Test Solution to the connection between the outlet assembly (330 thru 355, as
applicable. IPL Figures 1A thru 1J) and the Mating Connector. Adjust the Test Regulator to a
pressure of 125 psig (0.862 MPa), as indicated on the Pressure Gauge.
(4) There must be no leakage between the outlet assembly and the Mating Connector. Bubbles from
the Leak Test Solution are an indication of leakage.
(5) Reduce pressure to 55 ±2 psig (0.38 ±0.014 MPa).
(6) Disengage the Mating Connector from the outlet assembly, then engage. Disengage and engage a
total of five times. The outlet assembly must not bind, stick, or malfunctIon.
(7) Reduce pressure to 0 psig (0 MPa). Remove the outlet assembly from the test setup and dry using
clean, dry, oil-free air.
,
(8) Repeat paragraphs 6.A.(1) thru 6.A.(7) for each full-flow outlet assembly (330 thru 355, as
applicable, IPL Figures 1A thru 1J).
(9) Connect the Flowmeter (previously removed) to the test setup.
Pressure Gauge
Flowmeter
o - 200 psig (0 - 1.38 MPa)
Test Regulator
0- 250 psig (0 -1.72 MPa)
~
•
0.62 - 6.20 Ipm
DUllejAssem~~
~
~
Test Gas
)-------'-----1
~
Mating Connector
Outlet Assembly Test Setup
Figure 1002
EFFECTIVITY: ALL
35-32-18
Page 1006
20040415
•
•
.
t"CO/scotl
!scott
Technologies.Inc. Aviation
.....,
55OCV5600SERIES PORTABLE CYLINDER ASSEMBLY • CMM & IPL
6. Outlet Assembly Test (Continued)
Subtask 35-32-18-790-004
B. Leak Test of Test Setup
Prior to testing constant flow (metered) outlet assemblies (300-325, 370, IPL Figures 1A thru 1J, as
applicable), the test setup must be checked for leaks.
NOTE: Leaks in the test setup may cause errors in the measured flow rates.
(1) Apply Leak Test Solution to all connections in the test setup between the Mating Connector and the
Flowmeter.
(2) Apply 55 psig (0.38 MPa) pressure to the outlet assembly.
(3) There must be no leakage between the Mating Connector and the Flowmeter. Bubbles from the
Leak Test Solution are an indication of leakage.
(4) Tighten any connections that leak.
(5) Reduce inlet pressure to 0 psig (0 MPa).
Subtask 35-32-18-720-002
C. Constant Flow (metered) "Precision" Type Outlet Assemblies (305,315,325,
applicable).
IPL Figures 1A thru 1J, as
(1) Apply Leak Test Solution to the connection between the outlet assembly and the Mating Connector.
•
(2) Apply 55
±2 psig (0.38 ±0.014 MPa) to the outlet assembly .
(3) There must be no leakage between the outlet assembly and the Mating Connector. Bubbles from
the Leak Test Solution are an indication of leakage.
(4) Read the flow rate on the Flowmeter. The flow rate must be within the required flow rate range
shown in Table 1004.
NOTE: Specifications given in Table 1004 correspond to flow rate and altitude settings marked on
the outlet assembly being tested.
(5) Disengage the Mating Connector from the outlet assembly, then engage. Disengage and engage a
total of five times. The outlet assembly must not bind, stick, or malfunction.
(6) Reduce inlet pressure to 0 psig (0 MPa). Remove the outlet assembly from the test setup and dry
using clean, dry, oil-free air.
(7) Repeat paragraphs 6.C.(1} thru 6.C.(6) for each "precision" type constant flow outlet assembly (305,
315,325, IPl Figures 1A thru 1J).
•
EFFECTIVITY; ALL
35-32-18
Page 1007
20040415
't'-/ca/scorr
Technologies. Inc.
!scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
6. Outlet Assembly Test (Continued)
Table 1004
Flow Rate Requirements for Precision Outlet Assembly
Outlet Flow Rate
Setting
(shown on outlet
body}
Ipm atSTPD
0.5
2
5 (1.52)
I
2.47- 2.73
I
4.75- 5.25
I
2.5
3
4
4.5
7
8
Altitude Setting (shown on outlet body)
ft x 1000 (m x 1000)
20 (6.10)
10(3.05) I 15(4.57)
23 (7.01)
Required Ground level Flow Rate
(Min - Max) rpm at NTPD
N/A
0.95-1.05
0.95-1.05
2.47- 2.73 I 2.66- 2.94
2.66- 2.94
2.66-2.94
N/A
3.23- 3.57
3.23 -3.57
N/A
3.90-4.30
3.90-4.30
4.75- 5.25 I 4.94 -5.46
4.94 - 5.46
4.94- 5.46
N/A
5.60- 6.20
5.60-6.20
N/A
8.46- 9.34
8.46- 9.34
N/A
9.50-10.50 9.50-10.50
25 (7.62)
30 (9.14)
0.95-1.05
2.66-2.94
3.23 -3.57
3.90-4.30
4.94- 5.46
5.60-6.20
8.46- 9.34
9.50-10.50
0.95·1.05
2.66- 2.94
323- 3.57
3.90- 4.30
4.94- 5.46
5.60·6.20
B.46- 9.34
9.50-10.50
How To Use This Table:
1. Find the outlet flow rate setting in the left column (e.g., 2 Ipm).
2. Follow the row across to the altitude setting (e.g., 23,000 feet or 7,010 meters).
3. Make sure that the measured flow rate of the outlet assembly under test is within the Min - Max
range for the Required Ground level Flow Rate (e.g., 2.66 - 2.94 Ipm).
Subtask 35-32-18-720-003
D.
•
Constant Flow (metered) "Adjustable" Type Outlet Assemblies (300, 310, 320, 370, IPL Figures 1A
thru 1J, as applicable)
(1) Apply Leak Test Solution to the connection between the outlet assembly and the Mating Connector.
(2) Apply 55 ±2 psig (0.38 ±0.014 MPa) to the outlet assembly.
(3) There must be no leakage between the outlet assembly and the Mating Connector. Bubbles from
the Leak Test Solution are an indication of leakage.
(4) Read the flow rate on the Flowmeter. The flow rate must be within the required flow rate range
shown in Table 1005.
(a) If the flow rate is within the required flow range in Table 1005, proceed to Step 5.
(b) If the flow rate is not within specifications given in Table 1005, discard the "Adjustable" Type
Outlet Assembly (300,310, 320, 370, IPL Figures 1A thru 1J. as applicable), and replace with a
Precision Outlet Assembly. Refer to IPL Table 1, Sheets 1 thru 5 to select the proper precision
outlet assembly.
(5) Disengage the Mating Connector from the outlet assembly, then engage. Disengage and engage a
total of five times. The outlet assembly must not bind, stick, or malfunction.
(6) Reduce the inlet pressure to 0 psig (0 MPa). Remove the outlet assembly from the test setup and
dry using clean, dry, oil-free air.
EFFECTIVITY: ALL
35-32-18
Page 1008
20040415
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•
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1:I./CO/SCOtl
!scott
Technologies.Inc. Aviation
550015600 SERIES PORTABLE. CYLINDER ASSEMBLY·
CMM & IPt
6. Outlet Assembly Test (Continued)
(7) Repeat paragraphs
(300,310.320.370,
6.0.(1) thru 6.0.(6) for each "adjustable"
IPL Figures 1A thru 1J, as applicable).
Table 1005
Flow Rate Requirements for Adjustable
Outlet Flow Rate
Setting
(shown on outlet
body)
Ipm at STPD
5 (1.52)
10 (3.05)
Outlet Assembly
Altitude Setting (shown on outlet body)
ft x 1000 (m x 1000)
23 (7.0n
15 (4.57)
20 (6.10)
Required Ground Level Flow Rate
.(Min - Max) Ipm at NTPD
0.90-1.00
0.92 -1.02
0.94 -1.04
2.68 -2.96
2.58 -2.86
2.64-2.92
3.09 -3.41
3.23 - 3.57
3.26 - 3.60
3.39 - 3.75
3.46 - 3.82
3.50 - 3.86
3.91 -4.33
3.77 -4.17
3.85 -4.25
4.85 - 5.37
4.94 - 5.46
5.00 - 5.52
8.27 - 9.15
8.36 - 9.24
8.43 - 9.31
9.41 -10.40
9.57 -10.57
9.50 -10.50
25 (7.62)
I 3019.14)
0.95 -1.05
1.03 - 1.13
0.86 - 0.95
0.67 - 0.74
2.70 - 2.98
2.76 - 3.06
2.33 - 2.57
2.50 - 2.76
3.28 - 3.62
3.30 - 3.64
3.04 - 3.36
2.91 ·3.21
2.5
3.52 - 3.90
3.58 - 3.96
3.16-3.50
3.33 - 3.69
2.7
3.94 -4.36
3.99 - 4.41
3.44 - 3.80
3.66 - 4.04
3
5.04 - 5.58
5.11 - 5.65
4
4.59- 5.07
4.72 - 5.22
8.46 - 9.36
8.12-8.98
8.55 - 9.45
7
7.98- 8.82
9.60 -10.62
9.74 -10.76
9.26 -10.24
8
9.12-10.08
How To Use This Table:
4. Find the outlet flow rate setting in the left column (e.g., 2 Ipm).
5. Follow the row across to the altitude setting column (e.g., 23,000 feet or 7,010 meters).
6 . Make sure that the measured flow rate of the outlet assembly under test is within the Min - Max
range for the Required Ground Level Flow Rate (e.g., 2.68 - 2.96 Ipm).
0.5
2
•
type constant flow outlet assembly
TASK 35-32-18-70Q.-804
7. Respirator
Regulator (110, IPL Fig. 1H; 115, IPL Figure 1J) Tests
Refer to IPL Fig. 3 unless noted otherwise.
These tests apply to all respirator regulators
(-10 thru -40) unless noted otherwise.
For demand/pressure-demand
respirator regulator (-30, -40), put the slide button (170) on the case cover
(190) in the demand mode unless noted otherwise.
Subtask 35-32-18-790-005
A. Demand Valve Assembly
(240) Leakage
Refer to Figure 1003, Table 1002 and Table 1003.
(1) Observe the Pressure Gauge and apply 35 psig (0.24 MPa) pressure to the respirator regulator
inlet.
(2) Measure the demand valve assembly
more than 10 cern NTPO.
leakage (if present) with Flowmeter.
Leakage must not be
(3) Increase the inlet pressure to 75 psig (0.52 MPa). The demand valve assembly leakage
(if present) must not be more than 10 cem NTPD.
(4) Reduce the inlet pressure to 0 psig (0 MPa) and remove the respirator regulator from the test setup .
•
EFFECTIVITY:
ALL
35-32-18
Page 1009
20040415
1:'1ca/scott
Technologies.
Inc.
/scott
Aviation
5500'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
",
CMM & JPL
7. Respirator Regulator (Continued)
Pressure Gauge
0- 100 psig (0 - 0.69 MPa) .
\
Test Regulator
0- 250 psig (0 -1.72 MPa)
Test Gas
Flowmeter
5-50ccm
Respirator Regulator
\
~
•
\
J----/-----'--------:::;i~,<;~\"
I
I
Inlet
0.125 - 27 ANPT
Threads
/
Respirator Regulator
Mating Connector
Demand Valve Assembly Leakage Test Setup
Figure 1003
Subtask 35-32-18-790-006
B. Inward Leakage Test
Refer to Figure 1004, Table 1002 and Table 1003.
(1) Seal the respirator regulator inlet port.
(2) Apply a negative pressure of 1 in. WC, as indicated on Draft Gauge, to the outlet of the respirator
regulator.
•
(3) Leakage, as measured on the Flowmeter, must not be more than 100 ccm NTPD.
Subtask 35-32-18-790-007
C. Outward leakage Test
Refer to Figure 1004, Table 1002 and Table 1003.
(1) Seal the respirator regulator inlet port.
(2) Apply a positive pressure of 12 in.
respirator regulator.
we, as indicated
on the Draft Gauge, to the outlet of the
(3) Leakage, as measured on the Flowmeter, must not be more than 100 ccm NTPD.
EFFECTIVITY: ALL
35-32-18
Page 1010
20040415
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1:I.ICo/scott
jSCDtt
Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CUM & 'PL
7. Respirator Regulator (Continued)
,.----------~-------------------- - -- ---. -- -- - - - - ------------------~------------------------,,
Low Pressure Regulator
102 pslg (Vae to 14 KPa)
~ae
Draft Gauge
-5 to +5 in. we
Respirator Regulator
/I£:i:TlI)X
i
~
I~~';;:'I
1~~
0.125 -Inlet
27 ANPT
Threads
j
\ ~
.-+------'------'JJ\
\
Flowmeter ~
1
/
",/
•
Draft Gauge
,
~
i
i
i
Test Regulator
0 - 250 psig (0 -1.72 Mpa)
~ __
~
..
_
13.6 -136 cern
II/Shut
,
•
~
Flowmeter
0 to 15 in. /
Respirator Regulator
Mating Connector
Test Gas
0
Shut Off
Valve
13,6 -136 cern
Inward Leakage
Setup
~"c:'~~~
1/
Outlet
Off Valve
Vacuum
0
""
Outward Leakage
Setup
0Source
r"l
Low Pressure Regulator "\ ~Test
Vae to 2 psig (Vae to 14 KPa)
'-
Gas
"
Test Regulator
0 -250 psig (0 - 1.72 Mpa)
~------------------------------------ .._-----------------------------------------------------Inward/Outward Leakage Test Setup
Figure 1004
Subtask 35-32-18-720-004
D. Flow Test
Refer to Figure 1005, Table 1002 and Table 1003.
(1) Demand type respirator regulators, (-10 thru -40, IPL Figure 3)
This test applies to all demand type regulators, (-10 thru -40, IPL Figure 3)
(a) Close the Shut Off Valve, Flow Control Valve and Needle Valve.
(b) Observe the Pressure Gauge and slowly apply 40 psig (0.28 MPa) pressure to the inlet of the
respirator regulator.
(c) Apply vacuum to the test setup.
(d) Slowly adjust the Flow Control Valve until Flowmeter NO.2 indicates a flow of 20 Ipm NTPD.
(e) Carefully open the Shut Off Valve. Compare the respirator regulator outlet suction pressure
indicated on the Draft Gauge with requirements in Table 1006.
(f) Repeat paragraph 7.0.(1) for all flow rates (at inlet pressures) given in Table 1006.
(g) Close the vacuum source and reduce the inlet pressure to 0 psig (0 MPa) .
•
EFFECTIVITY: ALL
35-32-18
Page 1011
20040415
-t'lca/scot1
Technologies. Inc.
...
/scott
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
...
eMU & IPL
7. Respirator Regulator (Continued)
•
D. Flow Test (Continued)
Draft Gauge
-5.0 to +5.0 in. WC
Flowmeter No. 1
5-50ccm
Pressure Gauge
o - 100 psig (0 - 0.69
Needle Valve
MPa)
Shut Off Valve
Test Regulator
Vacuum
Source
~
/~/
'\
..
Flow Control Valve
0.125 ~n~ ANPT
Respirator Regulator
Threads
/
Respirator Regulator
Mating Connector
Flowmeter No. 2
12.6 - 126 Ipm
•
Flow Test Setup
Figure 1005
Table 1006
Flow Test Requirements for Demand Mode Respirator Regulators
REG INLET PRESSURE
psig (MPa)
40 (0.28)
60 (0.41)
(2) Demand/Pressure-Demand
REGULATOR OUTLET
FLOW RATE
Ipm at NTPD
20
70
100
20
70
100
MAX OUnET SUCTION
PRESSURE
in.WC
-0.75
-1.55
-2.00
-0.75
-1.55
-2.00
type respirator regulator (-30, -40, IPL Figure 3)
This test applies only to demand/pressure-demand
type respirator regulators (-3D, -40, IPL Fig. 3).
(a) Put the slide button (170) on the case cover (190) in the pressure-demand mode.
(b) Close Shut Off Valve, Flow Control Valve and Needle Valve.
(c) Observe the Pressure Gauge and slowly apply 40 psig (0.28 MPa) pressure to the inlet of the
respirator regulator.
(d) Apply vacuum to the test setup.
(e) Open the Shut Off Valve. Slowly adjust the Flow Control Valve until Flowmeter NO.2 indicates a
flow of 20 Ipm NTPD.
EFFECTIVITY: ALL
35-32-18
Page 1012
20040415
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1:L/cajscotl
Technologies, Inc.
/SCOft
Alliation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
7. Respirator Regulator (Continued)
D. Flow Test (Continued)
(f)
Compare the respirator regulator outlet pressure indicated on the Draft Gauge with the
requirements in Table 1007.
WARNING: FAILURE TO WEAR GLOVES WHEN BENDING COMPRESSION SPRING MAY
RESLILT IN INJURY TO THE HANDS.
(g) If the outlet pressure indicated on the Draft Gauge is not in agreement with the requirements
found in Table 1007, adjust the compression spring (140).
NOTE:
Carefully and in small increments, bend the ends of the compression spring (140)
closer together (inward) to reduce the outlet pressure or farther apart (outward) to
increase the outlet pressure.
(h) Repeat paragraph 7.D.(2)(a) thru 7.D.(2)(f) for a flow rate of 100 Ipm NTPD (at inlet pressures)
given in Table 1007.
m
Close the Flow Control Valve.
(k) Slowly adjust the Needle Valve until Flowmeter No. 1 indicates a flow of 0.01 Ipm NTPD.
(I)
Compare the respirator regulator outlet pressure indicated on the Draft Gauge with the
requirements found in Table 1007 for the respirator regulator inlet pressures of 40 and 60 psig
(0.28 and 0.41 MPa).
(m) Close the vacuum source and reduce the inlet pressure to 0 psig (0 MPa).
•
Table 1007
Flow Test Requirements for Pressure-Demand Mode Respirator Regulators
REG INLET PRESSURE
psiQ(MPa)
40 (0.28)
60 (0.41)
REGULATOR OUTLET
FLOW RATE
IpmatNTPD
20
100
0.01
20
100
0.01
ALLOWABLE
OUTLET PRESSURE
in. we
+0.5 to +2.0
+0.5 to +2.0
+0.5 to +2.5
+0.5 to +2.0
+0.5 to +2.0
+0.5 to +2.5
TASK 35-32-18-780-801
8. Regulator Assembly (-1 thru -1 E, IPL Fig. 9) Output Pressure Test
Refer to IPL Fig. 9 unless noted otherwise.
The regulator assembly must have the output pressure set correctly and checked for repeatability so that
the outlet assemblies will provide the required flows.
Refer to Figure 1006, Table 1002 and Table 1003.
A. Make sure that the on/off valve (10, -11) is in the closed position (fully clockwise). Insert the appropriate
Mating Connector into any outlet assembly and discharge any pressure remaining in the regulator
assembly. Remove the Mating Connector.
B. Remove the relief valve assembly (320 thru 340) and install the Pressure Gauge .
•
EFFECTIVITY: ALL
35-32-18
Page 1013
20040415
1:L/ca/scott
/scott
~
•
Technologies.Inc. Aviation
5500'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
a. Regulator Assembly (Continued)
•
C. Remove one outlet assembly (300 thru 370, IPL Figures 1A thru 1J, as applicable) or plug (-395. -396,
-397, as applicable, IPL Figures 1A thru 1E, 1H. 1J) from the body (510 thru -550, IPL Figure 9).
Connect the Needle Valve and Flowmeter where the outlet assembly or plug was removed. Close the
Needle Valve.
D. Apply 1800 psig (12.41 MPa) pressure to the inlet ofthe regulator assembly.
E. Rotate the handle (30) counterclockwise to open the on/off valve.
F. Carefully open and adjust the Needle Valve until the Flowmeter indicates 4.0 Ipm NTPD.
G. The regulator assembly output pressure, as indicated on the Pressure Gauge. must be 55 ±2 psig
(0.38 ±0.014 MPa). If necessary, adjust the regulator output pressure as follows.
NOTE: After the initial regulator output pressure adjustment is made at 55 ±2 psig (0.38 ±O.014 MPa).
further adjustments are to be made only if noted.
(1) If necessary. refer to the DISASSEMBLY section to remove the screws (360) and identification plate
(350) from the case (380).
(2) Turn the setscrew (370) until the Pressure Gauge indicates 55 ±2 psig (0.38 ±O.014 MPa).
NOTE: Turn the setscrew in (clockwise) to increase the output pressure. Scott recommends that
the pressure be set near 57 psig (0.39 MPa) initially.
H. Put the on/off valve in the closed position, then in the open position.
J. Observe the flow indicated on the Flowmeter and adjust, if necessary, to 4.0 Ipm using the Needle
Valve. With a flow rate set at 4.0 Ipm the regulator assembly output pressure, as indicated on the
Pressure Gauge, must be 55 ±2 psig (0.38 ±O.014 MPa).
K. Repeat paragraph a.H. and 8.J. ten times. With a flow rate set at 4.0 Ipm the regulator assembly output
pressure. as indicated on the Pressure Gauge, must be 55 ±2 psig (0.3a ±0.014 MPa).
•
L. Close the Needle Valve and make sure that the flow indicated on the Flowmeter is 0 Ipm.
M. The pressure indicated on the Pressure Gauge must be less than or equal to 75 psig (0.52 MPa).
N. Allow the regulator assembly to remain pressurized for 24 hours. Repeat paragraph a.J.
P. If necessary. refer to paragraph a.G. and adjust the regulator outlet pressure to 55 ±2 psig
(0.3a ±O.014 MPa).
Q. Repeat paragraph a.H. thru a.M.
R. Reduce the regulator assembly inlet pressure to 0 psig (0 MPa). Open the Needle Valve and discharge
any pressure remaining in the regulator assembly.
EFFECTIVITY: ALL
35-32-18
Page 1014
20040415
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tL/c:a/scotl
!scott
Technologies.Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPI
8. Regulator Assembly (Continued)
S. Remove the Needle Valve and Pressure Gauge from the regulator assembly. Refer to the ASSEMBLY
section and reinstall the outlet assembly (300 thru 370, as applicable, IPL Figures 1A thru 1J), plug
(-395, -396, -397, as applicable, IPL Figures 1A thru 1E, 1H, 1J), screws (360, IPL Figure 9) and
identification plate (350) previously removed.
Needle Valve
Flowmeter
0-100
,
To
To
Relief Valve Assy Port
(0.125·27 ANPT Thread)
Outlet Assy Port
(0.125·27 ANPT Thread)
Test Regulator
0-2500 psig (0 -17.2 MPa)
~
Pressure Gauge
psig (0 - 0.69 MPa)
~_.
~
j
Regulator Test Adapter
TestGas~
•
Output Pressure Test Setup
Figure 1006
TASK 35-32-18-780-802
9. Gauge (290 thru -310. IPL Fig. 9) Accuracy Test
Refer to IPL Fig. 9 unless noted otherwise.
Refer to Figure 1007, Table 1002 and Table 1003.
A. Close the Vent Valve.
B. Apply 1800 psig (12.41 Mpa) pressure to the test setup, as indicated on the Pressure Gauge. The
pressure indicated on the gauge (290 thru -310) must be within ±100 psig (±O.69 MPa) of pressure
indicated on the test setup Pressure Gauge.
C. Repeat paragraph 9.B. at test setup pressure of 1000 psig (6.89 MPa). The pressure indicated on the
gauge (290 thru -310) must be within ±100 psig (±0.69 MPa) of the pressure indicated on the test setup
Pressure Gauge.
D. Reduce the inlet pressure of the test setup to 0 psig (0 MPa). The pressure indicated on the gauge
(290 thru -310) must be within ±100 psig (±0.59 MPa) of the pressure indicated on the test setup
Pressure Gauge.
E. Open the Vent Valve and remove the gauge (290 thru -310) .
•
EFFECTIVITY: ALL
35-32-18
Page 1015
20040415
1:'-/CO/SCOlt
/SCOtf
Technologies,Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
.
.,
CMM & IPL
9. Gauge Accuracy Test (Continued)
Pressure Gauge
0-2000 psig (0-13.8 MPa)
Test Regulator
Vent Valve
•
Gauge
(Items 290 thru -310)
0.125 -27 ANPT Threads
\
0-2500 psig (o~pa)
Test Gas)
I------~
~
~
~
~
I
J
Gauge Accuracy Test Setup
Figure 1007
TASK 35-32-18-700-805
10. Valve (10, -11, IPL Fig. 9) Torgue Test
Refer to IPL Fig. 9 unless noted otherwise.
Refer to Figure 1008, Table 1002 and Table 1003.
A. Refer to the DISASSEMBLY section and remove the identification plate {20}, nut (40A), handle (30),
spring washer (60) and flat washer (70) from the on/off valve (10, -11).
,
B. Apply 1800 psig (12.41 MPa) to the inlet of the regulator assembly {-1 thru -1 E}.
C. Using the torque wrench rotate the stem (100) counterclockwise one full turn. The torque required to
rotate the stem one full turn must not be more than 16 in·lbs (1.8 N·m).
•
D. Using the torque wrench, and applying a torque of not more than 16 in·lbs (1.8 N·m), rotate the stem
(100) clockwise until the on/off valve {10, -11} is closed.
E. Attach the appropriate Mating Connector to any outlet assembly and discharge any pressure remaining
in the regulator assembly.
F. Attach the hose connecting the Graduated Cylinder and the Mating Connector. Leakage, if present,
must not be more than 5 cc in one hour.
G. Remove the hose connecting the Graduated Cylinder and the Mating Connector. Remove the Mating
Connector from the outlet assembly.
H. Refer to the ASSEMBLY section and install the identification plate (20), nut {40A}, handle (30), spring
washer (60), and flat washer (70) previously removed.
EFFECTIVITY: ALL
35-32-18
Page 1016
20040415
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1:qca/scotl
jSCDtt
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL.
10. Valve Torque Test (Continued)
Mating Connector
(Table 1002)
"..
Glass Container
w/ Water
... ~utIet ~emb~
~
On/Off Valve
~
5 cc Graduated Cylinder
(inverted and water filled)
'"
l. ---_
..
Test Gas
0 }--__
Regulator Test Adapter
---J
Test Regulator
~
0- 2500 psig (0 -17.2 MPa)
Valve Torque Test Setup
Figure 1008
TASK 35-32-18-700-806
11. PCA (-1. -2. -3. -4 (as applicable), IPL Figures 1A thru 1J) Final Test
•
Refer to IPL Fig. 9 unless noted otherwise .
Make sure the PCA is fully charged [1800 psig (12.41 MPa) minimum] before testing for external
leakage. Refer to the ASSEMBLY section for PCA charging procedure.
Subtask 35-32-18-790-008
A. External Leakage
(1) Apply Leak Test Solution to all PCA external surfaces.
(2) Rotate the handle (30) counterclockwise to open the on/off valve (10, -11).
(3) External leakage from all PCA external surfaces must be zero. Bubbles from the Leak Test Solution
are an indication that the PCA is leaking.
(4) Keep the on/off valve in the open position for 24 hours and recheck the PCA for external leakage.
(5) Put the on/off valve in the closed position. Insert the applicable Mating Connector into any outlet
assembly and discharge any remaining pressure in the regulator assembly. Remove the Mating
Connector .
•
EFFECTIVITY: ALL
35-32-18
Page 1017
20040415
-tyca/scotl
Technologies. Inc.
/SCOtf
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
11. PCA Final Test (Continued)
Subtask
35-32-18-720-005
B. Functional
Test
Perform a functional test of the PCA by connecting
assure the flow of oxygen.
an appropriate
mask to each outlet assembly
to
Additionally,
if the peA is a 5600 Series (equipped with a respirator regulator assembly),
also connect
demand type or demand/pressure-demand
type mask assembly (as appropriate)
to the respirator
regulator assembly.
Put on the face mask assembly and breathe to assure the flow of oxygen.
TASK
a
35-32-18-810-801
12. Fault Isolation
Refer to Table
1008 for troubleshooting
problems,
causes,
and solutions.
Table 1008
Troubleshooting
Chart
TROUBLE
PROBABLE CAUSE
SOLUTION
Malfunctioning or damaged relief valve
assembly.
Replace relief valve assembly.
Outlet assy and mating connector not
connected properly.
Disconnect and reconnect outlet assy
and mating connector.
Mating connector wom or damaged.
Replace mating connector.
Outlet assy wom or damaged.
Replace worn parts or replace outlet
assy.
Contaminated, worn, or damaged outlet
assy.
If a "precision" type outlet assembly,
clean or replace outlet assy.
RELIEF VALVE ASSEMBLY TEST (PARA 5.)
Relief valve assembly (320 thru 340, IPL Figure
9) operation pressure is out of limits.
OUTLET ASSEMBLY TEST (PARA 6.)
Outlet assy (300 thru 370, IPL Figures 1A thru
1J, as applicable) leaks at connection 10 mating
connector.
Outlet assy (300 thru 370, IPL Figures 1A thru
1J, as applicable) flow rate is out of limits.
•
If an "adjustable" type outlet assembly,
discard and replace with a "precision"
type outlet assembly.
Connection between outlet assy (300 thru 370,
IPl Figures 1A thru 1J, as applicable) and
maUngconnector is binding, sticking or
malfunctioning.
Outlet assy and mating connector
contaminated, worn, or damaged.
Clean or replace outlet assy or mating
connector.
DEMAND VALVE ASSEMBLY LEAKAGE TEST (PARA 7.A.)
Demand valve assy (240, IPL Fig. 3) leakage
exceeds maximum allowable.
Demand valve assy wom, binding, or
damaged.
Replace demand valve assy.
Demand valve assy not tight in regulator
case (350, IPL Fig. 3).
Tighten demand valve assy.
Wom
or damaged valve seat gasket
Replace valve seat gaskel
(280, IPL Fig. 3).
EFFECTIVITY:
ALL
35-32-18
Page 1018
20040415
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.-
t'lco/scott
!scott
Technologies. Inc. Aviation
550lJ15600 SERIES PORTABLE CYLINDER ASSEMBLY - CMM & IPI
12. Fault Isolation (Continued)
Table 1008 (Continued)
Troubleshooting
Chart
PROBABLE CAUSE
TROUBLE
SOLUTION
INWARD (PARA. 7.B.) AND OUTWARD (PARA. 7.C.) LEAKAGE TESTS
Respirator regulator assy (-10 thru -40,
IPL Fig. 3) leakage exceeds maximum
allowable.
Respirator regulator assy inlet not
sealed during testing.
Seal inlet to respirator regulator assy.
Diaphragm assy (200, IPL Fig. 3)
punctured or torn.
Replace diaphragm assy.
Diaphragm assy loose or improperly
installed.
Reinstall diaphragm assy.
Diaphragm cord (205, IPL Fig. 3) or
clamp (210) is loose or damaged.
Replace diaphragm cord or clamp.
Demand/pressure-demand respirator
regulator (-3D, -40, IPL Fig. 3) slide
button (170, IPL Fig. 3) not set to
demand mode.
Set slide button to demand mode.
Worn, binding, or damaged demand
valve assy (240, IPL Fig. 3).
Replace demand valve assy .
FLOW TEST - DEMAND MODE (PARA 7.D.(1))
Pressure of the demand/pressure -demand
respirator regulator assy (-3D, -40, IPL Fig. 3)
is out of limits.
•
•
I
Diaphragm assy (200, IPL Fig. 3) torn
punctured.
EFFECTIVITY:
ALL
or
Replace diaphragm assy.
Diaphragm assy (200, IPL Fig. 3) loose
or improperly installed.
Reinstall diaphragm assy.
Diaphragm cord (205, IPL Fig. 3) or
clamp (210) is loose or damaged .
Replace diaphragm cord or clamp.
35-32-18
Page 1019
20040415
1:IIeD/scott
Technologies.Inc.
/scott
•
Aviation
5SOO15600SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
12. Fault Isolation (Continued)
Table 1008 (Continued)
Troubleshooting Chart
TROUBLE
FLOW TEST - PRESSURE-DEMAND
PROBABLE CAUSE
SOLUTION
MODE (PARA 7.D.(2})
Pressure of demandlpressure-demand
respirator regulator assy (-30, -40, IPL Fig. 3)
is out of limits.
Demand/Pressure-Demand
respirator
regulator (-30, -40, IPL Fig. 3) slide
button (170, IPL Fig. 3) not set to
pressure..<Jemand mode.
Set slide button to pressure-demand
mode.
Worn, binding, or damaged demand
valve assy (240, IPL Fig. 3).
Replace demand valve assy.
Diaphragm assy (200, IPL Fig. 3) tom or
punctured.
Replace diaphragm assy.
Diaphragm assy (200, IPL Fig. 3) loose
or improperly installed.
Reinstall diaphragm assy.
Diaphragm cord (205, IPL Fig. 3) or
clamp (210) is loose or damaged.
Replace diaphragm cord or damp.
Compression spring (140, IPL Fig. 3)
out of adjustment or damaged.
Adjust or replace compression spring.
REGULATOR ASSEMBLY OUTPUT PRESSURE TEST (PARA. 8.)
Regulator assy (-1 thru -1E, IPL Figure 9) outlet
pressure is out of limits.
Regulator assy requires adjustment.
Adjust regulator assy ouUet pressure.
Damaged valve seat area in body
(510 thru -550), IPL Fig. 9).
Replace body.
Thrust pin (470, IPL Fig. 9) worn or
damaged.
Replace thrust pin.
Seat assy (460, IPL Fig. 9) worn or
damaged.
Replace seat assy.
Diaphragm (430, IPL FIQ. 9) worn or
damaged.
Replace diaphragm.
Diaphragm (430, IPL Rg. 9) not sealed
in body (510 thru -550, IPL Fig. 9).
Reposition diaphragm in body.
Spring (490, IPL Fig. 9) or adjusting
spring (400, IPL Fig. 9) damaged.
Replace spring or adjusting spring.
Damaged, obstructed, or malfunctioning
gauge.
Replace gauge.
•
GAUGE ACCURACY TEST (PARA. 9.)
Gauge (290 thru -310, IPl Fig. 9) indicated
pressure is out of limits.
EFFECTIVITY: ~LL
35-32-18
Page 1020
20040415
•
•
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•
-tL/co/SCOtl
!SCOft
Technologies. Inc. Aviation
550015liOO SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPi
12. Fault Isolation (Continued)
Table 1008 (Continued)
Troubleshooting Chart
PROBABLE CAUSE
SOLUTION
Threads on head assy (120, IPL Fig. 9)
binding or not lubricated.
lubricate threads.
Damaged threads on head assembly
(120, IPL Fig. 9) or bushing (140, IPL
Fig. 9).
Replace head assembly or bushing.
Stem assy (100, IPL Fig. 9) is bent.
Replace stem assy.
Head assy (120, IPL Fig. 9) wom or
damaged.
Replace head assy.
Damaged on/off valve seat area in body
(510 thru ·550, IPL Fig. 9).
Replace body.
Connection between elbow (105, IPL Fig. 1H,
1J), outlet assy (300 thru 370, IPl Figures 1A
thru 1J, as applicable), relief valve assy (320
thru 340, IPL Fig. 9), gauge (290 thru -310,
IPL Fig. 9), charging valve assy (170) and
body (51 0 thru ·550, IPL Fig. 9) leaks.
Parts do not have correct seal with
thread sealing tape.
Disassemble and assemble parts that
leak to the regulator body.
Threads damaged.
Replace damaged part.
Part not tight in body.
Retighten or retorque part as required.
Connection between on/off valve (10, -11, IPL
Fig. 9) and body (510 thru -550, IPL Fig. 9)
leaks.
Bushing (140, IPL Fig. 9) threads
damaged,
Replace bushing.
Worn, damaged, or non-lubricated
preformed packing (130, IPL Fig. 9).
Replace preformed packing.
Bushing (140, IPL Fig. 9) not tight in
body.
Retorque bushing.
Safety plug washer (280, IPL Fig. 9)
damaged,
Replace safety plug washer.
Safety plug (250, IPL Fig. 9) not tight in
body.
Retorque safety plug.
Leakage at relief valve assy (320 thru 340, IPL
Fig. 9).
Relief valve assy malfunctioning or
damaged.
Replace relief valve assy.
Leakage past valve core (-190, IPL Fig. 9) of
charging valve (170, IPL Fig. 9).
Worn or damaged valve core (-190, IPL
Fig. 9) or body (·180,IPL Fig. 9).
Replace valve core or body.
Valve core (-190, IPL Fig. 9) not tight in
body (-180, IPL Fig. 9) .
Retorque valve core.
TROUBLE
VALVE TORQUE TEST (PARA. 10.)
Torque required to open and close on/off
valve (10, -11, IPL Fig. 9) is out of limits.
Regulator assy (-1 thru -1E, IPL Figure 9)
leaks when on/off valve (10, -11, IPL Fig. 9) is
set to the closed position.
PCA FINAL TEST (PARA. 11.)
•
Connection between safety outlet assy (-220,
IPL Fig. 9) and body (510 thru -550, IPL Fig.
9) leaks.
•
EFFECTIVITY: ALL
35-32-18
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!scott
•
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPl
12. Fault Isolation (Continued)
Table 1008 (Continued)
Troubleshooting Chart
TROUBLE
I SOLUTION
PROBABLE CAUSE
PCA FINAL TEST (PARA. 11.) (Continued)
Leakage past safety outlet assy
(-220, IPL Fig. 9).
Leakage past safety plug (210, IPL Fig. 9)
Connection between packing nut (80, IPL
Fig. 9) and bushing (140,IPL Fig. 9) leaks.
I
Connection between elbow assy (105, IPL Fig.
1H, 1J), connector assy (100, IPL Fig. 1H, 1J).
and respirator regulator assy (110, IPl Fig. 1H;
115, IPl Figure 1J) leaks.
Connection between plug (210, Fig. 9) and
body (510 thru -550, IPL Fig. 9) leaks.
EFFECTIVITY: ALL
Safety disc (270, IPL Fig. 9) or gasket
(240, IPL Fig. 9) damaged.
Replace safety disc or gasket.
Safety cap (230, IPL Fig. 9) not tight on
safety plug (250, IPL Fig. 9).
Retorque safety cap.
Safety disc (260, IPL Fig. 9) or safety
plug washer (280, IPL Fig. 9) damaged.
Replace safety disc or safety plug.
Safety plug (210, IPL Fig. 9) not tight in
regulator body (510 thru -550, IPL
Fig. 9).
Retorque safety plug.
Packing nut (80, IPL Fig. 9) does not
have correct seal using preformed
packing (90, IPL Fig. 9) and PTFE seat
(110, IPL Fig. 9).
Replace preformed packing.
Packing nut (80, IPL Fig. 9) not tight in
bushing (140, IPL Fig. 9).
Retorque packing nut.
Nut (part of connector assy) not light on
tube (part of elbow assy).
Tighten nul on tube.
Worn or damaged ferrule (part of
connector assy).
Replace connector assy.
Connector assy (100, IPl Fig. 1H, 1J)
does not have correct seal with thread
sealing tape.
Disassemble and assemble connector
assy to respirator regUlator assy.
Connector assy (100,IPl Fig. 1H, lJ)
threads damaged.
Replace connector assy.
Connector assy (100,IPl Fig. 1H, 1J) not
Ught in respirator regulator assy
(105, IPl Fig. 1H; 115, IPL Fig. 1J).
Tighten connector assy.
Plug (210,IPL Fig. 9) not tight in body
(510 thru -550).
Retorque plug.
35-32-18
•
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t'lca/scolt
Technologies. Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY - CMM & IPL
SCHEMATICS AND WIRING DIAGRAMS
TASK 35-32-18-99C-801
1. Schematics and Wiring Diagrams
Not applicable
•
•
EFFECTIVITY:
ALL
35-32-18
Page 2001/2002
20040415
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tf/ca!scotl
/scott
Technologies. Inc. Aviation
550lJ15600SERIES PORTABLE CYLINDER ASSEMBLY·
eMM & 'PL
DISASSEMBLY
TASK 35-32-18-000-801
1. General
This section describes the equipment and procedures necessary to disassemble the 5500 and 5600 Series
Portable Cylinder Assemblies (PCA). Most repair procedures do not need complete disassembly of the
PCA. Disassemble units only to the level necessary, as determined in TESTING AND FAULT ISOLATION
section, to repair or replace components. Disassembly is organized as follows:
Paragraph
3
4
5
6
Description
General PCA Disassembly
Respirator Regulator Disassembly
Regulator Port Device Removal and Disassembly
General Regulator Assy Disassembly
IPL Figure No.
2, 9
3
2, 4 thru 12
2, 9
The instructions in this section apply to all 5500 and 5600 Series PCA unless noted otherwise. Refer to the
ILLUSTRATED PARTS LIST section of this manual for the item numbers given in parentheses.
Unless otherwise noted, all disassembly procedures requiring turning, twisting, or unthreading will be in the
counterclockwise direction.
NOTE:
Unless otherwise noted, any use of an item number in this section includes all alpha variants and
dashed variants (i.e., items not shown) of that number. For example, item (SOD) includes 500,
-500, -500A thru -5000, unless otherwise noted.
TASK 35-32-18-94B-802
•
2. Special Tools, Fixtures, and EqUipment
A list of special tools, fixtures, and equipment necessary for disassembly of the 5500 and 5600 Series PCA
is shown in Table 3001. Special tools, fixtures, and equipment must be cleaned for oxygen service before
use. Figure number information provided in the "NOMENCLATURE" column corresponds to the toollistin9
in Table 9001 of the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section. Unless
noted otherwise, one of each item listed is required. Equivalents may be substituted.
Table 3001
Special Tools. Fixtures, and Test Equipment
PART NUMBER
(or DESCRIPTION)
MANUFACTURER
(VENDOR CODE)
Pneumatic Bench Vise
Model BV-101-P
PIN 58634
Getz Fire Equipment Co.
Peoria, IL 61602-1711
USA (V58013)
Core Wrench
(Figure 9001)
800216- T91-1
Scott Aviation
Lancaster, NY 14086-9502
USA (V53655)
NOMENCLATURE
TASK 35-32-18-060-801
3. General PCA Disassembly
WARNING:
FAILURE TO FULLY DISCHARGE THE PCA OF OXYGEN PRIOR TO DISASSEMBLY OF
ANY PART MAY CAUSE SERIOUS PERSONAL INJURY OR DEATH.
FAILURE TO USE SUITABLE EYE PROTECTION DURING DISASSEMBLY
PROCEDURES MAY CAUSE INJURY TO THE EYES.
•
FAILURE TO SECURE THE CYLINDER, REGULATOR ASSEMBLY AND ATTACHED
HOSE DURING OXYGEN DISCHARGE MAY CAUSE SERIOUS PERSONAL INJURY OR
DEATH .
EFFECTIVITY: ALL
35-32-18
Page 3001
20040415
1:'1COJscott
/scott
Technologies. Inc. Aviation
5504'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
3. General PCA Disassembly (Continued)
Attach a hose equipped with a mating connector (Refer to Figure 6 in the DESCRIPTION AND
OPERATION section) to the outlet port equipped with a constant flow or full flow outlet assembly. Slowly
rotate the handle (30, IPL Figure 9) of the onloff valve (10, -11, IPL Figure 9) to the open (fUlly
counterclockwise) position. Release all the oxygen from the PCA through the attached hose into a well
ventilated area. Rotate the handle of the onloff valve to the closed (fully clockwise) position and remove
the hose from the outlet assembly.
Subtask 35-32-18-070-001
A. 5600 Series Only
(1) Unthread the nut on the connector (100, IPL Figure 1Hand 1J) to allow the connector to be
separated from the elbow assembly (105).
NOTE: The nut and compression ferrule (both part of the connector) will be retained on the elbow
assembly after the connector and elbow assembly are separated. Do not attempt to remove
the nut or compression ferrule from the elbow assembly. If the elbow assembly must be
replaced, the elbow assembly and connector must be replaced as a set.
(2) On the 5600 Series PCA (2, IPL Figure 1), loosen and remove the upper clamp (75, IPL Figures 1H
and 1J) with the respirator regulator assembly (110, IPL Figure 1H; 115, IPL Figure 1J) attached.
Remove the clamp from the bracket (125). Unthread and discard the self-locking screws (120) and
remove the bracket from the respirator regulator.
(3) On the 5600 Series PCA (2, IPL Figure 1), remove the harness (200, IPL Figures 1H and 1J) from
PCA. Separate the strap assemblies (201, 202) to disassemble the harness (200).
Subtask 35-32-18-070-002
B. 5500 & 5600 Series
•
(1) Loosen and remove lower clamp (70, IPL Figures 1A thru 1E and 1G thru 1J) from cylinder (500570, IPL Figures 1A thru 1E and 1G thru 1J, as applicable).
(2) On the 5500 Series (1, IPL Figure 1) or 5600 Series (2, IPL Figure 1) PCA remove the harness (205
thru 225, 250 thru 285, IPL Figures 1A thru 1E and 1G thru 1J, as applicable) from the neck of the
cylinder.
NOTE: Although a close til, the loop-end of the hamess is large enough to go over the regUlator
assembly (-1 IPL Figure 9).
(3) Remove the 10 plate (55, IPL Figure 1A thru 1F; 80, IPL Figure 1G; -60 IPL Figure 1Hand 1J) from
the cylinder only if damaged.
(4) Remove instruction decal (20, IPL Figures 1A thru 1G, 25; IPL Figures 1H and 1J)from cylinder
only if damaged.
(5) Remove oxygen ID decal (30, IPL Figures 1A thru 1J), if equipped, from cylinder only if damaged.
NOTE: The painted text, "BREATHING OXYGEN ONLY - USE NO OIL", was used in place of the
oxygen ID decal (30, IPL Figures 1A thru 1J) on some 5500 Series and 5600 Series PCA's.
(6) Remove the aviators oxygen placard (-50, IPL Figures 1A, 1C, 1E, 1H, and 1J) and instruction
placard (-40, IPL Figures 1A, 1C, 1E, 1H, and 1J) from the cylinder. Remove label (45, IPL Figures
1A, 1C, 1E, 1H, and 1J) from the pressure gauge (290 thru -300, IPL Figure 9).
EFFECTlVITY: ALL
35-32-18
Page 3002
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/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY • ClAM & IPL
3. General PCA Disassembly (Continued)
Subtask 35-32-18-070-003
C. 5500 Series Only
(1) Unfasten the hook and loop type fastener strap (45, 50, IPL Figure 2) and remove the mask storage
bag assembly (55, 60) from the cylinder (500 thru 565. IPL Figure 1A thru 1E, as applicable).
Remove the PAX mask assembly (35 thru 41, IPL Figure 2) from the mask storage bag assembly.
If the PAX mask assembly is in a clear protective bag, cut open the clear plastic bag and remove
the connector (15, 20), coupling (-25), or nipple (-30) from the mask assembly (35 thru 41) only if
damaged.
NOTE: Refer to Scott CMM 35-22-26 for more information on the PAX mask assembly (35 thru 41,
IPL Figure 2).
(2) On the 5500 Series PCA (1, IPL Figure 1) loosen and remove the upper clamp (75, IPL Figures 1A
thru 1C) from the cylinder. Remove the harness (200) from PCA. Separate the strap assemblies
(201 and 202) to disassemble the harness (200).
(3) On the 5500 Series PCA (1, IPL Figure 1) loosen and remove the upper clamp (75, IPL Figures 1B
and ~IE)from the cylinder. Remove the harness (225) from the PCA.
(4) On the 5500 Series PCA (-1, -2, -3, -4, as applicable), IPL Figures 1A thru 1G) remove the FAAPMA label (35) from the cylinder only if damaged.
TASK 35-32-18-060-802
•
4. Respirator RegUlator Assembly (110, IPL Figure 1H, 115.IPL Figure 1J) Disassembly
Refer to IPL Figure 3, unless noted otherwise.
Disassemble the respirator regUlator as follows.
Subtask 35-32-18-070-004
A. Cover Assembly (-50, -60) Removal, and Disassembly.
(1) Unthread the pan head screws (70) and remove the cover assembly (-50, -60) from the regUlator
case (350).
(2) Remove the rivets (100,130) and the identification plate (80, 90,110,120) from the case cover
(180, 190) only if the identification plate is damaged. Discard the rivets if removed.
(3) Carefully remove the slide button (170), spring (160), compression spring (140) and plate with lever
assembly (150) from the case cover (190).
NOTE: The plate with lever assembly is not procurable. If a replacement part is required, a complete
cover assembly (-60) must be ordered.
Subtask 35-32-18-070-005
B. Diaphragm (200) Removal
(1) Carefully remove the diaphragm damp (210) from the diaphragm (200).
NOTE: If diaphragm (200) is secured by diaphragm cord (205), the diaphragm cord should not be
removed unless necessary. Diaphragm cord is no longer procurable. If the diaphragm cord
is removed, it must be replaced with a diaphragm clamp (210).
(2) CarefUlly remove the diaphragm (200) from the regulator case (350) .
•
EFFECTIVITY; ALL
35-32-18
Page 3003
20040415
1:'-/ca/SCOII
Technologies. Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
4. Respirator Regulator Assembly Disassembly (Continued)
Subtask 35-32-18-070-006
C. Deflector (220) and Demand Valve Assembly (240) Removal and Disassembly
(1) Unthread the pan head screws (230) and remove the deflector (220) from the regulator case
(350).
(2) Unthread the pan head screws (250) and remove the lock washer (260), flat washer (270), and
demand valve assembly (240) from the regulator case (350).
(3) Remove and discard the valve seat gasket (280) from the regulator case (350).
Subtask 35-32-18-070-007
D. General Disassembly
Remove the remaining components of the respirator regulator assembly (110, IPL Figure 1H; 115,
IPL Figure 1J) components from regulator case (350) as follows.
(1) Unthread the connector (100, IPL Figures 1Hand 1J) from the regulator case (350, IPL
Figure 3). Remove the screen (340) from the regulator case.
(2) Remove the adapter (290, 300) from the regulator case (350).
(3) Remove the external retaining ring (-330) and cover assembly (-310) from the adapter body (-320).
TASK 35-32~18-060-803
5. Regulator Port Device Removal and Disassembly
t
Unless specified, all removal and disassembly procedures for regulator port devices apply equally to the
5500 and 5600 Series PCA. Place the PCA in a Pneumatic Bench Vise (Table 3001) for removal of items
attached to the regulator ports.
•
Refer to IPL Figure 9 unless noted otherwise.
Subtask 35-32-18-070-008
A. Gauge (290 thru -310, IPL Figure 9)
Refer to IPL Figure 12 unless noted otherwise.
Remove the gauge and disassemble as follows.
CAUTION:
ONLY THE LENS, BEZEL, BEZEL WITH LENS, GASKET OR RELIEF LABEL MAY BE
REMOVED FROM THE GAUGE OR DAMAGE MAY OCCUR.
(1) If damaged, remove and discard the lens (30.40). bezel (10. 20). and bezel with lens (50, 60) from
the gauge (1 thru 1F, as applicable).
(2) If damaged, remove and discard the relief label (80) or gasket (70) from the gauge (1D, 1F).
Subtask 35-32-18-070-009
B. Relief Valve Assembly (320 thru 340, IPL Figure 9)
Remove relief valve assembly from the body (510 thru -550).
EFFECTIVITY: ALL
35-32-18
Page 3004
20040415
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tllca/scott
/scott
Technologies, Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY - CMM & IPL
5. Regulator Port Device Removal and Disassembly
(Continued)
Subtask 35-32-18-070-010
C. Charging Valve (170, IPL Figure 9)
Remove the charging valve and disassemble as follows.
(1) Remove the charging valve (170) from the body (510 thru -550).
(2) Remove the filler cap (160) from the charging valve (170).
NOTE: Older style filler caps (158) had removable filler cap seats (159). The older filler cap and filler
cap seat are non-procurable parts. Do not disassemble the filler cap seat (159) from filler
cap (158). If replacement parts for the old filler cap (158) or filler cap seat (159) are required,
the filler cap (160) must be ordered as a replacement part.
(3) Remove the filter (-200) from the body (-180).
(4) Remove the valve core (-190) from the body (-180) using the Core Wrench (Table 3001).
Subtask 35-32-18-070-011
D. Safety Plug Assembly (210, IPL Figure 9) or Safety Outlet Assembly (-220, IPL Figure 9)
Remove the safety plug assembly or safety outlet assembly and disassemble as follows.
(1) Remove the safety plug assembly (210) or safety outlet assembly (-220) from the body
(510 thru -550, as applicable).
•
(2) Remove and discard the safety disc (260) from the body (510 thru -540) .
(3) Remove and discard the safety plug washer (280) from the body (510 thru -550).
(4) Remove the safety cap (230), safety disc (270), and gasket (240) from the safety plug (250).
Discard the safety disc and gasket.
Subtask 35-32-18-070-012
E. On/Off Valve (10, -11, IPL Figure 9)
Remove and disassemble the on/off valve kit as follows.
(1) Remove on/off valve (10, -11) from the body (510 thru -550).
(2) Remove the filter (150) from the body (510 thru -550).
(3) Disassemble the on/off valve as follows.
(a) Remove and discard the identification plate (20) from the handle (30).
(b) Unthread the nut (-40, 40A) and remove washer (-50), handle (30), spring washer (60), and flat
washer (70) from the stem assembly (100).
(c) Unthread the packing nut (80) from the bushing (140). Remove the preformed packing (90) and
seat (110) from the stem assembly (100). Discard the preformed packing.
(d) Remove the stem assembly (100) and unthread the head assembly (120) from the bushing
(140).
(e) Remove and discard the preformed packing (130) from the bushing (140) .
•
EFFECTIVITY: ALL
35-32-18
Page 3005
20040415
f:I./CCI/scott
Technologies. Inc.
!scott
•
Aviation
5500/5600 SERIES PORTABLE CYlINDER ASSEMBLY·
CMM & IPL
5. Regulator Port Device Removal and Disassembly
(Continued)
Subtask 35-32-18-070-013
F. SPN 800503-00 (-4, IPL Figure 5), 5009-00 (-1, IPL Flgure 5), or 5009 Series (-2 thru -3F, IPL Figure 5)
Outlet Assembly
Refer to IPL F~gure 5 unless noted otherwise.
Remove and discard the 800503-00 (-4) or 5009-00 (-1) outlet assembly. Replace with a precision type
outlet assembly (-2 thru -3F).
NOTE: Replacement parts are not available for the outlet assembly (-50, -60), flow port (120, 130), filter
(150), retaining ring (140), gasket (160), stud (70), glass cord (40), screen (30), screw (20), or
orifice (180). Do not disassemble these parts.
(1) Remove the dust cover (10) from the receptacle (170) only if damaged.
(2) For precision type outlets (-2 thru -3F), unthread the receptacle (170) from the stud (70, 80).
(3) For precision type outlets (-2 thru -3F), remove the spring (110), valve (100) and gasket (90) from
the receptacle (170). Discard the gasket.
Subtask 35-32-18-070-014
G. 5041-00 (-1, IPL Figure 4) and 5041 Series (-2 thru -2P, IPl Figure 4) Outlet Assembly
Refer to IPL Figure 4 unless noted otherwise
Remove and discard the 5041-00 outlet assy (-1). Replace with a precision outlet assy (-2 thru -2P) .
NOTE: Replacement parts are not available for the screw (50), SCreen (60, 80). glass cord (70),
coupling assembly (-90), outlet subassembly (-100), body (120. 130), or orifice (200). Do not
disassemble these parts.
(1) For precision outlets (-2 thru -2P), unthread the nut (20) and remove the cover assembly (10), cap
(30), and washer (40) from the case (190).
•
(2) For precision outlets (-2 thru -2P), remove the springs (170) from the pins (180) and remove the
pins from the case (190).
(3) For precision outlets (-2 thru -2P), unthread the setscrew (110) from the case (190).
(4) For precision outlets (-2 thru -2P), unthread the case (190) from the body (120, 130).
(5) For precision outlets (-2 thru -2P), remove the spring (140). valve (150), and valve seat (160) from
the case (190). Discard the valve seat.
Subtask 35-32-18-070-015
H. 5507-00 (-1, IPL Figure 7) and 5507 Series (-2 thru -2E, IPl Figure 7) Outlet Assembly
Refer to IPL Figure 7 unless noted otherwise.
Remove and discard the 5507-00 outlet assy. Replace with a precision outlet assy (-2 thru -2E).
NOTE: Replacement parts are not available for the screw (10), screen (30), glass cord (20), outlet
subassembly (-40), body (140, 150), or orifice (160). Do not disassemble these parts.
(1) For precision outlets (-2 thru -2E), unthread the fillister head screw (80) and remove the dust cover
(70) and torsion spring (60) from the threaded adapter (50). Discard the fillister head screw.
(2) For precision outlets (-2 thru -2E), Remove the threaded adapter (50) from the body (140, 150) and
remove the lockwasher (90), outlet washer (100), outlet gasket (110), outlet poppet (120), and f1owstop spring (130). Discard the gasket (110).
EFFECTIVITY: ALL
35-32-18
Page 3006
20040415
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•
_
t'lco/scott
7echnologies.
Inc.
!SCOtf
A lIiation
55OO1S6ooSERIES PORTABLE CYLINDER ASSEMBLY·
eM'" & IPL
5. Regulator Port Device Removal and Disassembly
(Continued)
Subtask 35-32-18-070-016
J. SPN 10003566 Oxygen Coupling (340, IPL Figure 1A, 1C, 1E, 1H) or SPN 802856-01 Outlet Assembly
(-1, IPL Figure 11)
Remove and disassemble the 10003566 oxygen coupling or 802856-01 outlet as follows.
Refer to IPL Figure 11 unless noted otherwise.
NOTE: Oxygen coupling (SPN 10003566) is replaced by outlet assembly (SPN 802856-01). Do not
disassemble oxygen coupling, SPN 10003566.
(1) Remove the warning label (50) and dust cover retainer (10) from the dust cover (40) only if
damaged.
(2) Twist and unlock the dust cover (40) from the groove pin (30) on the disconnect fitting (20). Remove
the dust cover (40).
(3) Remove the preformed packing (110,120), disconnect body (100), quad ring (90), disconnect
poppet (80), poppet spring (70), and gasket (60) from the disconnect fitting (20). Discard the quad
ring and preformed packing or gasket.
Subtask 35-32-18-070-017
K. SPN 5052-00 Outlet Assembly (370, IPL Figure 1H, -1, IPL Figure 8)
Remove and disassemble the 5052-00 outlet as follows.
•
Refer to IPL Figure 8 unless noted otherwise .
Replacement parts are not procurable for this outlet assembly. Do not disassemble the 5052-00 outlet
assembly. If replacement is required, the outlet assembly must be replaced by a different outlet
assembly. Refer to IPL Table 1, Sheet 5 to choose an outlet assembly that is procurable.
Subtask 35-32-18-070-018
L. SPN 36728-01 (-1, IPL Figure 13) Outlet Assembly
Remove the 36728-01 outlet.
Do not disassemble a 36728-01 outlet assembly.
Subtask 35-32-18-070-020
M. SPN 10006017 (355,IPL Figure 1C) Outlet Assembly
Remove the 10006017 outlet assembly.
Replacement parts are not procurable for this outlet assembly. Do not disassemble this outlet assembly.
Subtask 35-32-18-070-021
N. SPN 8572-02 (-1, IPL Figure 6) Outlet Assembly
Remove and disassemble the 8572-02 outlet as follows.
Refer to Figure 6 unless noted otherwise.
(1) Unthread the body assembly (10) from the adapter (90) and disassemble as follows.
(a) Remove the grooved pin (-20) from the body (-40).
(b) Remove the washer (-30) from the body (-40).
•
(2) Remove the gasket (50), poppet (60), spring (70), and inlet filter (80) from the adapter (90). Discard
the inlet filter.
EFFECTIVITY: ALL
35-32-18
Page 3007
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/scott
Technologies.Inc. Aviation
SSOOIS600SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMU & #PL
5. Regulator Port Device Removal and Disassembly
(Continued)
Subtask 35-32-18-070-022
P. SPN 802863-02 (-1, IPL Figure 10) Outlet Assembly
Remove and disassemble the 802863-02 outlet as follows.
Refer to Figure 10 unless noted otherwise.
(1) Unthread the nipple (10) from the outlet body (140).
(2) Remove the dust plug assembly (-20) from the outlet body (140) and disassemble as follows.
(a) Remove the dust plug (50) from the insert sleeve (80).
(b) Remove the preformed packing (40) from the dust plug (SO). Discard the preformed packing.
(c) Remove the dust cover (30) from the outlet body (140).
(3) Unthread the insert sleeve (80) from the outlet body (140). If damaged, remove the pins (70) from
the insert sleeve.
(4) Remove the preformed packing (110), retainer (100), seal (90), poppet (120) and spring (130) from
the outlet body (140). Discard the preformed packing and seal.
TASK 35-32-18-060-804
6. General Regulator Disassembly (-1 thru -1 E, IPL Figure 9)
Place the PCA in a Pneumatic Bench Vise (Table 3001) to remove the regulator body from the cylinder .
Refer to IPL Figure 9 unless noted otherwise.
Subtask 35-32-18-070-023
A. 5500 & 5600 Series
•
(1) Remove the screws (360), identification plate (350), and setscrew (370) from the case (380).
Discard screws.
(2) Carefully unthread the case (380) from the body (510 thru -550). Remove the guide (390), adjusting
spring (400), slip ring (420), diaphragm plate (410), diaphragm (430), and thrust plate (440) from the
case (380).
(3) Unthread the holder (450) and remove the seat assembly (460), thrust pin (470), thrust pin guide
(480), and spring (490) from the body (510 thru -550).
(4) Remove the tube (500) from the body (510 thru -550) only if damaged.
(5) Remove the drive screws (S80) securing the identification plate (560, 570) from the regulator body
(510 thru -550). Discard the drive screws.
(6) Unthread the regulator body (510 thru -550) from the cylinder (SOD thru 570, IPL Figures 1A
thru 1J, as applicable).
Subtask 35-32-18-070-024
B. 5500 Series Only
On 5500 Series PCA (-1, IPL Figure 1G), remove the following items.
(1) Remove the metal boss seal (475, IPL Figure 1G) from the regulator body (-550, IPL Figure 9).
Discard the metal boss seal.
EFFECTIVITY: ALL
35-32-18
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Technologies.Inc. A .,iation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
CLEANING
TASK 35-32-18-100-801
1. General
This section contains information about the equipment and the procedures for cleaning the 5500 and 5600
Series peA. Before cleaning, the units shall be disassembled using procedures in the DISASSEMBLY
section.
NOTE:
Unless otherwise noted, any use of an item number in this section includes all alpha variants and
dashed variants (i.e., items not shown) of that number. For example, item (500) includes 500,
-500, -SOOAthru -5000, unless otherwise noted.
2. Safety
WARNING:
FAILURE TO USE SUITABLE EYE PROTECTION DURING CLEANING PROCEDURES
MAY CAUSE INJURY TO THE EYES.
WHEN USING CLEANING SOLVENTS, AVOID PROLONGED OR REPEATED CONTACT
WITH SKIN AND INHALATION OF TOXIC VAPORS OR SERIOUS PERSONAL INJURY
MAY QCCUR.
MAKE SURE THAT CLEANING PROCEDURES ARE PERFORMED IN AN APPROVED
CLEANING CABINET, OR IN A WELL VENTILATED ROOM OR AREA, OR SERIOUS
PERSONAL INJURY MAY OCCUR.
DO NOT USE SOLVENTS NEAR OPEN FLAMES, OR IN AREAS WHERE THERE ARE
HIGH TEMPERATURES, OR SERIOUS PERSONAL INJURY; FIRE OR EXPLOSION MAY
OCCUR.
•
DO NOT ALLOW OIL, GREASE, FLAMMABLE SOLVENTS OR OTHER COMBUSTIBLE
MATERIALS TO COME IN CONTACT WITH PARTS THAT WILL BE EXPOSED TO
PRESSURIZED OXYGEN. DUST, LINT, AND FINE METAL PARTICLES ARE ALSO
POTENTIAL COMBUSTIBLES THAT CAN IGNITE WHEN EXPOSED TO PRESSURIZED
OXYGEN AND RESULT IN EXPLOSION OR FIRE.
REFER TO AND FOLLOW APPLICABLE MANUFACTURER'S OR SUPPLIER'S
MATERIAL SAFETY DATA SHEET (MSDS) BEFORE USING CLEANING MATERIALS
SPECIFIED IN THIS SECTION OR SERIOUS PERSONAL INJURY MAY OCCUR.
TASK 35-32-18-99E-802
3. Reference Documents
A list of applicable reference documents is given in Table 4001.
Table 4001
Reference Documents
DOCUMENT
NUMBER
•
DOCUMENT NAME
ORDERING INFORMATION
ARP 1176
Oxygen System and Component
Cleaning and Packaging
Society of Automotive Engineers InU.
Warrendale, PA 19428-2959
USA
MIL·[)'16791
Military Specification
Detergents, General Purpose
(liqUid. Non-ionic)
US Government Printing Office
Washington, DC 20402
USA
RR-C-901C
Cylinders, Compressed Gas;
High Pressure. Steel DOT 3M and Aluminum
Applications, General Specifications for:
US Government Printing Office
Washington. DC 20402
USA
EFFECTIVITY: ALL
35-32-18
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5501115600 SERIES PORTABLE CYLINDER ASSEMBLY • CMM & IPL
TASK 35-32-18-948-803
•
4. Special Tools, Fixtures, and Equipment
A list of special tools, fixtures, and equipment necessary for cleaning of the 5500 and 5600 Series peA are
shown in Table 4002. Special tools, fixtures, and equipment must be cleaned for oxygen service before
use. Unless noted otherwise, only one of each item is required. Equivalents may be substituted.
Table 4002
Special Tools, Fixtures, and Equipment
NOMENCLATURE
PART NUMBER
(or DESCRIPTION)
Protective Cap
1.188 in. (3.018 em) ID
1.125 in. (2.858 em) ID
1.250 in. (3.175 em) 10
PIN C234 SPN 33492-029
PIN C232 SPN 33492-027
PIN C336 SPN 33492-032
Wire Brush
1 in. diameter
Local Vendor
LiquidNapor Degreaser System
MSR-216LE
Baron Blakeslee
Long Beach, CA 90813
USA (VOFDJ7)
Stainless Steel Tubing
0.250
0.035
or
0.375
0.035
I
Ultrasonic Cleaning System
MANUFACTURER
(VENDOR CODE)
Alliance Plastics Inc.
Erie. PA 16510-3045
USA (V34669)
in. (6.35 mm) 00 x
in. (0.889 mm) Wall
Local Vendor
in. (9.53 mm) 00 x
in. (0.889 mm) Watt
TH-1418-9
Mass Technology
PO Box 795-T
East Moline, IL 61244-0795 USA
Fax: 309-755-1121
•
TASK 35-32-18-94A-802
5. Consumable Cleaninq Materials
A list of consumable cleaning materials is given in Table 4003. International environmental agreements
may limit the use of some consumable cleaning materials. Equivalent materials may be substituted.
Table 4003
Consumable Cleaning Materials
MANUFACTURER
(VENDOR CODE)
MATERIAL
DESCRIPTION
Flushing Agent
LenlumGS
(n-propyl Bromide)
Petroferrn
Fernandina Beach, FL 32034
USA (VOWUAB)
Cleaning Agent
HFE-71DE
(Azeotrope of Perlluorobutyl Methyl
Ether)
3M/SPLC
St. Paul, MN 55133-3900
USA (VDU817)
Non-ionic Detergent
Non-ionic Detergent
Mll-D-16791, Type I
Local Vendor
EFFECTIVITY: ALL
35-32-18
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Technologies. Inc. Aviation
55(K1I5600SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
5. Consumable Cleaning Materials (Continued)
Table 4003 (Continued)
Consumable Cleaning Materials
MANUFACTURER
(VENDOR CODE)
MATERIAL
DESCRIPTION
Ceramic Tumbling Media
XA Ceramic Media
30 mesh
Washington Mills Abrasive Co.
North Grafton, MA 01536-1558
USA (V89204)
Glass Tumbling Media
Ballotini Impact Beads
The PO Corp.
Valley Forge, PA 19482-0840
USA (V08867)
TASK 35-32-18-100-802
6. Cylinder Cleaning
The 5500 Series PCA uses either a steel or composite (fiber reinforced aluminum) cylinder to store oxygen,
while the 5600 Series PCA use only steel cylinders. External cleaning and general internal cleaning
procedures are the same for both types of cylinders used with the PCA. If corrosion or odor is present on
the inside of the cylinder, specific internal cleaning procedures must be followed.
Subtask 35-32~18-140-001
A. External Cleaning
•
(1) Seal the opening at the neck of the cylinder using a Protective Cap (Table 4002) .
(2) Prepare a 1 percent non-ionic detergent solution by mixing approximately 1.5 oz (40 cc) of
Non-ionic Detergent (Table 4003) into 1 gallon (4 liters) of clean water.
(3)' Clean the outside of the cylinder using a soft-bristled brush and clean, hot (104 - 140°F, 40 - 60°C)
1 percent solution of non-ionic detergent and water.
(4) Rinse the outside of the cylinder with clean water.
(5) Dry the outside of the cylinder with clean, dry, oil-free air.
(6) Remove Protective Cap from cylinder opening.
Subtask 35-32-18-160-001
B. General Internal Cleaning
CAUTION: THE NECK AND THREADED AREA OF COMPOSITE CYLINDERS MUST NOT BE
CLEANED USING ANY ABRASIVE ACTION OR ABRASIVE MATERIALS, INCLUDING
WIRE BRUSHES OR ABRASIVE PRODUCTS, OR DAMAGE TO SEALING SURFACES
OR THREADS MAY OCCUR.
(1) Clean the neck and threads of the steel cylinder (500 thru 565, IPL Figures 1A thru 1F, 1H, 1J, as
applicable) with a Wire Brush (Table 4002) as needed.
(2) Shake out any unwanted material from inside the cylinder.
(3) Setthe cylinder into
a cleaning tank as shown in Figure 4001.
(4) Use the Stainless Steel Tubing (Table 4002) and clean the inside of the cylinder with warm
(65 - 80°F, 18 - 27°C) Flushing Agent (Table 4003) for 3 minutes. The flow rate of the Flushing
Agent must be a minimum of 1.2 gallons (4.5 liters) per minute per cleaning station.
NOTE: The length of the Stainless Steel Tubing is a function of the size of the cylinder.
•
(5) Let the Flushing Agent drain from the cylinder for one minute .
EFFECTIVITY: ALL
35-32-18
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20040415
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Technologies. Inc.
I
Scott
Aviation
SS00l5600SERIES PORTABLE CYLINDER ASSEMBLY·
•
CUM & IPL
6. Cylinder Cleaning (Continued)
B. General Internal Cleaning (Continued)
DegreasingAgent
or
Water
or
Clean, Dry, Oil-Free HeatedAir
Cylinder
Vertical Position ___
(wi Neck Down)
___
~
Stainless SteelTube ...........
LiquidNapor
Cleaning Tank
"'~"'I'- ..
\1
Cylinder Internal Cleaning Setup
Figure 4001
(6) Dry the cylinder with clean, dry air that is oil-free and heated (180 - 200cF, 82 - 93°C). Flow
approximately 12.5 psig (0.086 MPa) air through Stainless Steel Tubing for one minute.
(7) Remove the cylinder from the cleaning setup and allow it to cool to room temperature.
(8) Make sure the cylinder is cleaned to General Specification RR-C-901 C (Table 4001), except
hydrocarbon contamination cylinder must be less than 1.0 mg per square foot of sUrfac~ area
cleaned.
(9) Make sure that the inside of the cylinder does not have an odor or contamination. If the cylinder has
an odor or contamination, perform the following specific cylinder internal cleaning procedures for a
steel cylinder or a composite cylinder.
•
Subtask 35-32-18-120-001
C. Steel Cylinder Internal Cleaning
Perform this operation only if signs of corrosion (including large amounts of irregular shaped deposits on
the inner cylinder surface) or odor are present inside of steel cylinders (500 thru 565, IPL Figures 1A
thru 1F, 1H, 1J. as applicable).
(1) Refer to Table 4004 to determine the amount of small (approximately 30 mesh) Ceramic Tumbling
Media (Table 4003) required for corrosion removal.
Table 4004
Cylinder Media Requirements
EFFECTIVITY: ALL
CYLINDER CAPACITY
cu ft (liters)
MEDIA REQUIRED
lbs. (gm)
4·11 (113-312)
0.5 (227)
22-49 (623-1388)
0.75 (340)
63-115 (1784-3257)
1.0 (454)
35-32-18
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Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY • CMM & IPL
6. Cylinder Cleaning (Continued)
C. Steel Cylinder Internal Cleaning (Continued)
(2) Fill cylinder with correct amount of Ceramic Tumbling Media determined from Table 4004. Cover
cylinder opening with Protective Cap (Table 4002). Shake and turn (at the same time) by hand the
media filled cylinder for approximately 3 to 5 minutes. Remove Protective Cap and empty media
from cylinder.
(3) Set the cylinder into the cleaning tank as shown in Figure 4001 and flush the cylinder with clean,
heated (160 - 190°F, 71 - 88°C) water through Stainless Steel Tubing (Table 4002) for two minutes
minimum. The flow rate for the heated water must be a minimum of 1.2 gallons (4.5 liters) per
minute per cleaning station.
(4) Let the water drain completely from the cylinder.
(5) Dry the cylinder with clean, dry air that is oil-free and heated (180 - 200°F, 82 - 93°C). Flow air
through the Stainless Steel Tubing for four minutes minimum.
Subtask 35-32-18-120-002
D. Composite Cylinder Internal Cleaning
CAUTION: THE NECK AND THREADED AREA OF COMPOSrrE CYLINDERS MUST NOT BE
CLEANED USING ANY ABRASIVE ACTION OR ABRASIVE MATERIALS, INCLUDING
WIRE BRUSHES OR ABRASIVE PRODUCTS, OR DAMAGE TO SEALING SURFACES
OR THREADS MAY OCCLIR.
•
Perform this operation only if signs of corrosion (including large amounts of irregular shaped deposits on
the inner cylinder surface) or odor are present inside of a composite cylinder (570, IPL Figure 1G).
(1) Use Table 4004 to determine the amount of Glass Tumbling Media (Table 4003) required for
corrosion removal.
(2) Fill cylinder with correct amount of Glass Tumbling Media (Table 4003). Cover cylinder opening with
Protective Cap (Table 4002). Shake and turn (at the same time) by hand the media filled cylinder for
approximately 3 to 5 minutes. Remove Protective Cap from cylinder and empty Glass Tumbling
Media from cylinder.
(3) Set the cylinder into a cleaning tank as shown in Figure 4001.
(4) Flush the cylinder with clean, heated (160 - 190°F. 71 - 88°C) water through the Stainless Steel
Tubing (Table 4002) for two minutes minimum. The flow rate for the heated water must be a
minimum of 1.2 gallons (4.5 liters) per minute per cleaning station.
(5) Let the water drain completely from the cylinder.
(6) Dry the cylinder with clean, dry air that is oil-free and heated (180 - 200°F, 82 - 93°C). Flow air
through the Stainless Steel Tubing for four minutes minimum.
(7) The inside afthe cylinder must be completely dry.
TASK 35-32-18-100-803
7. PAX Mask Assemblies (35 thru 41! IPL Figure 2)
Refer to CLEANING section of Scott CMM 35-22-26 for procedures on cleaning a PAX mask assembly .
•
EFFECTIVITY; ALL
35-32-18
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Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMU & IPL
TASK 35-32-18-110-801
..
•
8. Metallic Parts
Make sure that all metallic parts in direct contact with oxygen are cleaned to a maximum of
1 milligram of particulates per square foot of exposed surface (per ARP 1176, Table 4001). Clean metal
parts using a LiquidNapor Degreasing System (Table 4002) with Cleaning Agent (Table 4Q03). Immerse
the parts in the Cleaning Agent for 4 minutes followed by vapor rinse for 2 to 5 minutes. Slowly remove the
parts from the vapor rinse and allow them to cool and dry in a clean work area.
Do not clean the used drive screws (580, IPL Figure 9), metal boss seal (475, IPL Figure 1G), rivet (100,
130, IPL Figure 3), filters (80, Figure 6; 150, -200, IPL Figure 9), safety disc (260, 270, IPL Figure 9), or
identification plate (350, IPL Figure 9). These items must be replaced each time they are removed.
TASK 35-32-18-130-801
9. Non-Metallic Parts
Make sure that all non-metallic parts in direct contact with oxygen are cleaned to a maximum of 1 milligram
of particulates per square foot of exposed surface (per ARP 1176, Table 4001).
Do not clean the valve seat gasket (280, IPL Figure 3), gasket (90, IPL Figure 5; 50, IPL Figure 6; 110, IPL
Figure 7; 240, IPL Figure 9; 60, IPL Figure 11), preformed packing (90, 130, IPL Figure 9; 40, 110, IPL
Figure 10; 110, 120, IPL Figure 11), quad ring (90, IPL Figure 11), valve seat (160, IPL Figure 4), or seal
(90, IPL Figure 10). These items must be replaced each time they are removed.
Prepare a 1 percent non-ionic detergent and water solution by mixing approximately 1.5 oz (40 ec) of
Non-ionic Detergent (Table 4003) in 1 gallon (4 liters) of clean water. Using the non-ionic detergent
cleaning solution clean non-metallic parts in an Ultrasonic Cleaning System (Table 4002) for approximately
3 to 5 minutes. Rinse the cleaned parts with clear, warm (85 - 95°F, 29 - 35°C) water. Dry the parts using
clean, dry air that is oil-free and heated (180 - 200°F, 82 - 93°C).
,
TASK 35-32-18-140-801
•
10. Miscellaneous Parts
Do not clean the self-locking screws (120, IPL Figure 'I H, 1J), fillister head screw (80, IPL Figure 7), or
screw (360. IPl Figure 9). These items must be replaced each time they are removed for disassembly.
The pressure gauge (290 thru -310, IPL Figure 9) surfaces are cleaned with a moist cloth containing a
1 percent solution of Non-Ionic Detergent (Table 4003) and wiped with a moist cloth containing warm
(85· 95°F, 29 - 35°C) water. Dry the gauge using clean, dry air that is oil-free and heated (180 - 200°F,
82 - 93°C).
The Optional PCA Bracket Set (refer to paragraph 8 in the DESCRIPTION AND OPERATION section of
this manual) surfaces are cleaned with a moist cloth containing a 1 percent solution of Non-Ionic
Detergent (Table 4003) and wiped with a moist cloth containing warm (85 - 95°F, 29 - 35°C) water. Dry
the bracket set using clean, dry air that is oil-free and heated (180 - 200°F, 82 - 93°C).
EFFECTIVITY: ALL
35-32-18
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Technologies. Inc. Attiation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
eMM & IPL
CHECK
TASK 35-32-18-210-801
1. General
After disassembly and cleaning of any component, assembly, or unit, examine each part before
assembly. If you are not sure that a part is serviceable, replace it per instructions in ASSEMBLY.
Scott recommends an overhaul be performed on the PCA every 5 years for a PCA with a US Department
of Transportation (DOT) 3AA-1800 steel cylinder (500 thru 555A, IPL Figures 1A thru 1F, 1H, 1J, as
applicable) and every 6 years for a PCA with either a DOT 3HT-1850 steel cylinder (560 and 565, IPL
Figure 1E) or a DOT E-8162-1850 composite cylinder (570, IPL Figure 1G).
During an overhaul of the PCA, the following items must be replaced per instructions in ASSEMBLY.
Identification Plate (20, 350, IPL Figure 9)
Filter (150, IPL Figure 9)
Preformed Packings (90, 130, IPL Figure 9)
Seat (110, 460, IPL Figure 9)
Head Assembly (120, IPL Figure 9)
Safety Disc (260, 270, IPL Figure 9)
Gasket (240, IPL Figure 9)
Safety Plug Washer (280, IPL Figure 9)
Diaphragm (430, IPL Figure 9)
Screws (360, IPL Figure 9)
During an overhaul of a PCA, the following items may require replacement due to damage during disassembly or from rough handling. Replace per instructions in the ASSEMBLY section of this manual.
•
Identification Plate (55, IPL Figures 1A thru 1F; 60, IPL Figures 1H and 1J; 80, IPL Figure 1G; 80, 90,
110, 120, IPL Figure 3; 20, IPL Figure 9)
Instruction Decal (20, IPL Figures 1A thru 1G: 25,IPL Figures 1H and 1J)
Oxygen Identification Decal (30, IPL Figures 1A thru 1J)
Aviators Oxygen Placard (-50, IPL Figures 1A, 1C, 1E, 1H, and 1J)
Instruction Placard (-40, IPL Figures 1A, 1C, 1E, 1H, and 1J)
Label (45,IPL Figures 1A, 1C, 1E, 1H, and 1J)
FAA-PMA Label (35, IPL Figures 1A thru 1G)
Warning Label (65, IPL Figure 1G)
When removed or disassembled, the following items must be discarded and replaced with new parts.
•
Safety Disc (260, 270, IPL Figure 9)
Gasket (90, IPL Figure 5; 50, IPL Figure 6; 110, IPL Figure 7; 240, IPL Figure 9; 60, IPL Figure 11)
Identification Plate (20, IPL Figure 9)
Preformed Packing (90, 130, IPL Figure 9; 40, 110, IPL Figure 10; 110, 120, IPL Figure 11)
Valve Seat Gasket (280, 280A, IPL Figure 3)
Safety Plug Washer (280, IPL Figure 9)
Quad Ring (90, IPL Figure 11)
Self-Locking Screw (120, IPL Figures 1H and 1J; 360, IPL Figure 9)
Valve Seat (160, IPL Figure 4)
Rivet (100, 130, IPL Figure 3)
Diaphragm Cord (205, IPL Figure 3) [Replace with Diaphragm Clamp (210, IPL Figure 3)]
Fillister Head Screw (80, IPL Figure 7)
Drive Screw (580, IPL Figure 9)
Metal Boss Seal (475, IPL Figure 1G)
Filter (80, IPL Figure 6; 150, -200, IPL Figure 9)
Seal (90, IPL Figure 10)
EFFECTIVITY:
ALL
35-32-18
Page 5001
20040415
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Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPt
1. General (Continued)
When removed or disassembled, the following items should be discarded and replaced with new parts per
instructions in the ASSEMBLY section of this CMM. These items are attached by adhesive, and should not
be reused. Reuse of these items may cause them to detach from the PCA, creating potential for "foreign
object damage".
Identification Plate (80, IPL Figure 1G; 80, IPL Figure 3; 20, IPL Figure 9)
Instruction Decal (20, IPL Figures 1A thru 1G; 25, IPL Figures 1H and 1J)
Oxygen Identification Decal (30, IPL Figures 1A thru 1J)
Aviators Oxygen Placard (-50, IPL Figures 1A, 1C, 1E, 1H, and 1J)
Instruction Placard (-40, IPL Figures 1A, 1C, 1E, 1H, and 1J)
Placard (45, IPL Figures 1A, 1C, 1E, 1H, and 1J)
Warning Label (50, IPL Figure 11)
Relief Label (80, IPL Figure 12)
FAA-PMA Label (35, IPL Figures 1A thru 1G)
NOTE:
Unless otherwise noted, any use of an item number in this section includes all alpha variants and
dashed variants (Le., items not shown) of that number. For example, item (500) includes 500,
-500, -500A thru -5000, unless otherwise noted.
TASK 35-32-18-99E-803
2.
Reference Documents
A list of applicable reference documents is given in Table 5001.
Table 5001
Reference Documents
DOCUMENT
NUMBER
DOCUMENTNAME
ORDERINGINFORMATION
C-1
Methodsof HydrostaticTestingof CompressedGasCylinders
CompressedGasAssociationInc.
Arlington,VA 22202-4102USA
G-S
CylinderServiceLifefor SeamlessHighPressureCylinders
C-6
Standardsfor VisualInspectionof SteelCompressedGas
Cylinders
C-6.1
Standardfor VisualInspectionof High PressureAluminum
CompressedGasCylinders
C-6.2
Guidelinesfor VisualInspectionand Requalificationof Fiber
ReinforcedHighPressureCylinders
C-8
Standardfor Requalificationof DOT-3HTSeamlessSteel
Cylinders
DOT-E-8162-1850
ExemptionCertificatefor CompositeCylinder
US GovernmentPrintingOffice
Washington,DC 20402USA
49 CFR 173.34
Codeof FederalRegulations- Part49 Para173.34
(Requirementsfor DOT-3AA-1800and
DOT-3HT-18S0SteelCylinders)
US GovernmentPrintingOffice
Washington,DC 20402USA
EFFECTIVITY:
All
35-32-18
Page 5002
20040415
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Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
TASK 35-32-18-948-804
3. Special Tools, Fixtures, and Equipment
A list of special tools, fixtures, and equipment required to check the 5500 and 5600 Series PCA is
presented in Table 5002. Special tools, fixtures, and equipment must be cleaned for oxygen service before
use. Unless noted otherwise, one of each item is required. Equivalents may be substituted.
Table 5002
Special Tools, Fixtures, and Equipment
NOMENCLATURE
PART NUMBER
(or DESCRIPTION)
MANUFACTURER
(VENDOR CODE)
Bright Inspection Light
Il-24
Titan Tool Supply Co. Inc.
Buffalo, NY 14216-1784
USA (V51679)
TASK 35-32-18-210-802
4. PCA and PCA Components
Do a check of the PCA (1, 2, IPL Figure 1) as follows.
A. General
(1) Do a check of the surfaces and thread areas for signs of damage, contamination, galling, burrs,
corrosion or too much wear.
•
CAUTION: PCA MAY BE DAMAGED OR LEAK IF A PART THAT EITHER HAS, OR HAS CAUSED,
TOO MUCH WEAR OR DAMAGE TO ADJACENT SEALING SURFACES IS NOT
REPLACED.
(2) Do a check of the mating parts and sealing surfaces for scratches and other damage that will cause
leakage.
B. Gauge
Do a check of the gauge (290 thru -310, IPL Figure 9) for damage to the gauge case, lens (30, 40, IPL
Figure 12), bezel (10, 20, IPL Figure 12), lens w/bezel (50,60. IPL Figure 12), or pressure indicating
pointer.
C. Plates, Decals, Placards, and Labels
Make sure that all identification plates (55, IPL Figures 1A thru 1F; 60, IPL Figures 1Hand 1J; 80, IPL
Figure 1G; 20, 350,560,570, IPL Figure 9), instruction decals (20, IPL Figures 1A thru 1G; 25, IPL
Figures 1H and 1J), oxygen identification decals (30, IPL Figures 1A thru 1J). instruction placard (-40, IPL Figures 1A, 1C, 1E, 1H and 1J), aviators oxygen placard (-50, IPL Figures 1A, 1C, 1E, 1H, and 1J).
gauge label (45, IPL Figures 1A, 1C, 1E, 1Hand 1J), warning label (50, IPL Figure 11), relief label (80,
IPL Figure 12), FAA-PMA label (35, IPL Figures 1A thru 1G), and warning label (65, IPL Figure 1G) can
be read and are not damaged.
D. Harness Assemblies
Make sure that all harness assemblies (200 thru 225, IPL Figures 1A thru 1E, 1Hand 1J, as applicable),
strap assemblies (201, 202, IPL Figures 1A thru 1C, 1H and 1J), and fasteners (45,50, IPL Figure 2)
are not cut, worn or damaged.
E. Passenger Oxygen Mask Assemblies
•
Make sure that all Passenger Oxygen Mask Assemblies (35 thru 41, IPL Figure 2), Harness Assemblies
with mask and storage bag (-1 thru -1K, IPL Figure 2), and Storage mask bag assemblies (55, 60, IPL
Figure 2) are not damaged or past service life. See passenger mask service life recommendations in
CMM 35-22-26 .
EFFECTIVITY:
ALL
35-32-18
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Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
..
ClAM & IPL
TASK 35-32-18-210-803
5. Cylinder
•
Assembly
Table 5003 contains
information
about cylinder hydrostatic
testing and cylinder service-life
requirements.
Cylinder inspection frequency or service life information given in Table 5003 is valid for the date of issue for
the 5500,5600 Series PCA Component Maintenance Manual.
Determine actual cylinder condition (e.g., serviceable, rejected, repairable or condemned) by using the
applicable references from Table 5001. AU cylinder repairs must be made before a hydrostatic test of the
cylinder is performed. Any cylinder that has been repaired (as required in the references in Table 5001)
needs a hydrostatic test before it is available for use.
Check composite cylinder or steel cylinder
test must not be used (Le., condemned).
Cylinder
as shown in Table 5003. Any cylinder that fails the hydrostatic
Table 5003
Inspection Frequency
HYDROSTATIC TESTING
PERIOD
(NOTE 1)
years
CYLINDER
TYPE
ITEM No.
CYLINDER SERVICE LIFE
(NOTE 1 and NOTE 2)
years
Composite
570, IPL Figure 1G
15
3
Unlimited Lifetime
(Note 3)
5
Steel
500 thru 555A,
IPL Rgures 1A thru 1F,
1H and 1J
Note 1:
560,565,
24
IPL Figure 1E
(Note 4)
•
3
Specific information contained in these columns is taken directly from documents listed in Table
5001.
Note 2:
Note 3:
Note 4:
EFFECTIVITY:
ALL
Cylinder service-life begins at the initial hydrostatic test date of the cylinder.
Unlimited Iiretime on condition that the cylinder does not fail any remaining inspection or
hydrostatic test requirements.
24 years or 4.380 pressurization (that which occurs first).
35-32-18
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
5. Cylinder Assembly (Continued)
Subtask 35-32-18-210-001
A. Composite Cylinder (570, IPL Figure 1G)
(1) Look at the date of the last hydrostatic test of the cylinder. Hydrostatic test dates will be shown on
the cylinder neck or on a hydrostatic retest label. The cylinder may have more than one hydrostatic
retest label. The initial cylinder test date and US DOT exemption certificate number are shown on
the manufacturer's identification plate found on the cylinder sidewall.
(2) Hydrostatic tests must be performed as noted in Table 5003 using approved procedures by service
locations having up-to-date United States Department of Transportation approval. Additional
hydrostatic tests may be required in your country.
(3) The composite cylinder service-life is given in Table 5003.
(4) Do a check of the exterior of cylinders for twists or bends, cuts in the fiber over-wrap, either heat or
fire damage, contamination, or other damage.
(5) Make sure that identification plates and warning labels can be read and are not damaged.
(6) Do a check of the cylinder neck for cracks and distortion. Also check the cylinder threads for
damage and contamination.
NOTE: Make sure that the sealing surface between the regulator assembly and the cylinder does
not have nicks. cuts, or distortion. Leakage will occur between the regulator assembly and
cylinder if this surface is distorted or damaged.
•
(7) Put a Bright Inspection Light (Table 5002) inside the cylinder and do a check for contamination and
corroded surfaces.
(8) Make sure the inside of the cylinder does not have an odor.
Subtask 35-32-18-210-002
B. DOT-3HT-1850 Steel Cylinder {560, 565, IPL Figure 1E)
(1) Look at the last and initial cylinder hydrostatic test dates found on the cylinder crown, near the
cylinder neck.
Hydrostatic tests must be performed as noted in Table 5003 using approved procedures by service
locations having up-ta-date United States Department of Transportation approval. Additional
hydrostatic tests may be required in your country.
(2) DOT-3HT-1850 steel cylinder service-life is as noted in Table 5003.
(3) Do a check of the cylinder surfaces for either heat or fire damage.
(4) Do a check of the cylinder for dents. gouges, digs, or bulges.
NOTE: It may be necessary to remove any heavy paint coatings from the exterior surface ofthe
cylinder to correctly check for dents, gouges, digs, or bulges.
(5) Make sure that identification plates and warning labels can be read and are not damaged.
(6) Do a check of the cylinder neck for cracks, distortion, contamination, or thread damage.
(7) Put a Bright Inspection Light (Table 5002) inside the cylinder and do a check for contamination arid
corroded surfaces.
(8) Make sure the inside of the cylinder does not have an odor .
•
EFFECTIVITY:
ALL
35-32-18
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
oJ
•
...
CMAt & IPL
5. Cylinder Assembly (Continued)
•
Subtask 35-32-18-210-003
C. DOT-3AA-1800 Steel Cylinder (500 thru 555A, IPL Figures 1A thru 1F, 1Hand 1J, as applicable).
(1) Look at the last and initial cylinder hydrostatic test dates found on the cylinder crown, near the
cylinder neck.
Hydrostatic tests must be performed as noted in Table 5003 using approved procedures by service
locations having up-to-date United States Department of Transportation approval. Additional
hydrostatic tests may be required in your country.
(2) DOT-3AA-1800 steel cylinder service-life is given in Table 5003.
(3) Do a check of the cylinder surfaces for either heat or fire damage.
(4) Do a check of the cylinder for dents, gouges, digs, or bulges.
NOTE: It may be necessary to remove any heavy paint coatings from the exterior surface of the
cylinder to correctly check for dents, gouges, digs, or bulges.
(5) Make sure that identification plates and warning labels can be read and are not damaged.
(6) Do a check of the cylinder neck for cracks, distortion, contamination, or thread damage.
(7) Put a Bright Inspection Light (Table 5002) inside the cylinder and do a check for contamination and
corroded surfaces.
(8) Make sure the inside of the cylinder does not have an odor.
TASK 35-\32-18-210-804
6. Optional PCA Mounting Bracket Set
Refer to Paragraph 8 in the DESCRIPTION AND OPERATION section of this manual for information about
optional peA mounting bracket sets.
•
A. Do a check of the upper and lower bracket assembly surfaces for signs of damage, contamination,
burrs, corrosion. or too much wear.
B. Do a check of the upper bracket assembly for loose or broken latch or latch mounting pins. Do a check
of the latch and ensure it moves freely.
EFFECTIVITY:
ALL
35-32-18
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY • CMM & IPL
REPAIR
TASK 35-32-18-300-801
1. General
This section gives the repair procedures that can be perfonned on the 5500 and 5600 Series PCA. Before
repair, components must be examined using procedures in the CHECK section of this manual.
Do not repair filters, safety discs, gaskets, preformed packings, diaphragm cords. safety plug washers, seat
washers, quad rings, seats, drive screws, metal boss seals, or rivets. These items must be replaced each
time they are removed during disassembly.
Self-locking screws (120, IPL Figures 1Hand 1J; 360, IPL Figure 9) and fillister head screws (80, IPL
Figure 7) contain a one-time use (non-replaceable) plastic insert. These items must be replaced each time
they are removed during disassembly.
NOTE:
Unless otherwise noted, any use of an item number in this section includes all alpha variants and
dashed variants (i.e., items not shown) of that number. For example, item (500) includes 500,
-500, -SODAthru -5000, unless otherwise noted.
TASK 35-32-18-99E-804
2. Reference Documents
A list of applicable reference documents is given in Table 6001.
Table 6001
Reference Documents
•
DOCUMENT NUMBER
DOCUMENT NAME
ORDERING INFORMATION
DOD-P-16232
Phosphate Coatings, Heavy. Manganese or Zinc
Base, (For Ferrous Metals)
US Government Printing Office
Washington DC 20402
USA
TI-C-490
Cleaning Methods and Pretreatment of Ferrous
Surfaces for Organic Coatings
US Government Printing Office
Washington DC 20402
USA
FED STD-595
Colors Used in Govemment Procurement
US Government Printing Office
Washington DC 20402
USA
TASK 35-32-18-94B-805
3. Special Tools. Fixtures. and Equipment
A list of special tools, fixtures, and equipment necessary for repair is shown in Table 6002. Special tools,
fixtures, and equipment must be cleaned for oxygen service before use. Unless noted otherwise, one of
each item is required. Equivalents may be substituted.
Table 6002
Special Tools, Fixtures, and Equipment
•
NOMENCLATURE
PART NUMBER
(or DESCRIPTION)
MANUFACTURER
(VENDOR CODE)
Bright Inspection Light
IL-24
Titan Tool Supply Co. Inc.
Buffalo, NY 14216-1784
USA (V51679)
EFFECTIVITY:
ALL
35-32-18
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & JPL
3. Special Tools, Fixtures. and Equipment
(Continued)
,
-'
..
•
Table 6002 (Continued)
Special Tools, Fixtures, and Equipment
NOMENCLATURE
PART NUMBER
(or DESCRIPTION)
MANUFACTURER
(VENDOR CODE)
Spray Gun
Model 19
Binks Manufacturing Company
AMF Ohare, IL 60666-2887
USA (V07334)
Cylinder Hanger (Steel Cylinders)
0.500 in. -14 ANPT Threads
1.00 In. - 11.5 ANPT Threads
Cylinder Hanger (Composite Cylinders)
0.750 -16UNF-2A Threads
Local Vendor
SK87-117-Q8
Bolero Industries Inc.
Santa Fe Springs, CA 90670
USA (VOTRZ6)
TASK 35-32-18-94A-803
4. Consumable
Repair Materials
A list of applicable
substituted.
consumable
repair materials is given in Table 6003. Equivalent
materials may be
Table 6003
Consumable Repair Materials
DESCRIPTION
Abrasive Blasting Media
No. 16 Aluminum Oxide
PIN 1700164
Treibacher - Schleifmittel Co.
Niagara Falls, NY 14303 (USA)
Fax: 716-286-1224
Plastic Abrasive Pad
Scotch Brite Pad
No. 2 Size
PIN 10116NA
3M Abrasive Systems Division
St. Paul, MN 55144-1000
USA (V28124)
Hydrochloric Acid
Hydrochloric Acid
(HCI)
Mallinckrodl Baker Inc.
Phillipsburg, NJ 08865-2219
USA (V70829)
pH Test Paper Strips
4391-01
Mallinckrodt Baker Inc.
Phillipsburg, NJ 08865-2219
USA (V70829)
Chromic Acid
Chromium (VI) Trioxide
(CrOa)
Mallinckrodt Baker Inc.
Phillipsburg, NJ 08865-2219
USA (V70829)
Phosphoric Acid
Phosphoric Acid
(H3P04)
Mallinckrodt Baker Inc.
Phillipsburg, NJ 08865-2219
USA (V70829)
Catalyst
A3110
SPN 50761-03
A.P. Nonweiler Co.
Oshkosh, WI 54903-1007 USA
Fax: 920-231-8085
EFFECTIVITY:
ALL
•
MANUFACTURER
(VENDOR CODES)
MATERIAL
35-32-18
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550015600SERIES PORTABLE CYLINDER ASSEMBLY·
4. Consumable
Repair Materials
CMM & IPL
(Continued)
Table 6003 (Continued)
Consumable
Repair Materials
MATERiAl
DESCRIPTION
Primer (2 part catalyzed urethane)
Light Gray (No. 36628 per FED-STD-595)
4285A093
Paint (2 part catalyzed urethane)
Green (No. 24062 per FEO·STD-595)
Green (No. 14187 per FED-STD-595)
Gray-Green (No. 24159 per FED-STO-595)
Blue (No. 15102 per FED-5TD-595)
Yellow (No. 13538 per FED-STD-595)
White (No. 17875 per FED-STO-595)
4285A073
4285K123
4285A083
4624J010
4624J030
4624J020
Phosphate Coating Solution
MANUFACTURER
(VENDOR CODES)
A.P. Nonweiler Co.
Oshkosh, WI 54903-1007 USA
Fax: 920-231-8085
A.P. Nonweiler Co.
Oshkosh, WI 54903-1007 USA
Fax: 920-231-8085
Oakite Products Inc.
Berkeley Heights, NJ 07922-2712
USA (V44389)
CrysCoal*-OC
(Zn(H2P04)2 . 2H20)
* CrysCoat is a Registered Trademark of Oakile Products Inc.
TASK 35-32-18-300-802
•
5. Repair
limit
repairs to the procedures
• Cleaning
(refer to the CLEANING
Removal
Thread
given below.
section).
of sharp edges.
repair.
Replacement
of cracked.
bent, broken, scratched,
Steel cylinder
phosphate
coating (refer to paragraph
Steel cylinder
paint application
Composite
cylinder
Repair of optional
(refer to paragraph
paint application
PCA mounting
or otherwise
damaged
components.
6 in this section).
7 in this section).
(refer to paragraph
bracket assemblies
8 in this section).
(refer to paragraph
9 in this section).
TASK 35-32-18-330-801
6. Steel Cylinder Phosphate
Coating
Refer to Reference Document DOD-P-16232
(Table 6001) for additional
phosphate coating (Type "Zinc" Class "3") procedures.
WARNING:
•
information
FAILURE TO REFER TO AND FOLLOW THE MANUFACTURER'S OR SUPPLIER'S
MATERIAL SAFETY DATA SHEETS (MSDS) FOR HYDROCHLORIC ACID, CHROMIC
ACID, PHOSPHORIC ACID OR PHOSPHATE COATING SOLUTION FOR MORE
PRECAUTIONARY DATA, APPROVED SAFETY EQUIPMENT AND EMERGENCY
MEDICAL AID MAY RESULT IN SERIOUS PERSONAL INJURY OR DEATH.
Steel cylinders (500 thru 565, IPL Figures 1A thru 1F. 1Hand 1J, as applicable)
exterior protective treatment may be phosphate coated as follows .
EFFECTIVITY:
on steel cylinder
ALL
that require interior and
35-32-18
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
6. Steel Cylinder Phosphate Coating (Continued)
•
Subtask 35-32-18-380-001
A. Surface Preparation
Abrasive blasting with Abrasive Blasting Media (Table 6003) is preferred for interior and exterior
preparation of the cylinder before phosphate coating application. All paint must be removed from the
cylinder external surface during the abrasive blasting process.
(1) Abrasive blast the cylinder interior and exterior with Abrasive Blasting Media, to remove corrosion
and paint. Refer to Reference Document TT -C-490 (Table 6001) for approved method for interior
and exterior abrasive blasting of steel cylinders.
(2) Rinse the interior and exterior of the cylinder for at least one minute with clean water.
(3)
Dry the cylinder with clean, dry air that is oil-free and heated (180 - 200°F, 82 - 93°C).
(4) Put a Bright Inspection Llght (Table 6002) inside the cylinder and inspect for contamination and
corrosion.
(5) If corrosion remains on the interior or exterior surfaces of the cylinder, the cylinder may be treated
with hydrochloric acid solution as follows.
(a) Prepare a 20 percent (by volume) hydrochloric acid solution by mixing 5 gal (20 liters) of
Hydrochloric Acid (Table 6003) in approximately 20 gal (75 liters) of clean water.
(b) Place the cylinder in the 20 percent hydrochloric acid solution for one minute.
(c) Rinse the cylinder for at least one minute with clean water.
(d) Repeat paragraph 6A(3)
•
and 6.A.(4).
Subtask 35-32-18-330-001
B. Phosphate Coating
(1) Prepare a 2 to 3 percent (by volume) phosphate coating solution by mixing approximately 3 gallons
(12 liters) of Phosphate Coating Solution (Table 6003) in 125 gallons (475 liters) of clean water.
(2) Place the cylinder in a tank containing a heated (180 - 210°F, 82· 99°C) 2 to 3 percent
phosphate coating solution for a minimum of 30 minutes. The solution must be circulating at a rate
of 5 - 20 gallons (19 - 76 liters) per minute.
(3) Spray-rinse cylinder interior and exterior with cold, clean water for at least one minute.
NOTE: Cylinders may be placed in a suitable tank, rather than sprayed, if a continuous flow of cold,
clean rinse water is maintained. The cylinder should remain in the rinse water only for the
period of time necessary to remove any residual phosphate coating solution.
(4) Prepare a 0.06 percent (by volume) chromic acid rinse solution by mixing 8 oz. (240 ml) of
Chromic Acid (Table 6003) in 100 gallons (380 liters) of clean water.
(5) Place the cylinder in the heated (160 - 180°F, 71 - 82°C) chromic acid rinse solution for at least 1
minute.
(6) The hydrogen ion concentration (pH) of the chromic acid rinse solution must be maintained between
2 to 4 by the addition of a mixture of equal amounts of Chromic and Phosphoric Acids (Table
6003). Test the chromic acid rinse solution using pH Test Paper Strips (Table 6003). The chromic
acid rinse solution must be discarded after 24 hours, regardless of the number of cylinders
processed in the solution.
EFFECTIVITY: All
35-32-18
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
6. Steel Cylinder Phosphate Coating (Continued)
B. Phosphate Coating (Continued)
(7)
Dry the cylinder using clean, dry air that is oil-free and heated (180 - 200"F, 82 - 93"C).
NOTE: To produce a uniform phosphate coating thickness of 0.0004 ±0.0002 in.
(0.0102 ±0.0050 mm) on the cylinder surface a minimum weight of 1000 mg per sq. ft
(1.076 mg per sq. em) of phosphate coating must be applied.
(8) Place a Bright Inspection Light (Table 6002) inside the cylinder and inspect for a uniform phosphate
coating. A uniform phosphate coating is gray to black in color and free of loose particles.
TASK 35-32-18-380-801
7. Steel Cylinder Paint Application
Paint must only be applied to the exterior surface of the steel cylinder (500 thru 565, IPL Figures 1A thru
1F, 1Hand 1J, as applicable) and may consist of either small spot repairs or full repainting.
Hydrostatic test marks must remain visible and readable after the paint application.
WARNING:
FAILURE TO REFER TO AND FOLLOW THE MANUFACTURER'S OR SUPPLIER'S
MATERIAL SAFETY DATA SHEETS (MSDS) FOR PRIMER, PAINT, OR CATALYSTS
FOR MORE PRECAUTIONARY DATA, APPROVED SAFETY EQUIPMENT AND
EMERGENCY MEDICAL AID MAY CAUSE SERIOUS PERSONAL INJURY OR DEATH.
Subtask 35-32-18-350-001
•
A. Surface Preparation
(1) Steel cylinders (500 thru 565, IPL Figures 1A thru 1F, 1Hand 1J, as applicable) requiring a
complete repainting process should be phosphate coated before paint application. Refer to
paragraph 6 in this section to phosphate coat a steel cylinder.
(2) Steel cylinders requiring a spot repainting process should be lightly sanded around the spot repair
areas.
(3) Refer to paragraph 6.A in the CLEANING section and clean the exterior surface of the cylinder to
remove any contamination.
(4) Remove the instruction decals (20, IPL Figures 1A thru 1F; 25, IPL Figures 1H and 1J; oxygen
decals 30, IPL Figures 1A thru 1F; 1H, 1J), labels (35, IPL Figures 1A thru 'IF), placards (-40, -50,
IPL Figures 1A, 1C, 1E, 1H, and 1J) and gauge label (45, IPL Figures 1A, 1C, 1E, 1H, and 1J), or
install masking tape over these items to protect them from the primer and paint over spray_
Subtask 35-32-18-380-002
B. Primer Application
(1) Thread the Cylinder Hanger (Table 6002) into the cylinder.
(2) Mix the Light Gray Primer (Table 6003) and Catalyst (Table 6003) using the instructions supplied by
the manufacturer.
(3) Filter and spray the catalyzed primer on the cylinder surface with a Spray Gun using the instructions
supplied by the manufacturer.
(4) Allow the cylinder to air dry 15 to 20 minutes before the application of the paint.
Subtask 35-32-18-380-003
C. Paint Application
•
(1) Thread the Cylinder Hanger (Table 6002) into the cylinder .
EFFECTIVITY:
ALL
35-32-18
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
7. Steel Cylinder Paint Application
C. Paint Application
•
CMM & IPL
(Continued)
(Continued)
(2) Mix the Paint (Table 6003) and Catalyst (Table 6003) using the instructions supplied by the
manufacturer.
(3) Filter and spray the catalyzed paint onto the cylinder surface with a Spray Gun using instructions
supplied by the manufacturer.
(4) Air-dry cylinder for 60 to 90 minutes at approximately 70°F (21°C) or 25 ~ 30 minutes
at 100 - 150°F (38 - 66°C).
(5) Allow the paint to cool and stabilize for 24 hours before placing the cylinder into service.
(6) Instruction Decals (20, IPL Figures 1A thru 1F; 25, IPL Figures 1Hand 1J; Oxygen decals (30, IPL
Figures 1A thru 1F, 1H and 1J), labels (35, IPL Figures 1A thru 1F; and placards (-40. ~50,IPL
Figures 1A, 1C, 1E, 1H. and 1J), and gauge label (45, IPL Figures 1A. 1C, 1E, 1H, and 1J) removed
from cylinder before the paint application process must be replaced. Refer to the ASSEMBLY
section for the proper location and application of these items.
TASK 35-32-18-380-802
8. Composite Cylinder Paint Application
Paint must be applied only to the exterior surface of the composite cylinder (570. IPL Figure 1G) and may
consist of either small spot repairs or full repainting.
The hydrostatic retest labels and permanently affixed cylinder manufacturer's identification label must
remain visible and readable after the paint application.
Subtask 35-32~18~35~002
A. Surface Preparation
CAUTION:
THE COMPOSITE CYLINDER OVER-WRAP OR REINFORCING FIBERS, MUST NOT BE
ABRADED DURING THE PRE·PAINTING PREPARATION OR PERMANENT CYLINDER
DAMAGE MAY RESULT.
•
(1) Composite cylinders (570, IPL Figure 1G) that require spot repair or full repainting should be lightly
sanded with a Plastic Abrasive Pad (Table 6003) only enough to roughen the surface without
abrading through the existing paint layer.
(2) Refer to paragraph 6.A in the CLEAN ING section and clean the exterior surface of the cylinder to
remove contamination.
(3) Remove the identification plate (80, IPL Figure 1G), instruction decal (20. IPl Figure 1G), oxygen
decal (30. IPL Figure 1G). (label 35, IPL Figure 1G), and warning decal (65, IPL Figure 1G) from the
cylinder, or install masking tape over them to protect from paint over spray. Do not remove any
hydrostatic retest labels from the cylinder. The hydrostatic retest labels and the cylinder
manufacturers identification label on composite cylinders must be covered with masking tape before
painting.
Subtask 35~32~18-380~004
B. Paint Application
(1) Thread the Cylinder Hanger (0.750 - 16 UNF~2A Threads, Table 6002) into the cylinder.
(2) Mix the Green Paint (No. 14187, Table 6003) and Catalyst (Table 6003) using the instructions
supplied by the manufacturer.
(3) Filter and spray the catalyzed paint on the cylinder surface with a Spray Gun (Table 6002) using the
instructions supplied by the manufacturer.
EFFECTIVITY:
ALL
35-32-18
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
8. Composite Cylinder Paint Application
B. Paint Application
CMM & IPL
(Continued)
(Continued)
(4) Dry the cylinder for 60 to 90 minutes at approximately 70°F (21°C) or 25 to 30 minutes
at 100 - 125°F (38 - 52°C) in air.
(5) Allow the paint to cool and stabilize for 24 hours before placing the cylinder into service.
(6) The identification plate (80, IPL Figure 1G), instruction decal (20, IPL Figure 1G), oxygen decal (30,
IPL Figure 1G), (label 35, IPL Figure 1G), and warning decal (65, IPL Figure 1G) that were removed
from the cylinder before the paint application process must be replaced. Refer to the ASSEMBLY
section for the proper location and application of these items.
TASK 35-32-18-300-803
9. Optional PCA Mounting Bracket Set
Refer to paragraph 8 in the DESCRIPTION AND OPERATION section of this manual for information about
the optional PCA mounting bracket sets.
Cracked, broken, bent or excessively worn bracket assemblies must be replaced. Repairs to bracket
assembljes should be limited to:
•
If binding, apply a small amount of Oxygen Compatible Lubricant to latch (part of upper bracket
assembly) hinge pin area.
- If loose, apply adhesive on rubber cushion (part of lower bracket assembly) .
•
•
EFFECTIVITY:
ALL
35-32-18
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
l"
ASSEMBLY
TASK 35-32-18-400-801
1. General
This section describes the equipment and procedures necessary for assembly of the 5500 and 5600 Series
Portable Cylinder Assembly (PCA). All components of the PCA must be cleaned and checked in
accordance with the previous sections of this manual. Assembly is organized as follows.
Paragraph
6
7
8
9
10
11
WARNING:
IPL Figure No.
4,5,6,7,8,10,11,13
Description
Outlet Assemblies
Respirator Regulator Assembly
Regulator Assembly
PCA Assembly
PCA Charging Procedure
Final PCA Assembly
3
9, 12
1Athru 1J, 9
1A thru 1J. 9
1A thru 1J
DO NOT ALLOW OIL, GREASE, FLAMMABLE SOLVENTS, CONTAMINATED TOOLS OR
OTHER COMBUSTIBLE MATERIALS TO COME IN CONTACT WITH PARTS THAT WILL
BE EXPOSED TO PRESSURIZED OXYGEN OR FIRE OR EXPLOSION MAY OCCUR
CAUSING SERIOUS PERSONAL INJURY OR DEATH.
FAILURE TO USE SUITABLE EYE PROTECTION DURING ASSEMBLY PROCEDURES
MAY CAUSE INJURY TO THE EYES.
•
The instructions in this section apply to all 5500 and 5600 PCA's unless noted otherwise. Refer to the
ILLUSTRATED
PARTS LIST section of this manual for the item numbers given in parentheses.
NOTE:
Unless otherwise noted, any use of an item number in this section includes all alpha variants and
dashed variants (Le., items not shown) of that number. For example, item (500) includes 500,
-500, -500A thru -5000, unless otherwise noted.
TASK 35-32-18-99E-805
2. Reference
Documents
A list of applicable
reference
documents
is given in Table 7001.
Table 7001
Reference Documents
•
DOCUMENT NUMBER
DOCUMENT NAME
ORDERING INFORMATION
A-A-58092
Commercial Item Description Tape Antiseize,
Polytetrafluoroethylene
General services Administration
1600 F Street
Washington, DC 20405 USA
NASM33540
National Aeronautical Standard
Safety Wiring and Cotter Pinning. General Practices for
Aerospace Industries Association
of America
Washington, DC 20005
USA (V80205)
MIL-PRF-25567
Military Specification
Leak Detection Compound, Oxygen Systems
Standardization Documents Order Desk
Building 4D, 700 Robbins Avenue
Philadelphia, PA
19111-5094 USA
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550015600 SERIES PORTABLE CYlINDER ASSEMBL.Y • ClAM & IPL
2. Reference Documents (Continued)
..
•
Table 7001 (Continued)
Reference Documents
DOCUMENT NUMBER
DOCUMENT NAME
ORDERING INFORMATION
MIL-PRF-27210
Military Specification
Oxygen, Aviators Breathing, liquid and Gas
Standardization Documents Order Desk
Building 4D, 700 Robbins Avenue
Philadelphia, PA
19111-5094 USA
P2.5
TransfilJing of High Pressure Gaseous Oxygen To Be
Used For Respiration
Compressed Gas Association Inc.
Arlington, VA 22202-4102
USA (V0170 1)
AIR1059
Transfilling and Maintenance of Oxygen Cylinders
SAE International
Warrendale, PA 15096-0001
USA
TASK 35-32-18-94B-806
3. Special Tools, Fixtures, and Equipment
A list of special tools, fixtures, and equipment required for assembly of the 5500 and 5600 Series PCA's is
shown in Table 7002. Special tools, fixtures, and equipment must be cleaned for oxygen service before
use. The Figure number information provided in the "NOMENCLATURE" column corresponds to the tool
listed in Table 9001 of the SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES
section. Unless noted otherwise, one of each item is required. Equivalents may be substituted.
Table 7002
Special Tools, Fixtures, and Equipment
PART NUMBER
(or DESCRIPTION)
MANUFACTURER
(VENDOR CODE)
Pneumatic Bench Vise
Model BV-101-P
PIN 58634
Getz Fire Equipment Co.
Peoria, IL 61602-1711
USA (V58013)
Core Wrench
(Figure 9001)
800216-T91-1
Scott Aviation
Lancaster, NY 14086-9502
USA (V53655)
Test Regulator
0-2500 psig (0 -17.2 MPa) Outlet Pressure
44-1110 Series
44-1114-24
Tescom Corp.
Elk River, MN 55330-2445
USA (V5H642)
Pressure Gauge
(minimum accuracy ±O.25% full scale)
o - 2000 psig (0 - 13.8 MPa)
1404 Series
Ametek Inc. (US Gauge Division)
Sellersville, PA 18960-2625
USA (V61349)
Refill Coupling
CGA 540 x 0.563-18UNF·2B Threads
5020-01
Scott Aviation
Lancaster, NY 14086-9502
USA (V53655)
NOMENCLATURE
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TASK
CMM & IPL
35-32-18-94A-804
4. Consumable
Assembly
Materials
A list of consumable
assembly materials, required for assembly of the 5500 and 5600 Series PCA, is given
in Table 7003. Equivalent
materials may be substituted
except for the Oxygen and Oxygen Compatible
Lubricant.
Consumable
•
Table 7003
Assembly
Materials
MANUFACTURER
NENDOR CODE)
MATERIAL
DESCRIPTION
Thread Sealing Tape
0.250 in. (0.535 em) wide
PTFE Ribbon Tape
CID A-A-58092, size 1
SPN 50011-00
Local Vendor
Leak Test Solution
Sherlock Leak Detector
MIL-PRF-25567, Type 1
Winton Products Co. Inc.
Charlotte, NC 28236
USA (V23316)
Sealant
Clear
PIN RTV732
SPN S0067 -00
Dow Corning Corp.
Midland, MI48686-0097
USA (V71984)
Red Etching Ink
PIN 5-1141
SPN 50792-01
Marking Device Manufacturing Co.
Philadelphia, PA 19133-2891
USA (V26040)
Green Etching Ink
PIN AX GREEN
SPN 50791-01
Speciality Ink Co. Inc.
Deer Park, NY 11729-4702
USA (V18029)
Lockwire
MS20995C20
SPN 13603-00
Local Vendor
(V96906)
Oxygen
1850 psig (12.76 MPa) minimum
pressure
MIL-PRF-27210, Type I
Local Vendor
Primer
GradeT
SPN 50349-01
Loctite Corp.
Rocky Hill, CT 06067-3582
USA (V05972)
Adhesive
Grade 222 SPN 50004-15
Grade 271 SPN 50004-18
Loctite Corp.
Rocky Hill, CT 06067-3582
USA (V05972)
Oxygen Compatible Lubricant
Krytox· 240 AC
SPN 50527-00
E.I. du Pont de Nemours & Co. Inc.
Wilmington, DE 19898
USA (V23037)
Powdered Lubricant
MolyCoat·· Z
SPN 50021-01
Dow Cornill9 Corp.
Midland, MI 48686-0997
USA (V71984)
• Krytox is a Registered Trademark of E.I. du Pont de Nemours & Co. Inc.
•• MolyCoat is a Registered Trademark of Dow Corning Corp .
•
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
TASK 35-32-18-400-802
5. Pre-Assembly Information
WARNING:
FAILURE TO USE TOOLS THAT ARE FREE FROM DUST, LINT, FINE METAL FILINGS,
OIL, GREASE, FLAMMABLE SOLVENTS OR OTHER COMBUSTIBLE MATERIALS ON
PARTS THAT ARE EXPOSED TO PRESSURIZED OXYGEN MAY RESULT IN FIRE OR
EXPLOSION CAUSING SERIOUS PERSONAL INJURY OR DEATH.
• All components that are to be used in the assembly of the 5500 and 5600 Series PCA must be
cleaned and checked in accordance with the preceding sections of this manual. All components must
pass the required tests in the TESTING AND FAULT ISOLATION section.
- Refer to Table 7002 (Special Tools. Fixtures. and EqUipment) and Table 7003 (Consumable Assembly
Material) as required.
- Unless noted otherwise, all preformed packings shall be lubricated with a thin film of Oxygen
Compatible Lubricant prior to installation.
- Unless noted otherwise, all parts which require threading. twisting, or turning operations for assembly
will be threaded, twisted, or turned in a clockwise direction.
- When indicated, apply Thread Sealing Tape (Table 7003) according to Commercial Item Description
Specification A-A-58092 (Table 7001).
- When indicated, apply Lockwire (Table 7003) according to National Aeronautical Standard
NASM33540 (Table 7001).
- When indicated, apply Primer (Table 7003) and Adhesive (Table 7003) in small amounts and wipe off
excess with a clean cloth.
- A "text arrow", when used, shows the correct alignment of labels, decals, and placards put on the 5500
and 5600 Series PCA.
•
TASK 35-32-18-430~801
6. Outlet Assemblies
(300 thru 370. IPL Figures 1A thru 1J).
A. Constant Flow (metered) Type Outlet Assemblies
Refer -1 thru -2P, IPL Figure 4; -1 thru -3F, IPL Figure 5; -1 thru -2E, IPL Figure 7; -1, IPL Figure 8.
Reter to paragraph 7.E.(2) in the DESCRIPTION AND OPERATION section to determine if a constant
flow (metered) outlet assembly is an "adjustable" type (-1, IPL Figures 4, 5, 7 and 8) or "precision" type
(-2 thru -2P, IPL Figure 4; -2 thru -3F, IPL Figure 5; -2 thru -2E, IPL Figure 7).
After assembly, refer to paragraph 6 in the TESTING AND FAULT ISOLATION section and test all
constant flow outlet assemblies. Make sure that all constant flow assemblies pass all testing
requirements before use.
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
6. Outlet Assemblies
CMM & IPL
(Continued)
A. Constant Flow (metered) Type Outlet Assemblies (Continued)
Subtask 35-32-18-440-001
(1) 5009-00 (-1, IPL Figure 5) and 5009 Series (-2 thru -3F, IPL Figure 5) outlet assemblies.
Refer to IPL Figure 5 unless noted otherwise.
G) 5009-00 adjustable type outlet assembly (-1).
NOTE: The outlet assembly (-1) is not procurable. Replacement parts are not procurable for the
outlet assembly (-50), flow port (120), screen (30), filter (150), ring (140). gasket (160),
glass cord (40), or screw (20). If a replacement part is required, a complete precision
type outlet assembly must be ordered. Do not re-assemble the outlet assembly. Refer to
IPL Table 1 Sheet 5 (PCA Configuration Matrix) for information on how to order a
replacement outlet assembly.
(k) 5009 Series precision type outlet assemblies (-2 thru -3F).
NOTE: The orifice (180), stud (80), and outlet assembly (-60) are not procurable. If a
replacement part is required, a complete outlet assembly must be ordered. Refer to IPL
Table 1 Sheet 5 (PCA Configuration Matrix) for information on how to order a
replacement outlet assembly.
1 Install
•
the gasket (90), valve (100), and spring (110) in the receptacle (170).
~
Apply a thin coat of the Oxygen Compatible Lubricant to the threads of the stud (70, 80).
~
Install and tighten the receptacle (170) on the stud (70,80). Install the dust cover (10) on
the receptacle.
Subtask 35-32-18-440-002
(2) 5041-00 (-1, IPL Figure 4) and 5041 Series (-2 thru -2P, IPL Figure 4) outlet assemblies.
Refer to IPL Figure 4 unless noted otherwise.
(a) 5041-00 adjustable type outlet assembly (-1).
NOTE: The outlet assembly (-1) is not procurable. Replacement parts are not available for the
coupling assembly (-90), screen (60, 80), glass cord (70), screw (50), and body (120). If
a replacement part is required, a complete precision type outlet assembly must be
ordered. Do not re-assemble the outlet assembly. Refer to IPL Table 1 Sheet 5 (PCA
Configuration MatriX) for information on how to order a replacement outlet assembly.
(b) 5041 Series precision type outlet assemblies (-2 thru -2P).
NOTE: The orifice (200), body (130), and outlet subassembly (-100) are not procurable. If a
replacement part is required, a complete outlet assembly must be ordered. Refer to IPL
Table 1 Sheet 5 (PCA Configuration Matrix) for information on how to order a
replacement outlet assembly.
1
Position pins (180) on case (190) and hook springs (170) over the grooved end of the pins.
~
Install the valve seat (160), valve (150), and spring (140) in the case (190).
~ Apply a thin coat of the Oxygen Compatible Lubricant to the threads of the body (120, 130).
Screw the case (190) onto the body (120, 130) hand tight then tighten one fourth to one
third of a tum more.
~
•
Install the washer (40) and cap (30) over the threads on the case (190).
§ Assemble the nut (20) and cover assembly (10). Thread the nut (20) onto the case (190) .
EFFECTIVITY:
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550015600SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
6. Outlet Assemblies (Continued)
A. Constant Flow (metered) Type Outlet Assemblies (Continued)
Subtask 35-32-18-440-003
(3) 5507-00 (-1, IPL Figure 7) and 5507 Series (-2 thru -2E, IPL Figure 7) outlet assemblies.
Refer to IPL Figure 7 unless noted otherwise.
(a) 5507-00 adjustable type outlet assembly (-1).
NOTE: The outlet assembly (-1) is not procurable. Replacement parts are not procurable for the
outlet subassembly (-40), screen (30), glass cord (20), screw (10), and body (140). If a
replacement part is required, a complete precision type outlet assembly must be
ordered. Do not re-assemble the outlet assembly. Refer to IPL Table 1 Sheet 5 (PCA
Configuration Matrix) for information on how to order a replacement outlet assembly.
(b) 5507 Series precision type outlet assemblies (-2 thru -2E).
NOTE: The orifice (160), and body (140,150) are not procurable. If a replacement part is
required, a complete outlet assembly must be ordered. Refer to Table 1 Sheet 5 (PCA
Configuration Matrix) for information on how to order a replacement outlet assembly.
1 Install
the spring (130), outlet poppet (120), outlet gasket (110), and outlet washer (100) in
the body (140, 150).
£
Install the washer (90) on the threaded adapter (50).
;l Screw the threaded adapter (50) into the body (140, 150).
1:
Install the fillister head screw (80) through the dust cover (70) and torsion spring (60) into
the body (140, 150).
Subtask 35-32-18-440-004
•
(4) 5052-00 outlet assembly (-1, IPL Figure 8)
Refer to IPL Figure 8 unless noted otherwise.
NOTE: A replacement outlet assembly (-1) or parts (10 thru 120) are not procurable. If a complete
assembly or a replacement part is required, a different precision type outlet assembly must
be ordered. Refer to Table 1 Sheet 5 (PCA Configuration Matrix) for information on how to
order a replacement outlet assembly.
(a) Install the washer (40). screen (30), glass cord (20), and screen (30) into the base (60). Slowly
thread the orifice adjusting screw (10) into the base (60) only enough to retain the washer, glass
cord, and screens.
(b) Assemble the coupling (-50) as follows.
1 Install the spring
£ Apply a thin coat
(80) and retainer (110) into the body (120).
of Oxygen Compatible Lubricant to the valve seat gasket (100) and install
the valve seat gasket on the valve seat (90).
;l Thread the valve seat (90) into the body (120) and tighten.
1:
Apply a thin coat of Oxygen Compatible Lubricant to the body gasket (70) and install the
body gasket on the body (120).
Q Thread the base (60) on the body (120) and tighten.
EFFECTIVITY:
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55OD1S6ooSERIES PORTABLE CYUNDER ASSEMBLY·
CMM & IPL
6. Outlet Assemblies (Continued)
B. Full Flow (Non-metered) Type Outlet Assemblies (refer to IPl Figures 6,10,11,13;
and 355, IPl Figure 1C)
-4, IPl Figure 5;
After assembly, refer to paragraph 6 in the TESTING AND FAULT ISOLATION section and test all full
flow outlet assemblies. Make sure that all full flow assemblies pass all testing requirements before use.
Subtask 35-32-18-440-005
(1) SPN 36728-01 outlet assembly (-1, IPL Figure 13)
Replacement parts are not procurable for SPN 36728-01. If replacement parts are required, a
complete outlet assembly must be ordered.
Subtask 35-32-18-440-006
(2) SPN DPB153 outlet assembly
A replacement outlet assembly or replacement parts are not procurable for SPN DPB153.
Outlet SPN DPB153 is replaced by outlet SPN 36728-01 (-1, IPL Figure 13). If a replacement
SPN DPB 153 outlet is required, order a SPN 36728-01.
Subtask 35-32-18-440-007
(3) SPN 10008298 outlet assembly
Replacement parts are not procurable for SPN 10008298. If replacement parts are required, a
complete outlet assembly must be ordered.
•
Subtask 35-32-18-440-008
(4) SPN 800503-00 outlet assembly (-4, IPl Figure 5)
Refer to IPL Figure 5 unless noted otherwise.
A replacement outlet assembly is not procurable. If a replacement outlet assembly is required, a
different outlet assembly must be ordered.
(a) Apply a thin coat of Oxygen Compatible Lubricant to the gasket (160).
(b) Install the gasket (160) and the flow port (130) into the stud (70).
NOTE: Replacement parts for stud (70) and flow port (130) are not procurable. If replacement
parts are required, a different outlet assembly must be ordered.
(c) Apply a thin coat of Oxygen Compatible Lubricant to the gasket (90).
(d) Install the gasket (90), valve (100), and spring (110) in the receptacle (170).
(e) Install and tighten the receptacle (170) on the stud (70). Install the dust cover (10) on the
receptacle.
Subtask 35-32-18-440-009
(5) SPN 10006017 outlet assembly (355, IPL Figure 1C)
Replacement parts are not procurable for this outlet assembly. If replacement parts are required, a
complete outlet assembly must be ordered .
•
EFFECTIVITY:
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
6. Outlet Assemblies {Continued}
B, Full Flow (Non-metered) Type Outlet Assemblies (Continued)
Subtask 35-32-18-440-010
(6) SPN 10003566 oxygen coupling (-340.IPL Figures lA, lC, 'IE, 'IH)
A replacement oxygen coupling or replacement parts are not procurable. Oxygen coupling, SPN
10003566, is replaced by outlet SPN 802856-01 (-1. IPL Figure 11). If a replacement oxygen
coupling or replacement parts are required, a complete outlet assembly. SPN 802856-01, must be
ordered.
Subtask 35-32-18-440-011
(7) SPN 802856-01 outlet assembly (-1, IPL Figure 11)
Refer to IPL Figure 11 unless noted otherwise.
(a) If removed during disassembly, install the warning label (50) on the dust cover (40).
(b) Apply a thin coat of Oxygen Compatible Lubricant to the quad ring (90), gasket (60) and
preformed packings (110,120).
(c) Install the preformed packing (11 O) on the disconnect body (100).
(d) Install the quad ring (90), preformed packing (120), disconnect poppet (80), and poppet spring
(70) in the disconnect body (100).
(e) Press the groove pins (30) into the disconnect fitting (20) if removed during disassembly.
(f)
Install the gasket (60) on the mating thread of the disconnect fitting (20),
(g) Using the directions provided by the manufacturer. apply a thin coat of Adhesive (Grade 222,
Table 7003) on the first few exposed threads at the end of the disconnect fitting (20). Thread the
disconnect fitting into the disconnect body (100). Tighten the disconnect fitting and wipe excess
Adhesive (if present) from the disconnect fitting and disconnect body.
•
(h) Install the dust cover retainer (10) on the disconnect fitting (20) and dust cover (40). Twist and
lock the dust cover (40) on the groove pins (30) of the disconnect fitting (20).
Subtask 35-32-18-440-012
(8) SPN 802863-02 outlet assembly (-1. IPL Figure 10)
Refer to IPl Figure 10 unless noted otherwise.
(a) Apply the Thread Sealing Tape to the nipple (10). Thread the nipple into the outlet body (140).
Tighten the nipple wrench tight.
(b) Install the dust cover (30) onto the outlet body (140).
(c) Install the pins (70). preformed packing (110). and retainer (100) into the insert sleeve (80).
(d) Install the spring (130), poppet (120), and seal (90) into the outlet body (140).
(e) Apply a small amount of Adhesive (Grade 271, Table 7003) to the threads of the insert sleeve
(80). Thread the sleeve with pin assembly (-60) into the outlet body (140). Tighten the sleeve
with pin assembly.
(f)
Install the preformed packing (40) on the dust plug (50). Insert the dust plug assembly (-20) into
the sleeve with pin assembly (-60).
EFFECTIVITY: ALL
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & #PI.
6. Outlet Assemblies (Continued)
B. Full Flow (Non-metered) Type Outlet Assemblies (Continued)
Subtask 35-32-18-440-013
(9) SPN 8572-00 outlet assembly (-1, IPL Figure 6)
Refer to IPL Figure 6 unless noted otherwise.
(a) Install the inlet filter (80), spring (70), poppet (60), and gasket (50) into the adapter (90).
(b) Assemble the body with pin (10) by installing washer (-30) and grooved pin (-20) in body (-40).
(c) Carefully thread the body with pin (10) into the adapter (90). Tighten the body with pin wrench
tight.
TASK 35-32-18-430-802
7. Respirator Regulator (110, IPL Figure 1H; 115, IPL Figure 1J)
Refer to IPL Figure
3 unless noted otherwise.
Unless noted otherwise, assembly procedures apply to both the demand (-10, -20) and demand/pressuredemand (-30, -40) type respirator regulators.
After assembly, perform the Respirator Regulator Tests (paragraph 7) in the TESTING AND FAULT
ISOLATION section. Make sure that the respirator regulator passes all the tests before use.
Subtask 35-32-18-440-014
•
A. General Assembly
Assemble the following parts to the regulator case (350).
(1) Attach the bracket (125, IPL Figures 1H, 1J) to the case (350, IPL Figure 3) with self-locking screws
(120, IPL Figures 1H, 1J). Tighten the self-locking screws.
(2) Apply Thread Sealing Tape to the mating threads of the connector (100, IPL 'Figures 1H, 1J).
(3) Install the screen (340, IPL Figure 3) in the case (350). Thread the connector (100, IPL Figure 1H,
1J) into the case (350, IPL Figure 3) and tighten.
Subtask 35-32-18-440-015
B. Demand Valve (240) Assembly
(1) Install the valve seat gasket (280) on the demand valve assembly (240).
(2) Install and secure the demand valve assembly in the case (350) with pan head screws (250), flat
washers (270), and lock washers (260). Tighten the pan head screws .
•
EFFECTIVITY:
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
-
,
CMM & IPL
7. Respirator Regulator (Continued)
•
Subtask 35-32-18-790-009
C. Demand Valve Assembly (240) Leak Test
(1) Use a high pressure connector having 0.125 - 27 ANPT threads and connect a regulated source of
clean, dry air to the inlet of case (350).
(2) Apply 55 psig (0.38 MPa) pressure to the inlet of the case (350).
(3) Apply the Leak Test Solution around the demand valve assembly (240), valve seat gasket (280),
pan head screws (250), flat washers (270) and lock washers (260). There must be zero leakage. No
bubbles in the Leak Test Solution is an indication of zero leakage.
(4) Reduce the inlet pressure to 0 psig (0 MPa). Discharge the remaining pressure by pushing the
demand valve assembly downward.
(5) Remove case (350) from the regulated air source. Remove the connector from inlet of case.
(6) Dry all parts using clean, dry air.
(7) Remove the case (350) from the test setup.
Subtask 35-32-18-440-016
D. Deflector (220)
CAUTION: A DEMAND VALVE ASSEMBLY HELD IN THE OPEN POSITION BY CONTACT
BETWEEN THE DEFLECTOR AND DEMAND VALVE ASSEMBLY STEM MAY CAUSE
THE RESPIRATOR REGULATOR ASSEMBLY TO FAIL TO OPERATE PROPERLY.
(1) CarefUlly align the deflector (220) over the demand valve assembly (240) and attach the deflector to
the case (350) with pan head screws (230). Tighten the pan head screws.
(2) Make sure there is no contact between the deflector and the demand valve assembly. Carefully
bend the deflector if necessary.
•
Subtask 35-32-18-440-017
E. Diaphragm (200)
(1) Carefully install the diaphragm assembly (200) on the case (350) so that the diaphragm extends to
the lower edge of the grooved surface of the case. Make sure that the diaphragm is seated evenly
and not distorted (wrinkled).
.
(2) Secure diaphragm on case with a diaphragm clamp (210) as follows.
NOTE: Diaphragm cord (205) is no longer procurable. If the diaphragm cord was removed. it must
be replaced with a diaphragm clamp (210).
(a) Diaphragm clamp (210).
Put the wide edge of the beveled surface of the diaphragm clamp (210) toward the diaphragm
assembly (200). Carefully push the diaphragm clamp (210) over the diaphragm assembly (200)
until the clamp is seated in the grooved area of the case (350).
EFFECTIVITY: All
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SSOOIMOOSERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
7. Respirator Regulator (Continued)
Subtask 35-32-18-440-018
F. Cover Assembly (-50, -60).
Refer to Figure 7001, Figure 7002 and Figure 7003.
(1) Demand type cover assembly (-50).
(a) If necessary, put the respirator regulator SIN and DASH No. on the new identification plate (90)
with a metal stamp having 0.064 in. (1.63 mm) high characters.
(b) Align and install the identification plates (90,110) on the case cover (180) using the rivets
(100,130).
(2) Demand/Pressure-Demand
type cover assembly (-60).
(a) If necessary, put the respirator regulator SIN and DASH No. on the new identification plate (80)
with a permanent black ink marker using 0.064 in. (1.63 mm) high characters.
(b) Align and install the identification plate (80) on the case cover (190).
(c) Align and install the identification plate (120) on the case cover (190) using the rivets (130).
(d) Position the case cover (190) so that the identification plate (120) is visible and the "t"-shaped
slot is facing up. Also, the 0.75 in. (1.9 em) long raised lug on the side of the case cover will be
facing down.
•
(e) Refer to Figure 7002 to align and insert the "C"-shaped end of the slide button (170) through the
lower slot (closest to the raised lug) of the case cover (190). Align and insert the 'T-shaped end
of the slide button through the upper slot of the case cover .
(f) Hold the slide button (170) in the case cover (190) and put the inside of the case cover facing
up. The raised lug will be facing down and both the slide button and the identification plate (120)
will be out of view.
(g) Carefully secure the slide button (170) to the case cover (190) using the spring (160).
NOTE: Make sure the ends of the spring are secure and aligned under the "C"-shaped and 'T_
shaped ends of the slide button. Also, make sure the long loop end of the spring faces
away from the raised lug and that the open side of the loop faces the center of the case
cover.
CAUTION:
A PLATE WITH LEVER ASSEMBLY AND COMPRESSION SPRING THAT ARE
NOT PROPERLY POSITIONED MAY CAUSE THE RESPIRATOR REGULATOR
ASSEMBLY TO FAIL TO OPERATE PROPERLY.
(h) Refer to Figure 7003 to locate and install the plate with lever assembly (150) in the "C"-shaped
end of the slide button (170). Also, the end of the plate with lever assembly (150) must be in the
raised lug area of the case cover (190).
WARNING:
(j)
•
EFFECTIVITY:
FAILURE TO WEAR GLOVES WHEN BENDING COMPRESSION
RESUL" IN INJURY TO THE HANDS.
SPRING MAY
Insert one end of the compression spring (140) into the hole of the plate with lever assembly
(150). Insert the remaining end of the compression spring in the lower (bottom) hole of the case
cover (190) .
ALL
35-32-18
Page 7011
20040415
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/scott
Technologies. Inc. Aviation
550/ll5600 SERIES PORTABLE CYLINDER ASSEMBLY·
t
CMAl & IPL
7. Respirator Regulator (Continued)
•
F. Cover Assembly (Continued)
(k) Hold finger pressure on the plate with lever assembly (150) and push the slide button (170)
between the demand and pressure-demand mode settings. The slide button must operate
freely. Put the slide button in the demand mode position.
(I) Carefully locate and install the cover assembly {-50, -60} on the case (350). Secure the cover
assembly to the case using the pan head screws (70).
Slide Button
(170, IPL Fig. 3)
~
IDPlate
~ (90, IPL Fig. 3)
B'
0
ID Plate
(120, IPL Fig. 3)~
ID Plate
~
(80, IPL Fig. 3)~
10 Plate
~(110, IPL Fig. 3)
Demand Type
Respirator Regulator
Demand/Pressure-Demand Type
Respirator Regulator
•
Cover Assembly Identification Plate Placement
Figure 7001
'T'-Shaped End -----
I
Slide Button
"C"-Shaped End -
--
Slide Button and Spring Installation
Figure 7002
EFFECTIVITY:
ALL
35-32-18
Page 7012
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•
tL/co/SCOtl
Technologies,
Inc.
/scott
Aviation
5SO(V5600SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
7. Respirator Regulator (Continued)
F. Cover Assembly (Continued)
Compression Spring
~
V
.....::1
I
_______
Plate wI Lever Assembly
0
~
I
I
~caseCover
Side View
•
Case Cover
------
"c -Shaped
n
End
(of Slide Button)
Plate wI Lever Assembly
Compression Spring
Inside View
Plate with Lever Assembly and Compression Spring Installation
Figure 7003
•
EFFECTIVITY:
ALL
35-32-18
Page 7013
20040415
1:'1co/scott
/scott
Technologies.Inc. Aviation
55DO/5600SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
TASK 35-32-18-430-803
8. Regulator Assembly (400 thru 435, IPL Figures 1A thru 1J, as applicable).
Refer to IPL Figure 9 unless noted otherwise.
Subtask 35-32-18-440-019
A. General Assembly
Install the following components in the regulator body (510 thru -550).
(1) Apply Oxygen Compatible Lubricant to the tUbe (500) and push into the body (510 thru -550), if
removed during disassembly. Remove the excess Oxygen Compatible Lubricant using Cleaning
Agent and the procedures specified in the CLEANING section for metal parts.
(2) If necessary, put the PCA or regulator PIN and SIN on a new identification plate (560, 570) with a
metal stamp having 0.064 in (0.163 em) characters. Install the identification plate on the body (510
thru -550) using the drive screws (580).
(3) Install the spring (490), thrust pin guide (480), thrust pin (470), and seat assembly (460) in the body
(510 thru -550).
(4) Carefully align the holder (450) over the thrust pin (470) and thread the holder into the body
(510 thru -550). Torque the holder to 50 in·lbs (5.6 N·m).
CAUTION:
THE DIAPHRAGM PLATE MUST BE INSTALLED WITH THE RAISED CORNERS AWAY
FROM THE DIAPHRAGM OR DAMAGE MAY OCCUR TO THE DIAPHRAGM CAUSING
THE REGULATOR TO MALFUNCTION.
I
(5) Install the thrust plate (440), diaphragm (430), diaphragm plate (410), slip ring (420), adjusting
spring (400), and guide (390) in the case (380).
(6) Put the body (510 thru -550) with drain tube (500) pointing up and carefully thread the case (380)
onto the body (510 thru -550). Torque the case to 200 in·lbs (22.6 N·m).
•
(7) Thread the setscrew (370) into the case (380) until it is level with the top of the case.
NOTE:
Setscrew (370) must be used only with spring guide (390).
Setscrew (370A) must be used only with spring guide (390A).
Subtask 35-32-18-440-020
B. Safety Plug (210)
Install the safety plug in the body (510 thru -540) as follows.
(1) lightly lubricate the safety plug washer (280) with Powdered Lubricant and install in the body
(510 thru -540).
(2) Install the safety disc (260) in the body (510 thru -540).
(3) Thread the safety plug (210) into the body (510 thru -540). Torque the safety plug to 135 - 150 in·lbs
(15.2 - 16.9 N·m).
Subtask 35-32-18-440-021
C. Safety Outlet Assembly (-220)
Assemble and install the safety outlet assembly in the body (-550) as follows.
(1) Apply a thin layer of Oxygen Compatible Lubricant on the gasket (240) and install the gasket in the
safety plug (250).
EFFECTIVITY:
ALL
35-32-18
Page 7014
20040415
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•
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•
1:'1Co/scott
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CUM & IPL
8. Regulator Assembly (Continued)
C. Safety Outlet Assembly (Continued)
(2) Install the safety disc (270) in the safety plug {250}.
NOTE: One of two different safety discs (270) may be used with the safety outlet assembly (-220). SPN
10003742 is silver-colored and alternate SPN 10006001 is bronze-colored.
(3) Thread the safety cap (230) onto the safety plug (250). Torque the safety cap to 350 in·lbs
(39.5 N·m) when SPN 10003742 (silver-colored) safety disc is used. Torque the safety cap to 375
in·lbs (42.4 N·m) when alternate SPN 10006001 (bronze-colored) safety disc is used.
(4) Lightly lubricate the safety plug washer (280) with Powdered Lubricant and install in the body (-550).
(5) Thread the safety outlet assembly (-220) into the body (-550). Torque the safety outlet assembly to
150 in·lbs (16.9 N·m).
(6) Install Lockwire between the safety cap (230) and the safety plug (250).
Subtask 35-32-18-440-022
D. Charging Valve (170)
Assemble and install the charging valve in the body (510 thru -550) as follows.
(1) Thread the valve core (-190) into the body (-180). Using the Core Wrench, torque the valve core to
4.5 - 5.0 in·lbs (0.51 - 0.56 N.m).
•
(2) Install the filter (-200) in the body (-180).
(3) Apply Thread Sealing Tape to the charging valve (170) and thread the charging valve into the body
(510 thru -550). Torque the charging valve to 175 - 200 in·lbs (19.8 - 22.6 N·m).
Subtask 35-32-18-440-023
E. OnlOffValve (10, -11)
Assemble and install the onloff valve in the regulator assembly (-1 thru -1 E) as follows.
(1) Apply a thin layer of Oxygen Compatible Lubricant on the stem assembly (100), preformed packings
(90, 130), and the threads of the head assembly (120).
(2) Thread the head assembly (120) into the bushing (140).
(3) Install the PTFE seat (11 0) on the stem assembly {1 OO}. Align the stem assembly with the head
assembly and install in the bushing (140).
(4) Install the preformed packing (90) on the packing nut (80).
NOTE: Leave handle (30) unassembled until Valve Torque Test is performed [paragraph 8.G.(2)].
Then go to Final Assembly (paragraph a.H).
(5) Align the packing nut (80) on the stem assembly (100) and thread the packing nut into the bushing
(140). Torque the packing nut to 150 in·lbs (16.9 N·m).
(6) Install the filter (150) in the body (510 thru -550).
(7) Install the preformed packing (130) on the bushing (140).
(8) Thread the bushing (140) into the body (510 thru -550). Torque the bushing to 200 in·lbs (22.6 N·m).
(9) Refer to Figure 7004 and install Lockwire between the packing nut (80) and the body
(510 thru -550) .
•
EFFECTIVITY:
ALL
35-32-18
Page 7015
20040415
~I.fc:a/scott
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
8. Regulator Assembly (Continued)
On/Off Valve Kit Installation
Figure 7004
Subtask 35-32-18-440-025
F. Gauge (290 thru -310)
Assemble and install the gauge as follows.
Refer to IPL Figure 12 unless noted otherwise.
(1) If removed during disassembly, install the lens (30, 40), bezel (10, 20), and bezel with lens (50, 60)
on the gauge (1 thru 1 F, as applicable).
(2) If removed during disassembly, install the relief label (80) and gasket (70) on the gauge (10, 1F).
(3) Perform the Gauge Accuracy Test (paragraph 9) described in the TESTING AND FAULT
ISOLATION section of this manual before the gauge is installed on the regulator assembly. Make
sure the gauge passes the test before use.
(4) Apply Thread Sealing Tape to the gauge (290 thru -310, IPL Figure 9) and thread the gauge into the
body (510 thru -550, IPL Figure 9). Align the gauge with a torque of 40 - 150 in·lbs (4.5 - 16.9 N.m).
G. Testing
•
(1) Perform the Regulator Assembly Output Pressure Test (paragraph 8) described in the TESTING
AND FAULT ISOLATION section of this manual. Make sure the regulator assembly passes the test
before use.
(2) Perform the Valve Torque Test (paragraph 10) described in the TESTING AND FAULT ISOLATION
section of this manual. Make sure the regulator assembly passes the test before use.
Subtask 35-32-18-440-026
H. Final Assembly
Install the following components after performing the tests specified in paragraph B.G.
(1) Attach the identification plate (350) on the case (380) with the screws (360).
(2) Refer to Figure 7004 to align and install the flat washer (70), spring washer (60), and handle (30) on
the stem assembly (100). Secure the handle on the stem assembly using nut (40A). Torque the nut
to 20 - 25 in·lbs (2.3 - 2.8 N·m).
(3) Install the identification plate (20) on the handle (30).
EFFECTIVITY:
ALL
35-32-18
Page 7016
20040415
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Technologies. Inc.
/SCOtf
Aviation
550015500 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IP!
TASK 35-32-18-420-801
9. PCA Assembly (-1, -2, -3, and -4 (as applicable), IPL Figures 1A thru 1J)
Refer to IPL Figures 1A thru 1J unless noted otherwise.
Subtask 35-32-18-420-001
A. Regulator Assembly (400 thru 425)
Install the regulator assembly in a steel cylinder (500 thru 565, as applicable) as follows.
(1) Hold the cylinder (500 thru 565, as applicable) in the Pneumatic Bench Vise.
(2) Apply Thread Sealing Tape to the cylinder-mating threads on regulator assembly (400 thru 425).
Thread the regulator assembly into the steel cylinder (500 thru 565, as applicable) hand tight.
WARNING:
AFTER THE CORRECT TORQUE HAS BEEN APPLIED, THE REGULATOR BODY
MUST HAVE A MINIMUM OF FOUR THREADS ENGAGED WITH THE STEEL
CYLINDER OR SERIOUS PERSONAL INJURY OR DEATH MAY OCCUR WHEN THE
PCA IS FILLED WITH OXYGEN.
(3) Torque the regulator assembly (400, 410) in the steel cylinder (500 thru 515, 550 thru 555A) to 480
- 840 in·lbs (54.2 - 94.9 N·m).
(4) Torque the regUlator assembly (405, 415 thru 425) in the steel cylinder (520 thru 545, 560, 565) to
1320 - 1560 in·lbs (149 - 176 N·m).
NOTE: The regulator body outlet port where the gauge (290, 300, IPL Figure 9) is installed must be
aligned with the oxygen identification decal (3D) on the cylinder (500 thru 565, as
applicable).
•
Subtask 35-32-18-420-002
B. Regulator Assembly (435, IPL Figure 1G)
Refer to IPL Figure 1G unless otherwise noted. Install the regulator assembly in a composite cylinder
(570) as follows.
(1) Apply a thin layer of Oxygen Compatible Lubricant on the metal boss seal (475).
(2) Install the metal boss seal (475) on the cylinder mating threads of the regulator assembly (435) with
the sealing flange pointing away from the regulator.
CAUTION:
FAILURE TO HOLD A COMPOSITE CYLINDER IN A PNEUMATIC BENCH VISE MAY
CAUSE DAMAGE TO THE FIBER OVER·WRAP ON THE CYLINDER.
(3) Hold the cylinder (570, IPL Figure 1G) in the Pneumatic Bench Vise.
(4) Thread the regulator assembly (435) into the composite cylinder (570) and torque to
540 - 660 in·lbs (61.0 - 74.5 N·m).
NOTE: The regulator body outlet port where the gauge (-310, IPl Figure 9) is installed must be
aligned with the oxygen identification decal (20) on the cylinder (570).
Subtask 35-32-18-430-001
C. Relief Valve Assembly (320 thru 340, IPL Figure 9)
(1) Testing
Perform the Relief Valve Assembly Test (paragraph 5) described in the TESTING AND FAULT
ISOLATION section before the relief valve assembly is installed on the regulator assembly. Make
sure the relief valve assembly passes all the tests before use.
•
(2) Apply Thread Sealing Tape on the relief valve assembly (320 thru 340, IPL Figure 9) and thread into
the regulator assembly (400 thru 435, IPL Figures 1A thru 1J, as applicable). Torque the relief valve
assembly to 75 - 150 in·lbs (8.5 - 16.9 N·m) .
EFFECTIVITY:
ALL
35-32-18
Page 7017
20040415
1:'1ca/scott
Technologies. Inc.
/SCOft
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
9. PCA Assembly
•
CMM & /PL
(Continued)
Subtask 35-32-18-430-002
D. Harness (205, IPL Figures 1A thru 1E, 1G thru 1J; 10, IPL Figure 2)
Install the upper end of the harness over the regulator assembly (400 thru 410, 425, 435) and let it rest
on the upper end (crown) of the applicable cylinder (500 thru 570).
Subtask 35-32-18-420-003
E. Respirator Regulator Assembly (110, IPL Figure 1H; 115, IPL Figure 1J)
Refer to IPL Figures 1Hand 1J unless otherwise noted. Install the respirator regulator as follows.
(1) Apply Thread Sealing Tape to the elbow assembly (105).
(2) Thread the elbow assembly (105) into the regulator assembly (400, 405, 410, 425). Align and
tighten the elbow assembly wrench tight.
(3) Install the clamp (75) through the bracket (125) onto the respirator regulator assembly (110, IPL
Figure 1H; 115, IPL Figure 1J).
(4) Using the clamp (75), loosely attach the respirator regulator assembly (110, IPL Figure 1H; 115, IPl
Figure 1J) around the upper end of the applicable cylinder (500 thru 555A).
(5) Remove the nut and ferrule (parts of the connector) from the connector (100) and install them on
the end of the elbow assembly (105).
(6) Align the connector (100) of the respirator regulator assembly (110, IPl Figure 1H; 115, IPl Figure
1J) over the elbow assembly (105). Push the respirator regulator assembly onto the elbow
I
assembly until connector is fully engaged. Thread nut onto the connector and tighten wrench tight.
(7) Tighten the clamp (75) around the applicable cylinder (500 thru 555A).
Subtask 35-32-18-430-003
•
F. Outlet Assemblies (300 thru 370, IPl Figures 1A thru 1J, as applicable)
Refer to Figures 1A thru 1J unless otherwise noted. Locate, install, and mark the outlet assemblies as
follows.
(1) Outlet assembly location and marking instructions.
The outlet assemblies used on 5500 Series and 5600 Series PCA's are installed on the regulator
assembly (400 thru 435) in specific places and are identified by special marks.
Refer to Figure 7005 and Figure 7006 for information about the location and marks of outlet assemblies installed on the 5500 Series or 5600 Series PCA's.
(a) On the 5500 Series peA configured with more than one constant flow (metered) type outlet
assy (300 thru 325. 370, as applicable), the outlet assembly with the highest flow rate is
connected to the first regulator assy outlet port counterclockwise from pressure gauge. On a
5600 Series PCA conflgured with more than one constant flow (metered) type outlet assembly,
the outlet assembly with the highest flow rate is connected to the first regulator assembly outlet
port counterclockwise from the respirator regUlator (110, IPL Figure 1H; 115, IPl Figure 1J).
(b) The full flow (non-metered) type outlet assembly (330 thru 355, as applicable) is connected to
the regulator assembly outlet port clockwise from the on/off valve (10, -11, IPL Figure 9).
(c) When two constant flow (metered) outlets with different flow rates are installed, there must be a
mark on both outlets made with a rubber stamp and Etching Ink. A "HI" mark, with Red Etching
Ink, must be put on the outlet assembly with the highest flow rate. A "LO" mark, with Green
Etching Ink, must be put on the outlet assembly with the lowest flow rate.
EFFECTIVITY:
ALL
35-32-18
Page 7018
20040415
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•
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..
-tqca/scott
jscotf
Technologies.Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
9. PCA Assembly
CMM & IPL
(Continued)
F. Outlet Assemblies (Continued)
2 Outlet Regulator
(Top View)
3 Outlet Regulator
(Top View)
2 Outlet Regulator
('N' Configuration)
(Top View)
5500 Series PCA Outlet Assembly Position and Marks
Figure 7005
•
LO Flow
Two Outlet Regulator
(Top View)
One Outlet Regulator
(Top View)
5600 Series PCA Outlet Assembly Position and Marks
Figure 7006
(d) All constant flow (metered) outlet assemblies must have the flow rate and the altitude setting
callout codes metal-stamped on the outside of the outlet assembly. Refer to Fjgure 7 in the
DESCRIPTION AND OPERATION section if necessary.
(2) Apply Thread Sealing Tape to the outlet assembly (300 thru 370, as applicable) or the plug (-395.
396,397, IPL Figures 1A thru 1E, 1H. 1J, as applicable) to be installed on the regulator assembly
(400 thru 435. as applicable).
(3) Identify the correct location of each outlet assembly or plug on the regulator assembly.
(4) Thread the outlet assembly or plug into the regulator assembly. Align the "HI" or "LO" marks on the
outlet assembly while torquing the outlet assembly or plug to 40 - 80 in·lbs (4.5 - 9.0 N·m).
Make sure the "HI" or "LO" mark can be seen from the top (regulator end) of the PCA.
•
(5) If applicable. mark the constant flow (metered) outlet assembly (300 thru 325. 370, as applicable)
with Etching Ink. Refer to paragraph 9.F.(1 )(c) if necessary .
EFFECTIVITY:
ALL
35-32-18
Page 7019
20040415
t:yca/scott
Technologies. Inc.
I
-
Scott
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
9. PCA Assembly (Continued)
•
Subtask 35-32-18-430-004
G. Instruction Decal (20, IPL Figures 1A thru 1G; 25, IPL Figures 1H. 1J), Oxygen Decal (30 IPL Figures
1A thru 1J), Placards (-40, -50, IPL Figures 1A, 1C, 1E, 1H, 1J), PMA Label (35, IPl Figures 1A thru
1G; Gauge Label (45, IPL Figures 1A, 1C, 1E, 1H, and 1J), Identification Plate (80, IPL Figure 1G), and
Warning Decal (65, IPL Figure 1G).
Refer to Figure 7007 and 7008 and, align and install decals, plates, placards and labels as follows.
Scott uses some non-procurable decals, identification plates and instruction plates in the manufacture of
the Portable Cylinder Assembly. Replacement (procurable) decals, identification plates and instruction
plates noted in both the ILLUSTRATED PARTS LIST and this section may look different, however must
contain the same information as the non-procurable items used in the manufacture of the PCA.
All decals and plates requiring replacement have important information (Le., part number, serial number,
dash number, date of manufacture, etc.) that must be put on the replacement item before it is put on the
applicable cylinder (500 thru 570). A permanent ink marker pen may be used to mark information on the
replacement items with characters apprOXimately the same height and spacing as those contained on
the original item.
(1) Apply the oxygen identification decal (30A, IPL Figures 1A thru 1J) on the applicable cylinder
(500 thru 570, IPL Figures 1A thru 1J) of the 5500 Series and 5600 Series PCA.
NOTE: A cylinder (500 thru 570, as applicable) manufactured before 5/81 may have text painted on
the cylinder identical to that found on the oxygen identification decal (30A). Painted text, if
present, will be placed on the cylinder the same as the oxygen identification decal. Do not
apply an oxygen identification decal to a cylinder with painted text.
(2) Apply Instruction decal (20, 20A, IPl Figures 1A thru 1G; 25, 25A, IPl Figures 1H, 1J) as follows.
(a) Apply the instruction decal (20, 20A, IPL Figure 1A thru 1G) to the applicable cylinder (500 thru
570, IPl Figures 1A thru 1G) of the 5500 Series peA (-1 thru -4K, as applicable, IPl Figures 1A
thru 1G). Instruction decal (20A) must only be used on a PCA with a green handle (3D, IPL
Figure 9).
•
(b) Apply the instruction decal (25, 25A, IPL Figures 1H, 1J) to the applicable cylinder (500 thru
525; 540 thru 555, IPL Figures 1H, 1J) of the 5600 Series PCA (-1 thru -3M, as applicable, IPL
Figures 1H, 1J). Instruction decal (25A) must only be used on a PCA with a green handle (30,
IPl Figure 9).
HXm?
(25.IPL Figures 1H and 1J)
Iir
~
(3D, IPL Figures
1H and 1J)
5600 Series peA Labeling
Figure 7007
EFFECTIVITY:
ALL
35-32-18
Page 7020
20040415
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•
';,
t:'1CO /SCOlt
/scott
Technologies. Inc. Aviation
5500'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
9. PCA Assembly (Continued)
G. Decal, Plate, Placard, and Label (Continued)
B
I....xm-{>
~ (35. IPL Figures 1,..;A::..,lrhru,.,,1r-F)
__ <_2_0,--:1IPLL_Fi_'9
.....
u__
reS lA lhru 1F)
5500-010; 5500-030; 5500-050; 5500-060 Series PCA
(45.IPL Figures lA, le, lE)
2.50 In.
(6.35cm)
Nominal
•
(-SO, IPL Figures
1A, tC, 1E)
1-I)(m-1)
~-=r--
iit
~
(35, IPL Figures
lAthru 1F)
./'
~
Hxm-{>
l
(-40, IPL Figures lA, lC. 1E)
I....x m-{>
5500-090 Series PCA
<J-wXI-I
<20, IPL Figure 1G)
~
(30, IPI. Fig"" lG)
(80, IPL Figure tG)
l-txm-1)
Cylinder Manufacrurer
10 Plate
(Reference)
5500· T21J Series PCA
•
5500 Series PCA Labeling
Figure 7008
EFFECTIVITY:
ALL
35-32-18
Page 7021
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/SCOtf
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
9. PCA Assembly
.-
CMM & IPt
(Continued)
•
G. Decal, Plate, Placard, and Label (Continued)
(3) Apply the FAA-PMA label (35) to the 5500 Series PCA (-1, -2, -3, and -4, IPL Figures 1A thru 1G, as
applicable).
(4) Apply identification plate (80, IPL Figure 1G) and warning label (65, IPL Figure 1G) to the 5500
Series PCA (-1, IPL Figure1G).
(5) Apply the aviators oxygen placard (-50), and instruction placard (-40) to the 5500 Series and 5600
Series PCA (-3T thru -3Y, IPL Figure 1A; -4L thru -4U, IPL Figure 1C; -2F, -2G, rPL Figure 1E; -3F,
IPL Figure 1H; -1A, -1U, -2C, and -2L, IPL Figure 1J).
Apply the label (45) to the 5500 Series and 5600 Series PCA (-3T thru -3Y, IPL Figure 1A; -4L thru 4U, IPL Figure 1C; -2F, -2G, IPL Figure 1E; -3F,IPL Figure 1H; -1A, -1U, -2C, and -2L, IPL Figure
1J). Label (45) must be applied to the face of the gauge (290, 300, IPL Figure 9) but must not cover
the gauge needle or range markings. Label to indicate next required hydrostatic test date: 5 years
from cylinder date stamp.
TASK 3S-32-18-610-801
10. PCA Charging Procedure
Refer to IPL Figure 9 (unless noted otherwise), and Table 7004.
Subtask 35-32-18-610-001
•
A. PCA Charging Setup
(1) Remove the filler cap (160) from the charging valve (170).
(2) Attach the Refill Coupling (Table 7002) to the charging valve (170).
Subtask 3S-32-18-610-oo2
B. Charge the PCA
(1) Rotate handle (30) counterclockwise to the fully open on/off valve (10, -11).
(2) Refer to Table 7004 for cylinder type and charging pressure at temperatures from SO-100°F
(10.0-37.8°C).
Subtask 35-32-18-610-003
C. Disconnect the PCA
WARNING:
FAILURE TO FULLY DISCHARGE THE PCA CHARGING SETUP OF OXYGEN
BEFORE DISASSEMBLY OF ANY PART MAY RESULT IN SERIOUS PERSONAL
INJURY OR DEATH.
(1) Rotate handle (30) clockwise to fully close on/offvalve
charging setup.
(10, -11). Discharge all oxygen from the PCA
(2) Remove the PCA from the PCA charging setup.
D. Testing
Perform the applicable PCA Final Tests (paragraph 11) described in the TESTING AND FAULT
ISOLATION section of this manual. Make sure PCA passes all tests before use.
EFFECTIVITY: All
35-32-18
Page 7022
20040415
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1:'1CD/ Technologies.
Scott
Inc.
!
Scott
Aviation
550015600 SERiES PORTABLE CYLfNDER ASSEMBLY·
CMM & /PL
10. PCA Charging Procedure (Continued)
D. Testing (Continued)
Table 7004
Pressure vs. Temperature Data
•
•
TEMPERATURE
of (0C)
US DOT3-AA-1800 (Steel)
NOMINAL 1800 psig (12.41 MPa)
CHARGING PRESSURE
psig (MPa)
US DOT-3HT-1850 (Steel) or
US DOT-E-8162-1850 (Composite)
NOMINAL 1850 psig (12.76 MPa)
CHARGING PRESSURE
psig (MPa)
100 (37.8)
1935 (13.34)
1985 (13.69)
95 (35.0)
1910 (13.17)
1960 (13.51)
90 (32.2)
1890 (13.03)
1935 (13.34)
85 {29.4}
1870 (12.89)
1910 (13.17)
80 (26.7)
1850 (12.76)
1885 (13.00)
75 (23.9)
1825 (12.58)
1865 (12.86)
70 (21.1)
1800 (12.41)
1850 (12.76)
65 (18.3)
1775 (12.24)
1825 (12.58)
60 (15.6)
1750 (12.07)
1800 (12.41)
55 (12.8)
1730 (11.93)
1775 (12.24)
50 (10.0)
1710 (11.79)
1750 (12.07)
EFFECTIVITY:
ALL
35-32-18
Page 7023
20040415
1:'1c:a/scott
Technologies. Inc.
!SCOtf
Aviation
550015600SERIES PORTABLE CYUNDER ASSEMBLY·
..
#
eMM & IPL
TASK 35-32-18-400-803
•
11. Final peA Assembly
Refer to IPL Figures 1A thru 1J unless noted otherwise.
NOTE: The replacement PAX mask assembly (35 thru 41, IPL Figure 2) may contain either a cord and
pin on the mask tubing or a loose-packed spring clip and tube which must be removed and
discarded. Carefully cut off the corner of the protective bag containing the replacement (new) PAX
mask assembly and remove either the cord and pin from the mask tubing or the loose-packed
spring clip and tube. Reseal the protective bag with adhesive tape.
Subtask 35-32-18-430-005
A. PIN 801660-00 Harness Assembly (205, IPL Figures 1A thru 1E and 1G thru 1J)
Refer to Figure 7009 and install the harness (205) as follows.
NOTE: The upper (loop) end of the harness was previously installed.
(1) Align the remaining end of the harness (205) on the lower end of the cylinder (500 thru 570).
(2) Align and install the clamp (70) over the remaining end of harness. Depending on the cylinder size,
align and tighten the clamp on the cylinder approximately 2.5 - 4.0 in. (6.4 - 10.2 em) from the
bottom end of the cylinder.
Subtask 35-32-18-430-006
B. PIN 801658-00 Harness Assembly (200, IPL Figures 1A thru 1C, 1H, and 1J)
Refer to Figure 7009 and install the harness assembly (200) as follows.
(1) Align and install the strap assembly (201) on the cylinder (500 thru 525, 540 thru 555A).
(2) Align and install clamp (70) over strap assembly (201). Depending on the cylinder size, align and
tighten the clamp on the cylinder approximately 2.5 - 4.0 in. (6.4 - 10.2 em) from the bottom end of
cylinder.
•
(3) Align and install strap assembly (202) over the strap assembly (201) on the cylinder (500 thru 525,
540 thru 555A).
(4) Align and install the clamp (75) over the strap assemblies (201, 202). Align and tighten the clamp on
the cylinder approximately 3.5 in. (8.9 em) from the neck of cylinder.
Subtask 35-32-18-430-007
C. PIN 801662-00 Harness Assembly (225, IPL Figures 1Band 1E).
Refer to Figure 7009 and install the harness assembly (225) as follows.
(1) Align and install the harness assembly (225) on the cylinder (510, 515).
(2) Align and install the clamp (75) over the harness assembly (225). Align and tighten the clamp
approximately 3.5 in. (8.9 em) from the neck of cylinder.
EFFECTIVITY:
ALL
35-32-18
Page 7024
20040415
•
•
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•
tl./ca/scotl
Technologies. Inc.
I~c.ot~
A,natlon
550015600 SERIES PORTABLE CYLINDER ASSEAfBLY • CMM & IPL
11. Final PCA Assembly
(Continued)
C. PIN 801662-00 Harness Assembly (Continued)
5500 Series peA
PIN 801660-00 Harness (205.IPl
5600 Series PCA
Figures 1A thru 1E, and 1G thru 1J)
_----~~---~W.iSILOop
Strap Assembly
(202)
Strap Assembly
(201)
•
CI.",,(70)
Clamp (75)
PIN 801658-00 Harness (200, IPL Figures 1A thru 1C)
Clamp
PIN 801662-00 Harness (225, IPL Figures 18, 1E)
PCA Harness Configurations
Figure 7009
•
EFFECTIVITY:
ALL
35-32-18
Page 7025
20040415
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-fqeo/scott
/scott
Technologies. Inc. Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPt
11. Final PCA Assembly (Continued)
•
Subtask 35-32-18-430-008
D. PIN's 801660-03, -05 Harness Assemblies (215, IPL Figure 1C; 220, IPL Figures 1Hand 1J).
Refer to Figure 7010 and install the harness assembly (215, 220) as follows.
(1) Loop the harness (215, 220) around the neck ofthe cylinder (550, 550A, 5508, 555, 555A). Snap
the socket onto the stud (both are part of the harness assembly) to secure the harness to the neck
of the cylinder.
(2) Align the remaining end of the harness on the cylinder.
(3) Align and install the clamp (70) over the remaining end of the harness. Depending on the cylinder
size, align and tighten the clamp on the cylinder approximately 2.5 - 4.0 in. (6.4 - 10.2 cm) from the
bottom end of cylinder.
(4) Snap the remaining sockets onto the studs.
~
_~JI
y215
=
<:'11
~
,"'<:;t
.",-
•
PIN 801660-03 Harness (215, IPL Figure 1C)
"'''~lil
~
.
.
'"'~
PIN 801660-05 Harness (220, IPL Figures 1H and 1J)
PCA Harness Configurations
Figure 7010
EFFECTIVITY: All
35-32-18
Page 7026
20040415
•
•
"
•
tl./ca/scott
Technologies.Inc.
I
Scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
11. Final PCA Assembly (Continued)
Subtask 35-32-18-430-009
E. PIN's 801807-01, -02, -03 Mask Storage Bag and Harness Assembly (-1 thru -1B, IPL Figure 2).
Item numbers refer to IPL Figure 2 unless otherwise noted. Refer to Figure 7011.
(1) Install the fastener (45) through the mask storage bag assembly (55).
(2) Align and install the fastener with the attached mask storage bag assembly on the applicable PCA
(IPL Figures 1A thru 1C and 1F).
(3) Align and install the harness assembly (-1 thru -18, IPL Figure 2) on the PCA as follows.
(a) Install the harness assembly (-1 thru -18) on the cylinder.
(b) AUgn and install the clamp (75, IPL Figures 1A thru 1C and 1F) over the harness assembly.
Align and tighten the clamp approximately 3.5 in. (8.9 em) from the neck of the cylinder.
(4) As necessary, repackage and install the PAX mask assembly (35, IPL Figure 2) in the mask storage
bag assembly (55) as follows.
(a) Put the large diameter of the face piece down on a clean, flat, lint-free surface and spread the
reservoir bag out flat.
(b) Fold one third of the reservoir bag over the center of the bag parallel to the tubing.
(c) Fold the other one third of the reservoir bag over the first folded side even with the outer edge.
(d) Put the head strap into the face piece.
•
(e) Carefully put the folded reservoir bag into the face piece .
(f)
Make sure that the correct outlet assembly mating connector (15), coupling (-25), or nipple (-30)
is attached to the tUbe.
(g) Coil the tube inside of the face piece in a clockwise direction.
(h) Put the PAX mask assembly in the protective plastic bag. Close and seal the protective bag.
(j) Carefully put the sealed PAX mask assembly into the mask storage bag assembly (55).
Subtask 35-32-18-430-010
F. PIN's 801808-01, -02, -03, -05 Mask Storage Bag and Harness Assembly (-1C thru -1 F, IPL Figure 2).
Item numbers refer to IPL Figure 2 unless otherwise noted. Refer to Figure 7012.
(1) Install the fastener (45, 50) through the mask storage bag assembly (55, 60).
(2) Align and install the fastener with the attached mask storage bag assembly on the applicable PCA
(IPL Figures 1A thru 1E). If the PCA is equipped with a second mask storage bag assembly (60), it
is fastened to the opposite side of the cylinder.
(3) Align and install the harness (10) as follows.
NOTE: The upper (loop) end of the harness was previously installed on the appllcable PCA
(IPL Figures 1A thru 1E). Refer to paragraph 9.0.
(a) Align the loose end of the harness (10) on the lower end of the cylinder.
(b) Align and install the clamp (70, IPL Figures 1A thru 1E) over the harness assembly. Depending
on the cylinder size, align and tighten the clamp on the cylinder approximately 2.5 - 4.0 in. (6.4 10.2 em) from the bottom end of the cylinder .
•
EFFECTIVITY:
ALL
35-32-18
Page 7027
20040415
t:qca!scott
..
/scott
,
Technologies.
Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
11. Final PCA Assembly (Continued)
•
F. PIN's 801808-01, -02, -03, -05 Mask Storage Bag and Harness Assembly (Continued)
Outlet Assembly
Mating Connector
(15, -25, -30, IPL Figure
2"J-
}
PAX Mask Assembly
(35, IPL Figure 2)
Reservoir Bag
(folded)
Protective Bag
(wi PAX Mask Assy)
/
Adhesive Tape
•
r....
-- -----......
,
:,
__
-
Mask Storage Bag Assy
(55, IPL Figure 2)
Fastener
(45, IPL Figure 2)
Harness Assembly
(-1, -1A, -1B, IPL Figure 2)
~~J/
/
I
PIN's 801807-01, -02. -03 (-1 thru -18. IPL Figure 2) Mask Storage Bag and Hamess Assembly
Figure 7011
EFFECTIVITY:
ALL
35-32-18
Page 7028
20040415
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•
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tl./co/SCOtl
!SCDtt
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY - eMM & IPL
11. Final peA Assembly (Continued)
F. PIN's 801808-01, -02, -03, -05 Mask Storage Bag and Harness Assembly (Continued)
Outlet Assembly
Mating Connector --(15 thru -30, IPL Figure 2)
1III""'=:::;:::j~::'PAX Mask Assembly
} (35, 40, IPL Figure 2)
.-----~~--....,
~M>i'B"
(folded)
Protective Bag
(wI PAX Mask Assy)
/
•
I, "
Adhesive Tape
.-- - ------''''1
:
\-
I
~
.....~l
_,_\
I
'"
-"'"
------
Mask Storage Bag Assy
(55, 60, IPL Figure 2)
------
\ --l
Fastener
(45, 50, IPL Figure 2)
Harness
(10, IPL Figure 2)
.'1-,
\'.,
/
Cylinder
Clamp
•
PIN's 801808-01, -02, -03, -05 (-1 C thru -1 F, IPL Figure 2)
Mask Storage Bag and Harness Assembly
Figure 7012
EFFECTIVITY:
ALL
35·32·18
Page 7029
20040415
t'-/co/scott
Technologies.
Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
11. Final PCA Assembly (Continued)
F. PIN's 801808-01, -02, -03, -05 Mask Storage Bag and Harness Assembly (Continued)
(4) As necessary, repackage and install the PAX mask assembly (35, 40) in the mask storage bag
assembly (55, 60) as follows.
(a) Put the large diameter of the face piece down on a clean, flat, lint-free surface and spread the
reservoir bag out flat.
(b) Fold one third of the reservoir bag over the center of the bag parallel to the tubing.
(c) Fold the other one third of the reservoir bag over the first folded side even with the outer edge.
(d) Put the head strap into the face piece.
(e) Carefully put the folded reservoir bag into the face piece.
(f)
Make sure that the correct outlet assembly mating connector (15, 20), coupling (-25), or nipple
(-30) is attached to the tube.
(g) Coil the tube inside of the face piece in a clockwise direction.
(h) Put the PAX mask assembly in the protective plastic bag. Close and seal the protective bag.
G)
Carefully put the sealed PAX mask assembly into the mask storage bag assembly (55, 60).
(k) If the PCA is equipped with PAX mask assembly No.2, repeat paragraphs 11.F .(4 lea) thru
11.F.(4)(h).
(I)
Carefully put the sealed PAX mask assembly NO.2 into the remaining mask storage bag
assembly (60).
Subtask 35-32-18-430-011
\
G. PIN's 803177-01, -02, -03 Mask Storage Bag and Harness Assembly (-1G thru -1J, IPL Figure 2).
Item numbers refer to IPL Figure 2 unless otherwise noted. Refer to Figure 7013.
(1) Install the fastener (45) through the mask storage bag assembly (55).
•
(2) Align and install the fastener with the attached mask storage bag assembly on the applicable PCA
(IPL Figures 1A thru 1E).
(3) Align and install the harness (10) as follows.
NOTE: Item 1H, IPL Figure 2 does not include a harness (10, IPL Figure 2) or harness clamp.
NOTE: The upper (loop) end of the harness was previously installed on the applicable PCA
(IPL Figures 1A thru 1E). Refer to paragraph 9.0.
(a) Align the remaining end of the harness assembly (10) on the cylinder.
(b) Align and install the clamp (70, IPL Figures 1A thru 1E) over the harness. Depending on the
cylinder size, align and tighten the clamp on the cylinder approximately 2.5 - 4.0 in.
(6.4 - 10.2 em) from the bottom end of cylinder.
(4) As necessary, repackage and install the PAX mask assembly (36 thru 41) in the mask storage bag
assembly (55) as follows.
(a) Put the large diameter of the face piece down on a clean, flat, lint-free surface and spread the
reservoir bag out flat.
(b) Fold one third of the reservoir bag over the center of the bag parallel to the tubing.
(e) Fold the other one third of the reservoir bag over the first folded side even with the outer edge.
(d) Put the head strap into the face piece.
(e) Carefully put the folded reservoir bag into the face piece.
EFFECTIVITY: ALL
35-32-18
Page 7030
20040415
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•
~.
,
tl/cajscotl
!scott
Technologies, Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
11. Final PCA Assembly
G. PIN's 803177-01,
CMM & IPL
(Continued)
-02, -03, Mask Storage Bag and Harness Assembly
(Continued)
Facepiece
(No.1)
",;:,.::;--r.." ..l---
1.'i'""1r __
Facepieoe
(No.2)
PAX Mask Assy's
(36 thru 41, IPL Figure 2)
Outlet Assembly
Mating Connector
(20. -30, IPL Figure 2)
Mask Storage Bag Assembly
(55, IPL Figure 2)
~~
•
Fastener
(45, IPL Figure 2)
Harness
(10, IPL Figure 2)
\
OXYGEN
!
MASK
Clamp
NOTE: Items 3C, IPL Figure 1A and 3K, IPL Figure 1C)
do not include harness (275, IPL Figure 1A, 1C) or
clamp (70, IPL Figures 1A, 1C)
•
PIN's 803177-01, -02, -03 (-1G thru -1J,IPL Figure 2)
Mask Storage Bag and Harness Assembly
Figure 7013
EFFECTIVITY:
ALL
35-32-18
Page 7031
20040415
1:qca/scott
Technologies.
Inc.
,..
/scott
Aviation
5500'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
11. Final PCA Assembly (Continued)
G. PIN's 803177-01, -02, -03 Mask Storage Bag and Harness Assembly
•
(Continued)
(f) As necessary, make sure that the correct outlet assembly mating connector (20) or nipple (-30)
is attached to the tube.
(g) Coil the tube inside of the face piece in a clockwise direction.
(h) As necessary, repeat paragraphs 11.G.(4)(a) thru 11.G.(4)(d) for PAX mask assembly NO.2.
m
Put the repackaged PAX mask assembly NO.1 in the face piece of PAX mask assembly No.2.
(k) Carefully put the folded reservoir bag (PAX mask assembly No.2) into the face piece of PAX
mask assembly No.1.
(I) As necessary, make sure that the correct outlet assembly mating connector (20) is attached to
the tube.
(m) Coil the tUbe of PAX mask assembly No.2 around the outside of PAX mask assemblies NO.1
and No.2.
(n) As necessary, put the PAX mask assemblies in the protective plastic bag. Close and seal the
protective bag.
(p) Carefully put the sealed PAX mask assemblies into the mask storage bag assembly (55).
Subtask 35-32-18-430-012
H. PIN 805436-01 Mask Storage Bag and Harness Assembly (-1 K, IPL Figure 2).
Item numbers refer to IPL Figure 2 unless otherwise noted. Refer to Figure 7014.
(1) Install the fastener (45) through the mask storage bag assembly (55).
(2) Align and install the fastener with the attached storage bag assembly on the applicable PCA (IPL
Figures 1A and 1C).
(3) Align and install the harness (10) as follows.
•
NOTE: The upper (loop) end of the harness was previously installed on the applicable PCA
(IPL Figures 1A and 1C). Refer to paragraph 9.0.
(a) Align the remaining end of the harness (10) on the cylinder.
(b) Align and install the clamp (70, IPL Figures 1A and 1C) over the harness. Depending on the
cylinder size, align and tighten the clamp on the cylinder approximately 2.5 - 4.0 in. (6.4 10.2 em) from the bottom end of cylinder.
(4) As necessary, repackage and install the PAX mask assembly (35) in the mask storage bag
assembly (55) as follows.
(a) Put the large diameter of the face piece down on a clean, flat, lint-free surface and spread the
reservoir bag out flat.
(b) Fold one third of the reservoir bag over the center of the bag parallel to the tubing.
(c) Fold the other one third of the reservoir bag over the first folded side even with the outer edge.
(d) Put the head strap into the face piece.
(e) Carefully put the folded reservoir bag into the face piece.
(f)
Make sure that the plug-in connector (15) is attached to the tube.
(g) Coil the tube inside of the face piece in a clockwise direction.
(h) Put the PAX mask assembly in the protective plastic bag. Close and seal the protective bag.
0)
EFFECTIVITY:
Carefully put the sealed PAX mask assembly into the mask storage bag assembly (55).
ALL
35-32-18
Page 7032
20040415
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1:lIeD/scott
Technologies.
Inc.
jscott
Aviation
5500'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
11. Final PCA Assembly (Continued)
H. PIN 805436-01 Mask Storage Bag and Harness Assembly (Continued)
Outlet Assembly
Mating Connector .........
(15, IPL Figure 2)
.........
Coiled Tubing
}
PAX Mask Assembly
(35, IPL Figure 2)
Reservoir Bag
(folded)
Protective Bag
(wI PAX Mask Assy)
/
•
"""",",
Tape
Mask Storage Bag Assy
(55, IPL Figure 2)
Fastener
(45, IPL Figure 2)
Harness
(10, IPL Figure 2)
I
Cylinder
~
Clamp
PIN 805436-01 (-1 K, IPL Figure 2)
Mask Storage Bag and Harness Assembly
Figure 7014
•
EFFECTIVITY:
ALL
35-32-18
Page 7033/7034
20040415
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•
•
•
tl.lca/scott
Technologies. Inc.
.~
....
jSCDtt
Aviation
5500/5600 SERIES PORTABLE CYUNDER ASSEMBLY·
CMIA & IfL
FITS AND CLEARANCES
TASK 35-32-18-99C-802
Torque values, critical to the assembly and operation of the 5500 and 5600 Series PCA, are listed in
Table 8001.
Table 8001
Torque Values
IPL REFERENCE
•
FIG. NO.
ITEM NO.
1A thru 1J
300 thru 370
Outlet Assembly
40 - 80 (4.5 - 9.0)
1A thru 1E,
1H,1J
-395, -396, -397
Plug
40 - 80 (4.5 - 9.0)
1A thru 1C,
1E, 1H, 1J
400,410
Regulator Assembly
(0.500 - 14 ANPT Threads)
480 - 840 (54.2 - 94.9)
10 thru 1F,
1H,1J
405,415,425
Regulator Assembly
(1.00 - 11.5 ANPT Threads)
1320 -1560 (149.1 -176.2)
1G
435
Regulator Assembly
(0.750 - 16UNF-2A Threads)
540 - 660 (61.0 -74.5)
9
40A
Nut, Alternate SPN 804670-03 Only
20 - 25 (2.3 - 2.8)
9
80
Packing Nut
150 (16.9)
9
140
Bushing
200 (22.6)
9
170
Charging Valve
175 - 200 (19.8 - 22.6)
9
-190
Valve Core
4.5 - 5.0 (0.51 - 0.56)
9
210
Safety Plug
135 -150 (15.2 -16.9)
9
-220
Safety Outlet Assembly
150 (16.9)
9
230
Safety Cap
Note 1
9
290 thru -310
Gauge
40 -150 (4.5 -16.9)
9
320thru 340
Relief Valve Assembly
75 - 150 (8.5 - 16.9)
9
380
Case
200 (22.6)
9
450
Holder
50 (5.6)
Nole 1:
•
TORQUE VALUES
in·lbs (N·m)
NOMENCLATURE
SaFetydiscs. SPN 10003742 or SPN 10006001, may be used in lhe safely outlet assembly (-220, IPL Figure 9).
Torque the safety cap to 350 in·lbs (39.5 N'm) when safety disc SPN 10003742 (Item 270, IPL figure 9) is used.
Torque the safety cap to 375 in·lbs (42.4 N·m) when safely disc SPN 10006001 (Item 270, IPL Figure 9) is used.
EFFECTIVITY:
ALL
35-32-18
Page 8001/8002
20040415
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tqco/scott
/scott
Technologies, Inc. Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
SPECIAL
TOOLS,
CMM & IPL
FIXTURES,
EQUIPMENT,
AND CONSUMABLES
TASK 35-32-18-94B-807
This section contains a complete listing of all Special
Consumable
Materials (Table 9002) used throughout
Subtask
Tools, Fixtures,
this CMM.
Equipment
(Table 9001), and
35-32-18-94B-001
1. Special Tools, Fixtures,
and Equipment
Special tools, Fixtures, and Equipment required for disassembly,
assembly, testing, cleaning, checking or
repair of the PCA are presented in Tabfe 9001. Special tools (Figure number in "NOMENCLATURE"
column) required for testing, disassembly,
or assembly of the 5500 and 5600 Series PCA are shown in
Illustrations, Special Tools, and Fixtures (paragraph 3). Tools and equipment used in this manual, not listed
in Table 9001, are standard oxygen shop tools or equipment. Special tools, fixtures, and test equipment
must be cleaned for oxygen service before use. Unless noted otherwise, one of each item is required.
Equivalents may be substituted.
Table 9001
Special Tools, Fixtures, and Equipment
PART NUMBER
(or DESCRIPTION)
MANUFACTURER
(VENDOR CODE)
Pressure Gauge
(minimum accuracy ±0.25% full scale)
0- 100 psig (0 - 0.69 MPa)
200 psig (0 - 1.38 MPa)
0- 2000 psig (O - 13.8 MPs)
1404 Series
Ametek (US Gauge)
Sellersville, PA 18960-2625
USA (V61349)
Vent Valve
0.250 in. -18 ANPT Threads
P4T Series
B-4P4T4
Whitey Co.
Highland Heights, OH 441341533 USA (V12623)
Test Regulator
0-2500 psig (0 - 17.2 MPa)
Outlet Pressure
44-1110 Series
44-1114-24
0- 250 psig (0 -1.72 MPa)
Outlet Pressure
26-1600 Series
26-1612-24
Flowmeter
(minimum accuracy ±2% full scale)
5.0-50cem
13.6 - 136 cem
0.62 - 6,20 Ipm
12.6 - 1261pm
1110 Series
1110CC21ABGAA
1110CC11 BBGAA
1110CC71DBGAA
1110CJ42CBGM
Mating Connector for
800503-00, 5009-00, 5009 Series Outlet Assy
5041-00,5041 Series Outlet Assy
5507-00,5077 Series Outlet Assy
5052-00 Outlet Assy
10003566, 802856-01 Outlet Assy
36728-01, DPB153 Outlet Assy
10008298 Outlet Assy
10006017 Outlet Assy
802863-02 Outlet Assy
8572-02 OuUetAssy
5065-10
29559-00
14807-00
5067-08
802857-01
36857-01
10007498
LAC672163-103 (Lockheed)
802627-01
8570 Series
NOMENCLATURE
•
•
o-
I
EFFECTIVITY:
ALL
Tescom Corp.
Elk River, MN 55330-2445
USA (V5H642)
Emerson Electric Co,
Brooks Instruments Division
Hatfield, PA 19440-3052
USA (V91556)
Scott Aviation
Lancaster. NY 14086-9502
USA (V53655)
35-32-18
Page 9001
20040415
1:I./Co/scott
Technologies. Inc.
Aviation
550015600 SER/ES PORTABLE CYLINDER ASSEMBLY·
1. Special
Tools.
Fixtures.
...
/scott
CMM & IPI.
and Test Equipment
Special
(Continued)
Table 9001 (Continued)
Tools, Fixtures, and Equipment
PART NUMBER
(or DESCRIPTION)
MANUFACTURER
(VENDOR CODE)
Shut Off Valve (2 required)
1 Series
B-1VF4
Whitey Co.
Highland Heights, OH 44134-1533
USA (V12623)
Flow Control Valve
18 Series
B-18RF8
Whitey Co.
Highland Heights, OH 44134-1533
USA (V12623)
Needle Valve
1 Series
B-1RF4
Whitey Co.
Highland Heights, OH 44134-1533
USA (V12623)
NOMENCLATURE
Regulator Test Adapter
0.500 -14 ANPT x 0.250 -18 ANPT Threads
1.00 - 11.5 ANPT x 0.250 - 18 ANPT Threads
0.750 - 16UNF2A x 0.250 - 18 ANPT Threads
Scott Aviation
lancaster, NY 14086-9502
USA (V53655)
803213-558-12
803213-S58-10
803213-S58-1
Graduated Cylinder
5 cc Capacity
A2-15
Na~onal Glass and Plastics Co.
Vineland, NJ 08360
USA (VOUUR4)
low Pressure Regulator
Vae to 2 psig (Vac to 14 KPa)
(Vac to 55 in. WC)
16 Series
16112J
Fairchild Industrial Products Co.
Winston-Salem, NC 27103-6708
USA (V07282)
Note: REG requires both VAC
and PRESS to operate.
Maximum inlet pressure is
250 psig (1,72 MPa)
Draft Gauge
(minimum accuracy ±2% full scale)
-5.0 to +5.0 in. WC (-12.7 to +12.7 cm WC)
Differential Pressure
Oto 15 in. WC (0 - 38 em WC)
Respirator Regulator Mating Connector
Screw Type - Used with respirator regUlator assy
PIN 6379-2C (on 5600-1 Series PCA) or
PIN 800649-00 (on 5600-8 Series PCA)
AN Type - Used on respirator regUlator assy
PIN 6379-2D (on 5600-2 Series PCA) or
PIN 800649-01 (on 5600-9 Series PCA)
2000 Series Magnehelic·
231Q-A-321
•
Dwyer Instruments Inc.
Michigan City, IN 46360-0373
USA (V85274)
20 15-A-321
6210-00
Scott Aviation
lancaster, NY 14086-9502
USA (V53655)
13822-00
Pneumatic Bench Vise
Model BV-101-P
PIN 58634
Getz Fire Equipment Co.
Peoria, Il61602-1711
USA (V58013)
Core Wrench
(Figure 9001)
800216-T91-1
Scott Aviation
Lancaster, NY 14086-9502
USA (V53655)
• Magnehelic is a Registered Trademark of Dwyer Instruments Inc.
EFFECTIVITY: All
•
35-32-18
Page 9002
20040415
•
•
.~
...
1:'lca/scott
Technologies, Inc.
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
eMM & IPL
1. Special Tools. Fixtures. and Test Equipment (Continued)
Table 9001 (Continued)
Special Tools, Fixtures, and Equipment
NOMENCLATURE
PART NUMBER
(or DESCRIPTION)
Protective Cap
1.188 in. (3.018 em) ID
1.125 in. (2.858 em) 10
1.250 in. (3.175 em) 10
PIN C234 SPN 33492-029
PIN C232 SPN 33492-027
PIN C336 SPN 33492-032
Wire Brush
1 in. diameter
UquidNapor
Degreaser System
Stainless Steel Tubing
•
/SCOft
Aviation
MSR-216LE
0.250
0.035
or
0.375
0.035
in. (6.35 mm) 00 x
in. (0.889 mm) Wall
Alliance Plastics Inc.
Erie, PA 16510-3045
USA (V34669)
Local Vendor
Baron Blakeslee
, Long Beach, CA 90813
USA (VOFDJ7)
Local Vendor
in. (9.53 mm) 00 x
in. (0.889 mm) Wall
Ultrasonic Cleaning System
TH-1418-9
Mass Technology
PO Box 795-T
East Moline. IL 61244-0795 USA
Fax: 309-755·1121
Bright Inspection light
Il-24
Titan Tool and Supply Co.
Buffalo. NY 14216-1784
USA (V51679)
Spray Gun
Model 19
Binks Manufacturing Company
AMF Ohare, IL 60666-2887
USA (V07334)
Cylinder Hanger (Steel Cylinders)
0.500 in. -14 ANPT Threads
1.00 in, - 11.5 ANPT Threads
Local Vendor
Cylinder Hanger (Composite Cylinders)
•
MANUFACTURER
(VENDOR CODE)
0.750 -16UNF·2A Threads
SK87-117-08
Refill Coupling
CGA 540 x 0.563 -18UNF-2B Threads
5020-01
EFFECTIVITY:
ALL
Bolero Industries
Santa Fe Springs, CA 90670
USA (VOTRZ6)
Scott Aviation
Lancaster, NY 14086-9502
USA (V53655)
35-32-18
Page 9003
20040415
.,
'fLieD/scott
/SCOft
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
Subtask
•
CMM & IPL
35-32-18-94A-001
2. Consumable
•
Materials
A list of consumable
materials required for testing and fault isolation, cleaning, repair and assembly of PCA
are shown in Table 9002. Equivalent materials may be substituted, except for Oxygen Compatible
Lubricant and Oxygen (when used in Cylinder Charging Procedures in the ASSEMBLY
section of this
manual).
Also, Oxygen (MIL-PRF-27210,
Type I) is the Test Gas specified in the TESTING AND FAULT ISOLATION
section of this manual. Water pumped Nitrogen (A-A-59503)
or Air (equivalent in purity to MIL-PRF-27210,
Type I) may be substituted for Oxygen only when used as the Test Gas.
Table 9002
Consumable
Materials
MANUFACTURER
(VENDOR CODE)
MATERIAL
DESCRIPTION
Thread Sealing Tape
0.250 in. (0.635 cm) wide
PTFE Ribbon Tape
CID A-A-58092, size 1
SPN 50011-00
Local Vendor
leak Test Solution
Sherlock leak Detector
Mll-PRF·25567, Type 1
Winton Products Co. Inc.
Charlotte, NC 28236
USA (V23316)
Rust Inhibiting Leak Test Solution
5 cc Sodium Chromate per gallon of water.
Allied Chemical Corp.
Morristown, NJ 07960
USA (V70308)
Flushing Agent
leniumGS
(n-propyl Bromide)
Petroferm
Fernandina Beach, Fl 32034
USA (VOWUA8)
Cleaning Agent
HFE-71DE
(Azeotrope of Perfluorobutyl Methyl Ether)
3M/SPlC
St. Paul. MN 55133·3900
USA (VOU817)
Non-ionic Detergent
Non-ionic Detergent
Mll-D-16791, Type I
Local Vendor
Ceramic Tumbling Media
XA Ceramic Media
Washington Mills Abrasive Co.
North Grafton, MA 01536-1558
USA (V89204)
,
30 mesh
Glass Tumbling Media
Ballotini Impact Beads
The PO Corp.
Valley Forge, PA 19482-0840
USA (V08867)
Abrasive Blasting Media
No. 16 Aluminum Oxide
PIN 1700164
Treibacher - SChleifmittel Co.
Niagara Falls, NY 14303 (USA)
Fax: 716-286-1224
Scotch Brite Pad
NO.2 Size
PIN 10116NA
3M Abrasive Systems Division
St. Paul, MN 55144-1000
USA (V28124)
Plastic Abrasive Pad
EFFECTIVITY: ALL
35-32-18
Page 9004
20040415
•
•
•
.
....,
t"ca/scott
/scott
Technologies. Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
eMM & IPL
2. Consumable Materials (Continued)
Table 9002 (Continued)
Consumable Materials
MATERIAL
DESCRIPTION
Hydrochloric Acid
Hydrochloric Acid
(HCI)
pH Test Paper Strips
4391-01
Chromic Acid
Chromium (VI) Trioxide
MANUFACTURER
(VENDOR CODE)
Mallinckrodt Baker Inc.
Phillipsburg, NJ 08865-2219
USA (V70829)
Mallinckrodt Baker Inc.
Phillipsburg, NJ 08865-2219
USA (V70829)
Mallinckrodt Baker Inc.
Phillipsburg, NJ 08865-2219
USA (V70829)
(Cr03)
•
Phosphoric Acid
Phosphoric Acid
(H3P04)
Mallinckrodt Baker Inc.
Phillipsburg, NJ 08865-2219
USA (V70829)
Catalyst
A3110
SPN 50761-03
A.P. NonweilerCo.
Oshkosh, WI 54903-1007 USA
Fax: 920-231-8085
Primer (2 part catalyzed urethane)
Ught Gray (No. 36628 per FED-STD-595)
4285A093
Paint (2 part catalyzed urethane)
Green (No. 24062 per FED-STD-595)
Green (No. 14187 per FED-STD-595)
Gray-Green (No. 24159 per FEO-STD-595)
Blue (No. 15102 per FED-STD-595)
Yellow (No. 13538 per FED-STD-595)
White (No. 17875 per FED-STD-595)
4285A073
4285K123
4285A083
4624J01O
4624J03O
4624J020
A.P. Nonweller Co.
Oshkosh, WI 54903-1007 USA
Fax: 920-231-8085
A.P. Nonweiler Co.
Oshkosh, WI 54903-1007 USA
Fax: 920-231-8085
Phosphate Coating Solution
CrysCoat* - OC
(Zn(H2P04)2 • 2H20)
Oakite Products Inc.
Berkeley Heights, NJ 07922-2712
USA (V44389)
Lockwire
MS20995C20
SPN 13603-00
Local Vendor
(V96906)
Test Gas
1850 psig (12.76 MPa) min press
Oxygen
MIL-PRF-27210, Type I
(Refer to NOTE 1 and NOTE 2.)
Local Vendor
* CrysCoat is a Registered Trademark of Oakite Products Inc.
NOTE 1: Oxygen (MIL-PRF-27210, Type I) is specified in the TESTING AND FAULT ISOLATION section of the CMM.
If water pumped nitrogen or water pumped air (specified in Note 2) is used for the test gas, the applicable test
parameters must have the appropriate densny correction factors calculated and used, and the test eqUipment must
be calibrated for the test gas. (A copy of specification MIL-PRF-27210 is available from: Standardization Documents
Order Desk, BUilding 40, 700 Robbins Avenue, Philadelphia, PA 19111-5094 USA.)
NOTE 2:
•
Water pumped nnrogen per Federal Specification A-A-59503, Type I, Class I, Grade B. (A copy of Federal
Specification A-A-59503 is available from: General Services Administration, 1800 F Street, Washington, DC 20405
USA.)
Water pumped air, equivalent in purity to: MIL·PRF-27210, Type I
EFFECTIVITY:
All
35-32-18
Page 9005
20040415
..•
/SCOtf
Aviation
1:I./CO!scott
Technologies. Inc.
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
2. Consumable Materials (Continued)
•
Table 9002 (Continued)
Consumable Materials
MANUFACTURER
(VENDOR CODE)
MATERIAL
DESCRIPTION
Sealant
Clear
PIN RTV732
SPN 50067-00
Dow Corning Corp.
Midland, M1486BS-0097
USA (V719B4)
Red Etching Ink
PIN 5-1141
SPN 50792-01
Green Etching Ink
PIN AX GREEN
SPN 50791-01
Marking Device Manufacturing Co.
Philadelphia, PA 19133-2891
USA (V26040)
Speciality Ink Co. Inc.
Deer Park, NY 11729-4702
USA (V18029)
Oxygen
1850 psig (12.76 MPa) minimum pressure
MIL-PRF-27210, Type I
Local Vendor
Primer
Grade T
SPN 50349-01
loctite Corp.
Rocky Hill, CT 06067-3582
USA (V05972)
Adhesive
Loctite Corp.
Rocky Hill, CT 06067-3582
USA (V05972)
Grade 290 SPN 50004-20
Grade 222 SPN 50004-15
Grade 271 SPN 50004-18
I
Oxygen Compatible Lubricant
Krytoxh 240 AC
SPN 50527-00
E.I. du Pont de Nemours & Co. Inc.
Wilmington, DE 19898
USA (V23037)
Powdered lubricant
MoIyCoat**' Z
SPN 50021-01
Dow Coming Corp.
•
Midland, M148686-o997
USA (V71984)
•• Krytox is a Registered Trademark of E.!. du Pont de Nemours & Co.lnc .
... Molycoat is a Registered Trademark of Dow Coming Corp.
Subtask 35-32-18-998-001
3. Illustrations, Special Tools. and Fixtures
Top View
Side View
Core Wrench (PIN 800216- T91-1)
Figure 9001
EFFECTIVITY:
ALL
35-32-18
Page 9006
20040415
•
•
'>
•
t:qco/scott
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
ILLUSTRATED PARTS LIST
TASK 35-32-18-99C-803
1.
Introduction
This Illustrated Parts List section shows the illustrations and the authorized replacement parts for the
5500 Series and 5600 Series Portable Cylinder Assemblies (PCA).
A.
How To Use This Section
(1) If you do not know the part number you need:
(a) Find the part in the applicable figure.
(b) Note the ITEM number used for the part.
(c) Use the ITEM number to find the authorized replacement part number.
(2) If you know the part number, refer to the figure to be sure that the part illustration is the same as
the part that you need.
B. Numerical Index
The Numerical Index is used to locate parts in the unit when only the part number is known. The
Numerical Index is a cross-reference of numbers that include:
Airline Stock number, Figure No., Item No., and the number of parts required.
The character-sort-order for part numbers is: dashes first, letters A thru Z second, and then numbers
o thru 9.
•
C. Description of the Illustrated Parts List Entries
The section describes the information found in the Illustrated Parts List (IPL).
(1) FIG. ITEM
(a) Items not Illustrated
Items that are not shown in the figure have a dash in front of the item number.
(b) Alpha Variant Item Numbers
Alpha variants that are A-Z (except I and 0) added after the item number show configuration
differences in items, optional parts, parts that have had product improvement, or added
items.
(2) PART NUMBER
The numbers in this column are the part numbers that Scott gives to an item, the original part
number for an item that is from a vendor, or a common specification number (e.g., MIL
specification number) that is used for reference of an item. If a part number that Scott gives an
item is different than the vendor part number or the common specification number, the vendor
part number or the common specification number is shown in the PART NUMBER column and
the Scott part number (SPN) is shown in the NOMENCLATURE column for user convenience .
•
EFFECTIVITY:
ALL
35-32-18
Page 10001
20040415
..
tllCD/scott
/scott
Technologies.Inc. Aviation
~
55otV5600 SERIES PORTABLE CYLINDER ASSEMBLY • CMM & IPL
1. Introduction (Continued)
C.
•
Description of the Illustrated Parts List Entries (Continued)
Table 1, Sheet 1
PCA Configuration Matrix
5500-000-000
--
J-
Basic Series �
I
-
LII..-
Refer to Sheet 2
I
CYLINDER AND REGULATOR ASSY
CYLINDER FINISH
HARNESS ASSY
Regulator Assy PIN
Callout
Code
Cylinder
PIN
(Note 1)
Aluminum
Body
(Note 2)
Brass Body
Callout
Code
Finish
(Note 3)
Callout
Code
Harness
PIN
A
6084-01
5510-00
5510-10
1
A
801660-00
B
C
6084-02
6084-20
(Note 6)
6084-04
5510-00
5510-00
5510-10
5510-10
2
3
Gray-Green
(24159)
Green (14187)
Blue (15102)
B
C
801658-00
801662-00
5510-03
5510-13
5
D
801660-01
801660-03
801660-05
801663-00
6084-02
M
803177-03
M
6084-20
(Note 6)
6084-04
6084·04
5510-13
5510-13
5510-15
(Note 4)
5510-15
(Note 4)
5510-15
(Note 4)
5510·17
5510-19
(Note 4)
5510-17
5510-19
(Notes 4 & 5)
803199-04
E
F
G
L
5510-03
5510-03
5510-05
(Note 4)
5510-05
(Note 4)
5510-05
(Note 4)
5510-07
5510-09
(Note 4)
6
9
J
6084-06
6084-07
6084-01
N
805436-01
P
801808-05
801807-01
D
F
G
,
N
P
Q
S
6084-06
6084-34
T
21507-06
Green (14187)
and
Yellow (13538)
Green (24062)
Green (24062)
Q
5
801808-01
801807-02
T
U
V
W
X
y
801807-03
801808-02
801808-03
803177-01
No Harness
803177-02
R
•
Note 1: Cylinder PIN's 6084-01, -02 and -20 have 0.500 - 14 ANPT threads.
Cylinder PIN's 6084-04 -06, -07, -34 have 1.00 - 11.5 ANPT threads.
Cylinder PIN's 21507·06 has 0.750 - 16UNF-2A threads.
Note 2: After Apr 1/82 the regulators shown in this column were not procurable.
Note 3: Cylinder finish (paint) number (shown in parentheses) in this column is per specification FED STD-595.
Note 4: These regUlators are used when 3 outlet assembly ports are required.
Note 5: PCA SN 134269 and subsequent use regulator PIN 5510-19 (three outlet assembly ports).
PCA SN's before 134269 for Callout Code '5' used regUlator PIN 5510-17 (two outlet assembly ports).
Note 6: Cylinder PIN 6084-03 is replaced by cylinder PIN 6084-20.
EFFECTIVITY:
ALL
35-32-18
Page 10002
20040415
•
•
"
1:qco /scott
Technologies. Inc.
/SCOtf
Aviation
CMM & IPL
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
...
1. Introduction (Continued)
C.
Description of the Illustrated Parts List Entries (Continued)
Table 1, Sheet 2
PCA Configuration Matrix
5500Basic Series
Refer To Sheet 1
OUTLET FLOW RATE SETTING
Note 1)
•
I
I
I
OUTLET STYLE
(Notes 3 and 5)
ALTITUDE SETIING
Callout
Code
Flow
Ipm atNTPD
(Note 2)
Callout
Code
Altitude
feet (meters)
Callout
Code
Outlet
PIN
Outlet
Type
A
0.5
0
A
5009 Series
Constant Flow (Metered)
B
2.0
5
0(0)
(Note 4)
5,000 (1,524)
B
5041 Series
Constant Flow (Metered)
C
2.5
10
10,000 (3,048)
C
Constant Flow (Metered)
E
3.0
15
15,000 (4,572)
D
5052-00
(Note 6)
5507 Series
F
4.0
20
20,000 (6,100)
E
8572.02
Full Flow (Non-Metered)
G
7.0
23
23,000 (7,010)
K
6818-01
Plug
H
8.0
25
25,000 (7,620)
L
Full Flow (Non-Metered)
L
4.5
30
30,000 (9,144)
M
800503.00
(Note 7)
802856-01
X
0
N
y
FULL
P
36728-01
(Note 8)
802863-02
R
10006017
S
10008298
Full Flow (Non-Metered)
(Supsds DPB153)
Full Flow (Non-metered)
(Cessna Type)
Full Flow (Non-Metered)
(Lockheed Type)
Full Flow (Non-Metered)
Note
Note
Note
Note
1:
2:
3:
4:
Note 5:
Note 6:
Note 7:
Note 8:
•
:r~
_
DOD-DOD
-P""----
Constant Flow (Metered)
Full Flow (Non-Metered)
There may be 1, 2, or 3 OuUet Flow Rate Setting Callout Codes in the PIN.
Flow at 14.7 psia (760 mm Hg) at 32°F (DOC).
Outlet Style Callout Codes E, L, M, N, P, R, and S are full flow (non-metered) ouUets.
Altitude Setting Callout Code 0 identifies full flow (non-metered) outlets (Outlet Style Callout Codes E, L, M, N, P,
RorS).
There may be 1 or 2 Outlet Style Callout Cades in the PIN, however only one configuration of constant flow (metered)
Outlet Style (Callout Code A, B, C or D) is allowed on a PCA.
After Oct 1181 this outlet was not procurable.
After Jun 22195 this outlet was not procurable.
After Jan 01/01 outlet SPN 36728-01 replaced outlet SPN DPB153 .
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10003
20040415
!scott
1:'-/caJscott
Technologies. Inc.
--•
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
1. Introduction (Continued)
C.
•
Description of the Illustrated Parts List Entries (Continued)
Table 1, Sheet 3
PCA Configuration Matrix
-DODD-DOD
,---- LII..... Refer To Sheet 4
T
5600
Basic Series
I
RESPIRATOR
REGULATOR ASSY
HARNESS ASSY
Regulator Assy PIN
Aluminum
Body (Note 2)
Brass Body
Callout
Code
Finish
(Note 3)
Callout
Code
Harness PIN
6379-2C
(Demand)
6379-2D
(Demand)
A
6084-01
5510-00
5510-10
1
A
801660-00
B
6084-02
5510-00
5510-10
2
B
801658-00
800649-00
(Demand!
Press-Demand)
800649-01
(Demand!
Press-Demand)
C
6084-20
5510-03
5510-10
3
Gray-Green
(24159)
Green (14187)
and
White (17875)
Blue (15102)
C
801662-00
D
60B4-G4
5510-03
5510-13
5
D
801660-01
G
801660-Q3
801660-OS
6084-20
p
6084-G4
5510-13
5510-15
(Nole 4)
5510-15
(Note 4)
5510-19
(Note 4)
6
9
M
5510-03
5510-05
(Note 4)
5510-05
(Note 4)
E
J
6084-07
6084-01
Green (14187)
and Yellow
(13538)
Green (24062)
Green (24062)
1
9
CYLINDER FINISH
Cylinder
PIN
(Note1)
Reg PIN
8
CYLINDER AND REGULATOR ASSY
Callout
Code
Callout
Code
2
I
(Type)
F
•
Note 1: Cylinder PIN's 6084-01, -02 and -20 have 0.500 -14 ANPT threads.
Cylinder PIN's 6084-04, and -07 have 1.00 - 11.5 ANPT threads.
Note 2: After Apr 1/82 the regulators shown in this column were not procurable.
Note 3: Cylinder finish (paint) number (shown in parentheses) in this column is per specification FED 5TD-595.
Note 4: These regulators are used when two ouUet assembly ports (in addition to the respirator regulator port) are required.
EFFECTIVITY:
ALL
35-32-18
Page 10004
20040415
•
•
-;
...
1:I.ICO/SCOtl
!SCOft
Technologies. Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
1. Introduction
CMAt & IPL
(Continued)
C. Description of the Illustrated Parts List Entries (Continued)
Table 1. Sheet 4
PCA Configuration Matrix
5600 -DODD-ODD
Basic Series
Refer To Sheet 3
OUTLET FLOW RATE SETTING
(Nole 1)
Flow
Ipm alNTPD
Callout Code
A
0.5
•
:r~---""-P"'"
_
I
AL TlTUDE SETTING
Mitude
feet (meters)
Callout Code
0(0)
0
(Note 2)
5,000 (1,524)
5
I
OUTLET STYLE
(Nole3)
OUUet
Tvoe
Callout Code
A
Ol1lJet PIN
5009 Series
Constant Flow (Metered)
B
5041 Series
Constant Flow (Metered)
Constant Flow (Metered)
B
2.0
C
2.5
10
10,000 (3,048)
C
D
2.7
15
15,000 (4,572)
D
5052-00
(Note 4)
5507 Series
E
3.0
20
20,000 (6,100)
E
8572-02
Full Flow (Non-Metered)
F
4.0
23
23,000 (7,010)
K
6818-01
Plug
G
7.0
25
25,000 (7,620)
M
802856-01
Full Flow (Non-Metered)
H
8.0
30
30,000 (9,144)
N
36728-01
(Note 5)
Full Flow (Non-Metered)
(Replaces DPB 153)
K
L
X
Y
0.7
4.5
0
Full
Constant Flow (Metered)
Note 1: There may be 10r 2 Outlet Flow Rate Setting Callout Codes in the PIN.
Note 2: Altitude Setting Callout Code 0 identifies full flow (non-metered) outlets (Outlet Style Callout Codes E, M, or N).
Note 3: There may be 1 or 2 Outlet Style Callout Codes in the PIN, however only one configuration of constant flow
(metered) Outlet Style (Callout Code A, B, C, or D) is allowed on a peA.
Note 4: After Oct 1/81 this ouUet was not procurable.
Note 5: After Jan 01/01 this SPN DPB153 was not procurable. Outlet SPN 36728-01 replaces outlet SPN DPB153 .
•
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10005
20040415
t'lco/scott
/scott
Technologies. Inc. Aviation
550(115600SERIES PORTABLE CYLINDER ASSEMBLY·
<"
•
CUM & If!
1. Introduction (Continued)
•
C. Description of the Illustrated Parts List Entries (Continued)
Table 1, Sheet 5
PCA Configuration Matrix
5009
or
5041 or
DO
-- --
5507
Basic Series ~
FLOW RATE SETTING
\
AlTITUDE SETIING
CalloutCode
Flow
Ipmat NTPD
CalloutCode
.5
0.5
5
5,000 (1,524)
.7
0.7
10
10,000 (3,048)
2
2.0
15
15,000 (4,572)
2.5
2.5
20
20,000 (6,100)
2.7
2.7
23
23,000 (7,010)
3
3.0
25
25,000 (7,620)
4
4.0
30
30,000 (9,144)
4.5
4.5
7
7.0
8
8.0
EFFECTIVITY: ALL
35-32-18
Altitude
feet(meters)
Page 10006
20040415
•
•
•
...
•
1:'1ca/scott
Technologies.
Inc.
/SCOtf
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
1.
CMM & 'PL
Introduction (Continued)
C. Description of the Illustrated Parts List Entries (Continued)
(3) AIRLINE STOCK NUMBER
This column has space available for a number, up to eleven characters in length, given by the
airline.
(4) NOMENCLATURE
This column has the description of the part and may contain the following:
(a) Abbreviations
The abbreviations in this column in the table are shown in the List of Abbreviations in the
INTRODUCTION section of this manual.
(b) Level of Indenture
This information shows the relationship of one part to another. An example is shown:
123 (Assembly Number)
• SUbassembly Top No.
Attaching Parts for the Subassembly Top No. or Assembly Item
***
• Assembly Item
•• Sub-Subassembly Top Number
•
Attaching Parts for the Sub-Subassembly Top No. or Subassembly Item
***
•• Subassembly Item
NOTE: The three asterisks are used to separate the attaching parts of one Item from
another Item.
(5) EFFECTIVITY CODE
When the IPL applies to more than one top assembly, each top assembly is identified with an
alpha code (A, B, C, etc.). If a part number, subassembly, or item is identified with an alpha
code, that part can only be used with the top assembly that has that (EFF) CODE.
Any item or subassembly that does not have an (EFF) CODE may be used on any top assembly.
(6) UNITS PER ASSEMBLY
This column shows the number of parts that are used in the assembly .
•
EFFECTIVITY:
ALL
35-32-18
Page 10007
20040415
1:I./CCI/scott
Technologies. Inc.
!scott
55DOIS600SERIES PORTABLE CYLINDER ASSEMBLY·
1.
•
Aviation
CMM & IPL
Introduction (Continued)
D. Vendor Codes
The following is a list of the vendors that supply items in this section of the manual. Items that do not
specify a vendor code are available from Scott Aviation. All items, including standard parts, are
available from Scott Aviation.
CODE
V05AY8
V21343
V49315
V53655
V64528
V66295
V80205
V88044
V95138
V96906
EFFECTIVITY:
ALL
NAME AND ADDRESS
Aerospace Standards (AS)
Warrendale, PA 15096-0001
USA
Owens-Coming Fiberglas Corp.
Huntingdon, PA 16652-0382
USA
Puritan Bennett Corp.
Shawnee Mission, KS 66225
USA
Scott Aviation
Lancaster, NY 14086-9502
USA
Sierra Precision
Rancho Cucamonga, CA 91730-3007
USA
Wiltek ManufactUring Company
Galesburg, IL 61401
USA
National Aeronautical Standards (NAS)
Aeronautical Industries Association of America
Washington, DC 20005
USA
Aeronautical Standards (AN)
Department of Navy and Air Force
USA
Perfecting Corp.
Charlotte, NC 28206
USA
Military Standards (MS)
USA
35-32-18
•
Page 10008
20040415
•
•
""
tl../co/scott
Technologies,Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYlINDER ASSEMBLY - CMAt & IPL
TASK 35-32-18-99C-804
2.
Overhaul
Kits
Overhaul
kits are available
A.
Obtaining
Overhaul
for the 5500 and 5600 Series PCAs.
Kits
To buy Overhaul Kits or other parts for the 5500 and 5600 Series PCAs. contact any Scott
Authorized Distributor. Refer to the Scott web site (http://www.scottaviation.com)
for a list of Scott
Authorized Distributors.
B. 5500 Series PCA Overhaul Kit
Table 2 lists the parts included in Overhaul Kit PIN 28022-00. This kit includes all parts necessary to
overhaul one 5500 Series PCA with the exception of the safety disc (PIN 6364-00 or PIN 10003742)
and gasket (PIN 6555-00). The safety disc and gasket must be replaced during an overhaul. Refer to
IPL Figures 1A thru 1G for the part number of the safety disc used with your PCA. Other parts must
also be replaced if they are defective.
Table 2
Overhaul Kit PIN 28022-00
5500 Series PCA
Kit Item Number
•
•
Part Number
Quantity
Nomenclature
Per Kit
1
5032-01
DIAPHRAGM
1
2
5517-00
SEAT,PTFE
1
3
4
FILTER
WASHER,SAFETYPLUG
1
5
5522-00
6370-00
5562()..01
PACKING,PREFORMED
1
6
55620-02
PACKING,PREFORMED
1
7
5056-00
PLATE,IDENTIFICATION
1
8
22427-01
PLATE,IDENTIFICATION
1
1
9
803129-01
SEATASSEMBLY
1
10
802883-01
HEADASSEMBLY
1
11
59553-00
SCREW(CRESWI PLASTICINSERT)
(#2-64THD x 0.188in. LNG}
2
12
37008-02
SCREW,SET,LOCKING,OVALPOINT
(114-20THDUNC3Ax 0.375LNG)
EFFECTIVITY:
ALL
35-32-18
1
Page 10009
20040415
1:IIeD/scott
Technologies. Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
2.
•
CMM & IPL
Overhaul Kits (Continued)
C. 5600 Series PCA Overhaul Kit
Table 3 lists the parts included in Overhaul Kit PIN 28021-00. This kit includes all parts necessary to
overhaul one 5600 Series PCA with the exception of the safety disc (PIN 6364-00) and gasket (PIN
6555-00). The safety disc and gasket must be replaced during an overhaul. Other parts must also be
replaced if they are defective.
Table 3
Overhaul Kit PIN 28021-00
5600 Series PCA
Killtem Number
Part Number
Nomenclature
Quantity Per Kit
1
5032-00
DIAPHRAGM
1
2
5517-00
SEAT, PTFE
1
3
5522-00
FILTER
1
4
5601-00
ELBOW ASSEMBLY (Refer to Note 1)
1
5
33529-009
CONNECTOR, TUBE (ALUMINUM)
1
6
6066-01
WASHER, FLAT (CRES)
(0.281 in. 00 x 0.125 in. 10x 0.031 in. THK)
2
7
6370-00
WASHER, SAFETY PLUG
1
8
13374-00
DIAPHRAGM ASSEMBLY
1
9
6055E
VALVE ASSEMBLY, DEMAND
1
10
59553-00
SCREW (CRES W/PLASTIC INSERT)
(#2-64 THO x 0.188 in. LNG)
2
11
MS35207-201
SCREW, PAN HEAD (V96906) (CAD STEEL PLATED)
(#2-64 THO x 0.125 in. LNG) (SPN 33326-201)
2
12
55620-01
PAC~NG,PREFORMEO
1
13
55620-02
PAC~NG,PREFORMED
1
14
803129-01
SEAT ASSEMBLY
1
15
802833-01
HEAD ASSEMBLY
1
16
22427-01
PLATE, IDENTIFICATION
1
17
5056-00
PLATE, IDENTIFICATION
1
18
13362-00
GASKET, VALVE SEAT
1
19
MS35333-30
WASHER, LOCK (V96906) (CAD STEEL PLATED)
(#4 D1Ax 0.017 in. THK) (SPN 33460-036)
2
20
6812-00
SCREEN (BRASS)
1
21
37008-02
SCREW, SET, LOCKING, OVAL POINT
(1f4-20 THD x 0.375 LNG)
1
22
33321-213
SCREW, PAN HO
(#4-40 THO x 0.250 LNG)
2
•
NOTE 1: Elbow Assembly PIN 5601-00 is used only on PCA's with 4, 7, and 11 cu. ft. cylinders. Refer to IPL Figures 1H or 1J for the Elbow
Assembly to use on your PCA if your PCA has a cylinder larger than 11 cu. ft.
EFFECTIVITY:
All
35-32-18
Page 10010
20040415
•
•
...
•
...
1:qca/scott
Technologies. Inc.
jSCOtf
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
TASK 35-32-18-99C-B05
3.
Numerical Index
The following is a Numerical Index for this seclion.
Numerical Index
PART NUMBER
AD1983
AS3582-008
AS4860D01
A1215-1
A1119
A11208
A1126
EC9-5U
AIRLINE STOCK NO.
3
10
10
3
6
3
3
4
5
7
8
3
3
1A
18
1C
1D
1E
1F
1H
1J
9
1A
1A
18
1C
1C
10
1E
1E
1E
1H
1J
3
3
3
3
9
9
1A
1C
1E
1H
1J
1A
1C
1E
MS20470A2-2
MS21318-7
•
MS27769S2
MS35206-212
MS35206-213
MS35207-201
MS35333-36
MS3565Q-304
NAS1149C0332R
10001018
10001019
•
EFFECTIVITY:
FIGURE
ALL
ITEM NO.
-310
110
10
205
80
-280
220
70
40
20
20
100
130
65
65
65
65
65
65
-65
-65
580
-395
-396
-395
-395
-396
-395
-395
-396
-397
-395
-395
70
250
230A
260
-40
-50
-40
-40
-40
-40
-40
45
TTLREQ'D
1
1
1
1
1
1
1
AR
AR
AR
AR
2
2
2
2
2
2
2
2
2
2
2
1
1
1
1
1
1
1
1
1
1
1
3
2
2
2
1
1
1
1
45
1
1
1
1
1
45
1
35-32-18
Page 10011
20040415
'flleo/scott
/scott
Technologies. Inc. Aviation
•
550015600 SERIES PORTABLE CYLINDER ASSEMBLY - CMM & IPL
Numerical Index
PART NUMBER
AIRLINE STOCK NO.
10001019 (Continued)
10001020
10001112
10001296
10001297
10001493
10001494
10002684
10003305
10003566
10003742
10004838
10004839
10004840
10004841
10004844
10004845
10005272
10005326
10005511
10005614
10005615
10005616
10005617
10005750
10005922
FIGURE
ITEM NO.
1H
1J
1A
1C
1E
1H
1J
5
1H
1J
3
5
5
45
-45
6
6
-40
-30
1G
11
11
11
11
10
1A
18
1C
80
20
100
80
40
140
10
-30
1E
1F
1G
1H
-30
9
1J
1C
1G
1A
18
1C
10
1E
1F
EFFECTIVITY:
ALL
80
10
10
10
10
10
10
9
1A
1C
1E
1H
10006017
10006442
10006936
-50
·50
-50
-50
130
125
125
120
70
-200
500
340
340
340
340
270
130
120
90
100
70
80
9
I
-SO
-30
-30
-30
-30
-30
-30
-30
355
65
-20
-20
-20
-20
-20
-20
35-32-18
TTLREQ'D
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
2
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
Page 10012
20040415
•
•
•
..
tyco!scott
Technologies.
/scott
Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
Ilnricy
PART NUMBER
PART NUMBER
PART NUMBER
10006936 (Continued)
10007887
10008594
10008595
10008596
10008601
10008602
10008603
10008611
10008612
10008613
10008614
10008615
10008616
10008644
10008660
10008774
10008915
10008934
10008947
10009071
10009072
•
Inc.
\
10009255
,
1G
9
7
7
7
7
7
7
13
13
13
13
13
13
11
7
7
•
10
so
90
BO
1E
1F
1G
1A
1A
1B
1B
1C
ALL
60
130
150
25A
25A
20A
20A
20A
20A
20A
20A
20A
30A
30A
30A
30A
30A
30A
30A
30A
30A
60
210
35
35
35
35
35
35
35
70
75
70
75
70
10
EFFECTIVITY:
60
100
110
120
20
70
50
40
30
4
7
1H
1J
1A
1B
1C
10
1E
1F
1G
1A
1B
1C
1E
1F
1G
1H
1J
11
3
1A
18
1C
13160-00
·20
100
130
70
5
10
10009328
10009359
10009374
PART NUMBER
35-32-18
PART NUMBER
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
Page 10013
20040415
-tqca/scott
Technologies. Inc.
/scott
-
•
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
·'nnp'lI
PART NUMBER
PART NUMBER
13160-00 (Continued)
4
13161-00
13162-00
13164-00
13362-00
13374-00
13753-00
14807-00
21217-11
21217-12
21217-13
21217-14
21507-06
22427-01
22445-01
23274.Q3
23274-05
23393-01
23394-01
24823-00
24825-00
26565-00
26567-00
2661-03
2661-04
27170-01
27170-02
27170-03
27170-04
EFFECTIVITY: ALL
PART NUMBER
PART NUMBER
PART NUMBER
1C
1E
1E
1G
1H
1H
1J
1J
75
70
75
70
70
75
70
75
70
70A
75
,70A
75A
70A
75A
70B
70B
75B
70B
75B
-330
280A
200
30
-25
20
40
70
80
570
20
1
1
1
1
1
1
1
1
10
1E
1F
1H
1H
1J
1J
1E
1H
1H
1J
1J
3
3
3
12
2
12
12
12
12
1G
9
9
9
9
9
9
5
5
9
9
60
-30
30A
140
80
100
170
230
250
1
1A
1B
1C
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
RF
RF
RF
RF
RF
1
RF
1
1
290
1F
-310
510
9
-530
1
9
9
-520
-540
1
1
35-32-18
•
1
12
12
12
12
12
9
12
9
9
10
•
Page 10014
20040415
•
•
...
•
tl.lc:a/scolt
jSCDtt
Technologies.Inc. A tliation
5500'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
IlnrillY
PART NUMBER
PART NUMBER
27170-05
27434-01
27511-01
280OC10A
2800C14A
289-601-211
6
11
11
11
2
2
2
2
4
4
4
4
4
4
4
4
4
2
29550-00
29551-00
29552-00
29553-01
29554-00
29555-00
29556-00
29557-00
29558-01
29559-00
29567-00
33326-201
33529-009
4
3
1H
1J
11
11
13
1A
18
1C
1C
10
10
1E
1E
1H
1J
10
11
2
2
9
9
9
9
9
1A
5
1A
5
1A
5
1A
1C
36588-04
36636-01
36728-01
36862-05
36874-01
36879-01
37008-01
37008-02
5002-00
5003-00
5005-03
5009-.5-15
5009-.5-23
5009-.5-25
5009-00
•
EFFECTIVITY:
PART NUMBER
9
289-601-213
•
CMM & IPt
ALL
PART NUMBER
-550
-20
50
120
110
35
40
36
41
120
140
150
160
190
170
180
20
10
-30
110
230A
100A
100A
70
90
-1
345
PART NUMBER
1
1
1
1
1
1
2
1
2
1
1
1
1
1
2
2
1
1
1
1
1
1
1
1
1
RF
1
1
1
345
345
346
345
346
345
346
345
345
40
1
1
1
1
1
1
30
2
45
50
-370
370A
480
400
380
305
-2
30SA
1
2
1
1
1
1
1
1
-2A
3058
-28
300
300
35-32-18
1
1
RF
1
RF
1
RF
1
1
Page 10015
20040415
t:L/CCJ/scott
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & #PL
Inrll'Y
PART NUMBER
5009-00 (Continued)
5009-01
5009-2.5-20
5009-2.5-23
5009-2.5-25
5009-2.5-30
5009·2·10
I
5009-2·15
5009-2-20
5009-2-20
5009-2-23
PART NUMBER
PART NUMBER
1B
1C
10
1E
1F
1H
1J
5
5
10
10
1H
5
1B
5
1A
18
5
1A
1A
5
1A
1B
1E
1E
1F
5
1A
1A
1C
10
10
5
1A
1B
1C
1C
1E
1E
1H
5
1A
1A
1B
1C
10
1E
1E
1F
1H
5
1A
5009-2-25
EFFECTlVITY:
ALL
.
~'
•
PART NUMBER
300
300
300
300
300
300
300
-1
·50
3050
305E
305B
-2K
305E
-2L
305M
305F
-2M
305N
305P
-2N
305C
305
305
30SA
305
-20
3050
305E
305
305
305A
-2E
305F
305A
305A
305B
3056
305C
305
-2F
305G
305H
3058
305C
3056
3050
305E
305A
30SA
-2G
305J
35-32-18
PART NUMBER
1
1
1
1
1
1
1
RF
1
1
1
1
RF
1
RF
1
1
RF
1
1
RF
1
1
1
1
1
RF
1
1
1
1
1
RF
1
1
1
1
1
1
1
RF
1
•
•
1
1
1
1
1
1
1
1
RF
1
Page 10016
20040415
•
•
...~
tqca/scotl
Technologies. Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY· eMM & IPL
Numerical Index
PART NUMBER
5009-2·25 (COlltinued)
PART NUMBER
PART NUMBER
1A
1B
1C
10
1E
1E
5
1A
18
1C
1E
1E
1J
5
1A
1C
500902·30
5009-3-20
10
1E
1E
1E
1H
S
1C
1E
1H
5
1A
1A
1C
10
S
1A
1E
1E
1J
5
1E
5
1E
1E
1E
5
1A
18
1C
1C
1E
1F
1J
5
1C
5
5009·3·23
•
5009-3-25
5009-3-30
5009-3-30
5009-4.5-23
5009-4.5-30
5009-4-10
5009-4-15
•
EFFECTIVITY:
ALL
PART NUMBER
305K
305C
3050
305C
305F
305G
-2H
305l
3050
30SE
30SH
305J
305
-2J
3050
305F
305F
305K
305l
305M
305C
-2P
305G
30SN
3050
-20
305R
3055
30SH
305G
-2R
305T
305P
305Q
30SA
·25
305Y
-2Z
30SZ
306
306A
-3
305U
305G
30SJ
305K
305R
3058
3058
-2T
305l
-2U
35-32-18
PART NUMBER
1
1
1
1
1
1
RF
1
1
1
1
1
1
RF
1
1
1
1
1
1
1
RF
1
1
1
RF
1
1
1
1
RF
1
1
1
1
RF
1
RF
1
1
1
RF
1
1
1
1
1
1
1
RF
1
RF
Page 10017
20040415
'f:'-/ca/scott
Technologies. Inc.
-
/SCOft
Aviation
5504'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
t
CMM & /PL
Numerical Index
PART NUMBER
PART NUMBER
5009-4·20
PART NUMBER
1A
18
18
1C
1C
1E
1H
1J
5
1A
1A
1B
1C
1C
5009-4-23
10
1E
1E
1F
1H
1J
5
1A
18
1C
5009-4-25
10
I
1E
1E
1E
1H
PART NUMBER
305V
305H
305J
305M
305N
1
1
-2V
RF
305W
305X
305K
305P
3050
305H
305T
305U
305C
305F
3050
-2W
305Y
305L
305R
30SJ
305V
305W
305X
1
1
1
1
1
1
1
1
1
1
1
RF
1
1
1
1
1
1
1
1
RF
1
1
1
3000
1C
305V
3068
305H
30SJ
5009-8-23
1E
1J
1J
5
1C
5009·7-25
5009-7-30
EFFECTIVITY:
ALL
1
1
305E
30se
5009·8·2{)
5009-4·30
5009·7·23
1
1
1
-2X
305Z
305M
305S
30SH
30SE
305F
-2Y
3051
305J
-3A
30SK
-38
306
305U
305G
-3C
50094-30
PART NUMBER
1
30SS
1A
18
1C
1H
1J
1J
5
1C
1H
5
1H
5
1A
1C
1J
5
5
•
1
1
1
RF
1
1
RF
1
RF
1
-3D
1
1
RF
1
1
1
1
RF
305W
1
35-32-18
•
Page 10018
20040415
•
•
••
•
-tqca/scott
!scott
Technologies, Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMAt & IPL
Numerical Index
PART NUMBER
PART NUMBER
5009-8-23 (Continued)
5009-8-30
5013-00
5013-01
5014-00
5014-01
PART NUMBER
1E
5
1D
1D
5
5
8
4
4
7
5
8
4
7
•
9
9
9
9
5016-00
5023-00
5027-00
5028-00
5030-01
5031-00
5032-01
5033-00
5034-00
5041-.5-15
9
9
9
9
9
1A
1A
4
1E
4
1A
18
1C
1E
1G
1H
1J
4
4
lA
1G
1G
4
1A
18
1C
lC
1E
1E
1E
1H
4
1A
18
5041·.5·20
5041-00
5041-01
5041-2.5-30
5041-2.5-30
5041-2-20
5041-2-23
•
EFFECTIVITY:
ALL
PART NUMBER
306C
·3E
305K
305L
-3F
30
30
60
80
30
20
10
50
10
-158
-159
490
470
450
440
430
420
410
315
315A
-2
315
-2A
310
310
310
310
300
310
310
-1
90
315G
305
305A
-2F
315C
315
315
315A
315A
3158
315C
315
-28
315E
315A
35-32-18
PART NUMBER
1
RF
1
1
RF
1
2
1
1
2
1
1
1
1
1
1
1
1
1
1
1
3
1
1
1
RF
1
RF
1
1
1
1
1
1
1
RF
1
1
1
1
RF
1
1
1
1
1
1
1
1
RF
1
1
Page 10019
20040415
1:L/CO/SCOtl
/scott
•
Technologies. Inc. Aviation
5SDOI5600SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
Numerical
PART NUMBER
PART NUMBER
5041-2-23 (Continued)
5041-2-25
5041-2-30
5041-3-20
5041-3-23
5041-4-20
5041-4-23
Index
PART NUMBER
PART NUMBER
PART NUMBER
1C
1H
4
1A
4
1C
4
1A
18
1C
1E
1H
1J
4
1H
4
1A
18
1C
1E
1H
1J
4
1A
18
1C
1H
3158
315A
-2C
315F
-20
315C
-2E
315H
3158
3150
3150
3158
315
-2G
315C
-2H
315J
315C
315E
315E
3150
315A
-2J
315K
3150
315F
315E
-2K
315L
-2L
315G
-2M
315M
315H
315F
-2N
315J
-2P
30
40
320
330
340
370
-1
1
1
RF
1
RF
1
RF
1
1
1
1
1
1
RF
1
RF
1
1
1
1
1
1
RF
1
1
1
1
RF
1
RF
1
RF
1
4
5041-4-25
1A
5041-4-30
1C
4
1A
1C
1E
4
5041-7-20
4
5041-7-30
1C
4
4
4
5042-01
5042-02
5043-14
9
9
9
1H
5052-00
8
8
9
5052-02
5056-00
5057-00
1A
18
1C
10
EFFECTIVITY:
ALL
-50
350
55
55
55
55
35-32-18
•
1
1
RF
1
RF
1
1
1
1
1
1
RF
1
1
1
1
1
1
Page 10020
20040415
•
•
...,
1:'1Co/scott
!scott
Technologies. Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
Numerical Index
PART NUMBER
PART NUMBER
5057-00 (Continued)
5057-01
5057-14
5058-00
5065-02
5065-03
5065-04
5065-06
5065-08
5065-10
5067-01
5067-02
5067-03
5067.04
5067-Q5
5067-06
5067-07
50775 SERIES
•
•
eM'" & IPL
8
8
8
8
8
8
8
4
5
7
9
5092-00
5093-01
5500A SUB SERIES
5500A1M15A
5500A1MB23A
5500A1AB15A
5500A1AB20A
5500A1ABB23A
5500A1ABB25A
5500A1ABBF20B
5500A1ABC30A
5500A 1ABE20A
5500A1ABE2OB
5500A1ABF10A
5500A1ABF20B
5500A 1ABF23A
5500A1ABF23B
5500A1ABF230
5500A1ABF25A
5500A1ABF25B
5500A1ABF30A
5500A1AC30B
5500A1AE20A
5500A1AE20B
5500A1AF2OA
5500A1AF20B
5500A1AF200
5500A1AF23A
EFFECTIVITY:
PART NUMBER
1E
1F
9
1H
1J
9
8
5
5
5
5
5
2
2
ALL
PART NUMBER
55
55
570
-60
-60
560
40
140
160
150
110
90
15
20
60
70
120
80
110
100
90
200
180
160
-180
9
170
1
lA
lA
lA
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
lA
lA
1A
1A
1A
1A
1A
1A
-1A
-1B
-1
-15
-11
-10
-1E
-1C
-iF
-1G
-1H
-1J
-1K
-lL
-1M
-1N
-1P
-10
-1R
-1U
-w
-1W
-1X
-1Y
-1Z
-2
35-32-18
PART NUMBER
1
1
1
1
1
1
1
1
1
1
1
·1
1
2
1
1
1
1
1
1
1
1
1
1
1
1
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
Page 10021
20040415
1:'-/ca/scott
Technologies. Inc.
..
_
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
Numerical Index
PART NUMBER
5500A1AF25A
5500A 1AF25AN
5500A1AXOK
5500A 1AVYOE
5500A 1BF23A
5500A1MM15B
5500A 1NBF23A
5500A1OB30AD
5500A 1OB30D
5500A 1OB30DA
5500A 1REE25A
5500A 1SB20A
5500A 1SCC30A
5500A1TBF20B
5500A 1UBF23A
5500A 1UBF25A
5500A 1UEE25A
5500A 1UF30AN
5500A 1VBF20B
5500A 1VBF23B
5500A 1VBF25B
5500A WF20BM
5500A 1WBF23A
5500A 1WBF25A
5500A 1WBf30A
5500A lXBF20B
5500A1XFF23A
5500A1YBF20B
5500A3ABF23A
5500A5ABG20B
5500A6ABF23A
5500A6ABF23B
5500A6ABG20B
5500A6AF2OB
5500A6PFF23A
5500A6SB30A
5500A6UE30A
5500A6WBB 15A
5500A6WBB23A
5500A6WBB25A
5500A6WFF23A
5500A6WF30AP
5500A9AB30A
55OOA9SAC25A
5500A9SBF30A
5500A9SG30A
5500A9WEE25A
5500A9XF23A
55008 SUB SERIES
5500B1AB30A
5500B1ABE20B
5500B 1ABF20A
EFFECTIVITY:
PART NUMBER
ALL
PART NUMBER
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1A
1
1B
1B
1B
PART NUMBER
-2A
-2B
-2C
-20
-2E
-2F
-2G
-2H
-2J
-2K
-2l
-2M
-2N
-2P
-20
-2R
-2S
-2T
-2U
-2V
-2W
-2X
-2Y
-2Z
-3
-3A
-3B
-3C
-3D
-3E
-3F
-3G
-3H
-3J
-3K
-3L
-3M
-3N
-3P
-30
-3R
-3S
-3T
-3U
-3V
-3W
-3X
-3Y
-1B
-1G
-1
-1A
35-32-18
PART NUMBER
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
Page 10022
20040415
•
•
•
•
•
•
..
-tL/ca/scott
!scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
eMM & IPL
Numerical Index
PART NUMBER
PART NUMBER
5500B1ABF20B
5500B1 ABF20D
550081A8F23A
550081A8F238
5500B 1A8F25A
550081 ACF23A
550081ACF25A
550081AF200
5500B1AF23A
550081 AF30A
550081 AFF20A
5500B1AYOP
5500B1AYVOE
5500B1SB20A
5500B 15820AP
5500B 1UBF23A
55OO81VBE2QB
5500B1VBF20B
5500B1WBF1OA
550001 WBF20A
550081XYOE
550081XYYOE
550083BF25A
5500B6CBF25A
5500B6UBF25A
\ 5500B6UF30AN
5500C SUB SERIES
55ooC1AB23A
5500C1A8B20B
5500C1 ABF20A
5500c1ABF20B
5500C1 ABF20D
55OOC1ABF23A
55OOC1ABF23B
55OOC1ABF23D
5500C1ABF30A
5500C1ABG23A
5500C1AE20BN
5500C 1AE23AN
550OC1AEG23A
550OC1 AEY2DBM
550OC1AF20B
550OC1AF23A
5500C1 AF23AP
5500C1AF25A
5500C1 AFF20A
5500C1 AFF23A
5500C1 AFG23A
5500C1 AFH23A
5500C1AFY30BN
5500C1AXOK
5500C1AYOE
EFFECTIVITY:
ALL
PART NUMBER
PART NUMBER
PART NUMBER
1B
18
18
18
18
18
18
18
18
18
18
18
16
1B
18
18
18
18
18
18
18
18
18
1B
1B
18
1
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
-1B
-1C
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
-10
-1E
-1F
-1H
-1J
-1L
-1M
-1N
-1K
-10
·1P
-1R
·15
-1T
·1U
-1V
-1W
-1X
-1Z
-1Y
-2
-2A
-2B
-2C
-1C
-1J
-1
-1A
·18
-1C
-10
-1E
-1F
-1G
-1H
·1M
·1N
-1K
-lL
·1U
-w
-lW
-1X
-1P
-1Q
-1R
-15
-1T
-1Y
-2B
35-32-18
Page 10023
20040415
"t'-/ca/scott
Technologies. Inc.
/scott
Aviation
~J
•
550015600 SERIES PORTABLE CYLINDER ASSEMBLY • CMM & IPL
Numerical Index
PART NUMBER
PART NUMBER
5500C1AYOEE
5oo0C1AYON
5500C1AYVOE
5500C1AYVOEE
5500C1AYVON
5500C1BBF23D
5500C1BE25A
5500C1NBF23A
5500C1SB20AE
5500C1 SB20AP
5500C1 SBF20A
5OOOC1SBY20AE
5OO0C1 SF23A
550OCHBF20B
550OC1TF20BM
5500C1 UB23AN
5500C1UB25A
5500C111BF23A
5500C1 UBF25A
5500C1 UBF30A
5500C1 UF20AN
5500C1 UF23A
5500C1 UF30AN
5500C1 UFF23A
5500CWF20BM
5500CWF30AN
5oo0C1VF30BN
5oo0CWFG20B
5500C1VFY30AN
5OOOC1VFY30BN
5oo0C1WBF15A
5500C1 WBF23A
5500C1 WBF30A
550OC1XBF2OB
5500C1 XYON
5500C1YBF20B
550OC6ABF15A
550OC6ABF20B
550OC6ABF23A
550OC6ABF23B
5500C6ABF23D
5500C6ABF25A
5500C6ABG30B
5500C6AEF20A
5500C6AF20A
5500C6AF20AR
5500C6AF23AE
5500C6AF30A
5500C6AF30AE
5500C6AF30AN
5500C6AG30AN
5500C6AYON
EFFECTIVITY:
ALL
PART NUMBER
PART NUMBER
PART NUMBER
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
·2e
-2D
-1Z
-2
-2A
-2E
·2F
-2G
-2K
-2L
-2H
-2J
-2M
-2N
-2P
-2T
-2U
·20
-2R
-25
-2X
-2Y
·2V
-3B
-3C
-3D
-2Z
-3
-3A
-3E
-3F
-3G
-3H
.3J
·3K
-3L
-3M
-3N
·3P
-30
-3R
1C
-35
1C
1C
1C
1C
1C
1C
1C
1C
1C
-3T
-3U
-3V
-3W
-3X
-3Y·
-3Z
-4
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
.2W
-48
35-32-18
Page 10024
20040415
•
•
•
•
•
•
-,)
-t'lco/scott
!scott
Technologies, Inc. Aviation
55OCV56ODSERIES PORTABLE CYI.INDER ASSEMBLY - CMM & IPL
'~
NumericalIndex
PART NUMBER
PART NUMBER
5500C6AYVON
5500C6EBF230
5500C6RBF230
5500C6TG20B
5500C6UBF30A
5500C6UF23AP
5500C6UF30AN
5500C6WFF23A
5500C6XBF230
5500C9ABF2OA
5500C9ABF20B
5500C9AFF10A
5500C9SF30A
5500C9UF30AN
5500C9UH20A
5500C9WFF10A
5500C9WYOE
5500C9XBB20A
55000 SUB SERIES
550001ABF23A
550001AE20A
550001AE25A
550001AF23A
550001AYOE
550001AYON
550001AYVOE
550001AYVOP
5500D1PCC20A
5500D1WBB15A
5500D1XYOE
5500D1XYON
5500D6AY[lE
5500D6AYVOE
5500D6AYVON
5500D6PBF25A
5500D6XHH30A
5500F SUB SERIES
5500F1XFH20A
5500F6ABB30A
5500G SUB SERIES
5500G1AB23A
5500G1AF20A
550OG1WEE30A
5500J SUB SERIES
5500J1AABE20B
5500J1ABBF20A
5500J1ABBF20B
5500J1ABBF23A
5500J 1ABEG20B
5500Jl ABFL23A
5500l SUB SERIES
5500L1WBBF23A
5500L6CBBF23A
5500L6CBBF25A
5500L6UBBF25A
EFFECTIVITY:
PART NUMBER
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1C
1
10
10
10
10
10
10
10
10
10
10
10
10
1D
1D
10
10
10
1
lE
lE
1
lE
1E
1E
1
1E
1E
1E
1E
1E
1E
1
1E
1E
1E
1E
ALL
PART NUMBER
-4A
-4C
-40
-4E
-4F
-4G
-4H
-4J
-4K
-4L
-4M
-4N
-4P
-4Q
-4R
-4S
-4T
-4U
-10
·1
-1A
-1B
-lC
-IF
-1G
-10
-1E
-1H
-1J
-1K
-1L
-1P
-1M
-1N
-10
-lR
-1E
-1
-1A
·1F
-18
-1C
-10
-1G
-1E
-1F
-1G
-1H
-1J
-1K
-lH
-1L
-1M
-1N
·1P
35-32-18
PART NUMBER
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
Page 10025
20040415
1:'1ca/scott
Technologies. Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY - CMU & IPL
Numerical Index
PART NUMBER
5500l6WBBF25A
5500l6WBEF23A
5500l6WFF23AP
5500M SUB SERIES
5500M1ABBB20B
5500M1ABH23A
5500M1ABH23AN
5500M1AFFF25A
5500M1ALll30A
5500M1AXOK
5500M1WBF23AM
5500M6WBBF10A
5500M6WFF23AN
5500M6WFF23AP
5500N SUB SERIES
55OON6SBF10A
5500P SUB SERIES
55OOP6UEEE20A
55000 SUB SERIES
550006XBF10A
550006XBF23A
5500Q6XYVOEE
5500S SUB SERIES
5500S6XYYOE
5500S6XYYON
5500S9XYYYOE
5500S9XYVOE
5500 SERIES
5500T SUB SERIES
55ooT2ACC30B
5507-00
5507-2-20
5507-2-23
5507-2-30
5507-3-20
5507-4-20
5507-4-20
5507-4-23
EFFECTIVITY: ALL
PART NUMBER
PART NUMBER
1E
1E
1E
1
1E
1E
1E
1E
1E
1E
1E
1E
1E
1E
1
1F
1
1E
1
1F
1F
1F
1
1E
1E
1E
1E
1
1
1G
1A
1B
1C
1H
7
18
1C
7
1A
1C
-7
1A
7
1H
7
1A
18
1C
7
1A
1C
7
PART NUMBER
-10
-1R
-1S
-1J
-n
-1U
-1V
-1W
-1X
-w
-1Z
-2
-2A
-28
-1K
-1
-il
-2C
·1M
-1A
-1B
-1C
-1N
-2D
-2E
-2F
-2G
1
-1P
-1
320
320
320
320
-1
325
325
-2
325
325A
-2A
325A
-28
325
-2C
3258
325A
3258
-2D
325C
325C
-2E
35-32-18
PART NUMBER
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
1
1
1
1
RF
1
1
RF
1
1
RF
1
RF
1
RF
1
1
1
RF
1
1
RF
Page 10026
20040415
•
•
•
•
..,
1:'1ca/scott
!scott
Technologies. Inc. Aviation
5500'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & 'PL
Numerical Index
PART NUMBER
PART NUMBER
PART NUMBER
5510-10
1A
1B
1C
1H
1J
9
5510-13
10
5510-15
1E
1H
1J
9
1E
1H
1J
9
1F
400
400
400
400
400
-1
405
405
405
405
-1A
410
410
410
-1B
415
·1C
425
425
1
1
1
1
1
RF
1
1
1
1
RF
1
1
1
RF
1
RF
1
1
RF
2
1
1
1
1
1
1
1
1
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
PART NUMBER
PART NUMBER
5510-17
9
1E
1J
9
9
5510-19
•
•
5511-00
5517-00
5520-16
5520-17
5522-00
5533-00
5533-01
55620-01
55620-02
5600-1 SUB SERIES
5600·181 AE20B
5600-1B1AF23A
56oo·1C1AB20A
56oo·1C1AB20B
5600-1C1AB23A
5600-1C1AE20A
5600-1C1AE20B
56oo-1C1AE20D
56oo-1C1AE23A
5600-1C1AE23B
5600-1C1AF20A
5600-1C1AF20B
5600-1C1AF23A
56oo-1C1AF23B
56oo-1C1AF25A
5600-1C1AXOK
5600-1C1AXOM
5600-1C1AYOM
56oo-1C18XOK
5600-1C18XOM
5600-1C1BYOM
5600·1C6AE20A
EFFECTIVITY:
9
9
9
9
7
7
9
9
1
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
ALL
·10
70
110
11
·10
150
-40
140
90
130
-2A
-1
-1A
-1B
-1C
-10
-1E
·1F
-1G
·1H
-1J
-1K
-1L
-1M
·1N
-1P
-10
·1R
-15
-H
-1U
.1V
-1W
35-32-18
Page 10027
20040415
tyco/SCOtl
/scott
Technologies.Inc. Aviation
550(115600SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
Numerical Index
PART NUMBER
5600-1C6AF23A
5600-1C6AF23B
5600-1C6AXOK
5600-1D1AF23A
5600-1D1AF30A
5600·106AE20A
5600-1 G1AF20A
5600-1 M1AF20BM
5600-2 SUB SERIES
5600-2A1AB23B
5600-2A 1AF23A
5600-2B1AE20A
5600-2B1AF20A
5600-281AYOE
5600-2C1AB20B
5600-2C1AC20A
5600-2C1AE20A
5600-2C1AE20B
5600-2C1AE20C
5600-2C1AE200
5600-2C1AE23A
5600-2C1AE23B
5600-2C1AF20A
5600-2C1AF30A
5600·2C1AG25A
5600·2C1AXOK
5600-2C1AXOM
5600-2C1AYOM
56QO-2C1AYON
5600-2C1BXOK
5600-2C5AE20B
5600-2C6AB23A
5600-2C6AF23A
5600-2C6AXOK
5600-2C9FXOK
5600-201AXOK
5600-201 BXOK
5600-2G1AB20B
5600-2J1 ABF23A
5600-2M1ABF23A
5600-2M 1ABG23A
5600-8 SUB SERIES
5600-886AXOK
5600-8B9AXOK
5600-BC1AF23A
5600-8C1 AXOK
5600-8C1 BF23A
5600-8C6AF23A
5600-8C6AXOK
5600-8D1AXOK
5600-801AYON
56oo-8G2AXOK
EFFECTIVITY: ALL
PART NUMBER
PART NUMBER
1H
1H
1H
1H
1H
1H
1H
1H
1
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1H
1
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
PART NUMBER
-1X
-tY
-1Z
-2
-2A
-2B
-2C
-20
-2B
-2E
·2F
-2G
-2H
-2J
·2K
-2L
-2M
-2N
-2P
-20
-2R
-28
-21
-2U
-2V
-2W
-2X
-2Y
-2X
-3
-3A
-3C
-30
-3E
-3F
-3G
-3H
-3J
-3K
-3L
-3M
-2C
-1
-1A
-18
-1C
-10
-1E
-1F
-1G
-1H
.1J
35-32-18
PART NUMBER
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
Page 10028
20040415
•
•
•
•
•
~.
f:l.lco/scott
/scott
Technologies, Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
Numerical Index
PART NUMBER
PART NUMBER
5600-8G6AXOK
5600-9 SUB SERIES
5600-9C1AF20A
5600-9C1AF20B
5600-9C1AF23A
56oo-9C1AXOK
56oo-9C1AYOE
5600-9C1AYON
5600-9C6AXOK
5600-9C6AYOK
5600-9C9AF10A
5600-901 AE208
5600-901 AE30A
5600-90 1AF23A
5600-90 1AG30A
5600-901 AXOK
5600-901 AYON
5600-901 BXOK
5600-909AXOK
5600-9G1AXOK
5600-9J6AF3OAN
5600-9M1AHH20A
5600-9M6ABF30A
5600-9M6AF30AE
5600-9M6AF30AN
5600-9M6AFF30A
5600·9M9FF30AN
56oo-9P1AYOEN
5600-9P6AF30AN
5600 SERIES
5601
56018
5601C
5602-00
5603-00
5606-00
5606-01
5607-00
5607-01
5608-00
56750-00
56750-01
56750-02
57524-00
59447-00
59447-01
•
CMM & IPL
EFFECTIVITY:
ALL
PART NUMBER
PART NUMBER
PART NUMBER
1J
1
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1J
1
1H
1J
1H
1J
1H
1J
1H
lJ
3
3
3
3
3
1H
1J
12
12
12
9
13
5
10
-1K
-20
-1L
-1M
-1N
-1P
-1Q
·1R
-1S
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
-n
-1U
-1V
-1W
-1X
-1Y
-1Z
-2
-2A
-2C
-20
-2E
-2F
-2G
-2J
-2K
-2H
-2L
-2M
-2N
2
105
105
105A
105A
1058
1058
-100
-100
290
300
-320
350A
-350
-25
-25
10
50
60
-190
10
10
30
35-32-18
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
Page 10029
20040415
t'lCCI/scott
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
Numerical Index
PART NUMBER
59553-00
59602-00
59602-00
59776-01
6050-01
6050C
605SE
6066-00
6066-01
6084-01
6084-02
6084-03
6084-04
6084-06
6084-07
6084-20
6084-34
6350A13XA
6350A13XAH
6350A13XE
6350A13XG
6350A14XA
6350A14XAH
63SOA14XG
6350A2XA
6350A2XA
EFFECTIV',.y: ALL
PART NUMBER
PART NUMBER
9
lH
1J
lG
3
3
3
3
3
1A
lE
1H
1J
1B
1E
lH
lJ
1C
1E
lH
1J
10
lE
1F
1H
1J
1E
IF
1E
1H
1J
lC
lE
1H
1J
1E
lA
1J
1A
1A
1A
lE
1H
1B
1E
1J
1B
1B
1E
1H
lE
1F
PART NUMBER
360
120
:120
475
180
-50
240
-270
270
505
505
505
505
515
515
515
515
555
555
555
555
525
525
525
525
525
535
535
545
545
545
555A
555A
555A
555A
565
500C
500
500A
5006
500
SOO
500
SlOB
510A
510
510A
510
510
510
530A
530
35-32-18
PART NUMBER
2
4
4
1
1
1
1
2
2
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
Page 10030
20040415
•
•
•
~'.
t'lca/scott
/scott
Technologies,Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
Numerical Index
PART NUMBER
PART NUMBER
6350A2XG
6350A20XA
6350A20XA
6350A20XE
6350A20XG
6350A34XA
6350A4XA
6350A4XG
635OA5XA
6350A5XAN
6350A5XG
•
CMM & IPL
6363-01
6364-00
6370-00
6375-04
6378-00
6379·2C
PART NUMBER
1E
1C
1E
1H
1J
1H
1C
1E
1H
1J
1E
10
1E
1F
1H
1J
10
1H
1J
1J
1J
1E
1H
1J
9
9
9
3
3
1H
3
1H
3
9
3
3
3
3
3
3
3
1A
1A
1B
1C
1C
6379-20
6555-00
6582-00
6583-00
6584-00
6586-00
6588-00
6597-00
6812-00
6818-01
10
1E
1E
1E
1H
1J
•
EFFECTIVITY:
ALL
PART NUMBER
530
550A
550A
550B
550A
550A
550
550
550
550
560
520A
520
520
520A
520A
520
520
520
540B
540A
540
540
540
210
260
280
90
110
110
·10
110A
-20
240
190
160
170
140
150
120
340
-395
-396
-395
-395
-396
-395
-395
-396
-397
-395
-395
35-32-18
PART NUMBER
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
RF
1
RF
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
Page 10031
20040415
'tl./ca/scott
Technologies, Inc.
!scott
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
Numerical Index
PART NUMBER
8oo503.QO
800649-00
800649-01
800651-00
801421-01
801658-00
801659-00
801659-00
801660-00
PART NUMBER
PART NUMBER
5
1J
3
1J
3
3
9
1A
18
1C
1H
1J
1A
18
1C
1H
1J
1A
18
1C
10
I
801660-03
801660-05
801661-00
801662-00
801807-01
801807-02
1E
1G
1H
1J
2
1C
1H
1J
1A
1B
1C
1H
1J
18
1E
2
1A
2
1A
18
1C
1F
801807-03
801808-01
801808-02
EFFECTIVITY: All
2
1A
1C
2
1A
1C
2
1A
18
PART NUMBER
-4
115
-30
115A
-40
-60
-220
200
200
200
200
200
201
201
201
201
201
205
205
205
205
205
205
205
205
10
215
220
220
202
202
202
202
202
225
225
5
235
-1
240
240
240
240
-1A
245
245
-1B
250
250
-lC
255
255
35-32-18
PART NUMBER
RF
1
RF
1
RF
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
•
1
1
1
1
1
RF
1
1
1
1
RF
1
1
RF
1
1
RF
1
1
Page 10032
20040415
•
•
••
.,
tl/ca/scott
7echnologies.
Inc.
!scott
A lIiation
550015500 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
Numerical Index
PART NUMBER
801808-02 (Continued)
801808-03
801808-05
AIRLINE STOCK NO.
FIGURE
1C
1E
2
1A
18
1C
2
1A
10
2
2
2
10
6
9
12
11
1A
1C
1E
1H
10
1A
18
1C
10
10
1E
10
10
9
9
1A
18
1C
801809-01
802061-00
802233-01
80281-01
802821-01
802856-01
802863-02
•
802874-01
802877-01
802883-01
803129-01
803177-01
10
1E
2
1A
1C
2
1A
803177-02
803177-03
2
•
803199-04
1G
9
804201-01
804202-01
804329-01
804376-01
804670-03
805436-01
7
9
EFFECTIVITY:
4
5
9
1A
ALL
ITEM NO.
255
255
-10
260
260
260
-1E
265
265
-1F
55
60
-60
10
300
1E
-1
340A
340A
340A
340A
-1
350
350
350
350
351
350
-20
50
120
460
270
270
270
270
270
-1G
275
275
-1H
280
-1J
435
-1E
50
160
-100
-60
40A
285
35-32-18
TILREQ'D
1
1
RF
1
1
1
RF
1
1
RF
1
2
1
1
1
RF
RF
1
1
1
1
RF
1
1
1
1
t
1
1
1
1
1
1
1
1
1
1
RF
1
1
RF
1
RF
1
RF
1
1
1
1
1
1
Page 10033
20040415
1:L/Co/scott
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
Inrl",...
PART NUMBER
805436-01 (Continued)
8561.Q0
8561.Q2
8569.Q1
8572·02
PART NUMBER
PARTNUMB~R
1C
2
9
9
6
1A
1A
1B
16
1C
1C
10
10
8587-01
8579-00
8587-01
9036-00
\
EFFECTIVITY: ALL
1E
1E
1E
1F
1F
1H
1J
6
6
6
6
3
PART NUMBER
285
-lK
-390
390A
70
330
331
330
331
330
331
330
331
330
331
332
330
331
330
330
-1
60
50
90
-230
35-32-18
PART NUMBER
1
RF
1
1
1
1
1
1
1
1
1
1
1
1
1
I
1
1
1
1
RF
1
1
1
1
Page 10034
20040415
•
•
•
....
f:l./ca/scotl
Technologies, Inc.
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
•
•
/scott
Aviation
CMM & 'PL
THIS PAGE INTENTIONALLY LEFT BLANK
EFFECTIVITY:
ALL
35-32-18
Page 10035
20040415
'tl.lcoJscott
/scotr
Technologies. Inc. Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
C&lM & IPL
TASK 35-32-18-950-801
4.
Detailed Parts List
(--
--
•
5500 Series Portable Cylinder Assy
Figure 1
(Sheet 1 of 2)
EFFECTIVITY: ALL
35-32-18
Page 10036
20040415
•
•
-.
~'1CD/SCOlt
Technologies. Inc.
Aviation
5500'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
•
jscott
CMM & IPL
5600 Series Portable Cylinder Assy
Figure 1
(Sheet 2 of 2)
EFFECTIVITY:
ALL
35-32-18
Page 10037
20040415
1:'1ca/scott
Technologies.
Inc.
/scott
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
11
PART NUMBER
AIRLINE
STOCK NO.
.-
Aviation
CMM & IPL
NOMENCLATURE
EFF.
CODE
1234567
UNITS
PER
ASSY
5500 SERIES
CYLINDER ASSY, PORTABLE SERIES
(SPN 5500 SERIES)
RF
·lA
5500A SUB SERIES
CYliNDER ASSY, PORTABLE SERIES
(REFER TO FIG 1A FOR DET BKON)
RF
-1B
5500B SUB SERIES
CYliNDER ASSY, PORTABLE SERIES
(REFER TO FIG 1B FOR DET BKDN)
RF
-1C
5500C SUB SERIES
CYLINDERASSY, PORTABLE SERIES
(REFER TO FIG 1C FOR DET BKDN)
RF
-10
55000 SUB SERIES
CYLINDER ASSY, PORTABLE SERIES
(REFER TO FIG 10 FOR DET BKDN)
RF
-1E
5500F SUB SERIES
CYLINDER ASSY, PORTABLE SERIES
(REFER TO FIG 1E FOR DET BKDN)
RF
-1F
5500G SUB SERIES
CYLINDER ASSY, PORTABLE SERIES
(REFER TO FIG 1E FOR DET BKDN)
RF
-1G
5500J SUB SERIES
CYLINDER ASSY, PORTABLE SERIES
(REFER TO FIG 1E FOR DET BKDN)
RF
-1H
5500L SUB SERIES
CYliNDER ASSY, PORTABLE SERIES
(REFER TO FIG 1E FOR DEl BKDN)
RF
-1J
fi500M SUB SERIES
CYliNDER ASSY. PORTABLE SERIES
(REFER TO FIG 1E FOR DET BKDN)
RF
-1K
5500N SUB SERIES
CYlINDERASSY. PORTABLE SERIES
(REFER TO FIG 1F FOR DET BKDN)
RF
-1L
5500P SUB SERIES
CYLINDER ASSY, PORTABLE SERIES
(REFER TO FIG 1E FOR DET BKON)
RF
-1M
5500Q SUB SERIES
CYLINDER ASSY, PORTABLE SERIES
(REFER TO FIG 1F FOR DEl BKDN)
RF
-1N
5500S SUB SERIES
CYLINDER ASSY, PORTABLE SERIES
(REFER TO FIG 1E FOR DET BKDN)
RF
-1P
5500T SUB SERIES
CYLINDER ASSY, PORTABLE SERIES
(REFER TO FIG 1G FOR DEl BKDN)
RF
5600 SERIES
CYLINDER ASSY, PORTABLE SERIES
(SPN 5600 SERIES)
RF
-2A
5600-1 SUB SERIES
CYLINDER ASSY, PORTABLE SERIES
(REFER TO FIG 1H FOR DET BKON)
RF
-2B
5600-2 SUB SERIES
CYLINDER ASSY, PORTABLE SERIES
(REFER TO FIG 1H FOR DET BKON)
RF
-2C
5600-8 SUB SERIES
CYLINDER ASSY, PORTABLE SERIES
(REFER TO FIG 1J FOR DEl BKDN)
RF
-20
5600-9 SUB SERIES
CYLINDER ASSY, PORTABLE SERIES
(REFER TO FIG 1J FOR DEl BKDN)
RF
2
EFFECTIVITY:
ALL
35-32-18
Page 10038
20040415
•
•
•
•
...
tl./ca/scott
!scott
Technologies.Inc. Aviation
550Q'56oo SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & tPi
THIS PAGE INTENTIONALLY LEFT BLANK
•
•
- ITEM NOT IllUSTRATED
EFFECTIVITY:
ALL
35-32-18
Page 10039
20040415
tL/co/SCOtl
/scott
Technologies. Inc. Aviation
550015600 SERJES PORTABLE CYLINDER ASSEMBLY·
•
CMM & JPL
300 - 350
2 Outlet Regulator
(Top View)
•
500
505
5500A Sub Series peA
Figure 1A
(Sheet 1 of 3)
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10040
20040415
•
•
.
1:l./ca/scott
Technologies,Inc.
/scott
Aviation
55()(l15600 SERIES PORTABLE CYUNDER ASSEMBLY - CMM & ,PL
.-\,
200
I
I
201
202
75
801658-00
5500A Sub Series peA
Figure 1A
(Sheet 2 of 3)
•
•
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10041
20040415
tL/co/SCOtl
/scott
Technologies. Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
J.
CMM" IPL
•
.250 - 285
_____,."J.-_______ ~-----
/~~
OXYGEN
,
MASK
(
..
"
"---..,-..----------
-'
70
,
805436-01 Shown
.
801808 Series (Typ.ical)
803177 Series (Typical)
•
235
240
245
""\1-0)-'i,)1''/.
-~'Ii
Ji:k~:s;:mll
/'
.'
••-
l
•. ~-
~~:-,~-j
1(,-':('
"='"" 'iJ \;
---1
--"
I
..•. _~~.,.t/
801807 Series (Typical)
(801807-02 Shown)
5500A Sub Series peA
Figure 1A
(Sheet 3 of 3)
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10042
20040415
•
•
.'.
tl./Ca/SCOll
!scott
Technologies. Inc. Aviation
5500/5600 SERIES PORTABLE CYLINDERASSEMBLY· CMM & fPL
FIG.
ITEM
1A
-1
PART NUMBER
AIRLINE
STOCK NO.
5500A1AM323A
5500A1AA15A
•
U~IITS
PER
ASSY
A
RF
CYliNDER ASSY, PORTABLE
(SPN 5500-A1A-A15A)
C
RF
DELETED
-1C
•
CYLINDER ASSY, PORTABLE
(SPN 5500-A1A-AB23A)
EFF.
CODE
DELETED
-1A
-16
NOMENCLATURE
1234567
-10
5500A1AB623A
CYLINDER ASSY, PORTABLE
(SPN 5500-A1A-BB23A)
E
RF
-1E
5500A 1ABB25A
CYLINDER ASSY, PORTABLE
(SPN 5500-A1A-BB25A)
F
RF
-1F
5500A 1ABC30A
CYLINDER ASSY, PORTABLE
(SPN 5500-A1A-BC30Aj
G
RF
-1G
5500A1ABE20A
CYliNDER ASSY, PORTABLE
(SPN 5500-A1A-BE20Aj
H
RF
-1H
5500A 1ABE20B
CYLINDER ASSY, PORTABLE
(SPN 5500-A1A-BE20B)
J
RF
-1J
5500A 1ABF10A
CYLINDER ASSY, PORTABLE
(SPN 5500-A1A-BF10A)
K
RF
-1K
5500A1ABF20B
CYLINDER ASSY, PORTABLE
(SPN 5500-A1A-BF20B)
L
RF
-1L
5500A 1ABF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-A1A-BF23A)
M
RF
-1M
5500A 1ABF23B
CYliNDER ASSY, PORTABLE
(SPN 5500-A1A-BF23B)
N
RF
-1N
5500A1ABF23D
CYliNDER ASSY, PORTABLE
(SPN 5500-A1A-BF23D)
P
RF
-1P
5500A 1ABF25A
CYUNDER ASSY, PORTABLE
(SPN 5500-A1A-BF25A)
0
RF
-10
5500A 1ABF25B
CYLINDER ASSY, PORTABLE
(SPN 5S00-A1A-BF25B)
R
RF
-1R
5500A 1ABF30A
CYLINDER ASSY, PORTABLE
(SPN 5500-A1A-BF30A)
S
RF
-1S
5500A1AB15A
CYLINDER ASSY, PORTABLE
(SPN 5500-A1A-615A)
T
RF
-1T
5500A1AB20A
CYLINDER ASSY, PORTABLE
(SPN 5500-A1A-B20A)
U
RF
-tu
5500A1AC30B
CYLINDER ASSY, PORTABLE
(SPN 5500-A1A-G30B)
V
RF
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10043
20040415
.
.....
-tqCCJ/scott
/scott
Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
1A
PART NUMBER
AIRLINE
STOCK NO.
CMU & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
·w
5500A 1AE20A
CYUNDER ASSY, PORTABLE
(SPN 550o-A1A-E20A)
W
RF
·1W
5500A1AE20B
CYLINDER ASSY, PORTABLE
(SPN 550o-A1A-E20B)
X
RF
-1X
5500A1AF20A
CYLINDER ASSY, PORTABLE
(SPN 5500-A 1A·F20A)
Y
RF
-1Y
5500A1AF20B
CYUNDER ASSY, PORTABLE
(SPN 5500-A1A-F20B)
Z
RF
-1Z
5500A1AF20D
CYLINDER ASSY, PORTABLE
(SPN 5500·A1A-F20D)
M
RF
-2
5500A 1AF23A
CYLINDER ASSY, PORTABLE
(SPN 550o-A1A-F23A)
AB
RF
.2A
5500A 1AF25A
CYLINDER ASSY, PORTABLE
(SPN 550o-A 1A-F25A)
AC
RF
·2B
5500A 1AF25AN
CYLINDER ASSY, PORTABLE
(SPN 5500-A 1A-F25AN)
AD
RF
-2C
5500A1AXOK
CYLINDER ASSY, PORTABLE
(SPN 5500·A1A-XOK)
AE
RF
·20
5500A1AVYOE
CYUNDER ASSY, PORTABLE
(SPN 550o-A1A-VYOE)
AF
RF
I
·2E
5500A 1BF23A
CYLINDER ASSY, PORTABLE
(SPN 550o-A1B·F23A)
AG
RF
·2F
5500A 1MM 15B
CYLINDER ASSY, PORTABLE
(SPN 550Q..A1M-M15B)
AH
RF
-2G
5500A1NBF23A
CYLINDER ASSY, PORTABLE
(SPN 550Q..A1N-BF23A)
AJ
RF
-2H
5500A 1QB30AD
CYLINDER ASSY, PORTABLE
(SPN 5500·A1Q-BJOAD)
(SUPSDS ITEM -2K)
AK
RF
-2J
5500A1OB30D
CYLINDER ASSY, PORTABLE
(SPN 5500-A10·B30D)
Al
RF
-2K
5500A 1OB30DA
CYLINDER ASSY, PORTABLE
(SPN 5500-A 1Q.B30DA)
(REPlD BY ITEM -2H)
AM
RF
·2L
5500A 1REE25A
CYLINDER ASSY, PORTABLE
(SPN 5500·A1R-EE25A)
AN
RF
·2M
5500A 1SB2DA
CYLINDER ASSY, PORTABLE
(SPN 550Q..A1S·B20A)
AP
RF
-2N
5500A 1SCC30A
CYLINDER ASSY, PORTABLE
(SPN 550Q..A1S-CC30A)
AQ
RF
·2P
5500A 1TBF20B
CYLINDER ASSY, PORTABLE
(SPN 550Q..AH-BF20B)
AR
RF
-ITEM NOT ILLUSTRATED
EFFECT\VITY:
5500 SERIES
35-32-18
Page 10044
20040415
•
•
•
•
1:IIeD/scott
Technologies. Inc.
".
/scott
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
lA
•
•
-2Q
5500A 1UBF23A
CYUNDER ASSY, PORTABLE
(SPN 5500-A1 U-BF23A)
AS
RF
-2R
5500A 1UBF25A
CYUNDER ASSY, PORTABLE
(SPN 5500-A1U-BF25A)
AT
RF
·2S
5500A 1UEE25A
CYLINDER ASSY, PORTABLE
(SPN 5500-A1U-EE25A)
AU
RF
-21
5500A 1UF30AN
CYLINDER ASSY. PORTABLE
(SPN 5500-A 1U-F30AN)
AV
RF
·2U
5500A 1VBF20B
CYLINDER ASSY, PORTABLE
(SPN 5500-A1V-BF20B)
AW
RF.
-2V
5500A1VBF23B
CYUNDER ASSY. PORTABLE
(SPN 5500-A1V-BF23B)
I\X
RF
-2W
5500A WBF25B
CYLINDER ASSY, PORTABLE
(SPN 5500-AW-BF25B)
AY
RF
-2X
5500A 1VF20BM
CYUNDER ASSY, PORTABLE
(SPN 5500-AW-F20BM)
W.
RF
-2Y
5500A 1WBF23A
CYUNDER ASSY, PORTABLE
(SPN 550D-A1W-BF23A)
SA
RF
-27.
5500A1WBF25A
CYLINDER ASSY, PORTABLE
(SPN 5500-A1W-BF25A)
SS
RF
-3
5500A 1WBF30A
CYUNDER ASSY, PORTABLE
(SPN 550D-A1W-BF30Aj
BC
RF
-3A
5500A 1XBF20B
CYLINDER ASSY, PORTABLE
(SPN 550o-A1X-8F20B)
SO
RF
-38
5500A1XFF23A
CYUNDER ASSY. PORTABLE
(SPN 550D-A1X-FF23A)
BE
RF
·3C
5500A 1YBF20B
CYUNDER ASSY, PORTABLE
(SPN 5500-A1Y-BF20B)
BF
RF
-3D
5500A3ABF23A
CYUNDER ASSY, PORTABLE
(SPN 5500-A3A-BF23A)
BG
RF
-3E
5500A5ABG20B
CYUNDER ASSY, PORTABLE
(SPN 5500-A5A-BG2OB)
BH
RF
-3F
5500A6ABF23A
CYLINDER ASSY, PORTABLE
(SPN 550Q-A6A·BF23A)
BJ
RF
-3G
5500A6ABF23B
CYLINDERASSY, PORTABLE
(SPN 550o-A6A-BF23B)
BK
RF
-3H
5500A6ABG20B
CYLINDER ASSY, PORTABLE
(SPN 5500-A6A-BG20B)
BL
RF
-3J
5500A6AF20B
CYLINDER ASSY, PORTABLE
(SPN 5500-A6A..f20B)
BM
RF
-3K
5500A6PFF23A
CYUNDER ASSY, PORTABLE
(SPN 5500-A6P-FF23A)
BN
RF
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10045
20040415
.
-tqca!scott
. /scott
Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
1A
PART NUMBER
AIRLINE
STOCK NO.
.'
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
-3L
5500A6SB30A
CYLINDER ASSY. PORTABLE
(SPN 550D-A6S-B30A)
BP
RF
-3M
5500A6UE30A
CYLINDER AS8Y, PORTABLE
(SPN 550D-A6U·E30A)
BO
RF
-3N
5500A6WBB15A
CYLINDER ASSY, PORTABLE
(SPN 5500-A6W-BB15A)
BR
RF
-3P
5500A6WBB23A
CYLINDER ASSY, PORTABLE
(SPN 550D-A6W·BB23A)
BS
RF
·3Q
5500A6WBB25A
CYLINDER ASSY, PORTABLE
(SPN 550D-A6W·BB25A)
BT
RF
·3R
5500A6WFF23A
CYLINDERASSY, PORTABLE
(SPN 550D-A6W·FF23Aj
BU
RF
·38
5500A6WF3QAP
CYLINDER ASSY, PORTABLE
(SPN 5500-AGW-F30AP)
BV
RF
-3T
5500A9AB30A
CYLINDER ASSY, PORTABLE
(SPN 5500-A9A·B30A)
BW
RF
-3U
5500A9SAC25A
CYLINDER ASSY, PORTABLE
(SPN 5500-A9S-AC25A)
BX
RF
·3V
5500A9SBF30A
CYLINDER AS8Y, PORTABLE
(SPN 550D-A9S-BF30A)
BY
RF
·3W
5500A9SG30A
CYLINDER ASSY. PORTABLE
(SPN 550D-A9S-G30A)
BZ
RF
-3X
5500A9WEE25A
CYLINDER ASSY, PORTABLE
(SPN 550D-A9W·EE25Aj
CA
RF
-3Y
55ooA9XF23A
CYLINDER ASSY, PORTABLE
(SPN 550D-A9X-F23A)
CB
RF
·20
10006936
• PLATE, INSTRUCTION (REPlD BY 20A)
(SEE NOTE 1)
A-BV
1
20A
10009071
• DECAL, INSTRUCTION (REPlS ·20) (SEE NOTE1)
A-BV
1
-30
10005922
• DECAL, OXYGEN JD(REPLD BY 30A)
A-BV
1
30A
10009255
• DECAL, OXYGEN 10 (REPLS -30)
USED ONLY WHERE PAINTED TEXT
"BREATHING OXYGEN ONLY - USE NO Oil'
DOES NOT APPEAR ON SIDE OF CYLINDER
(ITEM SOD, 505)
A·BV
1
35
10009374
• LABEL, FAA-PMA ELIGIBILITY
(USED ONLY ON PCA's SHIPPED FROM THE
FACTORY FROM JULY 1995 AND LATER)
-40
10001018
• PLACARD, INSTRUCTION
(USED ONLY ON 5500A 9 SERIES)
45
10001019
• LABEL
-50
10001020
• PLACARD, AVIATOR'S OXYGEN
(USED ONLY ON 5500A 9 SERIES)
(USED ONLY ON 5500A 9 SERIES)
5500 SERIES
35-32-18
•
1
BW-CB
1
BW-CB
1
BW-CB
1
• ITEM NOT ILLUSTRATED
EFFECTlVITY:
•
Page 10046
20040415
•
•
''';
-t'lca /SCOtl
Technologies.
Inc.
/scott
Aviation
550015600 SERIES PORTABLE eYUNDER ASSEMBLY·
FIG.
ITEM
1A
PART NUMBER
55
5057..(}()
65
MS21318-7
AIRLINE
STOCK NO.
eMM & ,PL
UNITS
PER
ASSY
EFF.
CODE
NOMENCLATURE
1234567
• PLATE, IDENTIFICATION
1
ATTACHING PARTS
2
• SCREW, DRIVE (CRES) (V88044)
(#0 x 0.125 in. LNG) (SPN 33343-007)
...
•
•
10
13160-00
• CLAMP (ALT SPN WWD-120)
A·AJ,AN,
AS-Be, BG-BN,
BO·BW,CA
1
75
13160-00
• CLAMP (ALT SPN WWD-120)
AG, AK-AM, APAR, BP, BX-BZ
1
200
801658-00
• HARNESS
AG
1
201
801659-00
• • STRAPASSY
AG
1
202
801661-00
• • STRAPASSY
AG
1
205
801660-00
• HARNESS
A-AF, BG-BM, BW
1
235
801807-01
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
AK-AM
1
240
801807-02
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
AP,AO,BP,
BX-BZ
1
245
801807-03
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
AR
1
250
801808-01
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
AN
1
255
601808-02
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
AS·AV,BO
1
260
801808-03
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DEI BKON)
AW-AZ
1
265
801806-05
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
BN
1
270
803177-01
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
BA·BG, BR-BV, CA
1
275
803177-02
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
BF
1
280
803177-03
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
AH
1
285
805436-01
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
AJ
1
300
5009-00
• OUTLET ASSY
(SUPSD BY ITEM 305)
(REFER TO FIG 5 FOR DET BKDN)
A-H,K,M,O,S-U,W,
W,Y,AB-AD,AG AJ,
AK,AM-AO,AS-AV,
BA-BC,BE,BG,BJ,
BN-CB
1
NP
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10047
20040415
1:'-/ca/scott
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
,....
/scott
Technologies.Inc. Aviation
PART NUMBER
AIRLINE
STOCK NO.
.•
,
CMM & IPL
NOMENCLATURE
1234567
UNITS
PER
EFF.
CODE
ASSY
1A
305
5009-.5-15
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
C
1
305A
5009-.5-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
A
1
305B
5009-.5-25
• OUTLET ASSY (SUPSDS ITEM 3(0)
(REFER TO FIG 5 FOR DET BKDN)
BX
1
305C
5009-2-10
• OUTLET ASSY (SUPSDS ITEM 3(0)
(REFER TO FIG 5 FOR DET BKDN)
K
1
3050
5009-2-15
• OUTLET ASSY (SUPSOS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
T,BR
1
305E
5009-2-15
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
BR
1
305F
5009-2-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
H,U,AP
1
305G
5009-2-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
A, E, M, AJ, AS,
BA, BG, BJ, BS
1
30SH
5009-2-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
E,BS
1
30SJ
~009-2-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
F, a, AT, BB, BT
1
30SK
5009-2-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
F,BT
1
305L
5009-2-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
G, S, AK, AM, BC,
BP,BW,BY
1
305M
5009-2.5-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
BX
1
305N
5009-2.5-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
G,Aa
1
305P
5009-2.5-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AO
1
3050
5009-3-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
H,W
1
305R
5009-3-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AN,AU,CA
1
305S
5009-3-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AN,AU,CA
1
305T
5009-3-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
Ba
1
305U
5009-4-10
• OUTLET ASSY (SLlPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
K
1
305V
5009-4-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
Y
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10048
20040415
•
•
•
•
•
.~,
1:I.ICO!scott
/scott
Technologies. Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
1A
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
UNITS
PER
ASSY
EFF.
NOMENCLATURE
CODE
1234567
305W
5009-4-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
M, AB, AG, AJ,
AS, BA, BE, BG,
BJ, BN, BU, CB
1
305X
5009-4-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
BE, BN, BU
1
305Y
5009-4-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
a, AC, AD, AT,
1
305Z
5009-4-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
306
5009-7-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
310
5041-00
• OUTLET ASSY
(SUPSD BY ITEM 315)
(REFER TO FIG 4 FOR DET BKDN)
315
5041-,5-15
315A
5041-.5-15
315B
315C
BB
S,AV,BC,BV,BY
1
BZ
1
J,L,N,R,V,X,l,AH,
AR,AW-Al,BD,
BF,BH,BK-BM
1
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
AH
1
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
AH
1
J, L, AR, AW, BD,
1
NP
DELETED
5041-2-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DEl BKDN)
3150
8F, BH, BL
DELETED
315E
5041-2-23
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DFf BKDN)
N,AX,BK
1
315F
5041-2-25
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
R,AY
1
315G
5041-2,5-30
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
V
1
315H
5041-3-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DEl BKDN)
A,J,X
1
315J
5041-4-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DEl BKDN)
L, Z, AR, AW. Al,
BD, BF, BM
1
315K
5041-4-23
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
N,AX,BK
1
315L
5041-4-25
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DEl BKDN)
R,AY
1
315M
5041-7-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DEl BKDN)
BH, BL
1
320
5507-00
• OUTLET ASSY
(SUPSD BY ITEM 325)
(REFER TO FIG 7 FOR DET BKDN)
P,M,AK-AM
1
325
5507-2-23
• OUTLET ASSY (SUPSDS ITEM 320)
(REFER TO FIG 7 FOR DET BKDN)
P
1
NP
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10049
20040415
tileD/scott
Technologies. Inc.
/SCOtf
Aviation
5500'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
1A
PART
NUMBER
AIRLINE
STOCK NO.
I.
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
325A
5507-2-30
• OUTLET ASSY (SUPSDS ITEM 320)
(REFER TO FIG 7 FOR DET BKDN)
AK-AM
1
325B
5S07-4-20
• OUTLET ASSY (SUPSDS ITEM 320)
(REFER TO FIG 7 FOR DET BKDN)
AA
1
325C
5507-4-23
• OUTLET ASSY (SUPSDS ITEM 320)
(REFER TO FIG 7 FOR DET BKDN)
P
1
330
8572-02
• OUTLET ASSY
(REFER TO FIG 6 FOR DET BKDN)
AF
1
331
8572-02
• OUTLET ASSY
(REFER TO FIG 6 FOR DEl BKDN)
AF
1
340
10003566
• OXYGEN COUPLING (SUPSD BY 340A)
AZ
1
340A
802856-01
• OUTLET ASSY
(REFER TO FIG 11 FOR DET BKDN)
[SIMILAR TO PURITAN BENNETI (V49315)
PIN 110111-09] (SlIPSDS 340)
AZ
1
345
36728-01
• OUTLET ASSY (ALT SPN DPB 153)
(REFER TO FIG 13 FOR DET BKDN)
AD,AV
1
802863-02
• OUTLET ASSY
(REFER TO FIG 10 FOR DET BKDN)
BV
1
350
I
-395
MS27769S2
• PLUG, PIPE (CRES) (V96906)
(SPN 6818-01) (0.125 - 27 ANPT THD)
C, T-AC, AE, AG,
AL, AP, 8M, BP,
BQ, BW, Bl, CB
1
-396
MS27769S2
• PLUG, PIPE (CRES) (V96906)
(SPN 6818-01) (0.125 - 27 ANPT THO)
AE
1
400
5510-10
• REGULATOR ASSY
(REFER TO FIG 9 FOR DET BKDN)
500
63SOA13XG
• CYLINDER, STEEL (SPN 635().A13-X-G)
(4.25 CU FT, PAINTED, GRAY-GREEN)
A·BF
1
SOOA
63SOA13XAH
• CYLINDER, STEEL (SPN 635().A13-X-AH)
(4.25 CU FT, PAINTED, BLUE)
8G
1
500B
6350A13XE
• CYLINDER, STEEL (SPN 6350-A13-X-E)
(4.25 CU FT, PAINTED, GREEN AND YELLOW)
BH
1
500C
6350A13XA
• CYLINDER, STEEL (SPN 6350-A13-X-A)
(4.25 CU FT, PAINTED, WAKEFIELD GREEN)
BJ·CB
1
6084-01
• • CYLINDER, STEEL (DOT-3M-1800)
(4.25 CU FT, UNPAINTED)
505
.
~
•
•
•
1
1
NOTE 1: 5500 peA WITHOUT A YEllOW HANDLE (-30, IPL FIGURE 9) MUST USE INSTRUCTION DECAL ITEM 20A.
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10050
20040415
•
•
...
•
1:L/ca/scott
Technologies.
jscott
A "iat;on
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
•
Inc.
CalM & 'PL
THIS PAGE INTENTIONALLY LEFT BLANK
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10051
20040415
tl.lco/SCOtl
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
I .•
•
300 - 350
2 Outlet Regulator
(Top View)
~,
405
•
205
30A
<j::wm
70
55008 Sub Series PCA
Figure 18
(Sheet 1 of 3)
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10052
20040415
•
•
.•
•
1:L/CD
!scott
/Scotl
Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
,.l
255 - 270
.......
-.,-~
---.r----~
/~-
OXYGEN
(
MASK
.
",~
,
--f-f-
........
--------
70
801808-02 Shown
801808 Series (Typical)
803177 Series (Typical)
•
240
"\I-~'
"1" -£w"\,-._~
~
ltk~~mll
( ~ . -.:-.:-i- J
,
-1t=;;j~~~tr·/
_.-
•
';';:7<':
J
'/ --)
....
..c,'
.,.;
_.,,~:.!l>
801807 Series (Typical)
(801807-02 Shown)
55008 Sub Series PCA
Figure 18
(Sheet 2 of 3)
•
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10053
20040415
1:'-/ca/scott
/scott
Technologies.Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
"
J .••
CM'" & IPL
200
I
201
~
~i--=-n.....c:~
70
75
801658 Series (Typical)
•
75
801662 Series (Typical)
5500B Sub Series peA
Figure 1B
(Sheet 3 of 3)
EFFECT1VITY: 5500 SERIES
35-32-18
Page 10054
20040415
•
•
•
•
.~.
tl.lco/scott
Technologies. Inc.
ISCDtt
Alliation
550lJ15600SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
1B
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
-1
5500B1ABE20B
CYliNDER ASSY, PORTABLE
(SPN 5500-B1A-BE20B)
A
RF
-1A
5500B1ABF2QA
CYLlNDERASSY, PORTABLE
(SPN 5500-B1A-BF20A)
B
RF
-1B
550081ABF20B
CYLINDER ASSY, PORTABLE
(SPN 5500-B1A-BF2OB)
C
RF
-1C
5500B1ABF20D
CYLINDER ASSY, PORTABLE
(SPN 5500-B1A-BF20D)
D
RF
-10
5500B1ABF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-B1A·BF23A)
E
RF.
-1E
55ooB1ABF23B
CYLINDER ASSY, PORTABLE
(SPN 5500-81A-BF23B)
F
RF
-1F
55OOB1ABF25A
CYLINDER ASSY, PORTABLE
(SPN 5500-B1A-BF25A)
G
RF
-1G
5500B1ABJOA
CYLINDER ASSY, PORTABLE
(SPN 5500·B1A·B30A)
H
RF
-1H
550081 ACF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-B1A-CF23A)
J
RF
·1J
5500B1ACF25A
CYLINDER ASSY, PORTABLE
(SPN 5500-B1A-CF25A)
K
RF
-1K
5500B1AFF20A
CYLINDER ASSY, PORTABLE
(SPN 5500-B1A-FF20A)
l
RF
-1L
5500B1AF20D
CYLINDER ASSY, PORTABLE
(SPN 5500-B1A-F20D)
M
RF
-1M
5500B1AF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-B1A-F23A)
N
RF
-1N
55ooB1AFJOA
CYLINDERASSY, PORTABLE
(SPN 550Q-B1A-F30A)
P
RF
-1P
55OOB1AYVOE
CYliNDER ASSY, PORTABLE
(SPN 550Q-B1A-YYOE)
a
RF
-10
5500B1AYOP
CYliNDER ASSY, PORTABLE
(8PN 550D-81A-YOP)
R
RF
-1R
5500B 1S82DA
CYLINDER ASSY, PORTABLE
(SPN 550D-B18-B20A)
S
RF
-18
5500B1SB20AP
CYLINDER ASSY, PORTABLE
(SPN 5500-B1S-B20AP)
T
RF
-n
5500B1 UBF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-B111-BF23A)
U
RF
-1U
5500B1VBE208
CYLINDER ASSY, PORTABLE
(SPN 5500-B1V-BE20B)
V
RF
-1V
5500B1VBF20B
CYLINDER ASSY, PORTABLE
(SPN 5500-B1V-BF2OB)
W
RF
- ITEM NOT IllUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10055
20040415
1:lIca/scott
Technologies. Inc.
/scott
Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
EFF.
CODE
UNITS
PER
ASSY
CYLINDERASSY, PORTABLE
(SPN 5500-B1W-BF10A)
X
RF
5500B1WBF20A
CYLINDER ASSY, PORTABLE
(SPN 55OO-B1W-BF20A)
Y
RF
-w
5500B1XVYOE
CYLINDER ASSY, PORTABLE
(SPN 55oo-B1X-VYOE)
Z
RF
-1Z
5500B1XYOE
CYLINDER ASSY, PORTABLE
(SPN 55oo-B1X-YOE)
M
RF
-2
5500B3BF25A
CYLINDER ASSY, PORTABLE
(SPN 5500-B3B-F25A)
AB
RF
-2A
5500B6CBF25A
CYLINDER ASSY, PORTABLE
(SPN 550Q-B6C-BF25A)
AC
RF
-2B
5500B6UBF25A
CYLINDER ASSY, PORTABLE
(SPN 550Q-B6U-BF25A)
AD
RF
-2C
5500B6UF30AN
CYLINDER ASSY, PORTABLE
(SPN 550Q-B6U-F30AN)
AE
RF
-20
10006936
• PLATE, INSTRUCTION (REPLD BY 20Al
(SEE NOTE 1)
1
20A
10009071
• DECAL, INSTRUCTION (REPLS -20) (SEE NOlE1)
1
-30
10005922
• DECAL, OXYGEN 10 (REPLD BY 30A)
1
30A
10009255
• DECAL, OXYGEN 10 (REPLS -30)
USED ONLY WHERE PAINTED TEXT
"BREATHING OXYGEN ONLY - USE NO OIL"
DOES NOT APPEAR ON SIDE OF CYLINDER
(ITEM 510, 515)
1
35
10009374
• LABEL, FAA-PMA ELEGIBtLiTY
(USE ONLY ON PCA's SHIPPED FROM THE
FACTORY FROM JULY 1995 AND LATER)
1
55
5057-00
• PLATE, IDENTIFICATION
1
FIG.
ITEM
1B
PART NUMBER
-1W
5500B1WBF10A
-1X
AIRLINE
STOCK NO.
NOMENCLATURE
1234567
•
ATIACHING PARTS
65
MS21318-7
2
• SCREW, DRIVE (CRES) (V88044)
(#0 x 0.125 in. LNG) (SPN 33343-007)
...
70
13160-00
• CLAMP (All SPN WWD-120)
A-R, U-Y, AB,
AD,AE
1
75
13160-00
• CLAMP (All SPN WWD-120)
S, T,AB,AC
1
200
801658-00
• HARNESS
AB
1
201
801659--00
•• STRAPASSY
AB
1
202
801661-00
•• STRAPASSY
AS
1
205
801660-00
• HARNESS
A-R
1
225
801662-00
• HARNESS
AC
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10056
20040415
•
•
•
•
.~.
1:qCD/SCOtl
/scott
Technologies. Inc. Atliation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
1B
I
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
CODE
UNITS
PER
ASSY
EFF.
NOMENCLATURE
1234567
240
801807-02
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
5,T
1
255
801808-02
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
U,AD,AE
1
260
801808-03
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
V,W
1
270
803177-01
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
X, Y
1
300
5009-00
• OUTLET ASSY
(SUPSO BY ITEM 305)
(REFER TO FIG 5 FOR OET BKDN)
B,E-L,N,P,S,
U,X,Y,AB-AE
1.
305
5009-2-10
• OUTLET ASSY (SUPSOS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
X
1
305A
5009-2-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
B,S, T,Y
1
3058
5009-2-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
E,U
1
305C
5009-2-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR OET BKDN)
G,AC,AD
1
305D
5009-2-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
H
1
305E
5009-2.5-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
J
1
305F
5009-2.5-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
K
1
305G
5009-4-10
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
X
1
305H
5009-4-20
• OUTLET ASSY (SUPSOS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
B,L, Y
1
30SJ
5009-4-20
• OUTLET ASSY (SUPSOS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
L
1
305K
5009-4-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR OET BKDN)
E,J,N,U
1
305l
5009-4·25
• OUTLET ASSY (SUPSOS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
G, K,AB-AD
1
305M
5009-4-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
P,AE
1
310
5041-00
• OUTLET ASSY (SUPSO BY ITEM 315
(REFER TO FIG 4 FOR OET BKDN)
A,C,F,V,W
1
315
5041-2-20
• OUTLET ASSY (SUPSOS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
A,C,V,W
1
315A
5041-2-23
• OUTLET ASSY (SUPSOS ITEM 310)
(REFER TO FIG 4 FOR OET BKDN)
NP
NP
F
1
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10057
20040415
t'lco/scott
/scott
Technologies. Inc. Aviation
SS00l56DO SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
18
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
3158
5041-3-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
A,V
1
315C
5041-4-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
C,W
1
315D
5041-4-23
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
F
1
320
5507-00
• OUTLET ASSY
(SUPSD BY ITEM 325)
(REFER TO FIG 7 FOR DET BKDN)
D,M
1
325
5507-2-20
• OUTLET ASSY (SUPSDS ITEM 320)
(REFER TO FIG 7 FOR DET BKDN)
D
1
325A
5507-4·20
• OUTLET ASSY (SUPSDS ITEM 320)
(REFER TO FIG 7 FOR DET BKDN)
D,M
1
330
8572'()2
• OUTLET ASSY
(REFER TO FIG 6 FOR DET BKDN)
a,l,M
1
331
8572.()2
• OUTLET ASSY
(REFER TO FiG 6 FOR DEI BKDN)
a,l
1
345
36728-01
• OUTLET ASSY
(REFER TO FIG 13 FOR DET BKDN)
AE
1
350
802863-02
• OUTLET ASSY
(REFER TO FIG 10 FOR DET BKDN)
R, T
1
-395
MS27769S2
• PLUG, PIPE (CRES) (V96906)
(SPN 6818-01) (0.125·27 ANPTTHD)
H, M·P, R, S,
M,AB
1
400
5510-10
• REGULATOR ASSY
(REFER TO FIG 9 FOR DET BKDN)
510
6350A14XG
• CYLINDER, STEEL (SPN 635Q-A14-X-G)
(7.15 CU FT, PAINTED, GRAY-GREEN)
A-AA
1
510A
6350A14XAH
• CYLINDER, STEEL (SPN 635Q-A14-X-AH)
(7.15 CU FT, PAINTED, BLUE)
AB
1
510B
6350A14XA
• CYLINDER, STEel (SPN 635Q-A14-X-A)
(7.15 CU FT, PAINTED, WAKEFIELD GREEN)
AC-AE
1
6084.()2
•• CYLINDER, STEEL (DOT-3AA-1800)
(7.15 CU FT. UNPAINTED}
515
NP
•
•
1
1
NOTE 1: 5500 PCA WITHOUT A YEllOW HANDLE (-30, IPl FIGURE 9) MUST USE INSTRUCTION DECAl ITEM 20A.
-ITEM NOT ILLUSTRATED
EFFECTIViTY:
5500 SERIES
35-32-18
Page 10058
20040415
•
•
.~
•
.:
t'lco/scott
jSCDtt
Technologies, Inc. Aviation
55(}(}/5600 SERIES PORTABLE CYLINDER ASSEMBLY - CMM & /PL
THIS PAGE INTENTIONALLY LEFT BLANK
•
•
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10059
20040415
tileD/scott
Technologies, Inc.
/SCDtt
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY • CMAt & IPt
300 - 355
2 Outlet Regulator
(Top View}
•
20
5500C Sub Series PCA
Figure 1C
(Sheet 1 of 3)
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10060
20040415
•
•
'..
tileD/scott
/scott
Technologies.Inc. Aviation
5500'5600 SERIES PORTABLE CYLINDER ASSEMBLY - CMM & IPL
, &
200
I
201
C)'-l..J\----""
70
75
801658 Series (Typical)
•
•
5500C Sub Series PCA
Figure 1C
(Sheet 2 of 3)
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10061
20040415
tl.lCD/scotr
/scott
Technologies, Inc. Aviation
55Da'56oo SERIES PORTABLE CYLINDER ASSEMBLY - CMM & IfL
t ••
250 - 285
/~"----""""-"----~--- OXYGEN
,
MASK
(..
..
"~-"'f-(..------.--- ...
70
805436-01 Shown
801808 Series (Typical)
803177 Series (Typical)
•
240
245
_·l.,..
•• ~
\
/'
1
.,
._-
F.o
~-~~
'1"] '~$,r.....Y"-'-,
i-S
....
•• _~-I
~:-,
...
~ \
w--~~. ;
I~
'.
;-/
.
_"
i
"--' riJ' -.-
801807 Series (Typical)
(801807-02 Shown)
5500C Sub Series PCA
Figure 1C
(Sheet 3 of 3)
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10062
20040415
•
•
•
•
to,
1:'ICo/scott
/scott
Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY • CMM & JPL
of
FIG.
ITEM
1C
PART NUMBER
AIRLINE
STOCK NO.
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
-1
5500C1ABB20B
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-BB20B)
A
RF
-1A
550OC1ABF20A
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-BF20A)
B
RF
-1B
5500C1ABF20B
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-BF20B)
C
RF
-1C
5500C1ABF20D
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-BF20D)
D
RF
-10
5500C 1ABF23A
CYLINDER ASSY, PORTABLE
(SPN 550D-C1A-BF23A)
E
RF
-1E
5500C1ABF23B
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-BF23B)
F
RF
-1F
5500C1ABF23D
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A·BF23D)
G
RF
-1G
5500C1ABF30A
CYliNDER ASSY, PORTABLE
(SPN 5500-C1A-BF30A)
H
RF
-1H
5500C1ABG23A
CYliNDER ASSY, PORTABLE
(SPN 5500-C1A-BG23A)
J
RF
-1J
5500C1AB23A
CYLINDER ASSY, PORTABLE
(SPN 5500-C 1A-B23A)
K
RF
-1K
550OC1AEG23A
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-EG23A)
L
RF
-1L
550OC1AEY20BM
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-EY20BM)
M
RF
-1M
550OC1AE20BN
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-E20BN)
N
RF
-1N
5500C1AE23AN
CYLINDER ASSY, PORTABLE
(SPN 5500-e1A-E23AN)
P
RF
-1P
5500C1AfF20A
CYLINDER ASSY, PORTABLE
(SPN 5500-e1A-FF20A)
a
RF
-1a
5500C1AFF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-e1A-FF23A)
R
RF
-1R
5500C1AFG23A
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-FG23A)
S
RF
-1S
5500C1AfH23A
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-FH23A)
T
RF
-H
5500C1AFY30BN
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-FY30BN)
U
RF
-1U
5500C1AF20B
CYLINDER ASSY, PORTABLE
(SPN 5500-e1A-F20B)
V
RF
-1V
5500C1AF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-F23A)
W
RF
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10063
20040415
1:l./Co/scott
Technologies. Inc.
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
.•
!scott
Aviation
,
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
1C
-1W
5500C1AF23AP
CYLINDER ASSY. PORTABLE
(SPN 5500-C1A-F23AP)
X
RF
-1X
5500C1AF25A
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-F25A)
Y
RF
-1Y
5500C1AXOK
CYLINDER ASSY, PORTABLE
(SPN 5500-C1A-XOK)
l
RF
-il
5500C1AYVOE
CYLINDERASSY, PORTABLE
(SPN 5500-G1A-YYOE)
AA
RF
-2
5500C1AYVOEE
CYLINDER ASSY, PORTABLE
(SPN 5500-G1A·YYOEE)
AB
RF
-2A
5500C1AYVON
CYLINDER ASSY, PORTABLE
(SPN 5500-G1A-YYON)
AC
RF
-28
5500C1AYOE
CYLINDERASS-Y, PORTABLE
(SPN 5500-G1A-YOE)
AD
RF
-2C
5500CiAYOEE
CYLINDER ASSY, PORTABLE
(SPN 5500-G1A-YOEE)
AE
RF
-20
5500C1AYON
CYLINDER ASSY, PORTABLE
(SPN 5500-G1A-YON)
AF
RF
-2E
pSOOC1BBF23D
CYLINDER ASSY, PORTABLE
(SPN 5500-G1B-BF23D)
AG
RF
-2F
5500C1BE25A
CYLINDER ASSY, PORTABLE
(SPN 5500-G1B-E25A)
AH
RF
-2G
5500C1NBF23A
CYLINDER ASSY, PORTABLE
(SPN 55QO-G1N-BF23A)
AJ
RF
-2H
5500C1SBF20A
CYLINDER ASSY, PORTABLE
(SPN 5500-G1S-BF20A)
AK
RF
-2J
5500C1 SBY20AE
CYLINDER ASSY, PORTABLE
(SPN 5500..c1S-BY20AE)
Al
RF
-2K
5500C1 SB20AE
CYLINDER ASSY, PORTABLE
(SPN 5500-C1S-B20AE)
AM
RF
-2L
5500C1 SB20AP
CYLINDER ASSY, PORTABLE
(SPN 5500-C1 S-B20AP)
AN
RF
-2M
5500C1 SF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-G1S-F23A)
AP
RF
-2N
5500C1TBF20B
CYLINDER ASSY, PORTABLE
(SPN 5500-CH-BF20B)
AO
RF
-2P
5500C1TF20BM
CYLINDER ASSY, PORTABLE
(SPN 5500..(;1 T-F20BM)
AR
RF
-20
5500C1 LlBF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-C1 U-BF23A)
AS
RF
-2R
5500C1UBF25A
CYLINDER ASSY, PORTABLE
(SPN 550o-C1 lJ..SF25A)
AT
RF
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10064
20040415
•
•
•
n.
1:l./cojscott
/SCOft
Technologies,Inc. Aviation
550015600 SERJES PORTABLE CYLINOER ASSEMBLY - CMM & IPL
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
1C
•
•
·2S
550OC1UBF30A
CYLINDERASSY, PORTABLE
(SPN 5500-C1 U-BF30A)
AU
RF
-2T
5500C1 UB23AN
CYUNDER ASSY, PORTABLE
(SPN 5500-C1U-B23AN)
AV
RF
-2U
5500C1 UB25A
CYLINDER ASSY, PORTABLE
(SPN 5500-e1U-B25A)
AW
RF
-2V
5500C1UFF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-C1U-FF23A)
,.;x
RF
·2W
5500C1UF20AN
CYLINDER ASSY, PORTABLE
(SPN 5500-C1 U-F20AN)
AY
RF
-2X
5500C1UF23A
CYliNDER ASSY, PORTABLE
(SPN 5500-C1U-F23A)
AZ.
RF
-2Y
5500C 1UF30AN
CYLINDER ASSY, PORTABLE
(SPN 5500-e1U-F30AN)
BA
RF
-2Z
5500C1VFG20B
CYLINDER ASSY, PORTABLE
(SPN 5500-e1V-FG20B)
BB
RF
-3
5500C1VFY30AN
CYLINDER ASSY, PORTABLE
(SPN 5500-C1V-FY30AN)
Be
RF
-3A
5500C1VFY30BN
CYliNDER ASSY, PORTABLE
(SPN 5500-CtV-FY30BN)
BD
RF
-3B
5500C1VF20BM
CYLINDER ASSY, PORTABLE
(SPN 5SOO-e1V-F20BM)
BE
RF
-3C
5500C1 VF30AN
CYLINDER ASSY, PORTABLE
(SPN 5500-etV-F30AN)
BF
RF
-3D
5500C1 VF30BN
CYLINDER ASSY, PORTABLE
(SPN 5500-CtV-F30BN)
BG
RF
-3E
5500C1WBF15A
CYLINDER ASSY, PORTABLE
(SPN SSOO-e1W-BF15A)
BH
RF
-3F
5500C1 WBF23A
CYliNDER ASSY, PORTABLE
(SPN 5500-C1W-BF23A)
BJ
RF
-3G
5500C1 WBF30A
CYLINDER ASSY, PORTABLE
(SPN 5500-e1W-BF30A)
BK
RF
-3H
550OC1XBF20B
CYLINDER ASSY, PORTABLE
(SPN 5500-e1X-BF20B)
BL
RF
-3J
5500C1XYON
CYLINDER ASSY, PORTABLE
(SPN 5500-C1X-YON)
BM
RF
.JK
5500C1 YBF20B
CYLINDER ASSY, PORTABLE
(SPN 550o-C1Y-BF20B)
BN
RF
-3L
5500C6ABF15A
CYLINDER ASSY, PORTABLE
{SPN SSQO-CSA-BF15A}
BP
RF
-3M
5500C6ABF20B
CYLINDER ASSY, PORTABLE
(SPN 5500-C6A-BF20B)
BO
RF
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10065
20040415
t'lco/SCOtl
Technologies.
Inc.
/scott
Aviation
550015600 SERiES PORTABLE CYLINDER ASSEMBLY • CMM & IPL
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
•
1C
-3N
5500C6ABF23A
CYLINDER ASSY, PORTABLE
(SPN 550D-C6A-BF23A)
BR
RF
-3P
5500C6ABF23B
CYI.lNDERASSY, PORTABLE
(SPN 5500-C6A-BF23B)
BS
RF
-30
5500C6ABF23D
CYLINDER ASSY, PORTABLE
(SPN 5500-C6A-BF23D)
BT
RF
-3R
5500C6ABF25A
CYLINDER ASSY. PORTABLE
(SPN 5500-C6A-BF25A)
BU
RF
-3S
5500C6ABG30B
CYLINDER ASSY. PORTABLE
(SPN 550o-C6A-BG30B)
BV
RF
-3T
5500C6AEF2OA
CYLINDER ASSY, PORTABLE
(SPN 550o-C6A-EF20A)
BW
RF
-3U
5500C6AF20A
CYliNDER ASSY, PORTABLE
(SPN 550o-C6A-F20A)
BX
RF
-3V
5500C6AF20AR
CYLINDER ASSY, PORTABLE
(SPN 5500-C6A-F20AR)
BY
RF
-3W
5500C6AF23AE
CYLINDER ASSY, PORTABLE
(SPN 5500-C6A-F23AE)
BZ
RF
5500C6AF30A
CYLINDER ASSY, PORTABLE
(SPN 5SOO-C6A-F30A)
CA
RF
-3Y
5500C6AF30AE
CYLINDER ASSY. PORTABLE
(SPN 5500-C6A-F30AE)
CB
RF
-3Z
5500C6AF30AN
CYLINDER ASSY. PORTABLE
(SPN 5500-C6A-F30AN)
CC
RF
-4
5500C6AGJOAN
CYLINDER ASSY. PORTABLE
(SPN5500-C6A-G30AN}
CD
RF
-4A
5500C6AVYON
CYUNDER ASSY, PORTABLE
(SPN 550D-C6A-YYON)
CE
RF
-4B
5500C6AYON
CYliNDER ASSY. PORTABLE
(SPN 550o-C6A-YON)
CF
RF
-4C
5500C6EBF23D
CYlINDERASSY, PORTABLE
(SPN 5500-C6E-BF23D)
CG
RF
-40
5500C6RBF230
CYLINDER ASSY, PORTABLE
(SPN 5500-C6R-BF23D)
CH
RF
-4E
5500C6TG20B
CYUNDER ASSY, PORTABLE
(SPN 5500-C6T-G20B)
CJ
RF
-4F
5500C6UBF3OA
CYLINDER ASSY, PORTABLE
(SPN 5500-C6U-BF30A)
CK
RF
-4G
5500C6UF23AP
CYLINDER ASSY. PORTABLE
(SPN 5500-C6U-F23AP)
CL
RF
-4H
5500C6L1F30AN
CYLINDER ASSY, PORTABLE
(SPN 5500-C6U-F30AN)
CM
RF
-3X
I
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10066
20040415
•
•
•
•
".
t:qco/scott
!SCOff
Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & In
EFF.
CODE
UNITS
PER
ASSY
CYLINDER ASSY, PORTABLE
(SPN 550o-C6W-FF23A)
CN
RF
5500C6XBF23D
CYLINDER ASSY, PORTABLE
(SPN 550o..C6X-BF23D)
CP
RF
-4L
5500C9ABF20A
CYUNDER ASSY, PORTABLE
(SPN 550o..C9A-BF20A)
CO
RF
-4M
5500C9ABF20B
CYliNDER ASSY, PORTABLE
(SPN 550o..C9A-BF20B)
CR
RF
-4N
5500C9AFF10A
CYLINDER ASSY, PORTABLE
(SPN 550o..C9A-FF10A)
CS
RF.
-4P
55ooC9SF30A
CYLINDER ASSY, PORTABLE
(SPN 550o..C9S-F30A)
CT
RF
-40
55OOC9UF30AN
CYLINDER ASSY, PORTABLE
(SPN 550o-C9U·F30AN)
CU
RF
-4R
5500C9UH20A
CYLINDER ASSY, PORTABLE
(SPN 5500-C9U-H20A)
cv
RF
-48
5500C9WFF10A
CYLINDER AS8Y, PORTABLE
(SPN 5500-C9W-FF10A)
CW
RF
-4T
5500C9WYOE
CYLINDER ASSY, PORTABLE
(SPN 5500·C9W-YOE)
ex
RF
-4U
5500C9XBB20A
CYLINDER AS8Y, PORTABLE
(SPN 5500·C9X-BB20A)
CY
RF
-20
10006936
• PLATE, INSTRUCTION (REPLD BY 20A)
(SEE NOTE 1)
A-CP
1
FIG.
ITEM
1C
PART NUMBER
-4J
5ooOC6WFF23A
-4K
AIRLINE
STOCK NO.
I
NOMENCLATURE
1234567
20A
10009071
• DECAL, INSTRUCTION (REPLS -20) (SEE NOTE1)
A-CP
1
-30
10005922
• DECAL, OXYGEN 10 (REPLD BY 30A)
A-CP
1
30A
10009255
• DECAL, OXYGEN 10 (REPLS -30)
USED ONLY WHERE PAINTED TEXT
"BREATHING OXYGEN ONLY - USE NO OIL"
DOES NOT APPEAR ON SIDE OF CYLINDER
(ITEM 550 THRU 555A)
A-CP
1
35
10009374
• LABEL, FM-PMA ELIGIBILITY
(USED ONLY PCA's SHIPPED FROM THE
FACTORY FROM JULY 1995 AND LATER)
-40
10001018
• PLACARD, INSTRUCTION
(USED ONLY ON 5000C 9 SERIES)
45
10001019
• LABEL
-50
10001020
• PLACARD, AVIATOR OXYGEN
(USED ONLY ON 5500C 9 SERIES)
55
5057-00
• PlATE, IDENTIFICATION
(USED ONLY ON 5oo0C 9 SERIES)
1
CQ-CY
1
CQ-CY
1
CQ-CY
1
1
ATTACHING PARTS
65
•
MS21318·7
• SCREW, DRIVE (CRES) (V88044)
(00 x 0.125 in. LNG) (SPN 33343-007)
2
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10067
20040415
-tl./co/scott
Technologies.
Inc.
Aviation
S5M'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
...
!scott
CMM & IPL
UNITS
PER
ASSY
EFF.
CODE
NOMENCLATURE
1234567
•
1C
•••
70
13160-00
• ClAMP (ALT SPN WWD-120)
A-AJ, A5-BK,
BN-CH, CK-CN, caCS, Cu-cx,
1
75
13160-00
• ClAMP (ALT SPN WWD-120)
AG, AH, AK-AR,
CJ,CT
1
200
801658-00
• HARNESS
AG,AH
1
201
801659-00
•• STRAPASSY
AG,AH
1
202
801661-00
•• STRAPASSY
AG,AH
t
205
801660-00
• HARNESS
A-AF, BP-CF,
CO-CS
1
215
801660-03
• HARNESS
CG
1
240
801807-02
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
AK·AP,CT
1
245
801807-03
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
AO,AR,CJ
1
250
801808-01
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
CH
1
255
801808-02
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
AS-BA, CK-CM, CU, CV
1
260
801808-03
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DEl BKDN)
BB-BG
1
270
803177-01
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
BH-BK, CN,
cW,CX
1
275
803177-02
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
BN
1
285
805436-01
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
AJ
1
300
5009-00
• OUTLET ASSY (SUPSD BY ITEM 305)
(REFER TO FIG 5 FOR Del BKDN)
B,E,H-L,P-T,W,X,Y,
AH-AP,AS,AT,AU·BA,
AU-BA,BC,BF,BH-BK,
BP,BR,BU, BW-CD,
CK-CN, CQ,CS-CW, CY
1
305
5009-2-15
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
BH,BP
1
305A
5009-2-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
8,AK-AN,
CO,CY
t
3058
5009·2-20
• OUlLET ASSY (SUPSDS ITEM 3(0)
(REFER TO FIG 5 FOR DET BKDN)
CY
1
305C
5009-2-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR Del BKON)
E, .1,K, AJ, AS, AV, BJ,
BR
1
3050
5009-2-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR Del BKDN)
AT,AW,BU
1
NP
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10068
20040415
•
•
•
•
".
1:qca/scott
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
1C
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
CODE
UNITS
PER
ASSY
EFF.
NOMENCLATURE
1234567
305E
5009-2·30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
H,AU, BK,CK
1
30SF
5009-3·20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DEl BKDN)
BW
1
305G
5009-3-23
• OUTlET ASSY (SlIPSDS ITEM 300)
(REFER TO FIG 5 FOR DEl BKDN)
L,P
1
305H
5009·3·25
• OUTlET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AH
1
30SJ
5009-4-10
• OUTlET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
CS,CW
1
305K
5009-4-10
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
CS,CW
1
305L
5009-4-15
• OUTLET ASSY (SLlPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
BH,BP
1
305M
5009-4-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG S FOR DET BKDN)
B, Q,AK,AY,
BW-BY,CQ
1
305N
5009-4-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
Q
1
305P
5009-4-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
E, R·T, W,X,
AJ, AP, AS, AX, AZ.,
BJ, BR, BZ, CL, CN
1
305Q
5009-4-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DEl BKDN)
R,AX,CN
1
305R
5009-4-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKON)
Y. AT,
30SS
5009-4-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
H, AU, BA, BC, SF,
BK, CA-CC, CK,
CM.CT,CU
1
30ST
5009-7-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
J, L,S
1
305U
5009-7-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
CD
1
305V
5009-8-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
CV
1
305W
5009-8-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
T
1
310
5041-00
• OUTLET ASSY (SUPSD BY ITEM 315)
(REFER TO FIG 4 FOR DET BKDN)
A,C,F,M,N,U,V,AQ,
AR,BB,BD,BE,BG,
BL,BN,BQ,BS,BV,
CJ,CR
1
315
5041-2-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
A, C,AQ, BL,
1
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DEI BKDN)
A
315A
•
/SCOtf
Technologies.
Inc. Aviation
5041-2-20
NP
au
1
BN, BQ,CR
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10069
20040415
tlleo/scott
Technologies. Inc.
5500'5600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
....
/scott
Aviation
CMU & Iff.
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
1C
315B
5041-2-23
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
F,BS
1
315C
5041·2-30
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
BV
1
3150
5041-3-20
• OUTLET ASSY (SlIPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
M,N
1
315E
5041-4·20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
C, V,AQ,AR, BB,BE,
BE,Bl,BN,BQ,CR
1
315F
5041-4·23
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR Del BKDN)
F,BS
1
315G
5041-4-30
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
U,BD,BG
1
315H
5041·7-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
BB,CJ
1
315J
5041-7-30
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DEl BKDN)
BV
1
320
5507-00
• OUTLET ASSY (SUPSD BY ITEM 325)
(REFER TO FIG 7 FOR DET BKDN)
D,G,AG,ST,
CG,CH,CP
1
325
,5507·2-20
• OUTLET ASSY (SUPSDS ITEM 320)
(REFER TO FIG 7 FOR DET BKDN)
0
1
325A
5507·2·23
• OUTLET ASSY (SUPSDS ITEM 320)
(REFER TO FIG 7 FOR DEl BKDN)
G,AG,BT,
CG,CH,CP
1
3258
5507-4-20
• OUTLET ASSY (SUPSDS ITEM 320)
(REFER TO FIG 7 FOR DET BKDN)
D
1
325C
5507-4-23
• OUTLET ASSY (SUPSDS ITEM 320)
(REFER TO FIG 7 FOR DET BKDN)
G,AG,BT,
CG,CH,CP
1
330
8572-02
• OUTLET ASSY
(REFER TO FIG 6 FOR DET BKDN)
M"AB, AD, AE, AL,
AM, BZ, CB, CX
1
331
8572-02
• OUTLET ASSY
(REFER TO FIG 6 FOR DET BKDN)
M,AB,AE
1
340
10003566
• OXYGEN COUPLING (SUPSD BY 340A)
M,AR,BE
1
340A
802856-01
• OUTLET ASSY
(REFER TO FIG 11 FOR DET BKDN)
[SIMILAR TO PURITAN BENNETT (V49315)
PIN 110111-09] (SUPSDS 340)
M,AR,BE
1
345
36728-01
• OUTLET ASSY (ALT SPN DPB 153)
(REFER TO FIG 13 FOR DET BKDN)
N, P, U, AC,AF, AV,
AY, BA, BC, BD,
BF,BG,BM,
CC-CF, CM, CU
1
346
36728-01
• OUTLET ASSY (ALTSPN DPB 153)
(REFER TO FIG 13 FOR Del BKDN)
AC,CE
1
350
802863-Q2
• OUTLET ASSY (REFER TO FIG 10 FOR DET BKDN)
X, AN, Cl
1
355
10006017
• OUTLET ASSY
BY
1
NP
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10070
20040415
•
•
•
".
.~
1:qcCJ /scott
Technologies, Inc.
jscotf
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
NOMENCLATURE
1234567
UNITS
PER
EFF.
CODE
ASSY
lC
•
•
-395
MS27769S2
• PLUG, PIPE (CRES) (V96906)
(SPN 6818-01) (0,125 -27 ANPT THO)
K, V. W, Y, Z, AD.
AF. AH, AP, AW,
AZ, 8M, ex, CA.
CF, CJ,CT, CV,
CX
1
-396
MS27769S2
• PLUG, PIPE (GRES) (V96906)
(SPN 6818-01)(0.125-27 ANPTTHD)
Z
1
400
5510-10
• REGULATOR ASSY
(REFER TO FIG 9 FOR DET BKDN)
550
6350A20XG
• CYLINDER, STEEL (SPN 6350-A20-X-G)
(11 CU FT. PAINTED, GRAY-GREEN)
A-BN
,.
550A
6350A20XA
• CYLINDER, STEEL (SPN 6350-A2Q-X·A)
(11 CU FT, PAINTED, WAKEFIELD GREEN)
BP-CY
1
555
6084-03
•• CYLINDER, STEEL (DOT-3M-1800)
(11 CU FT, UNPAINTED)
(SUPSD BY ITEM 555A)
555A
6084-20
••
1
NP
CYLINDER, STEEL (DOT-3M-18oo)
[11 CU FT, UNPAINTEDl (SUPSDS ITEM 555)
1
1
NOTE 1: 5500 PCA WITHOUT A YELLOW HANDLE (-30. IPL FIGURE 9) MUST USE INSTRUCTION DECAL ITEM 2OA.
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10071
20040415
1:L/Co/scott
Technologies. Inc.
.'.
/SCOft
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
•
300·350
2 Outlet Regulator
(Top View)
•
35
205
1'\.-.
.(.,J-W
_
~ .....
70
520
525
55000 Sub Series peA
Figure 10
(Sheet 1 of 2)
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10072
20040415
•
...
f:l./ca/scott
Technologies.Inc.
jscott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
ClAM & fPL
265
270
---
/~- .............,.--------
OXYGEN
MASK
I
•
(
\
"
....
_-/-L...J--
-------
70
•
•
801808-01 Shown
801808 Series (Typical)
803177 Series (Typical)
5500D Sub Series PCA
Figure 1D
(Sheet 2 of 2)
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10073
20040415
..
1:'1ca/scott
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
10
PART NUMBER
AIRLINE
STOCK NO.
•
CMU & 'PL
NOMENCLATURE
1234567
EFF,
CODE
UNITS
PER
ASSY
-1
5500D1ABF23A
CYUNDER ASSY, PORTABLE
(SPN 5500-D1A-BF23A)
A
RF
-1A
5500D1AE20A
CYLINDER ASSY, PORTABLE
(SPN 55OO-D1A·E20A)
B
RF
·1B
5500D1AE25A
CYLINDER ASSY, PORTABLE
(SPN 5500-D1A·E25A)
C
RF
-1C
5500D1AF23A
CYLINDER ASSY, PORTABLE
(SPN5500-D1A-F23A)
D
RF
-10
5500D1AVYOE
CYLINDER ASSY, PORTABLE
(SPN 5500-D1A-VYOE)
E
RF
-1E
5500D1AVYOP
CYLINDER ASSY, PORTABLE
(SPN 550D-D1A·VYOP)
F
RF
-1F
5500D1AYOE
CYlINDER ASSY, PORTABLE
(SPN 550D-D1A-YOE)
G
RF
-1G
550001 AYON
CYlINDER ASSY, PORTABLE
(SPN 5500-D1A-YON)
H
RF
-1H
550001 PCC20A
CYlINDERASSY, PORTABLE
(SPN 5500-01 P-CC20A)
J
RF
-1J
550001WBB15A
CYLINDER ASSY, PORTABLE
(SPN 5500-D1W-BB15A)
K
RF
-1K
5500D1XYOE
CYLINDER ASSY, PORTABLE
(SPN 55OO-D1X-YOE)
L
RF
-1L
5500D1XYON
CYLINDER ASSY, PORTABLE
(SPN 55OO-D1X-YON)
M
RF
-1M
5500DGAVYOE
CYLINDER ASSY, PORTABLE
(SPN 5500-D6A·VYOE)
N
RF
-1N
5500DGAVYON
CYLINDER ASSY, PORTABLE
(SPN 5500-D6A· YVON)
P
RF
-1P
5500D6AYOE
CYLINDER ASSY, PORTABLE
(SPN 5500-D6A- YOE)
0
RF
-10
55OOD6PBF25A
CYLINDER ASSY, PORTABLE
(SPN 5500-D6P-BF25A)
R
RF
-1R
5500D6XHH30A
CYLINDER ASSY, PORTABLE
(SPN 5500-D6X-HH30A)
S
RF
-20
10006936
• PLATE, INSTRUCTION (REPLO BY 2OA)
(SEE NOTE 1)
1
20A
10009071
• DECAL, INSTRUCTION (REPlS -20) (SEE NOTE1)
1
-30
10005922
• DECAL, OXYGEN 10 (REPLD BY 3OA)
1
30A
10009255
• DECAL, OXYGEN 10 (REPLS -30)
USED ONLY WHERE PAINTED TEXT
"BREATHING OXYGEN ONLY - USE NO OIL'
DOES NOT APPEAR ON SIDE OF CYLINDER
(ITEM 520 THRU 525)
1
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10074
20040415
•
•
•.
".
:
1:qCD /SCOlt
Technologies, Inc.
jscott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
EFF.
NOMENCLATURE
1234567
CODE
UNITS
PER
ASSY
10
•
•
35
10009374
• LABEL, FAA-PMA ELIGIBILITY
(USED ONLY PCAlSHIPPED FROM THE
FACTORY FROM JULY 1995 AND LATER)
1
55
505HlO
• PLATE, IDENTIFICATION
1
65
MS2131B-7
• SCREW, DRIVE (CRES) (V88044)
(#0 x 0.125 IN. LNG) (SPN 33343..(07)
2
70
13161-00
• CLAMP (ALT SPN WWD-176)
A·K, N-R
1
205
801660·00
• HARNESS
A-H, N-Q
1
265
801808·05
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
J, R
1
270
803177-01
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
K
1
300
5009-00
• OUTLET ASSY (SUPSD BY ITEM 305)
(REFER TO FIG 5 FOR DET BKDN)
A-D,J,K,R,S
1
J05
5009-2-15
• OUTLET ASSY (SUPSDS ITEM JOO)
(REFER TO FIG 5 FOR DET BKDN)
K
1
J05A
5009-2·15
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
K
1
305B
5009-2-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
A
1
305C
5009-2-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
R
1
305D
5009-2.5-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
J
1
J05E
5009-2.5-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
J
1
305F
5009-3-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DEl BKDN)
B
1
305G
5009-3-25
• OUTlET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
C
1
30SH
50094-23
• OUTLET ASSY (SUPSDS ITEM JOO)
(REFER TO FIG 5 FOR DEl BKDN)
A,D
1
J05J
50094·25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
R
1
305K
5009-8-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DEl BKDN)
S
1
305L
5009-8-30
• OUTLET ASSY (SUPSDS ITEM JOO)
(REFER TO FIG 5 FOR DET BKDN)
S
1
330
8572-02
• OUTLET ASSY
(REFER TO FIG 6 FOR DEl BKDN)
331
8572..Q2
• OUTLET ASSY
(REFER TO FIG 6 FOR DET BKDN)
NP
E,G,L,N,Q
E,N
1
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10075
20040415
-tYCCI/scott
Technologies. Inc.
/scott
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
..
•
Aviation
eMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
10
345
36728-01
• OUTLET ASSY
(REFER TO FIG 13 FOR DET BKDN)
H.M,P
1
346
36728-01
• OUTLET ASSY
(REFER TO FIG 13 FOR DET BKDN)
P
1
350
802863-02
• OUTLET ASSY
(REFER TO FIG 10 FOR DET BKDN)
F
1
351
802863-02
• OUTLET ASSY
(REFER TO FIG 10 FOR DET BKDN)
F
1
-395
MS27769S2
• PLUG, PIPE (CRES) (V96906)
(SPN 6818-01) (0.125-27 ANPTTHD)
B-D, G, H, L, M, Q
1
405
5510-13
• REGULATOR ASSY
(REFER TO FIG 9 FOR DET BKDN)
520
6350A4XG
• CYUNDER, STEEL (SPN 6350-A4-X-G)
(22 CU FT, PAINTED, GRAY-GREEN)
A-M
1
520A
6350A4XA
• CYUNDER, STEEL (SPN 6350-A4-X-A)
(22 CU FT, PAINTED, WAKEFIELD GREEN)
N-5
1
525
6084-04
•• CYLINDER, STEEL (DOT-3AA-1800)
(22 CU FT, UNPAINTED)
1
1
NOTE 1: 5$00 PCA WITHOUT A YELLOW HANDLE (-30, IPL FIGURE 9) MUST USE INSTRUCTION DECAL ITEM 20A.
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10076
20040415
•
•
.',
t'lco/SCOtl
/scott
Technologies, Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
THIS PAGE INTENTIONALLY LEFT BLANK
•
•
EFFECTIVITY:
5500 SERIES
35-32-18
.
Page 10077
20040415
1:l.Ica!scott
/SCOtf
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
.
~
•
.•
~
CMM & #PL
300 - 350
300 - 350
'--'-"~
-...--ml1IIIrI.
2 Outlet Regulator
(Top View)
300 - 350
3 Outlet Regulator
(Top View)
65
•
35
~WXl-f
205
30A
~1IJ)o-1
70
500 - 565
5500F, 5500G, 5500J, 5500L, 5500M, 5500P, and 5500S Sub Series peA
Figure 1E
(Sheet 1 of 2)
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10078
20040415
•
•
."
t'lco/scott
Techn%gies,
Inc.
ISCDtt
A lIiation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & 'PL
255
270
___..... -.J.
/~..
~----_..
OXYGEN
MASK
(
.
,
"-.._-~---------70
801808-01 Shown
803177 Series (Typical)
•
75
801662-00
5500F. 5500G. 5500J, 5500L, 5500M, 5500P, and 5500S Sub Series peA
Figure 1E
(Sheet 2 of 2)
•
EFFECTIVITY:
5500 SERIES
35·32·18
Page 10079
20040415
t:qca/scott
!scott
Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
1E
PART NUMBER
AIRLINE
STOCK NO.
CMM & JPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
-1
5500F1XFH20A
CYLINDER ASSY, PORTABLE
(SPN 5500-F1X-FH20A)
A
RF
·1A
5500F6ABB30A
CYLINDER ASSY, PORTABLE
(SPN 5500.f6A-BB30A)
B
RF
-1B
5500G1AB23A
CYLINDER ASSY, PORTABLE
(SPN 5500-G1A-B23A)
C
RF
-1C
5500G1AF20A
CYliNDER ASSY, PORTABLE
(SPN 550D-G1A·F20A)
D
RF
·10
5500G1WEE30A
CYLINDER ASSY, PORTABLE
(SPN 550D-G1W-EE30A)
E
RF
-1E
5500J1MBE20B
CYLINDER ASSY, PORTABLE
(SPN 550D-J1A-ABE20B)
F
RF
-1F
5500J1ABBF20A
CYLINDER ASSY, PORTABLE
(SPN 550D-J1A-BBF20A)
G
RF
-1G
5500J1ABBF20B
CYLINDER ASSY, PORTABLE
(SPN 550D-J1A-BBF20B)
H
RF
-1H
5500J1ABBF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-J1A-BBF23A)
J
RF
5500J1ABEG20B
CYLINDER ASSY, PORTABLE
(SPN 5500-J1A-BEG20B)
K
RF
-1K
5500J1ABFl23A
CYLINDER ASSY, PORTABLE
(SPN550D-J1A-BFl23A)
L
RF
-1L
5500L1WBBF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-l1 W-BBF23A)
M
RF
-1M
5500L6CBBF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-l6C-BBF23A)
N
RF
-1N
5500L6CBBF25A
CYLINDER ASSY, PORTABLE
(SPN 5500-l6C-BBF25A)
P
RF
·1P
5500L6UBBF25A
CYliNDER ASSY, PORTABLE
(SPN 5500-l6U-BBF25A)
0
RF
·10
5500L6WBBF25A
CYLINDER ASSY, PORTABLE
(SPN 5500-l6W-BBF25A)
R
RF
-1R
5500L6WBEF23A
CYLINDER ASSY, PORTABLE
(SPN 5500-l6W-BEF23A)
5
RF
-1S
5500L6WFF23AP
CYLINDER ASSY, PORTABLE
(SPN 5500-l6W-FF23AP)
T
RF
-1T
5500M1ABBB20B
CYliNDER ASSY, PORTABLE
(SPN 5500-t.11A-BBB20B)
U
RF
-1U
5500M1ABH23A
CYLINDER ASSY, PORTABLE
(SPN 5500-t.11A-BH23A)
V
RF
-1V
5500M1ABH23AN
CYLINDER ASSY, PORTABLE
(SPN 5500-t.11A-BH23AN)
W
RF
·1J
I
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10080
20040415
•
•
•
•
•
",
1:I.Ica/scott
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
EFF.
CODE
UNITS
PER
ASSY
CYLINDER ASSY, PORTABLE
(SPN 5500-M1A-FFF25A)
X
RF
5500M1 ALLL30A
CYliNDER ASSY, PORTABLE
(SPN 5500-M1A-LLL30A)
Y
RF
-1Y
5500M1 AXOK
CYLINDER ASSY, PORTABLE
(SPN 5500-M1A-XOK)
Z
RF
-1Z
5500M1WBF23AM
CYLINDER ASSY, PORTABLE
(SPN 5500-M1W-BF23AM)
AA
RF
-2
5500M6WBBF10A
CYLINDER ASSY, PORTABLE
(SPN 5500-t.16W-BBF10A)
AB
RF
-2A
5500M6WFF23AN
CYLINDER ASSY, PORTABLE
(SPN 5500-M6W-FF23AN)
AC
RF
-2B
5500M6WFF23AP
CYLINDER ASSY, PORTABLE
(SPN 5500-M6W-FF23AP)
AD
RF
-2C
5500P6UEEE20A
CYLINDER ASSY, PORTABLE
(SPN 5500-P6U-EEE20A)
AE
RF
-2D
5500S6XYYOE
CYLINDER ASSY, PORTABLE
(SPN 5500-S6X-YYOE)
AF
RF
-2E
5500S6XVYON
CYLINDER ASSY, PORTABLE
(SPN 5500-S6X-VYON)
AG
RF
·2F
5500S9XVYYOE
CYliNDER ASSY, PORTABLE
(SPN 5500-S9X-YVYOE)
AH
RF
-2G
5500S9XVYOE
CYliNDER ASSY, PORTABLE
(SPN 5500-S9X-YYOE)
AJ
RF
-20
10006936
• PlATE, INSTRUCTION (REPLD BY 20A)
(SEE NOTE 1)
A-AG
1
20A
10009071
• DECAL, INSTRUCTION (REPLS -20) (SEE NOTE1)
A-AG
1
-30
10005922
• DECAL, OXYGEN 10 (REPLD BY 30A)
A-AG
1
30A
10009255
• DECAL, OXYGEN ID (REPLS -30)
USED ONLY WHERE PAINTED TEXT
'BREATHING OXYGEN ONLY - USE NO OIL'
DOES NOT APPEAR ON SIDE OF CYLINDER
(ITEM 500 THRU 565)
A-AG
1
35
10009374
• LABEL, FAA-PMA ELIGIBILITY
(USED ONl Y PC~HIPPED FROM THE
FACTORY FROM JULY 1995 AND LATER)
-40
10001018
• PLACARD, INSTRUCTION
(USED ONLY ON 55005 9 SERIES)
AH,AJ
1
45
10001019
• lABEL
(USED ONLY ON 55005 9 SERIES)
AH,AJ
1
·50
10001020
• PLACARD,AVIATION OXYGEN
(USED ONLY ON 55005 9 SERIES)
AH,AJ
1
55
5057-00
• PLATE, IDENTIFICATION
FIG.
ITEM
1E
PART NUMBER
-1W
5500M1 AFFF25A
-1X
AIRLINE
STOCK NO.
NOMENCLATURE
1234567
1
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10081
20040415
t:qco/scott
Technologies. Inc.
/SCOtf
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
..
"
CMM & IPL
NOMENCLATURE
1234567
UNITS
PER
ASSY
EFF.
CODE
1E
ATTACHING PARTS
65
MS21318-7
...
70
13160-00
• CLAMP (ALT SPN WWD-120)
F-M, Q-AD
1
AE
1
• SCREW, DRIVE (CRES) (V88044) (#(J x 0.125 in. LNG)
2
70A
13161-00
• CLAMP (ALT SPN WWD-176)
70B
13162-00
• CLAMP (AU SPN WWD-224)
B-E
1
75
13160-00
• CLAMP (ALT SPN WWD-120)
N,P
1
205
801660-00
• HARNESS
8-0, F-l, U-Z
1
225
801662-00
• HARNESS
N,P
1
255
801808-02
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
Q,AE
1
270
803177-01
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 2 FOR DET BKDN)
E. M, R-T. AA-AD
1
300
5009-00
• OUTLET ASSY (SUPSD BY ITEM 305)
(REFER TO FIG 5 FOR DET BKDN)
A-E,G,J,L-T,
V-Y,AA-AE
1
305
5009-2-10
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AS
1
5009-2-10
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AS
1
3058
5009-2-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
G
1
305e
5009-2-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DEl BKDN)
G
1
305D
5009-2-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
C, J, L, M, N, S, V,
W,M
1
305E
5009-2-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DEl BKDN)
J,M,N
1
305F
5009-2-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DEl BKDN)
P-R
1
305G
5009-2-25
• OUTLET ASSY (SUPSDS ITEM 300)
P-R
1
305A
I
NP
•
(REFERTO FIG 5 FOR DET BKDN}
305H
5009-2-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DEl BKDN)
B
1
305J
5009-2-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET 8KDN)
B
1
305K
5009-3-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AE
1
305L
5009-3-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AE
1
305M
5009-3-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AE
1
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10082
20040415
•
•
•
•
.-.
t'lca/scou
Technologies. Inc.
jSCDtt
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
1E
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
NOMENCLA lURE
1234567
EFF.
CODE
UNITS
PER
ASSY
305N
5009·3·23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
S
1
305P
5009·3·30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
E
1
305Q
5009-3-30
• OUTlET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
E
1
305R
5009-4-10
• OUTlET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AS
1
305S
5009-4·20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDNl
A,D,G
1.
305T
5009-4-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
J, L-N, S, T,
M,AC.AD
1
305U
5009-4·23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
T,AC,AD
1
305V
5009-4·25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
P-R.X
1
305W
5009-4·25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG FOR DET BKDN)
X
1
305X
5009-4-25
• OUTlET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
X
1
305Y
5009-4.5-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
L
1
305Z
5009-4.5-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
Y
1
306
5009-4.5-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
Y
1
306A
5009-4.5-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
Y
1
306B
5009-8·20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
A
1
306C
5009-8·23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
V,W
1
310
5041-00
• OUTLET ASSY (SUPSD BY ITEM 315)
(REFER TO FIG 4 FOR DET BKDN)
F.H.K,U
1
315
5041-.5-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
F
1
315A
5041·2·20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
F.H,K,U
1
315B
5041·2·20
• OUTlET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
H,U
1
315C
5041·2·20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
U
1
NP
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10083
20040415
~'1C;CJ/scott
Technologies. Inc.
Aviation
550015600 SERIES PORTABI.E CYLINDER ASSEMBLY·
FIG.
ITEM
1E
PART NUMBER
AIRLINE
STOCK NO.
.•
/scott
~
CMM & IPI.
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
3150
5041-3-20
• OUTLET ASSY (SUPSOS ITEM 310)
(REFER TO FIG 4 FOR OET BKDN)
F,K
1
315E
5041-4-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
H
1
315F
5041-7-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
K
1
330
8572~2
• OUTLET ASSY
(REFER TO FIG 6 FOR DET BKON)
AF,AH,AJ
1
331
8572~2
• OUTLET ASSY
(REFER TO FIG 6 FOR DET BKON)
AF,AH,AJ
1
332
8572-02
• OUTLET ASSY
(REFER TO FIG 6 FOR DET BKDN)
AH
1
340
10003566
• OXYGEN COUPLING (SUPSD BY 340A)
M
1
340A
802856-01
• OUTLET ASSY
(REFER TO FIG 11 FOR DET BKDN) (SUPSDS 340)
M
1
345
36728-01
• OUTLET ASSY
(REFER TO FIG 13 FOR DET BKDN)
W,AC,AG
1
346
36728-01
• OUTLET ASSY
(REFER TO FIG 13 FOR DET BKDN)
AG
1
350
802863-02
• OUTLET ASSY
(REFER TO FIG 10 FOR DET BKDN)
T,AD
1
-395
MS27769S2
• PLUG, PIPE (GRES) (V96906)
(SPN 6818-01) (0.125-27 ANPT THD)
C.D,V,Z,
AF, AG,AJ
1
-396
MS27769S2
• PLUG, PIPE (GRES) (V96906)
(SPN 6818-01) (0.125-27 ANPT THO)
Z
1
-397
MS27769S2
• PLUG, PIPE (GRES) (V96906)
(SPN 6818-O1) (0.125-27 ANPT THD)
Z
1
405
5510-13
• REGULATOR ASSY
(REFER TO FIG 9 FOR DET BKDN)
A-E
1
410
5510-15
• REGULATOR ASSY
(REFER TO FIG 9 FOR DET 8KDN)
F-AD
1
425
5510-19
• REGULATOR ASSY
(REFER TO FIG 9 FOR DET BKDN)
AE-AJ
1
500
6350A13XG
• CYLINDER, STEEL (SPN 6350-A13-X-G)
(4.25 CU FT, PAINTED, GRAY-GREEN)
F-L
1
505
6084-01
•• CYLINDER, STEEL (DOT-3M-1800)
(4.25 eu FT, UNPAINTED)
F-L
1
510
6350A14XG
• GYLINDER, STEEL (SPN 6350-A14-X-G)
(7.15 CU FT, PAINTED, GRAY-GREEN)
M
1
510A
6350A14XA
• CYLINDER, STEEL (SPN 6350-A14-X-A)
(7.15 GU FT, PAINTED, WAKEFIELD GREEN)
N-T
1
515
6084-02
•• CYLINDER, STEEL (DOT-3M-1800)
(7.15 GU FT, UNPAINTED)
M-T
1
-ITEM NOT ILLUSTRATED
EFFECT\VITY:
5500 SERIES
35-32-18
Page 10084
20040415
•
•
•
•
....
1:L/Co/scott
Technologies. Inc.
IScotf
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
1E
PART NUMBER
AIRLINE
STOCK NO.
CAtAt & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
520
6350A4XA
• CYlINDER, STEEL (SPN 6350-A4-X·A)
(22 CU FT, PAINTED, WAKEFIELD GREEN)
AE
1
525
60B4·04
• • CYLINDER, STEEL (DOT-3M·1800)
(22 CU FT, UNPAINTED)
AE
1
530
6350A2XG
• CYLINDER, STEEL (SPN 6350-A2·X-G)
(38.4 CU FT, PAINTED, GRAY-GREEN)
A
1
530A
6350A2XA
• CYLINDER, STEEL (SPN 6350·A2-X-A)
(38.4 CU FT, PAINTED, WAKEFIELD GREEN)
B
1
535
6084·06
• • CYLINDER, STEEL (DOT-3M· 1BOO)
(38.4 CU FT, UNPAINTED)
A,B
1
540
6350A5XG
• CYliNDER, STEEL (SPN 6350-A5-X·G)
(48.3 CU FT, PAINTED, GRAY-GREEN)
C-E
1
545
6084-07
• • CYLINDER, STEEL (DOT·3M·1800)
(48.3 CU FT, UNPAINTED)
C-E
1
550
6350A20XG
• CYLINDER, STEEL (SPN 635Q.A20-X-G)
(11 CU FT, PAINTED, GRAY·GREEN)
U-AA
1
550A
6350A20XA
• CYLINDER, STEEL (SPN 635Q.A20·X-A)
(11 CU FT, PAINTED, WAKEFIELD GREEN)
AB-AD
1
555
6084-03
NP
• • CYUNDER, STEEL (DOT-3AA-1BOO)
(11 eu FT, UNPAINTED) (SUPSD BY ITEM 555A)
U-AD
1
555A
6084-20
•• CYLINDER, STEEL (DOT-3M-1800)
(11 CU FT,lINPAINTED) (SUPSDS ITEM 555)
U-AD
1
560
6350A34XA
• CYLINDER, STEEL (SPN 6350·A34-X·A)
(115 CU FT, PAINTED, WAKEFIELD GREEN)
Af-AJ
1
565
6084-34
• • CYLINDER, STEEL (DOT·3HT·1850)
(115 ell FT. UNPAINTED)
AF·AJ
1
NOTE 1: 5500 PCA WITHOUT A YELLOW HANDLE (-30, IPL FIGURE 9) MUST USE INSTRUCTION DECAL ITEM 20A.
•
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10085
20040415
1:ycO/SCOlt
Technologies. Inc.
...
!scott
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IfL
300
305
330
300
305
330
2 Outlet Regulator
(Top View)
2 Outlet Regulator
('N' Configuration)
(Top View)
65
•
35
4
20A
i
wXI-
I
.
I
'
30A
~wxH
520·535
5500N and 55000 Sub Series PCA
Figure 'IF
(Sheet 1 of 2)
-ITEM NOT ILLUSTRATED
EFFECTiVITY:
5500 SERIES
35-32-18
Page 10086
20040415
•
....
1:L/Co/scott
!scott
Technologies. Inc. Aviation
55DlV56ODSERIES PORTABLE CYLINDER ASSEMBLY·
eMM & 'PL
240
"'\
~'"/
l
I0
P..i)
-~l:V"'"
"fOJ
~~:
i$ •
~'-"1
:
_.7:",,~_1
~:-.,\1'
/'
..
I(,-":t'j,'
"'.
••_.-
...~
: __ "
,t/
I
..
801807 Series
(801807-02 Shown)
•
•
5500N and 55000 Sub Series PCA
Figure 1F
(Sheet 2 of 2)
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10087
20040415
1:'-/ca/scott
Technologies,
Inc.
/scott
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
•...
Aviation
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
1F
-1
5500N6SBF10A
CYLINDER ASSY. PORTABLE
(SPN 550Q-N6S-BF10A)
A
RF
-1A
5500Q6XBF10A
CYLINDER ASSY. PORTABLE
(SPN 5500-Q6X-BF10A)
B
RF
-1B
55OOQ6XBF23A
CYLINDER ASSY, PORTABLE
(SPN 55oo-Q6X-BF23A)
C
RF
-1C
5500Q6XYVOE
CYLINDER ASSY, PORTABLE
(SPN 5500-Q6X·YYOE)
D
RF
-20
10006936
• PLATE, INSTRUCTION
(SEE NOTE 1)
(REPlD
BY 2OA)
1
20A
10009071
• DECAL, INSTRUCTION
(REPLS -20) (SEE NOTE1)
1
-30
10005922
• DECAL, OXYGEN 10 (REPlD BY 30A)
1
30A
10009255
• DECAL, OXYGEN ID (REPlS -30)
USED ONLY WHERE PAINTED TEXT
"BREATHING OXYGEN ONLY - USE NO Oil"
DOES NOT APPEAR ON SIDE OF CYLINDER
(ITEM 520 THRU 535)
1
35
10009374
• LABEL, FAA-PMA ELIGIBILITY
(USED ONLY ON PCAlSHIPPED FROM THE
FACTORY FROM JULY 1995 AND LATER)
1
55
5057-00
• PLATE, IDENTIFICATION
1
AITACHING
65
MS21318-7
PARTS
2
• SCREW, DRIVE (CRES) (V86044)
(#0 x 0.125 in. LNG) (SPN 33343-007)
•
•••
75
13161-00
• CLAMP (AL T SPN 1NWO-176)
A
1
240
801807-02
• HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIGURE 2 FOR DET BKDN)
A
1
300
5009-00
• OUTLET ASSY (SUPSD BY ITEM 305)
(REFER TO FIG 5 FOR DET BKDN)
A-e
1
305
5009-2-10
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
A,B
1
305A
5009-2-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
C
1
305B
5009-4-10
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
A,B
1
305C
5009-4-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
C
1
330
8572-02
• OUTLET ASSY
(REFER TO FIG 6 FOR DET BKDN)
D
1
331
8572-02
• OUTLET ASSY
(REFER TO FIG 6 FOR DET BKDN)
D
1
NP
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10088
20040415
•
•
. '.
..
t'lCO /SCOtl
/scott
Technologies. Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
EFF.
CODE
NOMENCLATURE
1234567
UNITS
PER
ASSY
1F
415
520
5510-17
525
6084.04
•• CYLINDER, STEEL (DOT-3M·1800)
(22 CU FT, UNPAINTED)
530
6350A2XA
535
6084-06
• REGULATORASSY
• CYLINDER, STEEL (SPN 6350-A4-X-A)
(22 CU FT, PAINTED, WAKEFIELD GREEN)
6350A4XA
1
A
1
A
1
• CYLINDER, STEEL (SPN 6350-A2-X-A)
(38.4 CU FT, PAINTED, WAKEFIELD GREEN)
B·D
1
• • CYLINDER, STEEL (DOT-3M-1800)
(38.4 CU FT, UNPAINTED)
B-D
1
NOTE 1: 5500 PCA WITHOUT A YELLOW HANDLE (-30, IPL FIGURE 9) MUST USE INSTRUCTION DECAL ITEM 20A.
•
•
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10089
20040415
1:l./ca/scott
Technologies. Inc.
/scott
Aviation
550015600SERIES PORTABLE CYUNDER ASSEMBLY·
CMM & IPL
300
305
2 Outlet Regulator
(Top View)
435
•
I
__ --.
..............
-475
Cross Sectional View
Item 475
65
35
205
<}-WXH
80~
570
5500T Sub Series PCA
Figure 1G
(Sheet 1 of 1)
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10090
20040415
•
•
• >.
t'lca/scotl
!scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEAfBLY • CMM & lPi
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
EFF.
CODE
NOMENCLATURE
1234567
UNITS
PER
ASSY
1G
•
RF
-1
5500T2ACC30B
CYliNDER ASSY, PORTABLE
(SPN 5500-T2A-GC30B)
-20
10006936
• PLATE, INSTRUCTION (REPLD BY 2OA)
(SEE NOTE 1)
1
20A
10009071
• DECAL,INSTRUCTION (REPLS -20) (SEE NOTE1)
1
-30
10005922
• DECAL, OXYGEN ID (REPlD BY 30A)
1
30A
10009255
• DECAL, OXYGEN 10 (REPLS -3D)
USED ONLY WHERE PAINTED TEXT
"BREATHING OXYGEN ONLY - USE NO OIL"
DOES NOT APPEAR ON SIDE OF CYLINDER
(ITEM 570)
1
35
10009314
• LABEL, FM-PMA ELIGIBILITY
(USED ONLY ON PCAliSHIPPEO FROM THE
FACTORY FROM JULY 1995 AND LATER)
1
65
10006442
• DECAL, WARNING
1
70
13160-00
• CLAMP (ALT SPN WWD-120)
1
80
10005511
• PLATE, IDENTIFICATION
1
205
801660-00
• HARNESS
1
NP
1
300
5041-00
• OUTLET ASSY (SUPSD BY ITEM 305)
(REFER TO FIG 4 FOR DET BKDN)
305
5041-2.5-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 4 FOR DET BKDN)
1
30SA
5041-2.5-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 4 FOR DEl BKON)
1
435
803199-04
• REGULATOR ASSY
(REFER TO FIG 9 FOR DET BKDN)
1
475
59776-01
• SEAL, METAl BOSS
1
570
21507-06
• CYLINDER, COMPOSITE (DOT-E-8162-1850)
(11 CU FT, GREEN)
1
NOTE 1: 5500 PCA WITHOUT A YEllOW HANDLE (-3D, IPl FIGURE 9) MUST USE INSTRUCTION DECAl ITEM 20A.
•
EFFECTIVITY:
5500 SERIES
35-32-18
Page 10091
20040415
1:l.Jcojscott
..
/SCOtf
•
Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
~'
CMM & IPI.
•
300 - 370
120
LO Flow
Two Outlet Regulator
(Top View)
One Outlet Regulator
(Top View)
400
______ 405
,-.-,--..
41 0
•
205
220
ji
75
75A
30A
~
110
758
T
70
70A
708
I
125
25A
<}uJX>-1
5600-1 and 5600-2 Sub Series PCA
Figure 1H
(Sheet 1 of 2)
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10092
20040415
•
q.
1:'1ca/scotl
Technologies,
Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYUNDER ASSEMBL.Y • eMM & 'PL
200
I
201
75A
801658-00
5600-1 and 5600-2 Sub Series peA
Figure 1H
(Sheet 2 of 2)
•
•
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10093
20040415
.' .
-tyca/scott
/scott
Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
EFF.
CODE
UNITS
PER
ASSY
CYLINDER ASSY, PORTABLE
(SPN 5600-1B1A-E20B)
A
RF
5600-1 B1AF23A
CYLINDER ASSY, PORTABLE
(SPN 5600-1B1A-F23A)
B
RF
-18
5600-1 C1AB20A
CYLINDER ASSY, PORTABLE
(SPN 560D-1C1A-B20A)
C
RF
-1C
5600-1 C1AB20B
CYLINDER ASSY, PORTABLE
(SPN 560D-1C1A-B20Bj
0
RF
·10
5600-1 C1AB23A
CYLINDER ASSY, PORTABLE
(SPN 560Q..1C1A-B23Aj
E
RF
-1E
5600·1C1AE20A
CYLINDERASSY, PORTABLE
(SPN 5600-1C1A-E20A)
F
RF
-1F
5600-1C1AE20B
CYLINDER ASSY, PORTABLE
(SPN 5600-1C1A-E20B)
G
RF
-1G
5600-1C1AE20D
CYLINDER ASSY, PORTABLE
(SPN 5600-1C1A-E20D)
H
RF
-1H
5600-1 C1AE23A
CYLINDER ASSY, PORTABLE
(SPN 56lXl-1C1A-E23A)
J
RF
-1J
5600-1C1AE23B
CYLINDER ASSY, PORTABLE
(SPN 56lXl-1C1A-E23B)
K
RF
-1K
5600-1C1AF20A
CYLINDER ASSY, PORTABLE
(SPN 5600-1C1A-F20Aj
L
RF
-1L
5600-1C1AF20B
CYLINDER ASSY, PORTABLE
(SPN 5600-1C1A-F20B)
M
RF
-1M
5600-1C1AF23A
CYLINDER ASSY, PORTABLE
(SPN 560D-1C1A-F23A)
N
RF
-1N
5600-1C1AF23B
CYLINDER ASSY, PORTABLE
(SPN 560D-1C1A-F23B)
P
RF
-1P
5600-1 C1AF25A
CYLINDER ASSY, PORTABLE
(SPN 560D-1C1A-F25A)
0
RF
-10
5600·1 C1AXOK
CYLINDER ASSY, PORTABLE
(SPN 560D-1C1A-XOK)
R
RF
-1R
5600-1 C1AXOM
CYLINDER ASSY, PORTABLE
(SPN 560D-1C1A·XOMj
S
RF
-1S
5600-1 C1AYOM
CYLINDER ASSY, PORTABLE
(SPN 560D-1C1A·YOM)
T
RF
-H
5600-1C1BXOK
CYLINDER ASSY, PORTABLE
(SPN 560Q..1C1B·XOK)
U
RF
-1U
5600-1 C1BXOM
CYLINDER ASSY, PORTABLE
(SPN 560Q..1C1B-XOM)
V
RF
.1V
5600-1 C1BYOM
CYLINDER ASSY, PORTABLE
(SPN 560D-1C1B-YOM)
W
RF
FIG.
ITEM
1H
PART NUMBER
-1
5600-1B1AE20B
·1A
EFFECTIVITY:
AIRLINE
STOCK NO.
5600 SERIES
.•
~
CMM & IPL
NOMENCLATURE
1234567
35-32-18
Page 10094
20040415
•
•
•
".
t'lca/scott
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRliNE
STOCK NO.
eMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
1H
•
•
-1W
5600-1 C6AE20A
CYLINDER ASSY, PORTABLE
(SPN 5600-1C6A-E20A)
X
RF
-1X
5600-1 C6AF23A
CYLINDER ASSY, PORTABLE
(SPN 5600-1CSA-F23A)
Y
RF
-w
5600-1 CSAF23B
CYLINDER ASSY, PORTABLE
(SPN 5600-1C6A-F23B)
Z
RF
-1Z
5600-1C6AXOK
CYLINDER ASSY, PORTABLE
(SPN 5600-1C6A-XOK)
AA
RF
-2
5600-1D1AF23A
CYLINDER ASSY. PORTABLE
(SPN 5600-101 A-F23A)
AB
RF
-2A
5600-1D1AF30A
CYLINDER ASSY. PORTABLE
(SPN 5600-1D1A-F30A)
AC
RF
-2B
5600-1 D6AE20A
CYLINDER ASSY, PORTABLE
(SPN 5600-1D6A-E20A)
AD
RF
-2C
5600-1 G1AF20A
CYLINDER ASSY, PORTABLE
(SPN 5600-1 G1A-F20A)
AE
RF
-20
56oo-1M1AF20BM
CYLINDER ASSY, PORTABLE
(SPN 5600-1M1A-F20BM)
AF
RF
-2E
5600-2A1AB23B
CYliNDER ASSY, PORTABLE
(SPN 5600-2A1A-B23B)
AG
RF
-2F
5600-2A 1AF23A
CYLINDER ASSY. PORTABLE
(SPN 5600-2A1A-F23A)
AH
RF
-2G
5600-2B 1AE20A
CYLINDER ASSY, PORTABLE
(SPN 5600-2B1A-E20A)
AJ
RF
-2H
5600-2B1AF20A
CYLINDER ASSY, PORTABLE
(SPN 5600-2B1A-F20A)
AK
RF
·2J
5600-2B1AYOE
CYLINDER ASSY. PORTABLE
(SPN SSOD-281A-YOE)
Al
RF
-2K
5600-2C1AB20B
CYliNDER ASSY, PORTABLE
(SPN 5600-2C1A-820B)
AM
RF
-2L
5600-2C1 AC20A
CYLINDER ASSY. PORTABLE
(SPN 5600-2C1A-C20A)
AN
RF
-2M
5600-2C1 AE20A
CYLINDER ASSY. PORTABLE
(SPN 5600-2C1A-E20A)
AP
RF
-2N
5600-2C1AE20B
CYLINDER ASSY, PORTABLE
(SPN 5600-2C1A-E2OB)
AO
RF
-2P
5600-2C1 AE20C
CYLINDER ASSY, PORTABLE
(SPN 5600-2C1A-E20C)
AR
RF
-20
5600-2C1 AE20D
CYLINDER ASSY, PORTABLE
(SPN 5600-2C1A-E20D)
AS
RF
-2R
56oo-2C1AE23A
CYLINDERASSY,
PORTABLE
(SPN 5600-2C1A-E23A)
AT
RF
- ITEM NOT IllUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10095
20040415
't'lca/scott
/scott
Technologies. Inc. Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
~
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
.•
1H
-2S
5600-2C1AE23B
CYLINDER ASSY, PORTABLE
(SPN 5600-2C1A-E23B)
AU
RF
-2T
5600-2C1AF20A
CYLINDER ASSY, PORTABLE
(SPN 560D-2C1A-F20A)
AV
RF
-2U
56Q0.2C1AF30A
CYLINDER f>SSY, PORTABLE
(SPN 560D-2C1A-F30A)
AW
RF
-2V
5600·2C1AG25A
CYLINDER ASSY, PORTABLE
(SPN 5600-2C1A-G25A)
AX
RF
-2W
5600·2C1AXOK
CYLINDER ASSY, PORTABLE
(SPN 5600-2C1A-XOK)
AY
RF
-2X
5600·2C1AXOM
CYLINDER ASSY, PORTABLE
(SPN 5600-2C1A-XOM)
AZ
RF
-2Y
5600·2C1AYOM
CYLINDER ASSY, PORTABLE
(SPN 560D-2C1A-YOM)
BA
RF
-2Z
5600·2C1AYON
CYLINDER ASSY, PORTABLE
(SPN 560D-2C1A·YON)
BB
RF
-3
5600-2C1 BXOK
CYLINDER ASSY, PORTABLE
(SPN 560D-2C1B-XOK)
BC
RF
5600-2C5AE20B
CYLINDER ASSY, PORTABLE
(SPN 5600-2CSA-E20B)
BO
RF
-3A
I
DELETED
-3B
·3C
5600-2C6AB23A
CYLINDER ASSY, PORTABLE
(SPN 5600-2C6A-B23A)
BF
RF
-3D
5600·2C6AF23A
CYLINDER ASSY, PORTABLE
(SPN 5600-2C6A-F23A)
BG
RF
-3E
5600-2CSAXOK
CYLINDER ASSY, PORTABLE
(SPN 560D-2C6A-XOK)
BH
RF
-3F
5600·2C9FXOK
CYLINDER ASSY, PORTABLE
(SPN 560D-2C9F-XOK)
BJ
RF
-3G
5600-2D1AXOK
CYLINDER ASSY, PORTABLE
(SPN 560D-2D1A-XOK)
BK
RF
-3H
5600-201 BXOK
CYliNDER ASSY, PORTABLE
(SPN 5600-2D1B-XOK)
BL
RF
-3J
5600·2G1AB20B
CYLINDER ASSY, PORTABLE
(SPN 5600-2G1A-B20B)
BM
RF
-3K
5600-2J1ABF23A
CYLINDER ASSY, PORTABLE
(SPN 5600-2J1A-BF23A)
BN
RF
-3L
5600-2M1ABF23A
CYLINDER ASSY, PORTABLE
(SPN 5600-2M1A-BF23A)
BP
RF
-3M
5600-2M1ABG23A
CYLINDER ASSY, PORTABLE
(SPN 5600-2M1A-BG23A)
BO
RF
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10096
20040415
•
•
•
".
..•
-t'lco/scott
Technologies.
!scott
Inc. Aviation
550(115600SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
CMM & fPL
NOMENCLA lURE
1234567
EFF.
CODE
UNITS
PER
ASSY
1H
-25
5608-00
• PLATE, INSTRUCTION (REPLD BY 2M)
(SEE NOTE 1)
A-BH, BK-BQ
1
25A
10009071
• DECAL, INSTRUCTION (REPLS -25) (SEE NOTE1)
A-BH, BK-BQ
1
-30
10005922
• DECAL, OXYGEN 10 (REPLD BY 30A)
A-BH, BK·BQ
1
30A
10009255
• DECAL, OXYGEN 10 (REPLS -30)
USED ONLY WHERE PAINTED TEXT"BREATHING
OXYGEN ONLY - USE NO OIL" DOES NOT APPEAR
ON SIDE OF CYLINDER (ITEMS 500 THRU 555A)
A-BH, BK·BQ
1
-40
10001018
• PLACARD, INSTRUCTION
(USED ONLY ON 5600 2C9 SERIES)
BJ
1
-45
10001019
• LABEL
(USED ONLY ON 5600 2C9 SERIES)
BJ
1
-50
10001020
• PLACARD, AVIATORS OXYGEN
(USED ONLY ON 5600 2C9 SERIES)
BJ
1
-60
5057-01
• PLATE, IDENTIFICATION
1
ATTACHING PARTS
-65
•
MS21318-7
2
• SCREW, DRIVE (CRES) (V8B044)
(#0 x 0.125 in. LNG) (SPN 33343-007)
...
70
13160-00
• CLAMP, HARNESS (ALT SPN WWD-120)
A·AA, AF-BJ,
BN-BQ
1
70A
13161-00
• CLAMP, HARNESS (ALT SPN WWD-176)
AB-AD, BI<, BL
1
70B
13162-00
• CLAMP, HARNESS (ALT SPN WWD-224)
AE,BM
1
75
13160-00
• CLAMP (All SPN WWD-120)
A-M, AF-BJ,
BN-BQ
1
7M
13161-00
• CLAMP (All SPN WWD-176)
AB·AD, BK, BL
1
75B
13162-00
• CLAMP (All SPN WWD-224)
AE,BM
1
-100
5602-00
• CONNECTOR ASSY (REPLD BY 100A)
100A
33529-009
• CONNECTOR, TUBE (AlUMINUM) (REPLS -100)
105
5601
• ELBOWASSY
A·M, AF-8J,
BN-BO
1
1
1
105A
5601B
• ELBOWASSY
AB-AD, BK, BL
1
1058
5601C
• ELBOWASSY
AE,BM
1
110
6379-2C
• REGULATOR, DEMAND RESPIRATOR
(REFER TO FIG 3 FOR DET BKDN)
A·AF
1
110A
6379-20
• REGULATOR, DEMAND RESPIRATOR
(REFER TO FIG 3 FOR DET BKDN)
AG-BQ
1
ATTACHING PARTS
120
•
59602-00
• SCREW, SELF-LOCKING (CRES WI PLASTIC INSERT)
(#8-32 THO x 0.250 in. LNGl
4
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10097
20040415
t:'-/co/scott
/scott
Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
.' .
CMM & /PL
~'
•
UNITS
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
NOMENCLATURE
PER
ASSY
EFF.
CODE
1234567
1H
***
125
10001296
200
801658-00
201
1
• BRACKET
• HARNESS
u-w, Be, BL
1
801659-00
•• STRAPASSY
U-W, Be, BL
1
202
B01661-OO
•• STRAPASSY
U-W, BC, BL
1
205
B0166o.00
• HARNESS
A-T, X-BB, BD-BH.
BK, BM-BQ
1
220
801660-05
• HARNESS
BJ
1
300
5009-00
• OUTLET ASSY (SUPSD BY ITEM 305)
(REFER TO FIG 5 FOR DET BKDN)
B,C,E,F,J.L,a,x, Y,
AB·AE,AH-AK,AN,
AP,AT,AV-AX, BF,
BG,BN-Ba
1
305
5009-2-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR OET BKON)
C
1
30M
5009·2-23
• OUTLET ASSY (SUPSOS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
E, BF, BN-BO
1
305B
5009-2.5-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AN
1
305C
6009-3-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKON)
F, X, AD, AJ, AP
1
305D
5009·3-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
J,AT
1
305E
5009-4-20
• OUTLET ASSY (SUPSOS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
L,AE,AK,AV
1
305F
5009-4-23
• OUTLET ASSY (SUPSOS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
B, N, Y, AB, AH, BG,
BN,BP
1
305G
5009-4-25
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
a
1
305H
5009-4-30
• OUTLET ASSY (SUPSOS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AC,AW
1
305J
5009-7-23
• OUTLET ASSY (SUPSOS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
Ba
1
305K
5009·7-25
• OUTLET ASSY (SUPSOS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AX
1
310
5041-00
• OUTLET ASSY (SUPSD BY ITEM 315)
(REFER TO FIG 4 FOR DET BKDN)
A,O,G,K,M,P,Z,
AF,AG,AM,AO,AU.
BD,BM
1
315
5041·2-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR OET BKDN)
D,AM,BM
1
315A
5041·2-23
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
AG
1
315B
5041-3-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
A,G,AO. BD
1
NP
NP
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10098
20040415
•
•
•
•
•
....
tL/co/SCOtl
jSCDtt
Technologies,Inc. Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
..•
FIG.
ITEM
1H
I
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
315C
5041-3-23
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DEl BKDN)
K,AU
1
315D
5041-4-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DEl BKDN)
M,AF
1
315E
5041-4-23
• OUTlET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
P~
1
320
5507-00
• OUTlET ASSY (SUPSD BY ITEM 325)
(REFER TO FIG 7 FOR DET BKDN)
H,AS
1
325
5507-3-20
• OUTlET ASSY (SUPSDS ITEM 320)
(REFER TO FIG 7 FOR DET BKDN)
H,AS
1
330
8572-02
• OUTLET ASSY
(REFER TO FIG 6 FOR DET BKDN)
AL
1
340
10003566
• OXYGEN COUPLING (SUPSD BY 340A)
S, T, V, W,AF,
AZ,BA
1
340A
802856-01
• OUTLET ASSY (REFER TO FIG 11 FOR DET BKDN)
[SIMILAR TO PURITAN BENNETT (V49315)
PIN 110111-09] (SPSDS 340)
S, T, V, W, AF,
AZ,BA
1
345
36728-01
• OUTLET ASSY
(REFER TO FIG 13 FOR DET BKDN)
BB
1
370
5052-00
• OUTLET ASSY
(REFER TO FIG 8 FOR DET BKDN)
AR
1
-395
MS27769S2
• PLUG, PIPE (GRES) (V96906)
(SPN 6818-01)(0.125 -27 ANPTTHD)
R, U,AA,AY,
BC, BH-Bl
1
400
5510-10
• REGULATOR ASSY
(REFER TO FIG 9 FOR DET BKDN)
A-AA,AG-BJ
1
405
5510-13
• REGULATOR ASSY
(REFER TO FIG 9 FOR DET BKDN)
AB-AE, BK-BM
1
410
5510-15
• REGULATOR ASSY
(REFER TO FIG 9 FOR DEI BKDN)
AF, BN-BO
1
500
6350A13XG
• CYLINDER, STEEL (SPN 635Q-A13-X-G)
(4.25 CU FT, PAINTED, GRAY-GREEN)
AG,AH,BN
1
505
6084-01
• • CYLINDER, STEEL (DOT-3AA-1800)
(4.25 CU FT, UNPAINTED)
AG,AH, BN
1
510
6350A14XG
• CYLINDER, STEEL (SPN 6350-A14-X-G)
(7.15 CLI FT, PAINTED, GRAY-GREEN)
A, B,AJ-Al
1
515
6084-02
• • CYLINDER, STEEL (DOT-3AA-1800)
(7.15 CU FT, UNPAINTED)
A, B,AJ-AL
1
520
6350A4XG
• CYLINDER, STEEL (SPN 635Q-A4-X-G)
(22 CU FT, PAINTED, GRAY-GREEN)
AB, AG, BK, Bl
1
520A
6350A4XA
• CYLINDER, STEEL (SPN 635Q-A4-X-A)
(22 CU FT, PAINTED, WAKEFIELD GREEN)
AD
1
525
6084-04
• • CYLINDER, STEEL (DOT-3AA-1800)
(22 CU FT, UNPAINTED)
AS-AD, BK, Bl
1
NP
NP
- ITEM NOT IllUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10099
20040415
'tileD/scott
/scott
Technologies.Inc. Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
NOMENCLATURE
1234567
CODE
UNITS
PER
ASSY
EFF.
1H
540
6350A5XG
• CYLINDER, STEEL (SPN 6350-A5-X-G)
(48.3 CU FT, PAINTED, GRAY-GREEN)
AE,BM
1
545
6084-07
• • CYLINDER, STEEL (DOT-3M-18oo)
(48.3 CU FT, UNPAINTED)
AE,BM
1
550
6350A20XG
• CYLINDER, STEEL (SPN 6350-A20-X-G)
(11 CU FT, PAINTED, GRAY-GREENj
CoW,AF, AM-BC,
BP,BQ
1
550A
6350A20XE
• CYLINDER, STEEL (SPN 6350-A20-X-E)
(11 CU FT, PAINTED, GREEN AND YELLOW)
BD
1
550B
6350A20XA
• CYLINDER, STEEL (SPN 6350-A20·X-A)
(11 CU FT, PAINTED, WAKEFIELD GREEN)
X-M, BF-BJ
1
555
6084.03
• • CYLINDER, STEEL (DOT-3AA-18oo)
(11 CU FT, UNPAINTED)
(SUPSD BY ITEM 555A)
C-M, AF, AM-BJ,
BP,BQ
1
555A
6084-20
• • CYLINDER, STEEL (DOT-3M-1800)
(11 CU FT, UNPAINTED)
iSUPSDS ITEM 555)
CoM, AF, AM-BJ,
BP,BQ
1
NP
NOTE 1: 5600 PCA WITHOUT A YELLOW HANDLE (-30, IPL FIGURE 9) MUST USE INSTRUCTION DECAL ITEM 2M.
•
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10100
20040415
•
. •
tL/c:a/scotl
Technologies. Inc.
/scott
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPI
THIS PAGE INTENTIONALLY LEFT BLANK
•
•
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10101
20040415
tyco/SCOtl
Technologies. Inc.
" .
/scott
Aviation
~
5SOOI5600SERIES PORTABLE CYLINDER ASSEMBLY • CUM & IPL
.•
300 - 345
120
LOFJow
Two Outlet Regulator
(Top View)
One Outlet Regulator
(Top View)
•
205
220
i
75
75A
~ 30A
'"
115
758
T
~
125
70
70A
70B
5A
<}-WXH
500 - 555A
5600-8 and 5600-9 Sub Series peA
Figure 1J
(Sheet 1 of 2)
EFFEC1W\TY:
5600 SERIES
35-32-18
Page 10102
20040415
•
. '.
tl.lco/scott
!scott
Technologies,Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL.
200
I
201
70A
801658-00
5600-8 and 560Q...9Sub Series PCA
Figure 1J
(Sheet 2 of 2)
•
•
EFFECTIVITY: 5600 SERIES
35-32-18
Page 10103
20040415
1:'-/cojscott
Technologies.
Inc.
I
Scott
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
1J
PART NUMBER
AIRLINE
STOCK NO.
"
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
5600-8B6AXOK
CYLINDER ASSY, PORTABLE
(SPN 5600-8B6A-XOK)
A
RF
-tA
5600-8B9AXOK
CYLINDER ASSY, PORTABLE
(SPN 5600-8B9A-XOK)
B
RF
-1B
S600-8C1AF23A
CYLINDER ASSY, PORTABLE
(SPN 5600-8C1A-F23A)
C
RF
-1C
5OO0-8CtAXOK
CYLINDER ASSY, PORTABLE
(SPN 560Q..8C1A-XOK)
D
RF
-10
5600-8C1 BF23A
CYLINDER ASSY, PORTABLE
(SPN 560Q..8C1B-F23A)
E
RF
-1E
5600-8C6AF23A
CYLINDER ASSY, PORTABLE
(SPN 560Q..8C6A-F23A)
F
RF
-1F
5SllO-8CSAXOK
G
RF
-1G
5600-801 AXOK
CYLINDER ASSY, PORTABLE
(SPN 560Q..8C6A-XOK)
CYLINDER ASSY, PORTABLE
(SPN 560Q..8D1A-XOK)
H
RF
-1H
5600·8D1AYON
CYLINDER ASSY, PORTABLE
(SPN 5S00-8D1A-YON)
J
RF
·1J
5OO0-8G2AXOK
CYLINDER AS5Y, PORTABLE
(SPN S600-8G2A-XOK)
K
RF
-1K
5OO0-8G6AXOK
CYLINDER ASSY, PORTABLE
(SPN 5600-8G6A-XOK)
L
RF
-1L
5OOO-9Ct AF20A
CYLINDER ASSY, PORTABLE
(SPN 5600-9C1A-F20A)
M
RF
-1M
SOO0-9C1AF20B
CYLINDER ASSY, PORTABLE
(SPN 5600-9C1A-F20B)
N
RF
-1N
5OO0-9CtAF23A
CYLINDER ASSY, PORTABLE
(SPN 5SllO-9C1A-F23A)
P
RF
-1P
5OOO-9C1AXOK
CYLINDER ASSY, PORTABLE
(SPN 56llO-9C1A-XOK)
0
RF
·10
5OOO-9C1AYOE
CYLINDER ASSY, PORTABLE
(SPN 5600-9C1A-YOE)
R
RF
-1R
5OOO-9C1AYON
CYLINDER ASSY, PORTABLE
(SPN 5600-9C1A-YON)
S
RF
-15
5600-9C6AXOK
CYLINDER ASSY, PORTABLE
(SPN 5600-9C6A-XOK)
T
RF
-H
5600·9C6AYOK
CYLINDER ASSY, PORTABLE
(SPN 5600-9C6A- YOK)
U
RF
-1U
5600·9C9AF10A
CYLINDER ASSY, PORTABLE
(SPN 5600-9C9A-FtOA)
V
RF
-w
5600-9D1AE20B
CYLINDER ASSY, PORTABLE
(SPN 5600-901A-E20B)
W
RF
·1W
5600-9D1AE3OA
CYLINDER ASSY, PORTABLE
(SPN 5600-9D1A-E30A)
X
RF
5600 SERIES
..•
'
eMU & IPL
-1
EFFECTIVITY:
.
35-32-18
Page 10104
20040415
•
•
•
",
1:'1ca/scott
!scott
Technologies. Inc. Aviation
5500I560O SERIES PORTABLE CYLINDER ASSEMBLY - CMM & IPL
'~
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
1J
•
-1X
5600-9D1AF23A
CYLINDER ASSY, PORTABLE
(SPN 5600-9D1A-F23A)
Y
RF
-w
5600-901 AG30A
CYliNDER ASSY, PORTABLE
(SPN 5600-9D1A-G30A)
Z
RF
-1Z
5600-9D1AXOK
CYliNDER ASSY, PORTABLE
(SPN 5600-9D1A-XOK)
M
RF
-2
5600·9D1AYON
CYLINDER ASSY, PORTABLE
(SPN 5600-9D1A-YON)
AS
RF
-2A
5600-901 BXOK
CYliNDER ASSY, PORTABLE
(SPN 5600-9D1B-XOK)
AC
R~
AE
RF
56oo-9D9AXOK
-2D
56oo-9G1AXOK
CYliNDER ASSY, PORTABLE
(SPN 5600-9G1A-XOK)
AF
RF
-2E
56oo-SJ6AF30AN
CYLINDER ASSY, PORTABLE
(SPN 5600-SJ6A-F30AN)
AG
RF
-2F
56oo-9M1AHH20A
CYLINDER ASSY, PORTABLE
(SPN 5600-SM1A-HH20A)
AH
RF
-2G
56oo-SM6ABF30A
CYLINDER ASSY, PORTABLE
(SPN 5600-SM6A-BF30A)
AJ
RF
-2H
56oo-9M6AFF30A
CYliNDER ASSY, PORTABLE
(SPN 5600-9M6A-FF30A)
AK
RF
-2J
5600-SM6AF30AE
CYliNDER ASSY, PORTABLE
(SPN 560o-9M6A-F30AE)
Al
RF
-2K
5600-9M6AF30AN
CYlINDERASSY, PORTABLE
(SPN 560o-SM6A-F30AN)
AM
RF
-2L
5600-SM9FF30AN
CYLINDER ASSY, PORTABLE
(SPN 5600·9M9F·FJOAN)
AN
RF
-2M
5600-9P1AYOEN
CYUNDER ASSY, PORTABLE
(SPN 5600-9P1A-YOEN)
AP
RF
-2N
5600-9P6AF30AN
CYLINDER ASSY, PORTABLE
(SPN 5600-9P6A-F30AN)
AQ
RF
-25
5608-00
• PLATE, INSTRUCTION (REPLD BY 25A) (SEE NOTE 1)
A,C-U,W-AC
AF-AM,AP,AQ
1
25A
10009071
• DECAL, INSTRUCTION (REPlS -25) (SEE NOTE1)
A,C-U,W-AC
AF-AM,AP,AQ
1
-30
10005922
• DECAl, OXYGEN 10 (REPLD BY 30A)
A,C-U,W-AC
AF-AM,AP,AQ
1
10009255
• DECAL, OXYGEN ID (REPLS -30)
USED ONLY WHERE PAINTED TEXT "BREATHING
OXYGEN ONLY - USE NO Oil" DOES NOT APPEAR
ON SIDE OF CYLINDER (ITEMS 500 THRU 555A)
A,G-U,W-AC
AF-AM,AP,AQ
1
30A
•
DELETED
CYliNDER ASSY, PORTABLE
(SPN 5600-9D9A-XOK)
-2B
-2C
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10105
20040415
t"lcojscott
/SCOft
Technologies.Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
1J
PART NUMBER
AIRLINE
STOCK NO.
~
eMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
-40
10001018
• PLACARD, INSTRUCTION (USED ONLY ON 5600
8B9, 9C9, 909, AND 9M9 SERIES)
B,V,AE,AN
1
-45
10001019
• LABEL (USED ONLY ON 5600 8B9, 9C9, 909,
AND 9M9 SERIES)
B,V,AE,AN
1
-50
10001020
• PLACARD, AVIATORS OXYGEN (USED ONLY ON
5600889, 9C9, 909, AND 9M9 SERIES)
B, V,AE, AN
1
-60
5057-01
• PLATE, IDENTIFICATION
.•
1
ATTACHING PARTS
-65
MS21318-7
2
• SCREW, DRIVE (CRES) (V88044)
(#0 x 0.125 in. LNG)(SPN 33343-007)
•••
7D
13160-00
• CLAMP, HARNESS (ALT SPN WWD-120)
A-G, M-V.
AG-AN
1
70A
13161-00
• CLAMP HARNESS (ALT SPN WWD-176)
H,J, W-AE,
AP,AQ
1
70B
13162-00
• CLAMP HARNESS (ALT SPN WWD-224)
K. L,AF
1
75
13160-00
• CLAMP (ALT SPN WWD-120)
A-G,M-V,
AG-AN
1
75A
13161-00
• CLAMP (ALT SPN WWD-176)
H,J, W-AE,
AP,AQ
1
75B
13162-00
• CLAMP (ALT SPN WWD-224)
K, L,AF
1
-100
5602-00
• CONNECTOR ASSY (REPLD BY 100A)
1
1DOA
33529-009
• CONNECTOR, TUBE (ALUMINUM) (REPLS -100)
1
105
5601
• ELBOWASSY
A-G,M-V,
AG-AN
1
105A
5601B
• ELBOWASSY
H, J, W-AE,
AP,AQ
1
105B
5601C
• ELBOWASSY
K, L, AF
1
1
1
115
800649-00
• REGULATOR RESPIRATOR
(DEMAND I PRESSURE-DEMAND TYPE)
(REFER TO FIG 3 FOR DET BKDN)
A-L
115A
800649-01
• REGULATOR RESPIRATOR
(DEMAND I PRESSURE-DEMAND TYPE)
(REFER TO FIG 3 FOR DEl BKDN)
M-AQ
•
ATTACHING PARTS
4
• SCREW, SELF-LOCKING CRES WI PLASTIC INSERT)
(#8-32 THO x 0.250 in. LNG)
120
59602-00
125
10001296
-
1
• BRACKET
200
801658-00
• HARNESS
E,AC
201
801659-00
•• STRAP ASSY
E,AC
1
1
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10106
20040415
•
e·
..
• '.
-f'lCO/SCOU
Technologies.Inc.
/scott
A lIiation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
CMM & 'PL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
E,AC
1
1J
e
•
202
801661·00
•• STRAP ASSY
205
801660-00
• HARNESS
A-D, F-AB,
AE-AM, AP, AQ
1
220
801660-05
• HARNESS
AN
1
300
5009-00
• OUTLET ASSY (SUPSD BY ITEM 305)
(REFER TO FIG 5 FOR DET BKDN)
C-F,H,P,V,
X-Z,AG-AN,AQ
1
305
5009-2·30
• OUTLET ASSY (SUPSDS ITEM 300l
(REFER TO FIG 5 FOR DET BKDN)
AJ
1
305A
5009-3-30
• OUTlET ASSY (SUPSDS ITEM 300l
(REFER TO FIG 5 FOR DET BKDN)
X
1
305B
5009-4·10
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
V
1
305C
5009-4-20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DEI BKDNl
M
1
305D
5009-4-23
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
305E
5009-4-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AG, AJ-AN, AQ
1
305F
5009-4-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AK
1
305G
5009-7-30
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
Z
1
305H
5009-8-20
• OUTlET ASSY (SUPSDS ITEM 300l
(REFER TO FIG 5 FOR DET BKDN)
AH
1
305J
5009-8·20
• OUTLET ASSY (SUPSDS ITEM 300)
(REFER TO FIG 5 FOR DET BKDN)
AH
1
310
5041-00
• OUTLET ASSY (SUPSD BY ITEM 315)
(REFER TO FIG 4 FOR DEI BKDN)
N,W
1
315
5041-3-20
• OUTlET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
W
1
315A
5041-4-20
• OUTLET ASSY (SUPSDS ITEM 310)
(REFER TO FIG 4 FOR DET BKDN)
N
1
330
8572-02
• OUTLET ASSY
(REFER TO FIG 6 FOR DET BKON)
R,AL,AP
1
345
36728-01
• OUTLET ASSY
(REFER TO FIG 13 FOR DET BKDN)
J, S, AB, AG, AMAQ
1
-395
MS27769S2
• PLUG, PIPE (CRES) (V96906)
(SPN 6818-01) (0.125-27ANPT THO)
A, B, D, G, H, K,
L, Q, T, U, AA,
AC-AF
1
400
5510-10
• REGULATOR ASSY
(REFER TO FIG 9 FOR DET BKDN)
A·G,M-V
1
405
5510-13
• REGULATOR ASSY
(REFER TO FIG 9 FOR DEl BKDN)
H-L, W-AF
1
NP
C,E,F,P,Y
NP
1
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10107
20040415
..
tqco/scott
/scott
Technologies.Inc. Aviation
55Da'56OOSERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
~
~
CMM & IPL
NOMENCLAlURE
1234567
EFF.
CODE
UNITS
PER
ASSY
.•
1J
410
5510-15
• REGULATOR ASSY
(REFER TO FIG 9 FOR DEI BKDN)
AG-AN
1
425
5510-19
• REGULATOR ASSY
(REFER TO FIG 9 FOR DET BKDN)
AP,AQ
1
500
6350A13XA
• CYLINDER, STEEL (SPN 635D-A13-X-A)
(425 CU FT, PAINTED, WAKEFIELD GREEN)
AG
1
505
6084-01
• • CYLINDER, STEEL (DOT-3M-1800)
(4.25 CU FT, UNPAINTED)
AG
1
510
6350A14XA
• CYLINDER, STEEL (SPN 6350-A14-X-A)
(7.15 CU FT, PAINTED, WAKEFIELD GREEN)
A,B
1
515
6084-02
• • CYLINDER, STEEL (DOT-3M-18oo)
(7.15 CLI FT, UNPAINTED)
A,B
1
520
6350A4XG
• CYLINDER, STEEL (SPN 6350-A4-X-G)
(22 eLi FT, PAINTED, GRAY-GREEN)
H, J, W-AC, AP
1
520A
6350A4XA
• CYLINDER, STEEL (SPN 6350-A4-X-A)
(22 CU FT, PAINTED, WAKEFIELD GREEN)
AE,AQ
1
525
6084-04
•• CYLINDER, STEEL (DOT-3M-18oo)
(22 CU FT, UNPAINTED)
H, J, W-AE,
AP,AQ
1
540
~350ASXG
• CYliNDER, STEEL (SPN 635D-A5-X-G)
(48.3 CLI FT, PAINTED, GRAY-GREEN)
AF
1
540A
6350A5XAN
• CYLINDER, STEEL (SPN 635D-AS-X-AN)
(48.3 CU FT, PAINTED, GREEN AND WHITE)
K
1
540B
6350ASXA
• CYLINDER, STEEL (SPN 635D-A5-X-A)
(48.3 CLI FT, PAINTED, WAKEFielD GREEN)
l
1
545
6084-07
• • CYLINDER, STEEL (DOT-3M-1800)
(48.3 CLI FT, UNPAINTED)
K,l,AF
1
550
6350A20XG
• CYLINDER, STEEL (SPN 6350-A20-X-G)
(11 CLI FT, PAINTED, GRAY-GREEN)
550A
6350A20XA
• CYLINDER, STEEL (SPN 6350-A20-X-A)
(11 CLI FT, PAINTED, WAKEFIELD GREEN)
555
6084-03
• • CYLINDER, STEEL (DOT-3M-1aOO)
(11 CU FT, UNPAINTED)
(SUPSD BY ITEM 555A)
555A
6084-20
•• CYLINDER, STEEL (DOT-3M-18oo)
(11 CLI FT, UNPAINTED)
(SUPSDS ITEM 555)
C-E, M-S, AH
1
F, G, T-V, AJ-AN
1
NP
•
1
C-G, M-V,
AH-AN
1
NOTE 1: 5600 PCA WITHOUT A YEllOW HANDLE (-30, IPL FIGURE 9) MUST USE INSTRUCTION DECAL ITEM 25A.
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10108
20040415
•
e
".
>
..
tqc:a/scott
jSCDtt
Technologies,Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
e
e
CMM & IPL
THIS PAGE INTENTIONAlLY LEFT BLANK
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10109
20040415
'tileD/scott
Technologies. Inc.
jSCOtf
Aviation
.' .
~
55D015600 SERIES PORTABLE CYLINDER ASSEMBL. Y . CMM & /Pl
.•
5
..~
\ _-..
0-...
'-·:._··
....
'/ I"'].t:~..
l
F.
..><fj"."
1
~.
o . _.;~,~j-'+'1!
.........
._-
.'
1...
~
I
\
'11i';...":i j
~ .......
-'
., .. -;;.....;.,~
...t/
~'
801807 Series (Typical)
(801807-01 Shown)
55
60
15
I,
35
36
•
r--------'"1
i
:
\'
f
~
!
"-
I
10
45
50
+/9XmEf{
I
,g
MASK"
~
I
\
/'
t.:.:.;=)~~~
20
~"I
_Ej.''l'''!'J[."'\
.~
' ......
-J
....
"~
40
. .t;. ·
)
.~.~11-.·J
,;.
805436-01 Shown
801808 Series (Typical)
803177 Series (Typical)
41
5500 and 5600 Series PCA
Harness Assembly with Mask and Storage Bag
Figure 2
EFFECTIVITY:
ALL
35-32-18
Page 10110
20040415
•
•
1:QCD /SCOtl
".
Technologies, Inc.
!scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
..•
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
2
•
•
-1
801807·01
HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 1A FOR NHA)
A
RF
-1A
801807·02
HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIGS 1A THRU 1C, AND 1F FOR NHA)
B
RF
-1B
801807·03
HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIGS 1A AND 1C FOR NHA)
C
RF
-1C
801808·01
HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIGS 1A AND 1C FOR NHA)
0
RF
-10
801808-02
HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIGS 1A THRU 1C, AND 1E FOR NHA)
E
RF
-1E
801808-03
HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIGS 1A THRU 1C FOR NHA)
F
RF
-1F
801808-05
HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIGS 1A AND 10 FOR NHA)
G
RF
-1G
803177-01
HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIGS 1A THRU 1E FOR NHA)
H
RF
-1H
803177-02
HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIGS 1A AND 1C FOR NHA)
J
RF
·1J
803177-03
HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIG 1A FOR NHA)
K
RF
-1K
805436-01
HARNESS ASSY WI MASK & STORAGE BAG
(REFER TO FIGS lAAND 1C FOR NHA)
L
RF
5
801662-00
• SLiNGASSY
A-C
1
1
10
801660-00
• HARNESS
D-H,L
15
5065-10
• CONNECTOR, PLUG IN
B,E,L
1
20
5065-10
• CONNECTOR, PLUG IN
G,H
2
-25
14807-00
• COUPLING
A,D
1
C, F,J,K
1
A-F, L
1
J
1
G,H
2
K
2
• FASTENER,VELSTRAP
A-F, H-L
1
36879-01
• FASTENER, VELSTRAP
G
2
55
801809-01
• BAG ASSY, STORAGE MASK
A·F, H-L
1
60
801809-01
• BAG ASSY, STORAGE MASK
G
2
-30
29559-00
• NIPPLE, OUTLET
35
289-601-211
• MASK ASSY, PASS OXYGEN (ALT SPN 289-601·211-2
MAY BE USED UNTIL STOCK IS DEPLETED)
(REFER TO CMM 35-22-26 FOR DET BKDN)
36
289-601-213
• MASK ASSY, PASS OXYGEN
(REFER TO CMM 35-22-26 FOR DEl BKDN)
40
289-601-211
• MASKASSY, PASS OXYGEN (ALT SPN 289-601-211-2
MAY BE USED UNTIL STOCK IS DEPLETED)
(REFER TO CMM 35-22-26 FOR DET BKDN)
41
289-601-213
• MASK ASSY, PASS OXYGEN
(REFER TO CMM 35-22-26 FOR DET BKDN)
45
36879-01
50
- ITEM NO IllUSTRATED
EFFECTIVITY:
ALL
35-32-18
Page 10111
20040415
.' .
t'lco/scotr
/scott
Technologies. Inc. Aviation
~
550015600 SERIES PORTABLE CYLINDER ASSEMBLY • CMM & IPi
.•
130
•
160
/
130 ~
PIN's 6379-2C, -20 and 800649-00, -01
Respirator Regulator Assembly
Figure 3
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10112
20040415
•
•
tl.lc:o/scott
Technologies. Inc.
".
....
ISCDtt
AviatiDn
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
eMM & IPL
EFF.
CODE
NOMENCLATURE
1234567
UNITS
PER
ASSY
3
-10
6379-2C
REGULATOR ASSY, RESPIRATOR
(DEMAND TYPE) (REFER TO FIG 1H FOR NHA)
A
RF
-20
6379·2D
REGULATOR ASSY, RESPIRATOR
(DEMAND TYPE) (REFER TO FIG 1H FOR NHA)
B
RF
-30
800649-00
REGULATOR ASSY, RESPIRATOR
(DEMAND/PRESSURE·DEMAND
TYPE)
(REFER TO FIG 1J FOR NHA)
C
RF
-40
800649·01
REGULATOR ASSY, RESPIRATOR
(DEMAND/PRESSURE-DEMAND
TYPE)
(REFER TO FIG 1J FOR NHA)
D
RF
-50
6050C
• COVERASSY
A,S
1
-60
800651·00
• COVERASSY
C,D
1
ATTACHING
70
MS35206-212
PARTS
3
• SCREW, PAN HEAD (V96906)
(CAD PLATED STEEL) (SPN 33321-212)
(#4-40 THO x 0.188 in. LNG)
•••
•
80
10001297
• • PLATE,IDENTIFICATION
C,D
1
90
6375-04
• • PLATE,IDENTIFICATION
A,S
1
A,B
2
ATTACHING
100
MS204 70A2-2
• • RIVET (ALUMINUM) (V96906)
(SPN 18415-00)
•••
110
6378-00
• • PLATE, IDENTIFICATION
A,B
1
120
6597-D0
• • PLATE, IDENTIFICATION
C,D
1
130
MS20470A2-2
140
6586-00
-
150
6588-00
• • PLATE ASSY, W/ LEVER (ORDER NHA, -60)
160
6583-00
ATTACHING
PARTS
2
• • RIVET (ALUMINUM) (V96906)
(SPN 18415.Q0)
C,D
1
C,D
1
• • SPRING
C,D
1
• • SPRING, COMPRESSION
NP
170
6584-00
• • BUTTON, SLIDE
C,D
1
180
6050-01
• • COVER, CASE
AS
1
100
6582-00
• • COVER, CASE
C,D
1
200
13374.()Q
• DIAPHRAGM ASSY (ALI SPN 803145.Q1)
205
A1215-1
• DIAPHRAGM CORD (SUPSD BY ITEM 210)
210
10009359
• CLAMP, DIAPHRAGM
ATTACHING
•
PARTS
1
PARTS
NP
(SUPSDS ITEM 205)
1
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10113
20040415
't'lco/SCOtl
/SCOtf
TechnoJogies.Inc. Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
3
PART NUMBER
AIRLINE
STOCK NO.
.' .
..•
~
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
....
220
A1126
·230
9036.00
• SCREW, PAN HEAD (REPLD BY 23OA)
2
230A
MS35207-201
• SCREW, PAN HEAD (V96906 (REPLS -230)
(CAD PLATED STEEL)
(#2-64 THO x 0.125 in. LNG) (SPN 33326-201)
2
• VALVEASSY, DEMAND
1
1
• DEFLECTOR (SPN A-1126)
AITACHING PARTS
....
240
6055E
AITACHING PARTS
250
MS35206-213
• SCREW, PAN HEAD (V96906)
(CAD PLATED STEEL) (SPN 33321·213)
(#4-40 THO x 0.250 in. LNG)
2
260
MS35333-36
• WASHER, LOCK (V96906)
(CAD PLATED STEEL) (SPN 33460-036)
(#4 OIA x 0.017 in. THK)
2
-270
6066-00
• WASHER, FLAT (CRES) (REPLD BY 270A)
2
270A
~066.o1
• WASHER, FLAT (CRES) (REPLS -270)
(0.281 in. 00 x 0.125 in. 10 x 0.031 in. THK)
2
....
-280
A1120B
• GASKET. VALVE SEAT (SPN A-1120B)
(REPLO BY 280A)
1
280A
13362-00
• GASKET, VALVE SEAT (REPLS -280)
1
290
5603-00
• ADAPTER
A,C
1
300
5606-00
• ADAPTER
B,O
1
-310
A01983
• • COVERASSY
(SPN AD-1983)
B,D
1
·320
5606.01
• • BODY, ADAPTER
B,D
1
·330
13164-00
• • RING, RETAINING EXTERNAL
(CARBON SPRING STEEL)
(0.925 in. 10 x 0.042 in. THK)
B,D
1
340
6812-00
• SCREEN (BRASS)
1
·350
5607-01
• CASE, REGULATOR
1
350A
5607-00
• CASE, REGULATOR
1
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
5600 SERIES
35-32-18
Page 10114
20040415
•
•
1:'1CD/scott
•
".
..
Technologies. Inc.
jscotf
Aviation
5500'5600
SERIES PORTABLE CYUNDER ASSEMBLY· eM" & IPL
..
THIS PAGEINTENTIONALL
Y LEFT BLANK
•
•
EFFECTIVITY:
ALL
35-32-18
Page 10115
20040415
t'-/ca/scotl
/scott
Technologies. Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
t•••
CMM & IPL
50
~
I
200
-@
60
70
• !
5041 SERIES
Only
130
•I
t
-i;'
5041-00 Only
80
---120
140
150
@
190
180
•
160
~
170
110
~
/
170
6
40
30
10
20
PIN 5041-00 and 5041 Series Outlet Assembly
Figure 4
EFFECTIVITY:
ALL
35-32-18
Page 10116
20040415
•
•
•
• '.
•!
t'lco/scott
!SCDtt
Technologies. Inc. AviatiDn
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
4
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPI
NOMENCLA lURE
124567
NP
EFF.
CODE
UNITS
PER
ASSY
A
RF
-1
5041-00
OUTLET ASSY (SUPSD BY ITEM -2)
(REFER TO FIGS 1A THRU 1C, 1E,
1G THRU 1J FOR NHA}
-2
5041-.5-15
OUTLET ASSY (SLlPSDS ITEM -1)
(REFER TO FIG 1A FOR NHA)
B
RF
-2A
5041-.5-20
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIG 1E FOR NHA)
C
RF
·2B
5041-2-20
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIGS 1A THRU 1C, 1E, AND 1H}
D
RF
-2C
5041-2-23
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIGS 1A THRU IC, AND 1H
FORNHA)
E
RF
-2D
5041-2-25
OUTLET ASSY (SUPSDS ITEM -1}
(REFER TO FIG 1A FOR NHA}
F
RF
-2E
5041-2-30
OUTlET ASSY (SUPSDS ITEM -1)
(REFER TO fiG 1C FOR NHA)
G
RF
-2F
5041-2.5-30
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIGS 1A, AND 1G FOR NHA)
H
RF
-2G
5041-3-20
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIGS 1A THRU 1C, 1E, 1H, AND 1J
FORNHA}
J
RF
-2H
5041-3-23
OUTLET ASSY (SUPSDS ITEM -1}
(REFER TO FIG 1H FOR NHA)
K
RF
-2J
5041-4·20
OUTLET ASSY(SUPSDS ITEM -1}
(REFER TO FIGS 1A THRU 1C, 1E, 1H, AND 1J
FORNHA)
L
RF
-2K
5041-4-23
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIGS 1A THRU 1C,AND 1H
FORNHA)
M
RF
-2L
5041-4-25
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIG 1A FOR NHA)
N
RF
-2M
5041-4-30
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIG 1C FOR NHA)
P
RF
-2N
5041-7-20
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIGS 1A, 1C, AND 1E FOR NHA)
Q
RF
-2P
5041-7-30
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIG 1C FOR NHA)
R
RF
10
29556-01
• COVERASSY
20
29557-00
1
ATIACHING PARTS
1
• NUT
•••
30
•
5042-01
1
• CAP
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
ALL
35-32-18
Page 10117
20040415
.' .
1:l./ca/scott
/scott
Technologies,Inc. Aviation
5~600
FIG.
ITEM
4
SERIES PORTABLE CYLINDER ASSEMBLY·
PART NUMBER
AIRLINE
STOCK NO.
',
CMM & IPL
NOMENCLATURE
EFF.
CODE
124567
UNITS
PER
ASSY
1
40
5042-02
• WASHER (AlUMINUM)
(1.00 in. OD x 0.641 in. 10 x 0.062 in. THK)
50
5014..()1
• SCREW (ORDER NHA)
NP
A
60
5013..()1
• SCREEN (ORDER NHA)
NP
A
1
AR
1
70
EC9-5U
• CORD, GLASS (V21343)
(SPN 50330-00) (ORDER NHA)
NP
A
80
5013-01
• SCREEN (ORDER NHA)
NP
A
1
-90
5041-01
• COUPLING ASSY (ORDER NHA)
NP
A
1
-100
804329-01
• OUTLET SLlBASSEMBL Y (ORDER NHA)
NP
B-R
1
110
29567..()0
• • SETSCREW (CRES) (#8-40 THO)
120
29550..()O
• • BODY (ORDER NHA)
NP
A
1
130
10008934
• • BODY (ORDER NHA)
NP
B-R
1
140
29551..()0
•• SPRING
1
150
29552..()0
•• VALVE
1
160
29553-01
• • SEAT, VAlVE
1
170
29555..()O
•• SPRING
2
180
l29556..()0
•• PIN
2
190
29554-00
•• CASE
1
200
50775 SERIES
• ORIFICE, SERIES
(SPN sons SERIES) (ORDER NHA)
1
NP
B-R
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY: ALL
.•
35-32-18
Page 10118
20040415
•
•
".
t'lca/scott
/scott
Technologies. Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
••
CMM & IPL
!
THIS PAGE INTENTIONAllY
LEFT BLANK
•
•
EFFECTIVITY:
All
35-32-18
Page 10119
20040415
l
1:,-/CD /
Scott
Technologies, Inc.
.' .
/ Scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & lPL
f.
.,
10 -
170 -
I
100 --
~
110
ii
6
120
130
0
160
J
@
80-
•
150
140
5009-00
I
or
5009 SERIES
800503-00
Only
180--
I
-
70
Only
~
•
40
~
20
I
I
@
30
I
PIN 5009-00. 5009 Series, and 800503-00 Outlet Assemblies
Figure 5
EFFECTIV\TY: ALL
35-32-18
Page 10120
20040415
•
•
'~.
..•
-tqca/scott
/SCOft
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
5
-1
PART NUMBER
•
NOMENCLATURE
1234567
NP
EFF.
CODE
UNITS
PER
ASSY
A
RF
5009-00
OUTLET ASSY
(REPLD BY ITEM -2) (REFER TO FIGS 1A
THRU 1F, 1H, AND 1J FOR NHA)
. -2
5009-.5-15
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIG 1A FOR NHA)
B
RF
-2A
5009-.5-23
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIG 1A FOR NHA)
C
RF
-2B
5009-.5-25
OUTLET A$$Y (REPLS ITEM -1)
(REFER TO FIG 1A FOR NHA)
D
RF
-2C
•
AIRLINE
STOCK NO.
CMM & In
DELETED
-20
5009-2-10
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS 1A, lB, lE, AND 1F FOR NHA)
F
RF
-2E
5009-2-15
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS 1A, 1C, AND 10 FOR NHA)
G
RF
-2F
5009-2-20
OUTlET ASSY (REPLS ITEM -1)
(REFER TO FIGS 1A THRU 1C, 1E, AND 1H
FORNHA)
H
RF
-2G
5009-2-23
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS lA THRU 1F, AND 1H FOR NHA)
J
RF
"-2H
5009-2-25
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS lA THRU 1E FOR NHA)
K
RF
-2J
5009-2-30
OUTlET ASSY (REPLS ITEM -1)
(REFER TO FIGS lA THRU 1C, 1E, AND 1J
FORNHA)
L
RF
-2K
5009-2.5-20
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS 10 AND 1H FOR NHA)
M
RF
-2L
5009-2.5-23
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIG 18 FOR NHA)
N
RF
-2M
5009-2.5-25
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS lA AND 18 FOR NHA)
P
RF
-2N
5009-2.5-30
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIG lA FOR NHA)
Q
RF
-2P
5009-3-20
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS lA, lC THRU 1E, AND 1H
FORNHA)
R
RF
-20
5009-3-23
OUTlET ASSY (REPLS ITEM -1)
(REFER TO FIGS lC, 1E, AND 1H FOR NHA)
S
RF
-2R
5009-3-25
OUTLET ASSY (REPlS ITEM -1)
(REFER TO FIGS lA, 1C, AND 10 FOR NHA)
T
RF
-2S
5009-3-30
OUTLET ASSY (REPlS ITEM -1)
(REFER TO FIGS lA, lE, AND 1J FOR NHA)
U
RF
- ITEM NOT IllUSTRATED
EFFECTIVITY:
ALL
35-32-18
Page 10121
20040415
~
1:'1ca/scolt
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
5
PART NUMBER
AIRLINE
STOCK NO.
..
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
-2T
5009-4-10
OUTlET ASSY (REPlS ITEM -1)
(REFER TO FIGS 1A THRU lC, 1E, 1F, AND lJ
FORNHA)
V
RF
-2U
5009-4-15
OUTLET ASSY (REPlS ITEM -1)
(REFER TO FIG 1C FOR NHA)
W
RF
-2V
5009-4-20
OUTLET ASSY (REPlS ITEM -1)
(REFER TO FIGS 1A THRU lC, 1E, 1H, AND 1J
FORNHA)
X
RF
-2W
5009-4-23
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS 1A THRU IF, 1H, AND 1J
FOR NHA)
Y
RF
-2X
5009-4-25
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS 1A THRU lE, AND 1H
FORNHA}
Z
RF
-2Y
5009-4-30
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS 1A THRU 1C, 1H, AND 1J
FORNHA)
AA
RF
-2Z
5009-4.5-23
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIG 1E FOR NHA)
AB
RF
-3
5009-4.5-30
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIG 1E FOR NHA)
AC
RF
-3A
5009-7-23
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS 1C AND 1H FOR NHA)
AD
RF
-38
5009-7-25
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIG 1H FOR NHA)
AE
RF
-3C
5009-7-30
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS 1A, 1C, AND 1J FOR NHA)
AF
RF
-3D
5009-8-20
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS 1C, 1E, AND 1J FOR NHA)
AG
RF
-3E
5009-8-23
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIGS 1C AND 1E FOR NHA)
AH
RF
-3F
5009-8-30
OUTLET ASSY (REPLS ITEM -1)
(REFER TO FIG 1D FOR NHA)
AJ
RF
-4
800503-00
OUTLET ASSY
AI<
RF
10
59447-00
• COVER, OUST
20
5014-00
• SCREW (ORDER NHA)
NP
A
1
30
5013-00
• SCREEN (ORDER NHA)
NP
A
1
40
EC9·5U
• CORD, GLASS (V21343)
(SPN 50330-00) (ORDER NHA)
NP
A
AR
-50
5009-01
• OUTLET ASSY (ORDER NHA)
NP
A
1
-60
804376-01
• OUTLET ASSY (ORDER NHA)
NP
8-AJ
1
70
10001494
• • STUD (ORDER NHA)
NP
A,AK
1
NP
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
ALL
•
35-32-18
Page 10122
20040415
•
1:l./ca/scotl
/scott
Technologies, Inc. Aviation
•
. '.
,
.
S50CV5600SERIES
PORTABLE CYLINDER ASSEMBLY·
~
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
B-AJ
1
5
NP
80
10008915
• • STUD (ORDER NHA)
90
5065-08
•• GASKET
1
100
24823-00
• • VPJ..VE
1
110
5065-06
•• SPRING
1
120
10001493
•• PORT, FLOW (ORDER NHA)
NP
A
130
10001112
• • PORT, FLOW (ORDER NHA)
NP
AK
1
140
5065-02
••
NP
A
1
150
5065-04
•• FILTER (ORDER NHA)
NP
A
1
160
5065-03
• • GASKET (ORDER NHA)
NP
A,AK
1
170
24825-00
••
180
50775 SERIES
• ORIFICE, SERIES (ORDER NHA)
(SPN 50775 SERIES)
RING (ORDER NHA)
RECEPTACLE
1
1
NP
8-AJ
1
•
•
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
ALL
35-32-18
Page 10123
20040415
1:'-/ca/scott
/scott
Technologies. Inc. Aviation
55D015600 SERIES PORTABLE CYLINDER ASSEMBLY·
eMM & IPL
THIS PAGE INTENTIONALLY LEFT BLANK
•
EFFECTIVITY:
ALL
35-32-18
Page 10124
20040415
•
1:'1COj Technologies.
Scott
Inc.
• '.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
~-10
@-~
60
8
>----
•
50
70
80
PIN 8572-02 Outlet Assembly
Figure 6
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
EFF.
CODE
NOMENCLATURE
1234567
UNITS
PER
ASSY
6
-1
8572-02
OUTLET ASSY
(REFER TO FIGS 1A THRU 1F, 1H, AND 1J
FORNHA)
10
802233-01
• BODY ASSEMBLY, WI PIN
1
-20
27434-01
••
PIN, GROOVED
1
-30
10005326
••
WASHER
1
10005272
••
BODY
1
-40
•
RF
50
8579-00
• GASKET
1
60
8578-00
• POPPET
1
70
8569-01
• SPRING
1
80
A1119
• FILTER, INLET (SPN A-1119)
1
90
8587-01
• ADAPTER
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
ALL
35-32-18
Page 10125
20040415
1:L/CO/SCOtl
Technologies. Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
....
..
10
•
~
I
30
I
20
5507-00Only
""
CMM & IPL
160
I
30
5507 SERIES
Only
I
--150
140
130
120
110
100
90
50
60
70
80
~
•
I
@
0
6
•
I
r
p
a
PIN 5507-00 and 5507 Series Outlet Assembly
Figure 7
EFFECTIVITY:
ALL
35-32-18
10126
20040415
Page
•
•
.".
tileD /scott
Technologies. Inc.
!scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPi
':
FIG.
ITEM
7
•
PART NUMBER
AIRLINE
STOCK NO.
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
-1
5507-00
OUTLET ASSY
NP
(SUPSD BY ITEM -2)
(REFER TO FIGS 1A THRU 1C, AND 1H FOR NHA)
A
RF
-2
5507-2-20
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIGS 1B AND 1C FOR NHA)
B
RF
-2A
5507-2-23
OUTlET ASSY (SUPSDS ITEM -1)
(REFER TO FIGS 1A AND 1C FOR NHA)
C
RF
·2B
5507-2-30
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIG 1A FOR NHA)
D
RF
·2C
5507-3-20
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIG 1H FOR NHA)
E
RF
-20
5507-4-20
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIG 1A THRU 1C FOR NHA)
F
RF
-2E
5507-4-23
OUTLET ASSY (SUPSDS ITEM -1)
(REFER TO FIG 1AAND 1C FOR NHA)
G
RF
10
5014-01
• SCREW (ORDER NHA)
NP
A
1
20
EC9-5U
• CORD (V21343)
(SPN 50330-00) (ORDER NHA)
NP
A
AR
30
5013-01
• SCREEN (ORDER NHA)
NP
A
2
-40
5533-00
• OUTLET SUBASSEMBLY
(ORDERNHA)
NP
50
804201..()1
• • ADAPTER ASSY, THREADED
60
10008596
• • SPRING, TORSION
1
70
10008595
• • COVER, DUST
1
1
1
ATTACHING PART
80
•• SCREW, FILLISTER HEAD
(CRES WI PLASTIC INSERT)
(#2-56 THO x 0.250 in. LNG)
10008660
1
•••
•
90
10008774
•• WASHER (CAD PLATED STEEL)
(0.985 in. 00 x 0.596 in. 10 x
0.050THK)
1
100
10008601
• • WASHER, OUTLET
(COPPER ALLOY)
(0.492 in. OD x 0.265 in. ID x
0.050 in. THK)
1
110
10008602
• • GASKET, OUTLET
1
120
10008603
••
1
130
10008594
• • SPRING, FLOW-STOP (CRES)
140
5533-01
• • BOOY (V493151 (ORDER NHAI
POPPET, OUTLET
1
NP
A
1
- ITEM NOT IllUSTRATED
EFFECTIVITY:
All
35-32-18
Page 10127
20040415
f:l./ca/scou
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
7
PART NUMBER
AIRLINE
STOCK NO.
,.-
.
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
150
10008947
•• BODY (ORDER NHA)
NP
B-G
1
160
50775 SERIES
• ORIFICE, SERIES (ORDER NHA)
(SPN 50775 SERIES)
NP
B-G
1
•
-ITEM NOT ILLUSTRATED
EFFECTIVITY: All
35-32-18
Page 10128
20040415
•
•
_.,
,~.
f:L/co/scott
jSCDtt
Technologies,Inc. Aviation
55OO15liOO SERIES PORTABLE CYLINDER ASSEMBLY - ClAM & IPL
THIS PAGE INTENTIONALLY LEFT BLANK
•
•
EFFECTIVITY:
ALL
35-32-18
Page 10129
20040415
tl.lco/scott
/scott
Technologies.Inc. Aviation
'.,
550015600 SERIES PORTABLE CYLINDER ASSEMpLY • CMM & IPt
e
•
10
30<!
20
,-::
70~
__
I
120
80
Gj-110
&--100
•
90--~
PIN5052-00 OutletAssembly
Figure 8
EFFECTIVITY:
ALL
35-32-18
Page 10130
20040415
•
•
•
•
. '.
.•
t'lCO/SCOll
/scott
Technologies.Inc_ Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY - CMM & IPL
FIG.
ITEM
8
PART NUMBER
AIRLINE
STOCK NO.
EFF.
CODE
NOMENCLATURE
1234567
UNITS
PER
ASSY
-1
5052-00
OUTLET ASSY
[REFER TO FIG 1H FOR NHA)
NP
RF
10
5014-00
• SCREW, ORIFICE ADJUSTING
NP
1
20
EC9-5U
• CORD (V21343) (SPN 50330-00)
NP
AR
2
30
5013-00
• SCREEN
NP
40
5058.{)O
• WASHER
NP
1
-50
5052-02
NP
1
60
5067-01
• COUPLING
•• BASE
NP
1·
70
5067-02
• • GASKET, BODY
NP
1
80
5067-04
•• SPRING
NP
1
90
5067-07
• • SEAT, VALVE
NP
1
100
5067-06
•• GASKET, VALVE SEAT
NP
1
110
5067-05
••
NP
1
120
5067-03
•• BODY
NP
1
RETAINER
Items -1 through 120 are not procurable. If replacement is required, the outlet assembly must be replaced by a different outlet assembly. To choose
an outlet assembly that is procurable referto Table 1, PCA Configuration Matrix, in the beginning ofthis section ofthe manual.
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
ALL
35-32-18
Page 10131
20040415
'tL/ca!scott
/scott
Technologies.
Inc. Aviation
550015600SERIES PORTABLf CYLINDfRASSfMSLY
• CMIA & IPL
350
/360
_370A~380
420
,--
..........
~390A
V
410~
400
430'6
L~
440~
460--:!
20
300
~~
""'+
--... @
490
510
30A__ ~
/
60.............
70 __
80 __
L..---Il-/ -I
210
•
270
~ '/' .-~?®
500
~
560
570
140-e
130~
280
280
90--$
:::--i
290i
.-/330
e:::r::o
~
110:1
d
340
470~
460 ____
~UJ)(
....
170
~
\240
160
250
\
230
I
PIN 5510 Series and 803199-04
Regulator Assembly
Figure 9
EFFECTIVITY: All
35-32-18
Page 10132
20040415
•
•
•
•
• _~
t'lca/scott
/scott
Technologies, Inc. Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
9
PART NUMBER
AIRLINE
STOCK NO.
CMM & IPL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
-1
5510-10
REGULATOR ASSY
(REFER TO FIGS 1A THRU 1C, 1H, AND 1J
FORNHA)
A
RF
-1A
5510-13
REGULATOR ASSY
(REFER TO FIGS 10, iE, 1H, AND 1J
FORNHA)
B
RF
-1B
5510-15
REGULA TOR ASSY
(REFER TO FIGS iE, 1H, AND 1J FOR NHA)
C
RF
-1C
5510-17
REGULATOR ASSY
(REFER TO FIG 1F FOR NHA)
0
RF
-10
5510-19
REGULATOR ASSY
(REFER TO FIGS 1E AND 1J FOR NHA)
E
RF
-1E
803199-04
REGULATOR ASSY
(REFER TO FIG 1G FOR NHA)
F
RF
-10
5520-17
• VALVE, ON-QFF (SUPSO BY -11)
A-E
1
11
5520-16
• VALVE, ON-OFF (SUPSOS 10)
1
20
22427-01
• • PLATE,IDENTIFICATION
1
-30
23274-03
• • HANDLE (YELLOW)
1
30A
23274-05
• • HANDLE (GREEN)
1
-40
MS356S0-304
• • NUT (CRES) (V96906)
(SUPSO BY ITEM 4OA)(SPN 18463-00)
(0.190-32 THO) (NOTE 1)
40A
804670-03
• • NUT (CRES) (0.190-32 THO) (NOTE 1)
-50
NAS1149C0332R
• • WASHER (V80205) (SUPSD BY ITEM 40A)
(SPN 19147-00) (CAD PLATEO STEEL)
(# 10 DlA x 0.025 in. THK) (NOTE 1)
60
22445-01
• • WASHER, SPRING
(0.706 in. 00 x 0.313 in. 10 x 0.016 in. THK)
1
70
5511-00
• • WASHER, FLAT (PHENOLIC)
(0.750 in. 00 x 0.281 in. 10 x 0.031 in. THK)
2
80
23394-01
• • NUT, PACKING
1
ATTACHING PARTS
NP
1
1
NP
1
90
55620-01
• • PACKING, PREFORMED
1
100
10007887
• • STEMASSY
1
110
5517-00
• • SEAT, PTFE
1
120
802883-01
• • HEADASSY
1
130
55620-02
• • PACKING, PREFORMED
1
140
23393-01
• • BUSHING
1
150
5522-00
• FILTER
1
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
All
35-32-18
Page 10133
20040415
'fqca/scott
/SCOtf
Technologies.Inc. Aviation
55D0156ooSERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
9
PART NUMBER
AIRLINE
$TOCKNO.
"
CMM & #PL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
-158
5016-00
• CAP, FILLER (REPLD BY 160)
1
-159
5023-00
• SEAT, FILLER CAP (REPLD BY 160)
1
160
804202-01
• CAP, FIllER (REPLS -158, -159)
1
170
5093-01
• VALVE, CHARGING
1
-180
5092-00
• • BODY
1
-190
57524-00
• • CORE, VALVE
1
-200
10002684
• • FILTER (BRONZE)
1
210
6363-01
• PLUG, SAFETY
-220
801421-01
230
26565-00
240
A-E
1
• OUTLET ASSY, SAFETY
F
1
• • CAP, SAFETY
F
1
6555-00
• • GASKET
F
1
250
26567-00
• • PLUG, SAFETY
F
1
260
6364-00
• • DISC, SAFETY
A-E
1
270
10003742
• • DISC, SAFETY (SILVER)
(ALT SPN 10006001 (BRONZE))
F
1
6370-00
• WASHER, SAFETY PLUG
280
•
1
I
290
2661-03
• GAUGE ASSY, PRESSURE
(REFER TO FIG 12 FOR DET BKDN)
A-C,E
1
300
802821-01
• GAUGE ASSY. PRESSURE
(REFER TO FIG 12 FOR DET BKDN)
D
1
-310
2661-04
• GAUGE ASSY. PRESSURE
(REFER TO FIG 12 FOR DET BKDN)
F
1
320
5043-14
• VALVE ASSY, RELIEF
A,S
1
330
5043-14
• VALVE ASSY, RELIEF
D,F
1
340
5043-14
• VALVE ASSY, RELIEF
C,E
1
350
5056·00
• PLATE, IDENTIFICATION
•
1
ATTACHING PARTS
2
360
59553-00
-370
37008-00
370A
37008-02
• SETSCREW, OVAL POINT (CRES)
(0.25Q-20UNC-3A x 0.375 in. LNG) (REF: UNBRAKO
PIN 28711L-4-6 [WITH LQC.WEL PATCH] OR EQUIV.)
(REFER TO NOTE 2)
1
380
5005-03
• CASE
1
• SCREW (CRES WI PLASTIC INSERT)
(#2-64 THD x 0.188 in. LNG)
-
• SETSCREW (REPLO BY 370A) (REFER TO NOTE 2)
A-E
1
- ITEM NOT ILLUSTRATED
EFFECTIVITY: ALL
35-32-18
Page 10134
20040415
•
•
tl./Ca!SCOll
!scott
Technolog;es. Inc. Aviation
"".
.
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
;
FIG.
ITEM
PART NUMBER
AIRLINE
STOCK NO.
CMM & 'PL
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
A-E
1
9
•
\
-390
8561-00
• GUIDE, SPRING (REPLD BY 390A)
(REFER TO NOTE 2)
390A
8561-02
• GUIDE, SPRING (REPLS -390) (REFER TO NOTE 2)
1
400
5003-00
• SPRING, ADJUSTING
1
410
5034-00
• PLATE, DIAPHRAGM
1
420
5033-00
• RING, SLIP
3
430
5032-01
• DIAPHRAGM
1
440
5031·00
• PLATE, THRUST
1-
450
5030-01
• HOLDER
1
460
803129-01
• SEAT ASSY
1
470
5028-00
• PIN, THRUST
1
480
5002-00
• GUIDE, THRUST PIN
1
49D
5027-00
• SPRING
1
500
10003305
• TUBE, DRAIN
1
510
27170-01
• BODY (BRASS - 2 OUTLET)
A"
1
1
-520
27170-03
• BODY (BRASS - 2 OUTLET)
B,D
-530
27170-02
• BODY (BRASS - 3 OUTLET)
C
1
-540
27170-04
• BODY (BRASS - 3 OUTLET)
E
1
-550
27170-05
• BODY (BRASS - 2 OUTLET)
F
1
560
5057-14
• PLATE, IDENTIFICATION
F
1
570
5057-00
• PLATE, IDENTIFICATION
A-E
1
580
MS21318-7
ATIACHING PARTS
• SCREW, DRIVE (CRES) (V88044)
(#0 x 0.125 in. LNG) (SPN 33343-007)
-
2
Note 1: Nut, SPN 804670-03, has a permanentiy attached washer. If SPN 804670-03 is used as a replacement part, washer (50) must be removed
and discarded.
Note 2: Setscrew (-370) must be used only with auide (-390). Setscrew (370A) must be used only with Quide (390A).
•
- ITEM NOT ILLUSTRATED
EFFECTIVITY:
ALL
35-32-18
Page 10135
20040415
-tqcO/scotl
/scott
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
"
CMU & IPL
•
i-
50
70,
~-40
70
e-o-t:::J- .........
80 ............
a_110
do;.-100
@-90
~-120
1-
130
30_~
~
10~-140
•
PIN 802863-02 Outlet Assembly
Figure 10
EFFECTIVITY:
ALL
35-32-18
Page 10136
20040415
•
•
•
•
.....
.
~•
1:I./ca/scolt
Technologies. Inc.
/scott
Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
10
PART NUMBER
AIRLINE
STOCKNQ.
CMM & IPL
EFF.
CODE
NOMENCLATURE
1234567
UNITS
PER
ASSY
-1
802863'()2
OUTLET ASSY
(REFER TO FIGS 1A THRU 1E FOR NHA)
RF
10
AS4860D01
• NIPPLE (VQ5AY8)
1
·20
802874-01
• PLUG ASSY, DUST
1
30
59447·01
• • COVER, DUST
1
40
36862-05
• • PACKING, PREFORMED
1
50
802877-01
••
1
-tiO
802061·00
• SLEEVE ASSY, WI PIN
1
70
10004844
•• PIN
2
80
10004845
• • SLEEVE, INSERT
1
90
10004840
• SEAL
1
100
10004841
• RETAINER
1
110
AS35B2-ooB
• PACKING, PREFORMED (V05AY8)
1
120
10004839
• POPPET
1
130
10004838
• SPRING
1
140
10005750
• BODY, OUTlET
1
PLUG, DUST
-ITEM NOT ILLUSTRATED
EFFECTIVITY:
ALL
35-32-18
Page 10137
20040415
-t'lcajscott
Technologies. Inc.
/SCOff
Aviation
5500/5600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMU & IPL
~~-!
60-70-~
80--~
90
~
10
100--~
110-0
1::__ ~
•
50-6
PIN 802856-01 Outlet Assembly
Figure 11
EFFECTIVITY: ALL
35-32-18
Page 10138
20040415
•
•
...."
.• "
1:yca/scotl
/SCDtt
Technologies, Inc. Aviation
55DO/5600SERIES PORTABLE CYLINDER ASSEMBLY·
FIG.
ITEM
11
-1
PART NUMBER
AIRLINE
STOCK NO.
802856-01
CMM & IPL
EFF.
CODE
NOMENCLATURE
1234567
OUTLET ASSY
(REFER TO FIGS 1A, lC, 1E AND lH FOR NHA)
UNITS
PER
ASSY
RF
10
10008644
• RETAINER, DUST COVER
1
20
10005614
• FITrlNG, DISCONNECT
1
30
36874-01
• PIN, GROOVE
2
40
10005617
• COVER, DUST
1
50
27511-01
• LABEL, WARNING
1
60
10009328
• GASKET
1
70
36588-04
• SPRING, POPPET
1
80
10005616
• POPPET, DISCONNECT
1
90
36636-01
• RING, QUAD
1
100
10005615
• BODY, DISCONNECT
1
110
280OC14A
• PACKING, PREFORMED
(AlTSPN 18012-00)
1
120
2800Cl0A
• PACKING, PREFORMED
(ALT SPN 55622-00)
1
•
•
- ITEM NOT ILLUSTRATED
EFFECTIVITY: ALL
35-32-18
Page 10139
20040415
t'lco/scott
Technologies.
Inc.
/scott
•
Aviation
SSW5600 SERIES PORTABLE CYLINDER ASSEMBLY· CAlM & /PL
•
PIN 2661-03, -04 and 802821-01
Pressure Gauge Assembly
Figure 12
EFFECTIVITY:
ALL
35-32-18
Page 10140
20040415
•
•
•
•
~~
-tl.lco/scott
/scott
Technologies, Inc. Aviation
•• 550015600 SERIES PORTABLE CYLINDER AS$EMBL Y • CMM & IPL
FIG.
ITEM
12
PART NUMBER
AIRLINE
STOCK NO.
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
1
2661-03
GAUGE ASSEMBLY, PRESSURE
(REFER TO FIG 9 FOR NHA)
(30 THREADS PER INCH, MACHINED)
(SUPSD BY ITEM 1A)
NP
A
RF
1A
2661-03
GAUGE ASSEMBLY, PRESSURE
(REFER TO FIG 9 FOR NHA)
(20 THREADS PER INCH, ROLLED)
(SUPSDS ITEM 1)
(SUPSO BY ITEM IB)
NP
B
RF
1B
2661-03
GAUGE ASSEMBLY, PRESSURE
(REFER TO FIG 9 FOR NHA)
(4 LUGS AT 90 DEGREES)
(SUPSOS ITEM 1A)
(SUPSO BY ITEM 1C)
NP
C
RF·
1C
2661-03
GAUGE ASSEMBLY, PRESSURE
(REFER TO FIG 9 FOR NHA)
(3 LUGS AT 120 DEGREES)
(SUPSDS ITEM 1B)
(SUPSD BY ITEM 10)
NP
D
RF
10
2661-03
GAUGE ASSEMBLY, PRESSURE
(REFER TO FIG 9 FOR NHA)
(24 THREADS PER INCH, ROLLED)
(SUPSDS ITEM 1C)
E
RF
1E
802821-01
GAUGE ASSEMBLY, PRESSURE
(REFER TO FIG 9 FOR NHA)
(20 THREADS PER INCH, ROLLED)
F
RF
1F
2661-04
GAUGE ASSEMBLY, PRESSURE
(REFER TO FIG 9 FOR NHA)
(24 THREADS PER INCH, ROLLED)
G
RF
10
56750-00
• BEZEL (METAL, BLACK)
A
1
20
21217-11
• BEZEL (METAL, BLACK)
E,G
1
30
13753-00
• LENS (PLASTIC)
A
1
40
21217-12
• LENS (PLASTIC)
E,G
1
50
56750-01
• LENS WITH BEZEL (ALL PLASTIC)
0
1
60
56750-02
• LENS WITH BEZEL (ALL PLASTIC)
B,e,F
1
70
21217-13
• GASKET
80
21217-14
• LABEL, RELIEF
I
NP
E,G
1
E,G
1
- ITEM NOT IllUSTRATED
EFFECTIVITY:
ALL
35-32-18
Page 10141
20040415
t:'1cajscott
jSCOtf
Technologies. Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & JPL
10
PIN 36728-01 Outlet Assembly
Figure 13
FIG.
ITEM
13
PART NUMBER
AIRLINE
STOCK NO.
NOMENCLATURE
1234567
EFF.
CODE
UNITS
PER
ASSY
-1
36728-01
OUTLET ASSEMBLY
(REFER TO FIGS 1A THRU 1E, 1H, AND 1J FOR NHA)
RF
NP
1
10
59447-00
• COVER, OUST
20
10008611
• BODY, OUTlET
NP
1
30
10008615
• SPRING, COMPRESSION
NP
1
40
10008614
• VALVE, POPPET
NP
1
50
10008613
• SEAL, GASKET
NP
1
60
10008616
• PACKING, PREFORMED
NP
1
70
10008612
• CARTRIDGE, OUTLET
NP
1
-ITEM NOT ILLUSTRATED
EFFECTIVITY: All
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Technologies. Inc. Aviation
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CUM & IPL
SPECIAL PROCEDURES
TASK 35-32-18-99C-804
1. Special Procedures
Not applicable
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EFFECTIVITY:
ALL
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tL/ca/scott
/scott
Technologies, Inc. Aviation
5S~OO
SERJESPORTABLE CYUNDER ASSEMBLY - CMM & /PL
REMOVAL
TASK 35-30-78-010-801
1. Removal
Not applicable
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•
EFFECTIVITY: AlL
35-32-18
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tl./co/scott
/SCOft
Technologies, Inc. Aviation
550015600 SERIES PORTABLE CYLINDER ASSEMBLY • CM&f& IPL
INSTALLATION
TASK 35-32-18-400-804
1. Installation
Not applicable
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EFFECTIVITY:
All
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550015600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & IPL
SERVICING
TASK 35-32-18-550-801
1. Servicing
Not applicable
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EFFECTIVITY:
ALL
35-32-18
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/scott
Technologies, Inc. Aviation
55OllIS600 SERIES PORTABLE CYLINDER ASSEMBLY·
CMM & 'PL
STORAGE
TASK 35-32-18-500-801
1. General
This section contains information on storage (including transportation) requirements for the 5500 Series
and 5600 Series PCA.
TASK 35-32-18-550-802
2. Storage
A. Ensure that the 5500 or 5600 Series PCA on/off valve (10, -11, IPL Figure 9) is in the "OFF" position
before the PCA is transported or put in storage. Rotate the handle (30, IPL Figure 9) fully clockwise to
put the PCA in the "OFF" position.
B. An 5500 Series or 5600 Series PCA should always be transported or put in storage with a minimum
oxygen pressure to prevent contamination from entering. A minimum of 50 - 100 psig
(0.34 - 0.69 MPa) pressure is recommended. A PCA, even when it contains a minimum amount of
oxygen pressure, must still be stored and transported under all applicable regulations. A PCA with less
than 50 psig (0.34 MPa) is an indication of possible contamination. Refer to the CLEANING section in
this manual and clean the PCA if the oxygen pressure is less than 50 psig (0.34 MPa).
C. Make sure all protective caps, plugs, and covers are tightly installed on the PCA.
D. Put the PCA in a clean polyethylene bag and seal it for protection from dust and dirt.
•
E. Store the PCA in a cool area, away from sources of high heat and humidity .
'TASK 35-32-18-510-801
3. Transportation
On August 19, 1999 the United States Department of Transportation (DOT) published a new rule
(Federal Register Vol. 64; No. 160 - Rules and Regulations) concerning transportation of compressed
oxygen cylinders aboard aircraft. This new rule took effect on March 01, 2000. The specific changes to the
Code of Federal Regulations (CFR) concerning transportation of compressed oxygen cylinders aboard
aircraft will be contained in 49 CFR Parts 171, 172 and 175.
The new ruling does not affect shipments of compressed oxygen cylinders by ground (motor freight)
transportation, but new requirements for compressed oxygen cylinder shipments aboard passenger
carrying aircraft and cargo aircraft are specified.
The specified number and size of cylinders to be shipped, certain packaging requirements (Air Transport
Association of America (ATA) Specification No. 300), hazardous materials descriptions, and proper
shipping names (Oxygen, compressed), as well as, hazardous materials identification numbers (UN1072
for Oxygen, compressed) are identified in the new ruling.
Additional requirements and regulations (e.g., Transport Canada) for transport of oxygen cylinders may
apply in other countries.
Subtask 35-32-18-99E-001
A. Reference Documents
Table 15001 contains a list of applicable reference documents for the transportation and packing of
compressed oxygen cylinders aboard aircraft. The information in Table 15001 was accurate on the
revision date of this manual.
•
EFFECTIVITY;
ALL
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550atS600 SERIES PORTABLE CYLINDER ASSEMBLY·
•
CMM & IPL
3. Transportation (Continued)
Table 15001
Reference Documents
DOCUMENT NUMBER
DOCUMENT NAME
ORDERING INFORMATION
Federal Register - Part V; Vol. 64; No. 160
US Department of Transportation
(Research and Special Programs
Administration)
Hazardous Materials: Chemical Oxidizers and
Compressed Oxygen Aboard Aircraft; Final
Rule
US Government Printing Office
Washington, DC 20402
USA
49 CFR Part 171
General Information, Regulations and
Definitions
US Government Printing Office
Washington, DC 20402
USA
49 CFR Part 172
Hazardous Materials Table, Special
Provisions, Hazardous Materials
Communications, Emergency Response
Information and Training Requirements
49 CFR Part 175
Carriage by Aircraft
49 CFR Part 177
Carriage by Public Highway
AlA Specification No. 300
Packaging of Airline Supplies
Air Transport Association of America
Washington, DC 20004-1707
USA
Subtask 35-32-18-530-001
B. Packaging
The optional Scott Air Shipment Cases (82004 Series) shown in Table 15002 comply with ATA
Spec. 300, Type I Reusable Containers requirements.
•
The part numbers given in Table 15002 are procurable from Scott Aviation or your Scott Authorized
Aviation Products Distributor.
Table 15002
Information for Optional Scott Air Shipment Cases
EFFECTIVITY:
ALL
SCOTT PART NUMBER
NOMINAL CYLINDER VOLUME
cu ft (liters)
82004-04
4 (113)
82004-07
7 (198)
82004-11
11 (311)
82004-15
115 (3256)
82004-22
22 (623)
82004-39
39(1104)
82004-49
49 (1388)
82004-66
66 (1869)
82004-76
77 (2180)
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Page 15002
20040415
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-tlleO/scort
Technologies, Inc.
!SCOft
Aviation
550015600SERIES PORTABLE CYLINDER ASSEMBLY·
CMM" 'PL
REWORK
TASK 35-32-18-99C-805
1.
Rework
Not applicable
•
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EFFECTIVITY:
ALL
35-32-18
Page 16001116002
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