TM-5-4930-234-13-and-P

TM-5-4930-234-13-and-P
TM 5-4930-234-13&P
TECHNICAL MANUAL
OPERATORS, ORGANIZATIONAL, AND DIRECT SUPPORT
MAINTENANCE MANUAL AND REPAIR PARTS AND
SPECIAL TOOLS LIST
This copy is a reprint which includes
current pages from changes 1
through 5.
INTRODUCTION
OPERATING INSTRUCTIONS
CLOSED CIRCUIT REFUELING NOZZLE
OPERATOR MAINTENANCE
INSTRUCTIONS
ORGANIZATIONAL MAINTENANCE
INSTRUCTIONS
DIRECT SUPPORT MAINTENANCE
INSTRUCTIONS
REFERENCES
MAINTENANCE ALLOCATION
CHART
COMPONENT OF END ITEM/BASIC
ISSUE ITEMS
ADDITIONAL AUTHORIZATION
LIST
EXPENDABLE/DURABLE
SUPPLIES AND MATERIALS LIST
REPAIR PARTS AND SPECIAL
TOOLS LIST
INDEX
MODEL NUMBERS
NSN 4930-01-194-2625 (AE83206R)
NSN 4930-01-214-2909 (AE83501R)
HEADQUARTERS, DEPARTMENT OF THE ARMY
24 NOVEMBER 1986
URGENT
TM 5-4930-234-13&P
C5
CHANGE
HEADQUARTERS
DEPARTMENT OF THE ARMY
WASHINGTON, D.C., 15 July 1995
NO. 5
OPERATORS, ORGANIZATIONAL, AND
DIRECT SUPPORT MAINTENANCE MANUAL AND
REPAIR PARTS AND SPECIAL TOOLS LIST
CLOSED CIRCUIT REFUELING NOZZLE
MODEL NUMBERS
NSN 4930-01-194-2625 (AE83206R)
NSN 4930-01-214-2909 (AE83501R)
DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.
TM 5-4930-234-13&P, 24 November 1986, is changed as follows:
1. Remove and insert pages as indicated below. New or changed text material is indicated by a vertical bar in
the margin. An illustration change is indicated by a miniature pointing hand.
2.
Remove pages
Insert pages
F-11 and F-12
F-25 and F-26
F-11 and F-12
F-25 and F-26
Retain this sheet in front of manual for reference purposes.
By Order of the Secretary of the Army:
DENNIS J. REIMER
General, United States Army
Chief of Staff
Official:
JOEL B. HUDSON
Acting Administrative Assistant to the
Secretary of the Army
00513
DISTRIBUTION:
To be distributed in accordance with DA Form 12-25-E, block no. 2482, requirements for TM 5-4930-234-13&P.
URGENT
TM 5-4930-234-13&P
C4
CHANGE
HEADQUARTERS
DEPARTMENT OF THE ARMY
WASHINGTON, D.C., 6 March 1991
NO. 4
Operator, Organizational, and Direct Support
Maintenance Manual and Repair Parts and
Special Tools List
CLOSED CIRCUIT REFUELING NOZZLE
MODEL NUMBERS
NSN 4930-01-194-2625 (AE83206R)
NSN 4930-01-214-2909 (AE83501R)
Approved for public release; distribution is unlimited
TM 5-4930-234-13&P, 24 November 1986, is changed as follows:
1. Remove and insert pages as indicated below. New or changed text material is indicated by a vertical bar in
the margin. An illustration change is indicated by a miniature pointing hand.
2.
Remove pages
Insert pages
iii
5-27 and 5-28
5-29 and 5-30
B-5(/B-6 blank)
E-1l and E-2
F-19/(F-20 blank)
iii/(iv blank)
5-27 and 5-28
B-5(/B-6 blank)
E-1 and E-2
F-19/(F-20 blank)
Retain this sheet in front of manual for reference purposes.
By Order of the Secretary of the Army:
CARL E. VUONO
General, United States Army
Chief of Staff
Official:
THOMAS F. SIKORA
Brigadier General, United States Army
The Adjutant General
DISTRIBUTION:
To be distributed in accordance with DA Form 12-25E, (qty rqr block no. 2482)
TM 5-4930-234-13&P
C3
CHANGE
NO. 3
}
HEADQUARTERS
DEPARTMENT OF THE ARMY
WASHINGTON, D.C., 28 August 1989
Operator, Organizational, and Direct Support
Maintenance Manual and Repair Parts and
Special Tools List
CLOSED CIRCUIT REFUELING NOZZLE
MODEL NUMBERS
NSN 4930-01-194-2625 (AE83206R)
NSN 4930-01-214-2909 (AE83501R)
Approved for public release; distribution is unlimited.
TM 5-4930-234-13&P, 24 November 1986, is changed as follows:
1. Remove and insert pages as indicated below. New or changed text material is indicated by a vertical bar in
the margin. An illustration change is indicated by a miniature pointing hand.
2.
Remove pages
Insert pages
2-5 and 2-6
5-13 through 5-16
5-19 and 5-20
F-i through F-15/F-16
F-17 through F-20
F-21 through F-23/F-24
F-25 through F-27/F-28
2-5 and 2-6
5-13 through 5-16
5-19 and 5-20
F-1 through F-15/F-16
F-17 through F-19/F-20
F-21 through F-24
Retain this sheet in front of manual for reference purposes.
By Order of the Secretary of the Army:
CARL E. VUONO
General, United States Army
Chief of Staff
Official:
WILLIAM J. MEEHAN, II
Brigadier General, United States Army
The Adjutant General
DISTRIBUTION:
To be distributed in accordance with DA Form 12-25A, Operator, Unit, and Direct and General Support
Maintenance requirements for Nozzle Assembly (4930-01-194-2625).
TM 5-4930-234-13&P
C2
CHANGE
HEADQUARTERS
DEPARTMENT OF THE ARMY
WASHINGTON, D.C., 14 April 1988
NO. 2
Operator, Organizational, and Direct Support
Maintenance Manual and Repair Parts and
Special Tools List
CLOSED CIRCUIT REFUELING NOZZLE
MODEL NUMBERS
NSN 4930-01-194-2625 (AE83206R)
NSN 4930-01-214-2909 (AE83501R)
TM 5-4930-234-13&P, 24 November 1986, is changed as follows:
1. Remove and insert pages as indicated below. New or changed text material is indicated by a vertical bar in
the margin. An illustration change is indicated by a miniature pointing hand.
2.
Remove pages
Insert pages
i and ii
2-1 and 2-2
4-13 and 4-14
I-1 and I-2
i and ii
2-1 and 2-2
4-13 and 4-14
I-1 and I-2
Retain this sheet in front of manual for reference purposes.
By Order of the Secretary of the Army:
CARL E. VUONO
General, United States Army
Chief of Staff
Official:
R. L. DILWORTH
Brigadier General, United States Army
The Adjutant General
DISTRIBUTION:
To be distributed in accordance with DA Form 12-25A, Operator, Unit, and Direct and General Support
Maintenance Requirements for Nozzle Assembly (4930-01-194-2625).
TM 5-4930-234-13&P
C1
CHANGE
NO. 1
}
HEADQUARTERS
DEPARTMENT OF THE ARMY
WASHINGTON, D.C., 1 May 1987
Operator, Organizational, and Direct Support
Maintenance Manual and Repair Parts and
Special Tools List
CLOSED CIRCUIT REFUELING NOZZLE
MODEL NUMBERS
NSN 4930-01-194-2625 (AE83206R)
NSN 4930-01-214-2909 (AE83501R)
TM 5-4930-234-13&P, 24 November 1986, is changed as follows:
1. Remove and insert pages as indicated below. New or changed text material is indicated by a vertical bar in
the margin. An illustration change is indicated by a miniature pointing hand.
2.
Remove pages
Insert pages
2-3 and 2-4
2-3 and 2-4
Retain this sheet in front of manual for reference purposes.
By Order of the Secretary of the Army:
Official:
JOHN A. WICKHAM, JR.
General, United States Army
Chief of Staff
R. L. DILWORTH
Brigadier General, United States Army
The Adjutant General
DISTRIBUTION:
To be distributed in accordance with DA Form 12-25A, Operator, Unit, and Direct and General Support
Maintenance Requirements for Nozzle Assembly (4930-01-194-2625).
TM 5-4930-234-13&P
WARNING
Ground dip and ground plug must be attached before connecting nozzle to aircraft. Failure to comply can result in severe
electric shock and injury or death to personnel.
WARNING
Aviation fuel is highly flammable. No smoking or open flames are permitted during fueling operations. Failure to comply
can result in injury or death to personnel.
WARNING
Proper eye protection must be worn. Failure to comply can result in loss of eyesight.
WARNING
Never attempt to connect a nozzle with a unisex inlet (nozzle part number AE83501 R) to any coupling produced by a
manufacturer other than Aeroquip Corporation. Failure to heed this warning could result in nozzle disconnecting and
possible loss of aircraft and/or life.
WARNING
For refueling operations, confirm that the inlet coupling is stamped with part number AE70725R before using a nozzle with
a unisex inlet coupling (nozzle part number AE83501 R). Failure to heed this warning could result in loss of aircraft and/or
life.
FIRST AID FOR SOLDIERS FM 21-11
Change 6 a/(b blank)
TM 5-4930-234-13&P
TECHNICAL MANUAL
HEADQUARTERS
DEPARTMENT OF THE ARMY
WASHINGTON, D.C., 24 November 1986
NO. 5-4930-234-13&P
Operator’s, Organizational, and Direct Support Maintenance Manual
and Repair Parts and Special Tools List
CLOSED CIRCUIT REFUELING NOZZLE
MODEL NUMBERS
NSN 4930-01-194-2625 (AE83206R)
NSN 4930-01-214-2909 (AE83501 R)
REPORTING ERRORS AND RECOMMENDING IMPROVEMENTS
You can help improve this manual. If you find any mistakes, or if you know of a way to improve these
procedures, please let us know. Mail your letter, DA Form 2028 (Recommended Changes to Publications
and Blank Forms) or DA Form 2028-2 located in the back of this manual directly to: Commander, US
Army Aviation and Troop Command, ATTN: AMSAT-I-MP, 4300 Goodfellow Blvd., St. Louis, MO 631201798. You may also submit your recommended changes by E-mail directly to <mpmt%/[email protected]>. A reply will be furnished directly to you. Instructions for sending an electronic 2028
may be found at the back of this manual immediately preceding the hard copy 2028.
DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited
TABLE OF CONTENTS
PAGE
CHAPTER 2
Section IV
Section V
Section VI
INTRODUCTION ....................................................................................................................
General Information ................................................................................................................
Equipment Description and Data ............................................................................................
Principles of Operation ...........................................................................................................
1-1
1-1
1-1
1-3
CHAPTER 3
Section I
Section II
Section III
Section IV
OPERATING INSTRUCTIONS ..............................................................................................
Description and Use of Operator’s Controls and Indicators....................................................
Operator Preventive Maintenance Checks and Services .......................................................
Operation Under Usual Conditions ........................................................................................
Operation Under Unusual Conditions .....................................................................................
3-1
2-1
2-2
2-3
2-9
CHAPTER 4
Section I
Section II
Section III
OPERATOR MAINTENANCE INSTRUCTIONS ...................................................................
Lubrication Instructions...........................................................................................................
Troubleshooting Procedures...................................................................................................
Maintenance Procedures........................................................................................................
4-1
3-1
3-1
3-2
CHAPTER 5
Section I
5-1
Section II
Section III
Section IV
Section V
ORGANIZATIONAL MAINTENANCE INSTRUCTIONS.........................................................
Repair Parts, Special Tools; Test, Measurement, and Diagnostic
Equipment (TMDE); and Support Equipment .........................................................................
Service Upon Receipt .............................................................................................................
Troubleshooting Procedures...................................................................................................
Maintenance Procedures........................................................................................................
Preparation for Storage or Shipment ......................................................................................
4-1
4-1
4-1
4-4
4-13
CHAPTER 6
Section I
Section II
DIRECT SUPPORT MAINTENANCE INSTRUCTIONS.........................................................
Troubleshooting Procedures...................................................................................................
Maintenance Procedures........................................................................................................
6-1
5-1
5-5
Change 6 i
TM 5-4930-234-13&P
Table of Contents (Continued)
APPENDIX A.
REFERENCES .......................................................................................................................
Page
A-1
APPENDIX B.
MAINTENANCE ALLOCATION CHART ................................................................................
B-1
APPENDIX C.
COMPONENTS OF END ITEM/BASIC ISSUE ITEMS ..........................................................
C-1
APPENDIX D.
ADDITIONAL AUTHORIZATION LIST ...................................................................................
D-1
APPENDIX E.
EXPENDABLE/DURABLE SUPPLIES AND MATERIALS LIST.............................................
E-1
APPENDIX F.
REPAIR PARTS AND SPECIAL TOOLS LIST.......................................................................
F-1
INDEX .....................................................................................................................................
AI-1
LIST OF ILLUSTRATIONS
Figure
Title
Page
1-1
CCR Nozzle Assembly ..................................................................................................................
1-0
2-1
2-2.
2-3
Operating Controls .......................................................................................................................
Operation of Nozzle, Model AE83206R.........................................................................................
Operation of Nozzle, Model AE835 01R........................................................................................
2-0
2-4
2-7
3-1
3-2
3-3
Cam-Lock Gasket Replacement ...................................................................................................
Unisex Seal Replacement ............................................................................................................
Strainer and O-ring Replacement..................................................................................................
3-3
3-4
3-5
4-1
4-2
4-3
4-4
4-5
4-6
Dust Cap Assembly.......................................................................................................................
Dust Plug Assembly ......................................................................................................................
Ground Plug Assembly..................................................................................................................
Ground Clip Assembly...................................................................................................................
Cam-Lock Coupling Assembly ......................................................................................................
Unisex Coupling Assembly............................................................................................................
4-4
4-6
4-8
4-9
4-11
4-12
5-1
5-2
5-3
5-4
5-5
5-6
5-7
5-8
5-9
5-10
5-11
5-12
5-13
5-14
Cam-Lock Coupling Removal ......................................................................................................
Cam Arm Disassembly..................................................................................................................
Cam Arm Assembly . ...................................................................................................................
Unisex Coupling Removal .............................................................................................................
Unisex Coupling Disassembly.......................................................................................................
CCR Nozzle Component Removal................................................................................................
CCR Nozzle Disassembly .............................................................................................................
Plunger Removal...........................................................................................................................
Nose Sleeve Removal...................................................................................................................
Adapter Removal...........................................................................................................................
Adapter Assembly .........................................................................................................................
Removal of Release Pin Mechanism Tool ...................................................................................
Body Installation ............................................................................................................................
Tool Installation .............................................................................................................................
5-6
5-7
5-7
5-8
5-9
5-11
5-13
5-14
5-16
5-16
5-19
5-20
5-21
5-21
ii
TM 5-4930-234-13&P
LIST OF ILLUSTRATIONS (Continued)
Figure
5-15
5-16
5-17
5-18
5-19
5-20
5-21
5-22
5-23
5-24
Title
Adapter Installation .......................................................................................................................
Torqueing Nose Sleeve ................................................................................................................
Piston and Rack Assembly ...........................................................................................................
Handle and Thumb Latch Assembly ............................................................................................
Plunger Assembly ........................................................................................................................
Rack Positioning Tool ...................................................................................................................
Pin Positioning Tool ......................................................................................................................
Pinion Assembly ...........................................................................................................................
Ring Assembly .............................................................................................................................
Deleted
Page
5-22
5-22
5-23
5-23
5-24
5-26
5-26
5-26
5-26
LIST OF TABLES
Table
Title
Page
2-1
Operator Preventive Maintenance Checks and Services .............................................................
2-3
3-1
Troubleshooting (Operator) ..........................................................................................................
3-1
4-1
Troubleshooting (Organizational) .................................................................................................
4-2
5-1
Troubleshooting (Direct Support) .................................................................................................
5-1
5-2
Spring Dimensions .......................................................................................................................
5-18
Change 4 iii/(iv blank)
TM 5-4930-234-13&P
Figure 1-1. CCR Nozzle Assembly
1-0
TM 5-4930-234-13&P
CHAPTER 1
INTRODUCTION
Section I. GENERAL INFORMATION
1-1.
SCOPE. This Operator’s, Organizational, and Direct Support Maintenance Manual and Repair Parts and Special
Tools List covers operation, maintenance, test, and repair procedures for the Closed Circuit Refueling Nozzle (models
AE83206R and AE83501R), hereafter referred to as "CCR nozzle", "nozzle assembly", or "nozzle". The purpose of the
CCR nozzle is to dispense aviation fuel to
aircraft.
1-2.
MAINTENANCE FORMS, RECORDS, AND REPORTS. Department of the Army forms and procedures used for
equipment maintenance will be those prescribed by DA PAM 738-750, The Army Maintenance Management System
(TAMMS).
1-3.
DESTRUCTION OF ARMY MATERIEL TO PREVENT ENEMY USE. This equipment shall be destroyed in
accordance with TM 750-244-3, Procedures for Destruction of Equipment to Prevent Enemy Use.
1-4.
PREPARATION FOR STORAGE OR SHIPMENT.
Shipment.
See Chapter 4, Section V, Preparation For Storage or
1-5.
REPORTING EQUIPMENT IMPROVENT RECOMMENDATIONS (EIR’S). If your nozzel assembly needs
improvement, let us know. Send us an EIR. You, the user, are the only one who can tell us what you don’t like about your
equipment .Let us know why you don’t like the design or performance. Put it on a SF 368 (Quality Deficiency Report).
Mail it to us at: Commander, U.S. Army Aviation and Troop Command, ATTN: AMSAT-I-MDO, 4300 Goodfellow Blvd.,
St. Louis, MO 63120-1798. We will send you a reply.
1-6.
WARRANTY INFORMATION. The nozzle assembly is warranted by Aeroquip Corporation for one year from date
of original delivery. Warranty starts on the date found on DA Form 2410 or DA Form 2408-16 in the logbook. Report all
defects in material or workmanship to your supervisor who will take appropriate action.
Section II. EQUIPMENT DESCRIPTION AND DATA
1-7.
EQUIPMENT CHARACTERISTICS, CAPABILITIES, AND FEATURES. (See Figure 1-1.)
CHARACTERISTICS:
*
Light weight. Can be hand carried to and from aircraft.
*
Manually operated.
*
Complete nozzle assembly. Includes protective caps and grounding connectors.
Change 6 1-1
TM 5-4930-234-13&P
CAPABILITIES AND FEATURES:
Do not use nozzle to dispense low lead fuel. Failure to comply can result in damage to seals.
1-8.
*
Will dispense aviation grade jet fuels to aircraft.
*
Inlet designed to connect to standard aircraft receptacle without use of additional adapters.
*
Model AE83206R will connect to standard cam-lock couplings.
*
Model AE83501R will connect to another unisex coupling.
*
Cam-lock and unisex couplings are interchangeable. All other parts and operating controls are identical.
*
Will not dispense fuel unless connected to aircraft receptacle.
EQUIPMENT DESCRIPTION AND DATA.
Manufacturer - Aeroquip Corporation
Models - AE83206R and AE83501R
Operating Temperature Range: -250F to 1250F (-320C to +520C)
Inlet Operating Pressure: 125 psig Maximum (862 kPag)
Outlet Operating Pressure (Handle in FLOW Position): 15 psig (105 kPag)
Flow Operating Range: 0 to 150 gpm (0 to 568 lpm)
Length - Handle in Flow Position:
Nozzle Subassembly Only: 13 inches (331 mm)
Nozzle with Coupling and Dust Cap, Model AE83206R: 13 1/2 inches (343 mm)
Nozzle with Coupling and Dust Cap, Model AE83501R: 13 1/2 inches (343 mm)
Length - Handle in No Flow Position:
Nozzle Subassembly Only: 15 1-2 inches (394 mm)
Nozzle with Coupling and Dust Cap, Model AE83206R: 16 inches (407 mm)
Nozzle with Coupling and Dust Cap, Model AE83501R: 16 inches (407 mm)
Width: 4 5/8 inches (117 mm)
Height - Handle in Flow Position:
Nozzle Subassembly Only: 7 3/4 inches (197 mm)
Nozzle with Coupling and Dust Cap, Model AE83206R: 9 3/4 inches (248 mm)
Nozzle with Coupling and Dust Cap, Model AE83501R: 9 1/4 inches (235 mm)
Height - Handle in No Flow Position:
Nozzle Subassembly Only: 6 1/2 inches (165 mm)
Nozzle with Coupling and Dust Cap, Model AE83206R: 8 1/2 inches (216 mm)
Nozzle with Coupling and Dust Cap, Model AE83501R: 8 inches (204 mm)
Weight:
Nozzle Subassembly Only: 6.2 pounds (2.8 Kg)
Nozzle with Coupling and Dust Cap, Model AE83206R: 8.4 pounds (3.8 Kg)
Nozzle with Coupling and Dust Cap, Model AE83501R: 8.4 pounds (3.8 Kg)
1-2
TM 5-4930-234-13&P
1-9.
NOMENCLATURE CROSS REFERENCE LIST.
Closed Circuit Refueling Nozzle - CCR nozzle, nozzle assembly, nozzle.
Adapter Assembly - Unisex coupling, coupling.
Cam-lock coupling - coupling.
Handle - Flow Handle.
1-10.
DIFFERENCES BETWEEN MODELS.
Model AE83206R: Equipped with cam-lock coupling and dust plug on inlet end.
Model AE83501R: Equipped with a unisex coupling and dust plug on inlet end.
1-11.
SAFETY, CARE, AND HANDLING.
SAFETY:
*
Grounding connectors must be attached before connecting nozzle to aircraft receptacle. Failure to comply
can result in injury or death to personnel.
*
No smoking or open flames are permitted in refueling areas. Failure to comply can result in injury or death to
personnel.
*
Do not use a nozzle that is damaged and/or leaking fuel.
CARE AND HANDLING:
*
Keep handle in NO FLOW (off) position when not in use.
*
Keep dust cap and plug installed when not in use. Dirt or dust can damage internal seals.
*
Do not leave laying on ground. Dirt or dust can interfere with handle and/or pullback sleeve operation.
*
Hand carry to and from aircraft. Do not drag on the ground.
*
Keep exterior clean. Remove dirt, dust, mud or moisture.
Section III. PRINCIPLES OF OPERATION
See Chapter 2, Section I, Description and Use of Operator’s Controls and Indicators.
1-3/(1-4 Blank)
TM 5-4930-234-13&P
Figure 2-1. Operating Controls
2-0
TM 5-4930-234-13&P
CHAPTER 2
OPERATING INSTRUCTIONS
Section I. DESCRIPTION AND USE OF OPERATOR’S CONTROLS AND INDICATORS
2-1.
OPERATING CONTROLS. (See Figure 2-1.)
A.
DUST CAP. Keeps dirt and foreign material out of nozzle body (F). To remove, pull pullback sleeve (B)
toward handle (D).
B.
PULLBACK SLEEVE. Releases latches to attach nozzle to aircraft receptacle or dust cap (A). Pull towards
handle (D) to release latches from aircraft receptacle or dust cap (A).
C.
INDICATOR PIN. Red color. Extends from nozzle body (F) to show aircraft fuel tank is full. Retracts flush
with nozzle body (F) when pressure/flow stops.
D.
HANDLE. Used to control flow of fuel. Has two positions, FLOW (on) and NO FLOW (off). To change
position, press thumb latch (E) and pull down (or up) on handle (D). Release thumb latch (E) to lock handle
(D) in position.
E.
THUMB LATCH. Spring-loaded to lock handle (D) in FLOW (on) or NO FLOW (off) position. Press thumb
latch (E) to move handle (D). Release thumb latch (E) to lock handle (D) in position.
F.
NOZZLE BODY. Internally regulates fuel flow.
G.
GROUND CLIP. Grounds aircraft to prevent static electric shock to personnel and fire hazards. Clamp to
grounding rod near aircraft before connecting nozzle body (F) to aircraft.
H.
GROUND PLUG. Grounds aircraft to prevent static electric shock to personnel and fire hazards. Connect to
aircraft before connecting nozzle body (F) to aircraft.
I.
STRAINER. Removes dirt and other foreign particles in fuel. Prevents material from damaging nozzle and/or
aircraft.
J.
CAN-LOCK COUPLING. Used with model AE83206R only. Connects nozzle body (F) to fuel hose using a
standard cam-lock connector. To install/remove fuel hose, or dust plug (K), pull cam arms away from
coupling (J). To lock fuel hose or dust plug (K) to coupling, push cam arms against coupling (J).
K.
DUST PLUG. Used with model AE83206R only. Keeps dirt and foreign material out of nozzle body (F). To
install or remove see cam-lock coupling (J).
2-1
TM 5-4930-234-13&P
L. UNISEX COUPLING. Used with model AE83501R only. Connects nozzle body (F) to fuel hose using a
unisex type connector. Equipped with a spring loaded locking pin to prevent separation of nozzle body (F) and
fuel hose. To disengage locking pin, pull ring away from coupling (L). To install fuel hose, insert in coupling
(L) and turn nozzle body (F) counterclockwise to lock. To remove fuel hose, pull ring and turn nozzle body (F)
clockwise.
M. DUST CAP. Used with model AE83501R nozzle only. Keeps dirt and foreign material out of nozzle body (F).
To install, insert in unisex coupling (L) and turn clockwise. To remove, turn counterclockwise.
Section II. OPERATOR PREVENTIVE MAINTENANCE CHECKS AND SERVICES
2-2.
GENERAL.
a. The nozzle must be inspected to ensure it is ready for operation at all times. A systematic inspection will
identify defects and allow them to be corrected before they can result in serious damage or failure.
b. Defects discovered during operation of the nozzle shall be noted for future corrections. These corrections
shall be done after operation has ceased, or as soon as possible. Stop operation which would damage the nozzle or
aircraft.
c. All deficiencies and shortcomings shall be recorded, together with corrective action taken, on DA form 2404,
"Equipment Inspection and Maintenance Worksheet", as soon as possible.
d. When performing Before Operation (B) and During Operation (D) PMCS, remember the CAUTIONS and
WARNINGS. After operation, be sure to perform After Operation (A) PMCS. If the nozzle fails to operate, troubleshoot
with proper equipment. Report any deficiencies using the proper form. Reference DA PAM 738-750.
2-3.
PREVENTIVE MAINTENANCE CHECKS AND SERVICES. See Table 2-1 for Operator Preventive Maintenance
Checks and Services.
a. Item Number Column. Checks and services are numbered in chronological order regardless of interval. This
column will be used as a source of item numbers for the "TM Item Number" column on DA Form 2404 in recording results
of PMCS.
b. Interval Columns. The columns headed "B", "D", "A", "W", and "M" will contain a dot(*) underneath the
appropriate column, indicating PMCS is to be performed Before, During, After, Weekly, and/or Monthly.
c. Item to be Inspected Column. The items listed in this column are divided into groups and identify the items to
be inspected.
d. Procedures Column. This column contains a brief description of the procedure by which the check is to be
performed.
e. For Readiness Reporting, Equipment is Not Ready/Available If: Column. This column will contain the criteria
which will cause the equipment to be classified as not Ready/Available because of inability to perform its primary mission.
Change 2 2-2
TM 5-4930-234-13&P
NOTE
If nozzle must be kept in continuous operation, check and service only those items that can be checked
and serviced without disturbing operation. Make a complete checks and services when nozzle can be
shut down.
Table 2-1. Operator Preventive Maintenance Checks and Services
NOTE: Within designated interval, these checks are to be performed in the sequential order listed.
B—Before
D—During
A—After
W--Weekly
Procedures
Item
No.
Interval
BDAWM
Item to be
Inspected
Check For and Have
Repaired or Adjusted
M--Monthly
For Readiness
Reporting,
Equipment is Not
Ready/Available if:
1.
* * *
*
Nozzle Assy
Check for damaged body, signs
of leaks or cracks.
Outward signs of
damage.
2.
*
*
*
Cap Assy
Check for signs of cracks,
loose or frayed cable.
N/A
3.
* * *
*
Ground Clip
Assy
Check for loose or frayed
cable. Check for damage to
clip or cable eye.
Outward signs of
damage.
4.
*
*
Coupling
Assy
Check for signs of cracks,
loose or frayed cable. Check
to ensure coupling gasket is
in place.
Outward signs of
damage.
5.
* * *
Cam-Lock
Coupling
Check for loose coupling
or signs of leakage.
Cam-Lock Coupling is
loose or leaking or
shows signs of leakage.
6.
* * *
*
Ground Plug
Assy
Check for loose or frayed
cable. Check for damage to
plug or cable eye.
Outward signs of
damage.
7.
*
*
Strainer
Check for damaged and/or
dirty screen.
N/A
*
*
Section III. OPERATION UNDER USUAL CONDITIONS
2-4.
CONNECTION OF NOZZLE, MODEL AE83206R. (See Figure 2-2.)
1.
Pull cam arms (1) away from coupling (2).
2.
Remove dust plug (3) from coupling (2).
3.
Slide end of fuel hose (4) into coupling (2).
4.
Push cam arms (1) against coupling (2).
Change 1 2-3
TM 5-4930-234-13&P
Figure 2-2. Operation of Nozzle, Model AE83206R
2-4
TM 5-4930-234-13&P
2-5.
OPERATION OF NOZZLE, MODEL AE83206R
WARNING
Ground dip and ground plug must be attached before connecting nozzle to aircraft. Failure to comply can
result in severe electric shock and injury or death to personnel.
1.
As required, uncoil cable on ground dip (5). Connect ground dip (5) to grounding rod.
2.
As required, uncoil cable on ground plug (6). Connect ground plug (6) to aircraft.
WARNING
Aviation fuel is highly flammable. No smoking or open flames are permitted during fueling operations.
Failure to comply can result in injury or death to personnel.
3.
Wipe area around fuel receptacle with a dean lint-free cloth to remove dust or foreign material.
4.
Remove fuel cap from aircraft fuel receptacle.
5.
Pull pullback sleeve (8) towards handle (10) and remove dust cap (7).
6.
Attach nozzle (12) to aircraft fuel receptacle.
7.
Press thumb latch (9). Move handle (10) up to FLOW (on) position.
8.
Operate fuel pump to dispense fuel to aircraft.
9.
Watch indicator pin (11). When it extends from the nozzle (12), shut off fuel pump.
NOTE
For multi-refueling operations, fuel pump does not have to be shut off.
10. Press thumb latch (9). Move handle (10) down to NO FLOW (off) position. Release handle (10).
Nozzle must be removed by pulling straight out from receptacle. Failure to remove properly may cause
damage to receptacle mounting.
11. Pull pullback sleeve (8) toward handle (10). Remove nozzle (12) from receptacle by pulling straight out.
NOTE
A firm pull is required to remove nozzle assembly away from fuel receptacle.
12. Wipe inside of dust cap (7), nozzle (12), and fuel receptacle with a dean lint-free cloth to remove dust, dirt or
fuel.
13. Install fuel cap on aircraft fuel receptacle.
14. Install dust cap (7) on end of nozzle (12) by pulling pullback sleeve (8) toward handle.
15. Disconnect ground plug (6) from aircraft. As required, coil ground plug cable.
16. Disconnect ground dip (5) from grounding rod. As required, coil ground dip cable.
Change 6 2-5
TM 5-4930-234-13&P
17. Wipe exterior of nozzle (12) and cables with a dean, lint-free cloth to remove dust, dirt, moisture, or fuel.
Do not leave nozzle laying on ground. Failure to comply can result in damage to nozzle.
18. Place nozzle (12) in a storage container away from aircraft
2-6.
DISCONNECTION OF N0771 F, MODEL AE83206R.
NOTE
Have a suitable container available to catch any fuel spillage.
2-7.
1.
pull cam arms (1) away from coupling (2).
2.
Remove fuel hose (4) from coupling (2).
3.
Slide end of dust plug (3) into coupling (2).
4.
Push cam arms (1) against coupling (2).
CONNECTION OF NOZZLE, MODEL AF83501R. (FIRGURE 2-3).
WARNING
Never attempt to connect a nozzle with a unisex inlet (nozzle part number AE83501 R) to any coupling
produced by a manufacturer other than Aeroquip Corporation. Failure to heed this warning could result in
nozzle disconnecting and possible loss of aircraft and/or life.
WARNING
For refueling operations, confirm that the inlet coupling is stamped with part number AE70725R before
using a nozzle with a unisex inlet coupling (nozzle part number AE83501 R). Failure to heed this warning
could result in loss of aircraft and/or life.
2-8.
1.
Turn dust cap (1) counterclockwise and remove from coupling (2).
2.
Insert end of fuel hose (4) in coupling (2).
3.
Turn fuel hose (4) clockwise to lock with coupling (2).
4.
Turn handle (5) on fuel hose coupling to FLOW position.
OPERATION OF NOZZLE, MODEL AE3501R
WARNING
Ground dip and ground plug must be attached before connecting nozzle to aircraft. Failure to comply can
result in severe electric shock and injury or death to personnel.
1.
As required, uncoil cable on ground dip (6). Connect ground dip (6) to grounding rod.
Change 6 2-6
TM 5-4930-234-13&P
Figure 2-3. Operation of Nozzle, Model AE83501R
2-7
TM 5-4930-234-13&P
2.
As required, uncoil cable on ground plug (7). Connect ground plug (7) to aircraft.
WARNING
Aviation fuel is highly flammable. No smoking or open flames are permitted during fueling
operations. Failure to comply can result in injury or death to personnel.
3.
Wipe area around fuel receptacle with a clean lint-free cloth to remove dust or foreign material.
4.
Remove fuel cap from aircraft fuel receptacle.
5.
Pull pullback sleeve (9) towards handle (11) and remove dust cap (8).
6.
Attach nozzle (13) to aircraft fuel receptacle.
7.
Press thumb latch (10). Move handle (11) up to FLOW (on) position.
8.
Operate fuel pump to dispense fuel to aircraft.
9.
Watch indicator pin (12). When it extends from the nozzle (13), shut off fuel pum p.
NOTE
For multi-refueling operations, fuel pump does not have to be shut off.
10. Press thumb latch (10). Move handle (11) down to NO FLOW (off) position. Release handle (11).
11. Pull pullback sleeve (9) toward handle (11). Remove nozzle (13) from fuel receptacle.
NOTE
A firm pull is required to remove nozzle assembly away from fuel receptacle.
12. Wipe inside of dust cap (8), nozzle (13), and fuel receptacle with a clean, lint-free cloth to remove dust, dirt or
fuel.
13. Install fuel cap on aircraft fuel receptacle.
14. Install dust cap (8) on end of nozzle (13) by pulling pullback sleeve (9) toward handle.
15. Disconnect ground plug (7) from aircraft. As required, coil ground plug cable.
16. Disconnect ground clip (6) from grounding rod. As required, coil ground clip cable.
2-8
TM 5-4930-234-13&P
17. Wipe exterior of nozzle (13) and cables with a clean, lint-free cloth to remove dust, dirt, moisture, or fuel.
Do not leave nozzle laying on ground. Failure to comply can result in damage to nozzle.
18. Place nozzle (13) in a storage container away from aircraft.
2-9.
DISCONNECTION OF NOZZLE, MODEL AE83501R.
NOTE
Have a suitable container available to catch any fuel spillage.
1.
Turn handle (5) on fuel hose coupling to NO FLOW position.
2.
Pull ring (3) on coupling (2). Turn nozzle (11) clockwise and remove from fuel hose (4). Release ring (3).
3.
Install dust cap (1) on coupling (2). Turn dust cap (1) clockwise to lock in place.
Section IV. OPERATION UNDER UNUSUAL CONDITIONS
2-10. OPERATION IN UNUSUAL CONDITIONS. The operating instructions for usual conditions are acceptable.
Operators must take special care in the following areas.
a. Exterior Cleanliness. Wipe the nozzle, dust caps, dust plugs, and cables with a clean, lint-free cloth to
remove dust, dirt, fuel, moisture, snow, or mud. Moisture, snow, and mud can clog or freeze in pullback sleeve and/or
handle. Never store nozzle if dirty or wet.
b. Dust Caps and Dust Plugs. When not in use, keep dust caps and dust plugs installed. Dust, dirt, moisture,
or mud can contaminate or damage internal seals. Never install dust caps or dust plugs when dirty or wet.
c. Storage. When not in use, keep nozzle stored in an area that will protect it from extreme temperatures, dust,
dirt, mud, and physical damage.
2-9/(2-10 Blank)
TM 5-4930-234-13&P
CHAPTER 3
OPERATOR MAINTENANCE INSTRUCTIONS
Section I. LUBRICATION INSTRUCTIONS
No lubrication is required for operation of this equipment.
Section II. TROUBLESHOOTING PROCEDURES
3-1.
GENERAL.
a. This section contains troubleshooting information for locating and correcting most of the operating troubles
which may develop in the nozzle. Each malfunction for an individual component is followed by a list of tests or inspections
which will help to determine corrective actions to take. Perform tests/inspections and U corrective actions in the order
listed.
b. This manual cannot list all malfunctions that may occur, nor all tests or inspections and corrective actions. If
a malfunction is not listed or is not corrected by listed corrective actions, notify your supervisor.
3-2.
TROUBLESHOOTING. Table 3-1 lists the common malfunctions which may occur during operation or
maintenance of the nozzle. Perform test/inspections and corrective actions in the order listed.
NOTE
Before using this table, be sure all applicable operating checks have been performed.
Table 3-1. Troubleshooting
MALFUNCTION
TEST OR INSPECTION
CORRECTIVE ACTION
1. HANDLE FAILS TO OPERATE SMOOTHLY.
Inspect handle area for signs of dirt or other foreign matter.
Clean area around handle.
2. LEAKAGE FROM COUPLING.
Step 1. Remove nozzle from fuel hose. Inspect inside coupling to ensure gasket or seals are in place. Inspect gasket
or seals for cuts, tears, or distortion.
If gasket or seals are missing or damaged, install a new gasket or seals in coupling.
3-1
TM 5-4930-234-13&P
Table 3-1. Troubleshooting (cont)
MALFUNCTION
TEST OR INSPECTION
CORRECTIVE ACTION
Step 2. Remove coupling from nozzle. Inspect coupling to ensure o-ring is in place. Inspect o-ring for cuts, tears, or
distortion.
If o-ring is missing or damaged, install a new o-ring on coupling. Install coupling in nozzle. Hand-tighten only.
3. INADEQUATE FUEL FLOW.
Step 1. Remove coupling and strainer from nozzle. Check strainer for dirt or other foreign matter.
Clean strainer by removing all dirt and foreign matter.
Step 2. While strainer is removed, inspect for any damage.
Replace strainer if damaged. Install strainer in nozzle, then install coupling. Hand-tighten only.
Section III. MAINTENANCE PROCEDURES
3-3.
GENERAL. This section consists of inspection, service, or replacement of those items which would cause
malfunction or hazardous operation of the nozzle.
3-4.
CAN-LOCK COUPLING GASKET (See Figure 3-1).
a.
Removal.
1.
Shut fuel off at source. Place handle down in NO FLOW (off) position.
NOTE
Have a suitable container available to catch any fuel spillage.
2.
Pull cam arms (2) away from coupling (3). Remove nozzle (1) from fuel hose.
3.
Remove gasket (4) from inside coupling (3).
b.
Inspection. Inspect gasket (4) for cuts, tears or distortion.
c.
Replacement. Replace gasket (4) if damaged.
d.
Reassembly.
1.
Place gasket (4) inside coupling (3).
2.
Attach fuel hose to nozzle (1). Push cam arms (2) toward coupling (3).
3-2
TM 5-4930-234-13&P
Figure 3-1. Cam-Lock Gasket Replacement
3-5.
UNISEX COUPLING SEALS (See Figure 3-2).
a.
Removal.
1.
Shut fuel off at source. Place handle down in NO FLOW (off) position.
NOTE
Have a suitable container available to catch any fuel spillage.
2.
Place handle (6), on fuel hose coupling, in NO FLOW position.
3.
Pull ring (3) toward nozzle (1). Turn nozzle (1) clockwise and remove from fuel hose.
4.
Remove seals (4) from inside coupling (2).
b.
Inspection. Inspect seals (4) on coupling and dust cap for cuts, tears, or distortion.
c.
Replacement. Replace seals (4) if damaged.
3-3
TM 5-4930-234-13&P
d.
Reassembly.
1.
Place seals (4) inside coupling (2) and dust cap.
2.
Connect nozzle (1) to fuel hose and turn counterclockwise to lock in place.
3.
Reconnect nozzle to fuel hose and turn handle (6) to FLOW position to operate nozzle.
Figure 3-2. Unisex Seal Replacement
3-6.
STRAIEKR AND O-RING (See Figure 3-3).
a.
Removal.
1.
Remove nozzle (1) from fuel hose per paragraph 3-4 (for a cam-lock coupling) or 3-5 (for a unisex
2.
Turn coupling (2) counterclockwise to unthread from nozzle (1).
coupling).
3-4
TM 5-4930-234-13&P
3.
Pull strainer (3) out of nozzle (1).
b. Inspection. Inspect strainer (3) for cracks, distortion, or damage to screen. Inspect o-ring (4) on coupling for
damage. Remove o-ring (4) if damaged.
c.
Replacement. Replace strainer (3) or o-ring (4) if damaged.
d.
Reassembly.
1.
Place strainer (3) inside nozzle (1).
2.
Thread coupling (2) into nozzle (1) and hand-tighten.
Figure 3-3. Strainer and O-ring Replacement
3-5/(3-6 Blank)
TM 5-4930-234-13&P
CHAPTER 4
ORGANIZATIONAL MAINTENANCE INSTRUCTIONS
Section I. REPAIR PARTS, SPECIAL TOOLS; TEST, MEASUREMENT
AND DIAGNOSTIC EQUIPMENT (TMDE); AND SUPPORT EQUIPMENT.
All references to these items can be found in Appendices B through F.
Section II. SERVICE UPON RECEIPT
4-1.
4-2.
UNPACKING.
a.
Remove any shipping receipts or documents attached to the outside of the container.
b.
Carefully open the container and remove any protective packing material.
c.
Remove nozzle from container.
INSPECTION.
a.
Inspect nozzle body for signs of damage or broken parts.
b.
Inspect dust cap, dust plug, ground clip, and ground plug for damage and attachment to nozzle.
c.
Report any damaged or missing parts to your supervisor immediately.
Section III. TROUBLESHOOTING PROCEDURES
4-3.
GENERAL.
a. This section contains troubleshooting information for locating and correcting most of the operating troubles
which may develop in the nozzle. Each malfunction for an individual component is followed by a list of tests or inspections
which will help to determine corrective actions to take. Perform the tests/inspections and corrective actions in the order
listed.
b. This manual cannot list all malfunctions that may occur, nor all tests or inspections and corrective actions. If
a malfunction is not listed or is not corrected by the listed corrective actions, notify your supervisor.
4-4.
TROUBLESHOOTING. Table 4-1 lists the common malfunctions which may occur during operation or
maintenance of the nozzle. Perform test/inspections and corrective actions in the order listed.
4-1
TM 5-4930-234-13&P
NOTE
Before using this table, be sure all applicable operating checks have been performed.
Table 4-1. Troubleshooting
MALFUNCTION
TEST OR INSPECTION
CORRECTIVE ACTION
1. DUST CAP ASSEMBLY DAMAGED.
Step 1. Inspect dust cap for corrosion, cracks, or distortion.
If damaged, remove from cable and install new dust cap.
Step 2. Inspect cable for corrosion, cuts, fraying and crimp of sleeves to cable.
If damaged, remove from dust cap and nozzle. Install new cable and sleeves.
2. DUST PLUG ASSEMBLY DAMAGED.
Step 1. Inspect dust plug for corrosion, cracks, or distortion.
If damaged, remove from cable. Install new dust plug.
Step 2. Inspect cable for corrosion, cuts, fraying, and crimp of sleeves to cable.
If damaged, remove from dust plug and nozzle. Install new cable and sleeves.
3. GROUND PLUG ASSEMBLY DAMAGED.
Step 1. Inspect ground plug for corrosion, cracks, or distortion.
If damaged, remove from cable. Install new ground plug.
Step 2. Inspect cable and cable eye for corrosion, cuts, fraying and crimp of sleeves to cable.
If damaged, remove from ground plug. Install new cable, cable eye, and sleeves.
4. GROUND CLIP ASSEMBLY DAMAGED.
Step 1. Inspect ground clip for corrosion, cracks, or distortion.
If damaged, remove from cable. Install new ground clip.
4-2
TM 5-4930-234-13&P
Table 4-1. Troubleshooting (cont)
MALFUNCTION
TEST OR INSPECTION
CORRECTIVE ACTION
Step 2. Inspect cable and cable eye for corrosion, cuts, fraying, and crimp of sleeves to cable.
If damaged, remove from ground clip and nozzle. Install new cable, cable eye and sleeves.
5. CAM-LOCK COUPLING ASSEMBLY LEAKING.
Remove nozzle from fuel hose. Remove coupling from nozzle. Inspect coupling to ensure o-ring is in place.
Inspect o-ring for cuts, tears, or distortion.
If o-ring is missing or damaged install new o-ring on coupling.
If coupling still leaks install a new coupling.
6. UNISEX DUST CAP DAMAGED.
Step 1. Inspect dust cap for corrosion, cracks, or distortion.
If damaged, remove from cable. Install new dust cap.
Step 2. Inspect cable for corrosion, cuts, fraying, and crimp of sleeves to cable.
If damaged, remove from dust cap and nozzle. Install new cable and sleeves.
7. UNISEX COUPLING ASSEMBLY LEAKING.
Remove nozzle from fuel hose. Inspect coupling to ensure seal is in place. Inspect seal for cuts, tears, or
distortion.
If seal is missing or damaged install new seal in coupling.
If coupling still leaks install a new coupling.
8. LEAKAGE AT OUTLET END.
Step 1. Inspect outlet end for dirt, foreign matter, or damage.
Remove dirt or foreign matter with a clean, lint free cloth. If there is any sign of damage send nozzle to Direct
Support for overhaul.
4-3
TM 5-4930-234-13&P
Section IV. MAINTENANCE PROCEDURES
4-5.
GENERAL. This section consists of inspection, service, or replacement of those items which would cause
malfunction or hazardous operation of the nozzle. Remove nozzle from fuel hose before doing any of these procedures.
Refer to paragraphs 3-4 or 3-5 for details.
4-6.
DUST CAP ASSEMBLY (See Figure 4-1).
a.
Removal.
1.
Hold nozzle (1) and pull back on pullback sleeve (2).
2.
Remove dust cap (4) from end of nozzle (1).
3.
Remove cable (6) from ring (3) on nozzle (1).
Figure 4-1. Dust Cap Assembly
4-4
TM 5-4930-234-13&P
b.
Disassembly. Cut cable (6) near sleeve (5) at dust cap (4) and remove.
NOTE
Clean parts with a clean cloth to remove dust, dirt, fuel or grease.
c.
1.
Inspect dust cap (4) for corrosion, cracks, or distortion.
2.
Inspect cable (6) for corrosion, cuts, or fraying.
d.
Replacement. Replace any damaged parts.
e.
Reassembly.
f.
4-7.
Inspection.
1.
Slide sleeve (5) down cable (6).
2.
Insert one end of cable (6) through hole in dust cap (4).
3.
Make a one inch loop with the cable (6) and slide sleeve (5) over end of cable (6).
4.
Crimp sleeve (5) in place on cable (6).
5.
Repeat steps 1 through 4 for other end of cable (6).
Installation.
1.
Install dust cap (4) on outlet end of nozzle (1).
2.
Install end of cable (6) on ring (3).
DUST PLUG ASSI4BLY (See Figure 4-2).
a.
b.
Removal.
1.
Hold nozzle (1) and pull cam arms (2) away from nozzle (1).
2.
Remove dust plug (4) from end of nozzle (1).
3.
Remove cable (6) from ring (3) on nozzle (1).
Disassembly. Cut cable (6) near sleeve (5) at dust plug (4) and remove.
NOTE
Clean parts with a clean cloth to remove dust, dirt, fuel or grease.
c.
Inspection.
1.
Inspect dust plug (4) for corrosion, cracks, or distortion.
4-5
TM 5-4930-234-13&P
2.
Inspect cable (6) for corrosion, cuts, or fraying.
d.
Replacement. Replace any damaged parts.
e.
Reassembly.
1.
Slide sleeve (5) down cable (6).
2.
Insert one end of cable (6) through hole in dust cap (4).
Figure 4-2. Dust Plug Assembly
4-6
TM 5-4930-234-13&P
f.
4-8.
3.
Make a one inch loop with the cable (6) and slide sleeve (5) over end of cable (6).
4.
Crimp sleeve (5) in place on cable (6).
5.
Repeat steps 1 through 4 for other end of cable (6).
Installation.
1.
Install dust plug (4) in inlet end of nozzle (1).
2.
Install end of cable (6) on ring (3).
GROUND PLUG ASSEMBLY (See Figure 4-3).
a.
Removal. Remove screw (2) from nozzle (1).
b.
Disassembly.
NOTE
If cable requires replacement, do not remove cable eye from cable.
1.
Cut cable eye (5) off end of cable (4)
2.
Loosen hex-head nut on ground plug (3).
3.
Remove cable (4) from ground plug (3).
c. Inspection.
1.
Inspect ground plug (3) for corrosion, cracks, or distortion.
2.
Inspect cable (4) for corrosion, cuts, or fraying.
3.
Inspect cable eye (5) for corrosion, or distortion.
d.
Replacement. Replace any damaged parts.
e.
Reassembly.
NOTE
Plastic coating must be stripped from end of cable to ensure metal to metal contact at both ends.
1.
Strip about 3/4 inch of plastic cover off each end of cable (4).
4-7
TM 5-4930-234-13&P
f.
2.
Insert one end of cable (4) in cable eye (5). Crimp end of cable eye (5) to cable (4).
3.
Insert other end of cable (4) in ground plug (3). Tighten hex-head nut on end of ground plug (3).
Installation. Insert screw (2) through hole in cable eye (5). Thread screw (2) into nozzle (1) and tighten.
Figure 4-3. Ground Plug Assembly
4-8
TM 5-4930-234-13&P
4-9.
GROUND CLIP ASSEMBLY (See Figure 4-4).
a.
Removal. Remove screw (2) from nozzle (1). Remove screw (2) from cable eye (5).
b.
Disassembly.
NOTE
If cable requires replacement do not remove cable eye from cable.
1.
Cut cable eye (5) off end of cable (4)
2.
Loosen two set-screws on ground clip (3).
Figure 4-4. Ground Clip Assembly
4-9
TM 5-4930-234-13&P
3.
c.
Remove cable (4) from ground clip (3).
Inspection.
1.
Inspect ground clip (3) for corrosion, cracks, distortion and spring tension.
2.
Inspect cable (4) for corrosion, cuts, or fraying.
3.
Inspect cable eye (5) for corrosion or distortion.
d.
Replacement. Replace any damaged parts.
e.
Reassembly.
NOTE
Plastic coating must be stripped from end of cable to ensure metal to metal contact at assembly.
f.
4-10.
1.
Strip about 3/4 inch of plastic cover off each end of cable (4).
2.
Insert one end of cable (4) in cable eye (5). Crimp end of cable eye (5) to cable (4).
3.
Insert other end of cable (4) in ground clip (3). Tighten two set-screws on ground clip (3).
Installation. Insert screw (2) through hole in cable eye (5). Thread screw (2) into nozzle (1) and tighten.
CAN-LOCK COUPLING ASSEMBLY (See Figure 4-5).
a.
Removal.
NOTE
Do not drop or lose gasket inside coupling.
b.
1.
Turn coupling (2) counterclockwise to remove from nozzle (1).
2.
Remove o-ring (3) from coupling (2). Replace o-ring (3) if cut or distorted.
Installation.
1.
Install o-ring (3) on threaded end of coupling (2).
2.
Install coupling (2) in nozzle (1) and turn clockwise until hand tight.
4-10
TM 5-4930-234-13&P
4-11.
UNISEX DUST CAP (See Figure 4-6).
a.
Removal.
1.
Hold nozzle (1) and turn dust cap (2) counterclockwise.
2.
Remove dust cap (2) from end of unisex coupling (5).
3.
Remove cable (3) from ring on nozzle (1).
Figure 4-5. Cam-Lock Coupling Assembly
4-11
TM 5-4930-234-13&P
b.
Disassembly. Cut cable (3) at dust cap (2) and remove.
NOTE
Clean parts with a clean cloth to remove dust, dirt, fuel or grease.
c.
Inspection.
1.
Inspect dust cap (2) for corrosion, cracks, or distortion.
Figure 4-6. Unisex Coupling Assembly
4-12
TM 5-4930-234-13&P
2.
d.
Replacement. Replace any damaged parts.
e.
Reassembly.
f.
4-12.
Inspect cable (3) for corrosion, cracks, or fraying.
1.
Slide sleeve (4) down cable (3).
2.
Insert one end of cable (3) through hole in dust cap (2).
3.
Make a one inch loop with the cable (3) and slide sleeve (4) over end of cable (3).
4.
Crimp sleeve (4) in place on cable (3).
5.
If required, repeat steps 1 through 4 for other end of cable (3).
Installation.
1.
Install dust cap (2) on end of unisex coupling (5) and turn clockwise.
2.
Install end of cable (3) on ring of nozzle (1).
UNISEX COUPLING ASSE4BLY (See Figure 4-6).
a.
b.
Removal.
1.
Turn coupling (5) counterclockwise to remove from nozzle (1).
2.
Remove o-ring (6) from coupling (5). Replace o-ring (6) if cut or distorted.
Installation.
1.
Install o-ring (6) on threaded end of coupling (5).
2.
Install coupling (5) in nozzle (1) and turn clockwise until hand-tight.
Section V. PREPARATION FOR STORAGE OR SHIPMENT
4-13.
ADMINISTRATIVE STORAGE
a. Placement of equipment in administrative storage should be for short periods of time when a shortage of
maintenance effort exists. Items should be in mission readiness within 24 hours or within the time factors as determined
by the directing authority. During the storage period appropriate maintenance records will be kept.
b. Before placing equipment in administrative storage, current maintenance services and equipment serviceable
criteria (ESC) evaluations should be completed, shortcomings and deficiencies should be corrected, and all modification
work orders (MWO’s) should be applied.
c. Storage site selection. Inside storage is preferred for items selected for administrative storage. If inside
storage is not available, trucks, vans, conex containers and other containers may be used.
Change 2 4-13
TM 5-4930-234-13&P
4-14.
PREPARATION.
1.
Remove nozzle from fuel hose. Refer to paragraphs 3-4 or 3-5 for details.
NOTE
Have a suitable container available to catch any fuel spillage. Drain fuel for shipment or storage.
4-15.
2.
Install dust cap and dust plug in nozzle.
3.
Coil ground clip and ground plug wires and secure with tape or string.
4.
Inspect nozzle for dirt or other foreign material. Clean nozzle with a clean, lint-free cloth.
5.
Inspect nozzle for physical damage or missing parts.
immediately.
Report any discrepancies to your supervisor
PACKAGING.
1.
Wrap nozzle in moisture barrier paper.
2.
Place nozzle in a sturdy cardboard or fiberboard container.
3.
Add moisture barrier paper to container so nozzle does not move.
4.
Seal container and mark the outside with the following information:
a.
Description
b.
Part Number
c.
National Stock Number (listed on data plate of nozzle).
d.
Date packaged
e.
Serial number
Change 2 4-14
TM 5-4930-234-13&P
CHAPTER 5
DIRECT SUPPORT MAINTENANCE INSTRUCTIONS
Section I. TROUBLESHOOTING PROCEDURES
5-1.
GENERAL.
a. This section contains troubleshooting information for locating and correcting most of the operating troubles
which may develop in the nozzle. Each malfunction for an individual component is followed by a list of tests or inspections
which will help to determine corrective actions to take. Perform the tests/inspections and corrective actions in the order
listed.
b. This manual cannot list all malfunctions that may occur, nor all tests or inspections and corrective actions. If
a malfunction is not listed or is not corrected by listed corrective actions, notify your supervisor.
5-2.
TROUBLESHOOTING. Table 5-1 lists the common malfunctions which may occur during operation or
maintenance of the nozzle. Perform test/inspections and corrective actions in the order listed.
For nozzle
disassembly/assembly procedures refer to paragraph 5-3.
Table 5-1. Troubleshooting
MALFUNCTION
TEST OR INSPECTION
CORRECTIVE ACTION
1. CAM-LOCK ARMS ARE LOOSE OR DO NOT LOCK IN PLACE.
Inspect cam arm and/or pin for cracks or looseness.
If damaged, replace cam arm and/or pin.
2. UNISEX COUPLING LEAKS BETWEEN BODY AND ADAPTER.
Step 1. Inspect body and adapter for cracks or damage.
If cracks or damage are found, disassemble and replace damaged parts.
Step 2. Disassemble and inspect internal o-ring for cuts or wear.
If damaged, replace internal o-ring and assemble.
5-1
TM 5-4930-234-13&P
Table 5-1. Troubleshooting (Cont)
MALFUNCTION
TEST OR INSPECTION
CORRECTIVE ACTION
3. INADEQUATE (SLUGGISH) FUEL FLOW.
Step 1. Remove coupling and strainer from nozzle. Check strainer for dirt or other foreign matter.
Clean strainer by removing all dirt and foreign matter.
Step 2. While strainer is removed, inspect for any damage.
Replace strainer if damaged. Install strainer in nozzle. Install coupling and hand-tighten.
4. FLOW HANDLE WILL NOT LOCK IN FLOW (ON) OR NO FLOW (OFF) POSITION.
Step 1. Inspect thumb latch and thumb latch spring.
Check thumb latch "ear" is not cracked, rounded or broken off. Check thumb latch spring is not broken or
missing. Replace either part if damaged.
Step 2. Inspect pinion teeth position on rack.
NOTE
This procedure can only be done during CCR Nozzle Sub-Assembly maintenance (See paragraph 5-6).
Remove snap ring, plug, washer, bushing and key from end cap. Check position of pinion teeth. As required,
move one tooth and assemble parts into end cap.
5. PRESSURE OR FLOW LEAKS INTO MATING HALF WHEN HANDLE IS IN NO FLOW (OFF) POSITION.
Inspect pinion teeth position on rack.
NOTE
This procedure can only be done during CCR Nozzle Sub-Assembly maintenance (See paragraph 5-6).
Remove snap ring, plug, washer, bushing and key from end cap. Check position of pinion teeth. As required, move one
tooth and assemble parts into end cap.
5-2
TM 5-4930-234-13&P
Table 5-1. Troubleshooting (Cont)
MALFUNCTION
TEST OR INSPECTION
CORRECTIVE ACTION
6. INDICATOR PIN DOES NOT OPERATE (DOES NOT EXTEND).
Inspect assembly of indicator pin and components for proper assembly and/or damaged parts.
NOTE
This procedure can only be done during CCR Nozzle Sub-Assembly maintenance (See paragraph 5-6).
Remove plunger and end cap. Check components for correct position. As required, assemble in the correct
position.
7. LEAKAGE FROM INDICATOR PIN HOLE.
Inspect seals and pressure regulator.
NOTE
This procedure can only be done during CCR Nozzle Sub-Assembly maintenance (See paragraph 5-6).
Disassemble nozzle and inspect seals for proper position, cuts or tears. Inspect pressure regulator for
scratches or nicks. Replace all damaged parts and assemble nozzle.
8. LEAKAGE BETWEEN ADAPTER AND BODY.
Inspect adapter and o-ring.
NOTE
This procedure can only be done during CCR Nozzle Sub-Assembly maintenance (See paragraph 5-6).
Disassemble nozzle and inspect adapter for wear, cracks or distortion. Inspect o-ring for cuts or tears. Replace
all damaged parts and assemble nozzle.
9. LEAKAGE FROM OUTLET END OF NOZZLE WHEN CONNECTED.
Remove nozzle from receptacle. Place handle in NO FLOW (off) position. Inspect seal.
Replace seal if cut or torn.
5-3
TM 5-4930-234-13&P
Table 5-1. Troubleshooting (Cont)
MALFUNCTION
TEST OR INSPECTION
CORRECTIVE ACTION
10. LEAKAGE FROM OUTLET END WHILE DISCONNECTED FROM RECEPTACLE.
Step 1. Look inside outlet end. See if leakage is coming from around outside of safety sleeve.
NOTE
This procedure can only be done during CCR Nozzle Sub-Assembly maintenance (See paragraph 5-6).
Remove plunger and safety sleeve. Inspect position of seal (facing the correct direction). If not, remove and
install seal in correct position. If seal is cut or torn, replace it. Install safety sleeve and plunger.
Step 2. Look inside outlet end. See if leakage is coming from around plunger.
NOTE
This procedure can only be done during CCR Nozzle Sub-Assembly maintenance (See paragraph 5-6).
Remove plunger and safety sleeve. Inspect parts for wear, cracks, or distortion. Replace any damaged parts.
Assemble nozzle.
11. NO ELECTRICAL CONTINUITY BETWEEN GROUND CLIP/GROUND PLUG AND NOZZLE.
Inspect ground cables, cap screw, and inlet coupling for dirt or corrosion.
Remove cap screw, ground cables, and inlet coupling. Remove any dirt or corrosion from ground cables,
screw, threads of inlet coupling, and body. Assemble parts and test for continuity. Replace any damaged
components.
12. PULLBACK SLEEVE DOES NOT ACTIVATE OR LOCK ON TO RECEPTACLE.
Disassemble nozzle and inspect parts.
NOTE
This procedure can only be done during CCR Nozzle Sub-Assembly maintenance (See paragraph 5-6).
Check for cracks, distortion, out of round condition, or improper assembly of parts. Replace all damaged
parts and assemble in the proper order.
5-4
TM 5-4930-234-13&P
Section II. MAINTENANCE PROCEDURES
WARNING
Aviation fuel is highly flammable. No smoking or open flames are permitted in maintenance area. Failure
to comply can result in injury or death to personnel.
Proper eye protection must be worn. Failure to comply can result in loss of eyesight.
5-3
GENERAL. This section consists of disassembly, inspection, replacement, cleaning, assembly, and testing of the
nozzle assembly and subassemblies.
5-4.
CAM-LOCK COUPLING ASSEMBLY.
a.
Removal (See Figure 5-1).
NOTE
Do not drop or lose gasket inside coupling, or strainer inside nozzle.
b.
c.
1.
Hold nozzle (1) and pull cam arms (2) away from nozzle (1).
2.
Remove dust plug (3) from coupling (4).
3.
Turn coupling (4) counterclockwise to remove from nozzle (1).
Disassembly (See Figure 5-2).
1.
Place cam-lock body (2) in a vise.
2.
Drive pin out of cam arm and cam-lock body using a punch and hammer.
3.
Repeat step 2 for other cam arm (1).
Inspection.
NOTE
Wipe parts with a clean, lint-free cloth before inspection.
d.
1.
Inspect cam arm and pin for wear, cracks, or distortion.
2.
Inspect cam-lock body (2) for wear in pin hole, cracks, or distortion.
Replacement. Replace any damaged parts.
5-5
TM 5-4930-234-13&P
e.
Reassembly (See Figure 5-3).
1.
Place cam-lock body on cam-lock stake plate, S1391-5, with pin hole sitting on dowel pin in cam-lock
2.
Insert cam arm between ears on cam-lock body.
3.
Insert pin through ear on cam-lock body and cam arm.
stake plate.
Figure 5-1. Cam-Lock Coupling Removal
5-6
TM 5-4930-234-13&P
NOTE
One side of pin has a recessed hole. Cam-lock stake tool goes in this hole.
4.
Stake pin in cam-lock body using cam-lock stake tool, S1391-3, and hammer.
5.
Remove cam-lock stake tool.
6.
Turn cam-lock body to position other side on dowel pin in cam-lock stake plate, S1391-5. Repeat steps
7.
Remove cam-lock body from cam-lock stake plate.
2 thru 5.
f.
Installation (See Figure 5-1).
1.
Install cam-lock coupling (4) in nozzle (1) and turn clockwise until hand-tight.
2.
Insert dust plug (3) in end of cam-lock coupling (4).
3.
Pull cam arms (2) toward nozzle (1) to lock in place.
Figure 5-2. Cam Arm Disassembly
Figure 5-3. Cam Arm Assembly
5-7
TM 5-4930-234-13&P
5-5.
UNISEX COUPLING ASSIEBLY.
a.
Removal (See Figure 5-4).
1.
Turn dust cap (2) counterclockwise and remove from unisex coupling (3).
2.
Turn unisex coupling (3) counterclockwise and remove from nozzle (1).
Figure 5-4. Unisex Coupling Removal
5-8
TM 5-4930-234-13&P
b.
c.
Disassembly (See Figure 5-5).
1.
Remove o-ring (1) and seal (2) from unisex coupling.
2.
Remove ring (3), pin (4), and spring (5) from adapter (9).
3.
Place unisex coupling in vise with wire hole facing up.
4.
Remove sealant from wire hole.
5.
Bend up end of wire (6). Pull wire (6) out of body (7).
6.
Remove unisex coupling from vise.
7.
Twist body (7) and adapter (9) in opposite directions, then pull apart.
8.
Remove o-ring (8) from groove in adapter (9).
Inspection.
NOTE
Wipe parts with a clean, lint-free cloth before inspection.
1.
Inspect body (7) for cracks, distortion, or corrosion. Inspect grooves for corrosion and cracks.
2.
Inspect adapter (9) for cracks, distortion, stripped threads, or corrosion.
12594A
Figure 5-5. Unisex Coupling Disassembly
5-9
TM 5-4930-234-13&P
3.
Inspect ring (3), pin (4), and spring (5) for cracks, wear, or distortion.
4.
Inspect o-ring (1) and seal (2) for tears, cuts, or distortion.
d. Replacement. Replace all cracked, distorted, or heavily corroded parts. Minor corrosion can be removed
with very fine emery cloth. Do not remove finish on metal.
e. Reassembly.
1. Lubricate o-ring (8) lightly with contents of grease pak supplied in repair kit. Install o-ring (8) in outer
groove of adapter (9).
2.
Install body (7) on adapter (9). Align wire hole in body (7) with groove in adapter (9).
3.
Place body (7) and adapter (9) in vise with wire hole facing up.
4. Insert tapered end of wire (6) through wire hole and into groove of adapter (9). Drive wire (6) into
adapter (9) until end drops into groove.
f.
5-6.
5.
Fill wire hole with sealant (Item 1, Appendix E). Allow to dry for one-half hour.
6.
Install spring (5) on end of pin (4).
7.
Insert pin (4) in adapter (9) until end extends through other side. Insert ring (3) through hole in pin (4).
8.
Install o-ring (1) in groove of body (7).
9.
Install seal (2) in groove of adapter (9).
Installation (See Figure 5-4).
1.
Install unisex coupling (3) in nozzle (1) and turn clockwise until hand-tight.
2.
Install dust cap (2) on unisex coupling (1) and turn clockwise until hand-tight.
CCR NOZZLE SUB-ASSEMBLY.
Before disassembly, wipe the exterior of the nozzle assembly with a clean, lint-free cloth to
remove dust, dirt, grease, or fuel residue. This will prevent contamination of internal parts.
a.
Disassembly (See Figure 5-6).
1.
Remove cap screw (1), ground clip (2), and ground plug (3) from nozzle (10).
5-10
TM 5-4930-234-13&P
Figure 5-6. CCR Nozzle Component Removal
5-11
TM 5-4930-234-13&P
2.
Remove dust plug (4) or dust cap (6) from nozzle (10). Remove cable from ring (11).
3.
Turn cam-lock coupling (5) or unisex coupling (7) counterclockwise and remove from nozzle (10).
4.
Remove strainer (8) from inside nozzle (10).
5.
Remove dust cap (9) from nozzle (10). Remove cable from ring (11). Remove ring (11) from nozzle
(10).
Do not over-tighten vise. Damage to body can result.
6.
Install nozzle (10) in vise with outlet end pointing up.
7. See Figure 5-7. Remove plunger (1), safety sleeve (2), and safety sleeve spring (3) from body (49)
using plunger torque tool, S1391-11, and ratchet wrench. See Figure 5-8.
8.
Turn body (49) in vise so handle (22) points up.
9.
Remove three cap screws (4 and 5) and end cap (6) from body (49).
10. Remove bonded guide (7) from back of end cap (6). Remove o-ring (8) and check valve (9) from
bonded guide (7).
11. Depress thumb latch (26) and push handle (22) toward piston (14). Pull rack (10) and piston (14) out of
end cap (6).
12. Remove piston return spring (11) from rack (10).
13. Remove o-ring (12) from piston (14).
14.
Do not remove spring pin from rack and piston unless inspection shows part replacement is
required. Damage to piston can result.
14. If required, remove spring pin (13) from rack (10) and piston (14). Pull rack (10) out of piston (14).
15. Clamp handle (22) in vise with thumb latch (26) pointing down.
NOTE
Flow control pin may drop out after parts are removed.
16. Remove retaining ring (15), plug (16), compression washer (17), bushings (18), pinion (19), and key (20)
from inside end cap (6).
17. Remove flow control pin (21) from bottom of handle (22).
5-12
TM 5-4930-234-13&P
Figure 5-7. CCR Nozzle Disassembly
Change 3 5-13
TM 5-4930-234-13&P
LEGEND FOR FIGURE 5-7. NOZZLE DISASSEMBLY
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
13.
14.
15.
16.
17.
PLUNGER
SAFETY SLEEVE
SAFETY SLEEVE SPRING
CAP SCREW
CAP SCREW
END CAP
BONDED GUIDE
O-RING
CHECK VALVE
RACK
PISTON RETURN SPRING
O-RING
SPRING PIN
PISTON
RETAINING RING
PLUG
COMPRESSION WASHER
18.
19.
20.
21.
22.
23.
24.
25.
26.
27.
28.
29.
30.
31.
32.
33.
34.
BUSHING
PINION
KEY
FLOW CONTROL PINSPRING
HANDLE
NON-METALLIC WASHER
WASHER
SPRING PIN
THUMB LATCH
LATCH SPRING
INDICATOR RETURN
SPRING
INDICATOR PIN
SAFETY SPRING
INDICATOR SHAFT
RETAINING RING
INDICATOR BUSHING
PULLBACK SLEEVE
Figure 5-8. Plunger Removal
Change 3 5-14
35. PRESSURE REGULATOR
SLEEVE
36. PRESSURE REGULATOR
37. PULLBACK SLEEVE SPRING
38. NOSE SLEEVE
39. LATCH
40. RELEASE PIN
41. BALL BEARING
42. RELEASE PIN SPRING
43. ADAPTER
44. ADAPTER SEAL
44A. SEAL VACUUM RELEASE
45. O-RING
46. PRESSURE REGULATOR
SEAL
47. PRESSURE REGULATOR
SEAL
48. I. D. LABEL
49. BODY
50. DECAL
TM 5-4930-234-13&P
18. Remove end cap (6) and washers (23 and 24) from handle (22). Remove handle (22) from vise.
CAUTION
Do not remove spring pin from handle and thumb latch unless inspection shows replacement is
required. Damage to handle can result.
19. If required, remove spring pin (25) from handle (22) and thumb latch (26).
20. Remove thumb latch (26) and latch spring (27) from handle (22).
21. Remove indicator return spring (28), indicator pin (29), safety spring (30), and indicator shaft (31) from
body (49).
NOTE
Do not remove parts from indicator shaft unless inspection shows replacement is required.
22. If required, remove retaining ring (32) and indicator bushing (33) from indicator shaft (31).
23. Turn body (49) and clamp in vise with outlet end pointing up.
24. Remove nose sleeve (38) from pullback sleeve (34) using torque spanner tool, S1391-12, and ratchet
wrench. See Figure 5-9.
NOTE
Latches will tend to drop out.
25. Remove six latches (39) from adapter (43).
26. Remove pullback sleeve (34) from body (49) by depressing release pins (40).
27. Remove two release pins (40), ball bearings (41), release pin springs (42) and pullback sleeve spring
(37) from end of adapter (43).
28. Remove adapter (43) from body (49) using adapter torque tool, S1391-7, and ratchet wrench. See
Figure 5-10.
29. Remove vacuum release seal (44A) and adapter seal (44) from inside adapter (43).
30. Remove pressure regulator sleeve (35), and pressure regulator spring (36) from body (49).
31. Remove o-ring (45) and pressure regulator seals (46 and 47) from inside body (49).
Change 3 5-15
TM 5-4930-234-13&P
Figure 5-9. Nose Sleeve Removal
Figure 5-10. Adapter Removal
NOTE
Do not remove label or decal unless replacement is required.
b.
Cleaning.
Do not use wire brushes or wire wheels to clean parts. Failure to comply earn result in damage to
metal finish of parts.
1.
Wipe metal parts with a clean, lint-free cloth to remove fuel, dust or other foreign material.
2. Remove heavy deposits of dirt or grease with a soft bristled brush dipped in cleaning solvent (Item 2,
Appendix E). Use low pressure, filtered air to dry parts.
3. As required, flush body (49) with cleaning solvent (Item 2, Appendix E) to remove fuel and foreign
material from internal passages. Use low pressure, filtered air to dry body (49).
5-16
TM 5-4930-234-13&P
c.
Inspection.
1.
Inspect piston (14), rack (10), and spring pin (13) as follows.
(a) Piston (14) must not have any nicks or scratches in o-ring groove or around outer edge. Metal
finish must not be damaged.
(b) Spring pin (13) must be below flush on both sides of piston (14), and not be loose in hole.
(c)
2.
Rack (10) teeth must not be chipped, cracked, or broken.
Inspect handle (22), thumb latch (26), and spring pin (25) as follows.
(a) Handle (22) must not have any cracks, or distortion in shape. Hole for plug (16) must be free of dirt
or corrosion.
(b) Spring pin (25) must be below flush on both sides of handle (22), and must not be loose in hole.
(c)
Thumb latch (26) must move freely when pressed. Ear at bottom must not be cracked or broken.
3. Inspect plunger (1) for straightness, nicks, burrs or distortion of slot in head. Metal finish of shaft must
not be worn through. Threads must not show any signs of stripping or cross-threading.
4. Inspect flow control pin (21) for straightness, cracks, and corrosion. Keyway and groove for retaining
ring (15) must have no nicks, burrs or distortion. Corners of head must not be broken off or rounded.
5. Inspect indicator pin (29) and indicator shaft (31) for straightness, corrosion, and wear of metal finish.
Groove for retaining ring (32) on indicator shaft (31) must not have any nicks or burrs.
6.
Inspect body (49) as follows.
(a) Check external surfaces for cracks, corrosion or wear of metal finish.
(b) Check internal surfaces for scoring, scratches, nicks or burrs in grooves for seals (46 and 47) or o-
ring (45).
(c)
Check internal passages for dirt or any residue of cleaning solvent.
(d) Check threaded holes for cross-threading, dirt, or corrosion.
7.
Inspect all springs for cracks, or distortion of shape. Check springs per Table 5-2.
5-17
TM 5-4930-234-13&P
Table 5-2. Spring Dimensions
DESCRIPTION
PART
NUMBER
LENGTH (INCHES)
FREE
COMPRESSED
DIAMETER
INSIDE
DIAMETER
(INCHES)
OUTSIDE
DIAMETER
Safety Sleeve Spring
AE10488-445
6.33
0.920
1.32
1.50
Piston Return Spring
AE10488-450
1.68
0.36
0.80
0.95
Pressure Regulator Spring
AE10488-447
4.69
0.83
1.24
Pullback Sleeve Spring
AE10488-446
5.16
0.60
2.45
2.65
Release Pin Spring
AE10488-451
0.49
0.20
0.14
0.18
Latch Spring
AE10488-453
1.70
0.60
0.19
0.25
Safety Spring
AE10488-448
0.50
0.210
0.30
0.37
Indicator Return Spring
AE10488-449
0.50
0.11
0.22
0.26
8.
1.43
Inspect all other metal parts as follows .
(a) Check for cracks, distortion, corrosion, or wear of finish.
(b) Check seal and o-ring grooves for nicks, scratches, or burrs that could damage seals and o-rings
during assembly.
(c)
d.
Check threads for stripping, nicks, cross-threading, or corrosion.
Replacement.
1.
Replace all cracked, distorted, or heavily corroded parts.
2.
Minor corrosion can be removed with very fine emery cloth. Do not remove finish on metal.
3.
Small nick’s or burrs can be removed with fine emery cloth. Do not change shape or size of grooves or
4.
Replace any decal or label that cannot be read.
threads.
5-18
TM 5-4930-234-13&P
e.
Reassembly (See Figure 5-7).
CAUTION
The nozzle must be assembled in the order shown using the special tools indicated. Failure to do
so can result in faulty operation of nozzle.
NOTE
A major overhaul kit is available for the nozzle. The kit contains all necessary seals, o-rings, small
metal parts, and a grease pak for lubricating seals and o-rings.
1.
Lightly lubricate adapter seal (44) and vacuum release seal (44A).
2. Install adapter seal and vacuum release seal in adapter, ensuring the ridges in the vacuum seal are
positioned to the open end of the nozzle and the web of the adapter seal faces the threaded end of the adapter.
NOTE
Be sure to seat both seals completely into the grooves without kinks or wrinkles.
3.
Insert release pin spring (42) in slot at back of release pin (40).
4. Insert release pin (40) in groove of adapter (43) with release pin spring (42) compressed against
shoulder of adapter (43). Install ball bearing (41) in hole of release pin (40).
5. Hold release pin (40), release pin spring (42), and ball bearing (41) against adapter (43). Turn adapter
(43) and install second set of parts in opposite groove of adapter (43).
6. Hold parts and slide adapter (43) into release pin mechanism tool, S1391-8. About 1/2 inch of adapter
(43) should extend beyond end of tool. See Figure 5-11.
Figure 5-11. Adapter Assembly
Change 3 5-19
TM 5-4930-234-13&P
7. Slide adapter (43) and release pin mechanism tool, S1391-8, inside pullback sleeve (34).
adapter (43) should extend beyond end of pullback sleeve (34).
End of
8.
Hold end of adapter (43) and pull release pin mechanism tool, S1391-8, out of pullback sleeve (34). See
9.
Insert six latches (39) in slots of adapter (43). Thread nose sleeve (38) onto pullback sleeve (34) until
Figure 5-12.
handtight.
10. Lightly lubricate pressure regulator seals (46 and 47), and o-ring (45).
11. Install small pressure regulator seal (47) in groove at back of body (49). Webbed side must face toward
handle end.
12. Install large pressure regulator seal (46) in second groove from outlet end of body (49). Webbed side
must face outlet end.
13. Install o-ring (45) in outlet end of body (49).
14. Install body (49) in vise jaws, S1391-15, and clamp in vise. See Figure 5-13.
15. Insert pressure regulator spring (36) in pressure regulator sleeve (35). Install both parts inside body
(49).
16. Install regulating positioning tool, S1391-9, in body (49) as follows. See Figure 5-14.
Figure 5-12. Removal of Release Pin Mechanism Tool
Change 3 5-20
TM 5-4930-234-13&P
(a) Remove large locating nut from end of threaded rod.
(b) Push down on pressure regulator sleeve (35) until it passes pressure regulator seals (46 and 47).
(c) Slide threaded rod through pressure regulator sleeve (35) until end extends out the bottom of body
(49).
(d) Thread locating nut on end of threaded rod and hand-tighten until pressure regulator (35) has 1/4
inch of travel. See Figure 5-14.
16. Install pullback sleeve spring (37) in pullback sleeve (34).
17. Install pullback sleeve (34) and adapter (43) on body (49). Push down on pullback sleeve (34).
18. Thread adapter (43) into body (49) using adapter torque tool, S1391-7, and a torque wrench. Tighten to
a torque of 40-50 ft-lbs. See Figure 5-15. Remove adapter torque tool.
19. Remove large locating nut from end of threaded rod. Remove regulating positioning tool, S1391-9, from
body (49).
Figure 5-13. Body Installation.
Figure 5-14. Tool Installation
5-21
TM 5-4930-234-13&P
20. Tighten nose sleeve (38) to a torque of 20-30 ft-lbs using torque spanner tool, S1391-12, and a torque
wrench. See Figure 5-16.
21. Remove body (49), from vise. Remove vise jaws, S1391-15, from body (49). Install body (49) in vise
with nose sleeve (38) pointing down.
22. If required, assemble piston (14) to rack (10) as follows. See Figure 5-17.
(a) Slide rack (10) into piston (14) and align pin hole.
(b) Place rack (10) and piston (14) in pin stake plate, S1391-6.
(c) Insert spring pin (13) in hole of piston (14). Drive spring pin (13) into position using pin stake tool,
S1391-4, and hammer.
(d) Remove pin stake tool. Remove rack (10) and piston (14) from pin stake plate.
Figure 5-15. Adapter Installation
Figure 5-16. Torqueing Nose Sleeve
5-22
TM 5-4930-234-13&P
(e)
Check spring pin (13). It must be flush on both sides of piston (14).
23. If required, assemble thumb latch (26) to handle (22) as follows. See Figure 5-18.
(a) Place handle (22) on a flat surface.
(b) Insert thumb latch (26) in side of handle (22) and align holes.
(c) Insert spring pin (25) in handle (22). Drive spring pin (25) through handle (22) and thumb latch (26)
using pin stake tool, S1391-4, and hammer.
(d) Remove pin stake tool. Check spring pin (25). It must be flush with surface of handle (22).
(e) Pivot thumb latch (26) away from handle (22). Install latch spring (27’ in thumb latch (26) and hole in
handle (22).
Figure 5-17. Piston and Rack Assembly
Figure 5-18. Handle and Thumb Latch Assembly
5-23
TM 5-4930-234-13&P
24.
Lightly lubricate o-ring (12). Install in groove of piston (14).
25.
Lightly lubricate o-ring (8). Install in groove of bonded guide (7).
26.
Lightly lubricate check valve (9). Insert pointed end through hole in bonded guide (7). Use a pair of needle nose
pliers inside bonded guide to pull on pointed end of check valve (9) until it snaps in place.
27.
Install piston (14) in bonded guide (7). Push on rack (10) until piston (14) stops in bonded guide (7).
28.
Install bonded guide (7) in body (49) with rack (10) pointing up. Three holes in bonded guide (7) must be aligned
with three holes in body (49).
29.
Remove body (49) from vise. Insert a metal rod through hole in rack (10) and clamp metal rod in vise. See Figure
5-19. Nose sleeve (38) on body (49) should point up.
30.
Install safety sleeve spring (3) in safety sleeve (2). Insert plunger (1) through safety sleeve (2). Install parts in
body (49).
Figure 5-19. Plunger Assembly
5-24
TM 5-4930-234-13&P
31. Press down to compress safety sleeve spring (3) and hand-thread plunger (1) into bonded guide (7). Tighten
plunger (1) to a torque of 5-7 ft-lbs. using plunger torque tool, S1391-11, and torque wrench. See Figure 5-19.
32. Remove body (49) from vise and metal rod from rack (10). Place body (49) in vise with nose sleeve (38)
pointing down.
33. Turn rack (10) clockwise until teeth point away from three holes in bonded guide (7) and toward inlet end of
body (49). Insert piston return spring (11) over rack (10) and into bonded guide (7).
34. If removed, assemble indicator bushing (33) and retaining ring (32) on end of indicator shaft (31). Install
indicator shaft (31) in body (49).
35. Install safety spring (30) on top on indicator shaft (31).
36. Install indicator return spring (28) on shaft of indicator pin (29).
Insert both parts in body (49) on top of safety spring (30).
37. Install end cap (6) on body (49) and align screw holes.
38. Install three cap screws (4 and 5) through end cap (6) and into body (49). Tighten in a criss-cross pattern to
a torque of 15-17 ft-lbs. Remove body (49) from vise.
39. Install handle (22), non-metallic washer (23), and washer (24), on end cap (6). Handle (22) must be in FLOW
(on) position.
40. Insert flow control pin (21) through handle (22) and into end cap (6).
Keyway must face thumb latch (26).
41. Install rack positioning tool, S1391-10, in outlet end of body (49). See Figure 5-20.
42. Install pin positioning block, S1391-13, on top of flow control pin (21).
See Figure 5-21.
43. Hold pin positioning block, S1391-13, against flow control pin (21) and turn body (49) over.
44. Lay body (49) on workbench with flow control pin (21) and pin positioning block facing down.
45. Install one bushing (18) and pinion (19) in handle (22). Keyway in pinion (19) must line up with keyway in flow
control pin (21). The tooth above pinion keyway must mesh with second full valley on rack (10). See Figure 5-22.
46. Install key (20) in keyways of rack (10) and pinion (19). Install other bushing (18), compression washer (17),
and plug (16) on top of pinion (19).
47. Install retaining ring (15) using expansion tool, S1391-14, as follows. See Figure 5-23.
(a) Install cone in handle (22).
5-25
TM 5-4930-234-13&P
Figure 5-21. Pin Positioning Tool
Figure 5-20. Rack Positioning Tool
Figure 5-23. Ring Assembly
Figure 5-22. Pinion Assembly
.
5-26
TM 5-4930-234-13&P
(b) Install retaining ring (15) on end of cone.
(c) Install pusher over end of cone. Push down until retaining ring (15) snaps into groove of flow control pin
(21).
(d) Remove pusher and cone from handle (22).
48. Remove pin positioning block, S1391-13, from body (49).
49. Remove rack positioning tool, S1391-10, from outlet end of body (49).
50. If removed, install new I.D. label (48) on side of body (49) using adhesive (Item 3, Appendix E).
NOTE
For nozzle assembly, model AE83206R, use label 23052-3. For nozzle assembly,
model AE83501R, use label 23052-4.
51. If removed, install new decal (50) on pullback sleeve (34).
52. Check handle operation as follows.
(a) Press thumb latch (26).
(b) Move handle (22) from FLOW (on) to NO FLOW (off) position.
(c) Release thumb latch (26).
NOTE
With thumb latch released handle must lock in flow or no flow positions.
(d) Handle (22) must move without sticking or binding. If it does not, disassemble handle components and
check for proper assembly. Repeat disassembly step 16 and assembly steps 41 through 49 above.
(e) Thumb latch (26) must engage in notches of end cap (6) and must lock handle (22) in position. If it does
not, check locking ear on thumb latch (26). If it is broken, replace thumb latch (26).
53. Check operation of pullback sleeve (34) and latches (39) as follows.
(a) Depress release pins (40). Pull pullback sleeve (34) towards handle (22). It must move freely without
binding. If it does not, disassemble nozzle and check parts for correct order of assembly.
( b) With pullback sleeve (34) pulled toward handle (22), all six latches (39) must pivot without binding. If
they do not, check latches (39) and adapter (43) for damage.
5-27
TM 5-4930-234-13&P
54. Install strainer (8) in nozzle (10). See Figure 5-6.
55. Install cam-lock coupling (5) or unisex coupling (7) on nozzle (10). Hand- tighten only.
Failure of any test is cause for rejection of nozzle assembly until fault is corrected.
f.
Testing. After repair and prior to release for aircraft refueling, test nozzle in an operating, pressurized
refueling system to ensure no leakage occurs.
All data on pages 5-29 and 5-30, including Figure 5-24, have been deleted.
Change 4 5-28
TM 5-4930-234-13&P
APPENDIX A
REFERENCES
A-1.
SCOPE. This appendix lists all forms, field manuals, technical publications and miscellaneous publications
referenced in this manual.
A-2.
FORMS.
Equipment Daily or Monthly Log....................................................................................................................DA Form 2408-1
Equipment Inspection and Maintenance Work Sheet ...................................................................................... DA Form 2404
Maintenance Request .................................................................................................................................... DA Form 2407
Quality Deficiency Report............................................................................................................................................. SF 368
Recommended Changes to DA Publications and Blank Forms ....................................................................DA Form 2028-2
Uncorrected Fault Record ...........................................................................................................................DA Form 2408-14
Component Removal and Repair/Overhaul Record......................................................................................... DA Form 2410
Aircraft Component Historical Record .........................................................................................................DA Form 2408-16
A-3.
TECHNICAL MANUALS.
Procedures For Destruction of Army Equipment to Prevent Enemy Use ........................................................ TM 750-244-3
A-4.
MISCELLANEOUS PUBLICATIONS.
The Army Maintenance Management System (TAMMS).............................................................................DA PAM 738-750
Expendable/Durable Items ................................................................................................................................... CTA 50-970
Classification, Reclassification, Maintenance, Issuance
and Reporting of Maintenance Training Aircraft..................................................................................................... AR 700-42
A-1/(A-2 Blank)
TM 5-4930-234-13&P
APPENDIX B
MAINTENANCE ALLOCATION CHART
Section I. INTRODUCTION
B-1.
GENERAL.
a. This section provides a general explanation of all maintenance and repair functions authorized at various
maintenance categories.
b. The Maintenance Allocation Chart (MAC) in section II designates overall authority and responsibility for the
performance of maintenance functions on the identified end item or component. The application of the maintenance
functions to the end item or component will be consistent with the capacities and capabilities of the designated
maintenance categories.
c. Section III lists the tools and test equipment (both special tools and common tool sets) required for each
maintenance function as referenced from section II.
d.
B-2.
Section IV contains supplemental instructions and explanatory notes for a particular maintenance function.
MAINTENANCE FUNCTIONS. Maintenance functions will be limited to and defined as follows:
a. Inspect. To determine the serviceability of an item by comparing its physical, mechanical, and/or electrical
characteristics with established standards through examination (e.g. by sight, sound, or feel).
b. Test. To verify serviceability by measuring the mechanical, pneumatic, hydraulic, or electrical characteristics
of an item and comparing those characteristics with prescribed standards.
c. Service. Operations required periodically to keep an item in proper operating condition, i.e., to clean
(includes decontaminate, when required), to preserve, to drain, to paint, or to replenish fuel, lubricants, chemical fluids, or
gases.
d. Adjust. To maintain or regulate, within prescribed limits, by bringing into proper or exact position, or by
setting the operating characteristics to specified parameters.
e.
Aline. To adjust specified variable elements of an item to bring about optimum or desired performance.
f.
Calibrate. To determine and cause corrections to be made or to be adjusted on instruments or test,
measuring, and diagnostic equipments used in precision measurement. Consists of comparisons of two instruments, one
of which is a certified standard of known accuracy, to detect and adjust any discrepency in the accuracy of the instrument
being compared.
B-1
TM 5-4930-234-13&P
g. Remove/Install. To remove and install the same item when required to perform service or other
maintenance functions. Install may be the act of emplacing, seating, or fixing into position a spare, repair part, or module
(component or assembly) in a manner to allow the proper functioning of an equipment or system.
h. Replace. To remove an unserviceable item and install a serviceable counterpart in its place. "Replace" is
authorized by the MAC and is shown as the 3rd position code of the SMR code.
i.
Repair.
The application of maintenance services, including fault location/troubleshooting,
removal/installation, and disassembly/assembly procedures, and maintenance actions to identify troubles and restore
serviceability to an item by correcting specific damage, fault, malfunction, or failure in a part, subassembly, module
(component or assembly), end item, or system.
j.
Overhaul. That maintenance effort (service/action) prescribed to restore an item to a completely
serviceable/operational condition as required by maintenance standards in appropriate technical publications (i.e.
DMWR). Overhaul is normally the highest degree of maintenance performed by the Army. Overhaul does not normally
return an item to like new condition.
k. Rebuild. Consists of those services/actions necessary for the restoration of unserviceable equipment to a
like new condition in accordance with original manufacturing standards. Rebuild is the highest degree of materiel
maintenance applied to Army equipment. The rebuild operation includes the act of returning to zero those age
measurements (hours/miles, etc.) considered in classifying Army equipment/components.
B-3.
EXPLANATION OF COLUMNS IN THE MAC, SECTION II.
a. Column (1) - Group Number. Column 1 lists functional group code numbers, the purpose of which is to
identify maintenance significant components, assemblies, subassemblies, and modules with the next higher assembly.
End item group number shall be "01".
b. Column (2) - Component/Assembly. Column 2 contains the names of components, assemblies,
subassemblies, and modules for which maintenance is authorized.
Column (3) - Maintenance Function. Column 3 lists the functions to be performed on the item listed in Column
2. (For detailed explanation of these functions, see paragraph B-2.)
d. Column (4) - Maintenance Category. Column 4 specifies, by the listing of a work time figure in the
appropriate subcolumn(s), the category of maintenance authorized to perform the function listed in Column 3. This figure
represents the active time required to perform the maintenance function at the indicated category of maintenance. If the
number or complexity of the tasks within the listed maintenance function vary at different maintenance catagories,
appropriate work time figures will be shown for each category. The work time figure represents the average time required
to restore an item (assembly, subassembly, component, module, end item, or system) to a serviceable condition under
typical
B-2
TM 5-4930-234-13&P
field operating conditions. This time includes preparation time (including any necessary disassembly/assembly time),
troubleshooting/fault isolation time, and quality assurance/ quality control time in addition to the time required to perform
the specific tasks identified for the maintenance functions authorized in the maintenance allocation chart. The symbol
designations for the various maintenance categories are as follows:
C......................................................................................
Operator or Crew
0 ......................................................................................
Organizational Maintenance
F ......................................................................................
Direct Support Maintenance
H......................................................................................
General Support Maintenance
L ......................................................................................
Specialized Repair Activity (SRA)
D......................................................................................
Depot Maintenance
e. Column (5) Tools and Equipment. Column 5 specifies, by code, those common tool sets (not individual
tools), and special tools, TMDE, and support equipment required to perform the designated function.
f.
Column (6) Remarks. This column shall, when applicable, contain a letter code, in alphabetic order, which
shall be keyed to the remarks contained in Section IV.
B-4.
EXPLANATION OF COLUMNS IN TOOL AND TEST EQUIPMENT REQUIREMENTS, SECTION III.
a. Column (1) Reference Code. The tool and test equipment reference code correlates with a code used in
the MAC, Section II, Column 5.
b. Column (2) Maintenance Catagory. The lowest category of maintenance authorized to use the tool or test
equipment.
B-5.
c.
Column (3) Nomenclature. Name or identification of the tool or test equipment.
d.
Column (4) National Stock Number. The National stock number of the tool or test equipment.
e.
Column (5) - Tool Number. The manufacturer’s part number.
EXPLANATION OF COLUMNS IN RMARKS, SECTION IV.
a.
Column (1) - Reference Code. The code recorded in column 6, Section II.
b. Column (2) Remarks. This column lists information pertinent to the maintenance function being performed
as indicated in the MAC, Section II.
B-3
TM 5-4930-234-13&P
Section II. MAINTENANCE ALLOCATION CHART FOR CCR NOZZLE ASSEMBLY
(1)
GROUP
NUMBER
01
(2)
COMPONENT ASSEMBLY
Nozzle Assembly
0101
Cap Assembly
0102
Ground Clip
Assembly
0103
0104
0105
0106
Coupling or
Adapter Assembly
Plug or Cap
Assembly
Ground Plug
Assembly
Nozzle SubAssembly
(3)
MAINTENANCE
FUNCTION
Inspect
Repair
Replace
Overhaul
Inspect
Replace
Inspect
Test
Repair
Inspect
Repair
Replace
Inspect
Repair
Replace
Inspect
Test
Repair
Replace
Inspect
Test
Repair
Replace
Overhaul
B-4
(4)
MAINTENANCE LEVEL
C
O
F
H
(5)
D
(6)
TOOLS AND
EQUIPMENT REMARKS
0.1
1.0
1.0
2.0
1 thru 17A
1 thru 17
A,B,C
0.1
0.1
A
0.1
0.1
A,C
A,C
0.1
0.1
0.2
9,10
A
0.1
0.1
0.2
A
A
0.1
0.1
0.1
A,C
A,C
A
0.2
0.1
0.1
1.0
1.0
1.0
2.0
A,C
1 thru 8,
11 thru 17
A,C
1 thru 8,
11 thru 17
A,B,C
TM 5-4930-234-13&P
Section III. TOOL AND TEST EQUIPMENT REQUIREMENTS FOR CCR NOZZLE ASSEMBLY
(1)
REFERENCE
CODE
(2)
MAINTENANCE
CATEGORY
1
2
3
4
F
F
5
F
6
7
8
9
10
11
12
13
14
15
16
17
F
F
F
F
F
F
F
F
F
F
F
F
(3 )
NOMENCLATURE
Deleted
Deleted
Jaw, Vise
Tool, Mechanical, Pin,
Release
Tool, Positioning, S 1391-9
Regulator
Tool, Expansion
Tool, Stake, Pin
Plate, Stake, Pin
Tool, Stake, Camlock
Plate, Stake, Camlock
Block, Positioning, Pin
Tool, Torque, Spanner
Tool, Torque, Plunger
Tool, Torque, Adapter
Pkg, Preformed, 0-ring
Tool, Positioning, Rack
Cam-lock Assembly
Section IV. REMARKS
A - Requires common tools from automotive shop set.
B - Requires major repair kit, p/n AE20074-053
C - Multimeter required
Change 4 B-5/(B-6 Blank)
(4)
NATIONAL
STOCK NUMBER
(5)
TOOL
NUMBER
S1391-15
S1391-8
S1391-14
S1391-4
S1391-6
S391-3
S1391-5
S1391-13
S1391-12
S1391-11
S1391-7
MS29513-134
S1391-10
AE83932R
TM 5-4930-234-13&P
APPENDIX C
COMPONENTS OF END ITEM/BASIC ISSUE ITEMS
Section I. INTRODUCTION
C-1.
SCOPE. This appendix lists components of end item and basic issue items for the CCR Nozzle Assembly to help
you inventory items required for safe and efficient operation.
C-2.
GENERAL. The Components of End Item/Basic Issue Items List is divided into the following sections:
a. Section II. Components of End Item. This listing is for informational purposes only, and is not authority to
requisition replacements. These items are part of the end item, but are removed and separately packaged for
transportation or shipment. As part of the end item, these items must be with the end item whenever it is issued or
transferred between property accounts. Illustrations are furnished to assist you in identifying the items.
b. Section III. Basic Issue Items. These are the minimum essential items required to place the CCR Nozzle
Assembly in operation, to operate it, and to perform emergency repairs. Although shipped separately packaged, BII must
be with the CCR Nozzle Assembly during operation and whenever it is transferred between property accounts. The
illustrations will assist you with hard-to-identify items. This manual is your authority to request/requisition replacement BII,
based on TOE/MTOE authorization of the end item.
C-3.
EXPLANATION OF COLUMNS. The following provides an explanation of columns found in the tabular listings:
a. Column (1) - Illustration Number (Illus Number). This column indicates the number of the illustration in
which the item is shown.
b. Column (2) - National Stock Number. Indicates the National Stock Number assigned to the item and will be
used for requisitioning purposes.
c. Column (3) - Description. Indicates the Federal item name and, if required, a minimum description to
identify and locate the item. The last line for each item indicates the FSCM (in parentheses) followed by the part number.
d. Column (4) - Unit of Measure (U/M).
Indicates the measure used in performing the actual
operational/maintenance function. This measure is expressed by a two-character alphabetical abbreviation (e.g. ea, in,
pr).
e. Column (5) - Quantity required (Qty rqr). Indicates the quantity of the item authorized to be used with/on
the equipment.
C-1
TM 5-4930-234-13&P
Section II. COMPONENTS OF END ITEN
(1)
ILLUS
NUMBER
(2)
NATIONAL
STOCK NUMBER
(3)
DESCRIPTION,
(FSCM) AND PART NUMBER
(4)
USABLE
ON CODE
U/M
(5)
QTY
RQD
There are no Components of End Item for the CCR Nozzle.
Section III. BASIC ISSUE ITEMS
(1)
ILLUS
NUMBER
1
(2)
NATIONAL
STOCK NUMBER
N/A
(3)
DESCRIPTION,
(FSCM) AND PART NUMBER
Technical Manual
TM 5-4930-234-13&P
C-2
(4)
USABLE
ON CODE
EAL,
EBV
U/M
(5)
QTY
RQD
EA
1
TM 5-4930-234-13&P
APPENDIX D
ADDITIONAL AUTHORIZATION LIST
Section I. INTRODUCTION
D-1.
SCOPE. This appendix lists additional items you are authorized for the support of the CCR Nozzle Assembly.
D-2.
GENERAL. This list identifies items that do not have to accompany the CCR Nozzle Assembly and that do not
have to be turned in with it. These items are all authorized to you by CTA, MTOE, TDA, or JTA.
D-3.
EXPLANATION OF LISTING.
a. National stock numbers, descriptions, and quantities are provided to help you identify and request the
additional items you require to support this equipment. The items are listed in alphabetical sequence by item name under
the type document (i.e., CTA, MTOE, TDA, or JTA) which authorizes the item to you.
b. If the item you require differs between serial numbers of the same model, effective serial numbers are shown
in the last line of the description. If item required differs for different models of this equipment, the model is shown under
the "Useable on code" heading in the description column.
Section II. ADDITIONAL AUTHORIZATION LIST
(1)
NATIONAL STOCK
NUMBER
(2)
DESCRIPTION
FSCM AND PART NUMBER
USABLE ON
CODE
There are no additional authorized items for use with the CCR Nozzle Assembly.
D-1/(D-2 Blank)
(3)
U/M
Auth
(4)
QTY
TM 5-4930-234-13&P
APPENDIX E
EXPENDABLE/DURABLE SUPPIES AND MATERIALS LIST
Section 1. INTRODUCTION
E-1.
SCOPE. This appendix lists expendable/durable supplies and materials needed to operate and maintain the CCR
Nozzle Assembly. These items are authorized by CTA 50-970, Expendable Items (Except Medical, Class V, Repair Parts
and Heraldic Items).
E-2.
EXPLANATION OF COLUMNS.
a.
Column (1) - Item number. This number is assigned to the entry in the listing and is referenced in the
narrative instructions to identify the material (e.g., "Use cleaning compound, Item 5, Appendix C").
b.
Column (2) - Level. This column identifies the lowest level of maintenance that requires the listed item.
These are as follows:
C - Operator/Crew
0 - Organizational Maintenance
F - Direct Support Maintenance
H - General Support Maintenance
D - Depot Maintenance
c. Column (3) - National Stock Number. This is the National stock number assigned
to the item; use it to request or requisition the item.
d. Column (4) - Description. Indicates the Federal item name and, if required, a description to identify the
item. The last line for each item indicates the Federal Supply Code for Manufacturer (FSCM) in parentheses followed by
the part number.
e. Column (5) - Unit of Measure (U/HM). Indicates the measure used in performing the actual maintenance
function. This measure is expressed by a two-character alphabetical abbreviation (e.g., ea, in, pr). If the unit of measure
differs from the unit of issue, requisition the lowest unit of issue that will satisfy the requirements.
E-1
TM 5-4930-234-13&P
(1)
ITEM
NUMBER
(2)
LEVEL
(3)
NATIONAL
STOCK
NUMBER
(4)
(5)
DESCRIPTION
U/M
1.
F
8040-00-701-9616
Sealant, RTV
1 PT
2.
F
6850-00-274-5421
Solvent, Cleaning PD-680 Type II
5 GL
3.
F
8040-01-033-7507Adhesive (Sico-met) 7000
Change 4 E-2
1 TU
TM 5-4930-234-13&P
OPERATOR, ORGANIZATIONAL AND DIRECT SUPPORT,
MAINTENANCE REPAIR PARTS AND SPECIAL TOOLS LIST
SECTION I. INTRODUCTION
1.
SCOPE. This RPSTL lists and authorizes spares and repair parts; special tools; special test,
measurement, and diagnostic equipment (TMDE); and other special support equipment required for
performance of operator, organizational and direct support of the CCR Nozzle Assembly. It
authorizes the requisitioning, issue, and disposition of spares, repair parts and special tools as
indicated by the source, maintenance and recoverability (SMR) codes.
2.
GENERAL. In addition to this section, Introduction, this Repair Parts and Special Tools List is
divided into the following sections:
a. Section II. Repair Parts List. A list of spares and repair parts authorized by this RPSTL
for use in the performance of maintenance. The list also includes parts which must be removed for
replacement of the authorized parts. Parts lists are composed of functional groups in ascending
alphanumeric sequence, with the parts in each group listed in ascending figure and item number
sequence. Bulk materials are listed in item name sequence. Repair parts kits are listed separately in
their own functional group within Section II. Repair parts for repairable special tools are also listed in
this section. Items listed are shown on the associated illustration(s)/figure(s).
b. Section III. Special Tools List. A list of special tools, special TMDE, and other special
support equipment authorized by this RPSTL (as indicated by Basis of Issue (BOI) information in
DESCRIPTION AND USABLE ON CODE column) for the performance of maintenance.
c. Section IV. Cross-references Indexes. A list, in National Item Identification Number
(NIIN) sequence, of all National stock numbered items appearing in the listing, followed by a list in
alphanumeric sequence of all part numbers appearing in the listings. National stock numbers and
part numbers are cross-referenced to each illustration figure and item number appearance. The
figure and item number index lists figure and item number in alphanumeric sequence and crossreferences NSN, FSCM and part number.
3.
EXPLANATION OF COLUMNS (SECTIONS II AND III).
a. ITEM NO. (Column (1)). Indicates the number used to identify items called out in the
illustration.
F-1
TM 5-4930-234-13&P
b. SMR Code (Column (2)). The Source, Maintenance, and Recoverability (SMR) code is a
5-position code containing supply/requisitioning information, maintenance category authorization
criteria, and disposition instruction, as shown in the following breakout:
*Complete Repair: Maintenance capacity, capability, and authority to perform all corrective
maintenance tasks of the "Repair" function in a use/user environment in order to restore serviceability
to a failed item.
(1) Source Code. The source code tells you how to get an item needed for maintenance,
repair, or overhaul of an end item/equipment. Explanations of source codes follows:
Code
Explanation
**
Stocked items; use the applicable NSN to request/requisition items
with these source codes. They are authorized to the category
indicated by the code entered in the 3d position of the SMR code.
**NOTE: Items coded PC are subject to deterioration.
Items with these codes are not to be requested/requisitioned
individually. They are part of a kit which is authorized to the
maintenance category indicated in the
3d position of the SMR code.
The complete kit must be
requisitioned and applied.
Explanation
Items with these codes are not to be requested/requisitioned
individually. They must be made from bulk material which is
identified by the part number in the DESCRIPTION and USABLE
ON CODE (UOC) column and listed in the Bulk Material group of
F-2
TM 5-4930-234-13&P
Explanation
Items with these codes are not to be requested/requisitioned
individually. The parts that make up the assembled item must be
requisitioned or fabricated and assembled at the level of
maintenance indicated by the source code. If the 3d position code
of the SMR code authorizes you to replace the item, but the source
code indicates the items are assembled at a higher level, order the
item from the higher level of maintenance.
Explanation
XA--Do not requisition an "XA"-coded item. Order its next higher assembly. (Also, refer to the NOTE
below.)
XB--If an "XB" item is not available from salvage, order it using the FSCM and part number given.
XC--Installation drawing, diagram, instruction sheet, field service drawing, that is identified by
manufacturer’s part number.
XD--Item is not stocked. Order an "XD"-coded item through normal supply channels using the FSCM
and part number given, if no NSN is available.
NOTE
Cannibalization or controlled exchange, when
authorized, may be used as a source of supply
for items with the above source codes, except
for those source coded "XA" or those aircraft
support items restricted by requirements of AR
750-1.
(2) Maintenance Code. Maintenance codes tells you the level(s) of maintenance
authorized to USE and REPAIR support items. The maintenance codes are entered
in the third and fourth positions of the SMR code as follows:
(a) The maintenance code entered in the third position tells you the lowest
maintenance level authorized to remove, replace, and use an item. The
maintenance code entered in the third position will indicate authorization to one of
the following levels of maintenance.
Code
Application/Explanation
C --Crew or operator maintenance done within organizational or aviation unit
maintenance.
0
--Organizational or aviation unit category can remove, replace, and use the
F
--Direct support or aviation intermediate level can remove, replace, and use
item.
the item.
F-3
TM 5-4930-234-13&P
H
--General support level can remove, replace, and use the item.
L
--Specialized repair activity can remove, replace, and use the item.
D
--Depot level can remove, replace, and use the item.
(b) The maintenance code entered in the fourth position tells whether or not the item
is to be repaired and identifies the lowest maintenance level with the capability to
do complete repair (i.e., perform all authorized repair functions.) NOTE: Some
limited repair may be done on the item at a lower level of maintenance, if
authorized by the Maintenance Allocation Chart (MAC) and SMR codes. This
position will contain one of the following maintenance codes.
Code
Application/Explanation
0
--Organizational or (aviation unit) is the lowest level that can do complete
F
--Direct support or aviation intermediate is the lowest level that can do
complete repair of the item.
H
--General Support is the lowest level that can do complete repair of the item.
L
--Specialized repair activity is the lowest level that can do complete repair of
D
--Depot is the lowest level that can do complete repair of the item.
Z
--Nonreparable. No repair is authorized.
B
--No repair is authorized. (No parts or special tools are authorized for the
maintenance of a "B" coded item). However, the item may be reconditioned
by adjusting, lubricating, etc., at the user level.
repair of the item.
the item.
(3) Recoverability Code. Recoverability codes are assigned to items to indicate the
disposition action on unserviceable items. The recoverability code is entered in the
fifth position of the SMR Code as follows:
Recoverability
Codes
Z
Application/Explanation
--Nonreparable item. When unserviceable, condemn and dispose of the item
at the level of maintenance shown in 3d position of SMR Code.
F-4
TM 5-4930-234-13&P
Recoverability
Codes
Application/Explanation
O
--Reparable item.
When uneconomically reparable,
dispose of the item at organizational or aviation unit level.
condemn
and
F
--Reparable item. When uneconomically reparable, condemn and dispose of
the item at the direct support or aviation intermediate level.
H
--Reparable item. When uneconomically reparable, condemn and dispose of
the item at the general support level.
D
--Reparable item. When beyond lower level repair capability, return to depot.
Condemnation and disposal of item not authorized below depot level.
L
--Reparable item.
Condemnation and disposal not authorized below
specialized repair activity (SRA).
A
--Item requires special handling or condemnation procedures because of
specific reasons (e.g., precious metal content, high dollar value, critical
material, or hazardous material). Refer to appropriate manuals/directives
for specific instructions.
c. FSCM (Column (3)). The Federal Supply Code for Manufacturer (FSCM) is a 5-digit
numeric code which is used to identify the manufacturer, distributor, or Government agency, etc., that
supplies the item.
d. PART NUMBER (Column (4)). Indicates the primary number used by the manufacturer,
(individual, company, firm, corporation, or Government activity), which controls the design and
characteristics of the item by means of its engineering drawings, specifications standards, and
inspection requirements to identify an item or range of items.
NOTE
When you use an NSN to requisition an item,
the item you receive may have a different part
number from the part ordered.
e. DESCRIPTION AND USABLE ON CODE (UOC) (Column (5)). This column includes the
following information:
(1) The Federal item name and, when required, a minimum description to identify the
item.
(2) The physical security classification of the item is indicated by the parenthetical entry,
e.g., Phy Sec C1 - Confidential, Phy Sec C1 (S) - Secret, Phy Sec C1 (T)- Top Secret.
F-5
TM 5-4930-234-13&P
(3) Items that are included in kits and sets are listed below the name of the kit or set.
(4) Spare/repair parts that make up an assembled item are listed immediately following
the assembled item line entry.
(5) Part numbers for bulk materials are referenced in this column in the line item entry for
the item to be manufactured/fabricated.
(6) When the item is not used with all serial numbers of the same model, the effective
serial numbers are shown on the last line(s) of the description (before UOC).
(7) The usable on code, when applicable (see paragraph 5, Special Information).
(8) In the Special Tools List section, the basis of issue (BOI) appears as the last line(s) in
the entry for each special tool, special TMDE, and other special support equipment.
When density of equipments supported exceeds density spread indicated in the basis
of issue, the total authorization is increased proportionately.
(9) The statement "END OF FIGURE" appears just below the last item description in
Column 5 for a given figure in both Section II and Section III.
(10)The indenture, shown as dots appearing before the repair part, indicates that the item
is a repair part of the next higher assembly.
f. QTY (Column (6)). The QTY (quantity per figure column) indicates the quantity of the item
used in the breakout shown on the illustration figure, which is prepared for a functional group,
subfunctional group, or an assembly. A "V" appearing in this column in lieu of a quantity indicates
that the quantity is variable and may vary from application to application.
4.
EXPLANATION OF COLUMNS (SECTION IV).
a. NATIONAL STOCK NUMBER (NSN) INDEX.
(1) STOCK NUMBER column. This column lists the NSN by National item identification
number
(NIIN) sequence. The NIIN consists of the last nine digits of the
NSN
NSN, i.e. (5305-01-574-1467).
NIIN
When using this column to locate an item, ignore the first 4 digits of the NSN.
However, the complete NSN should be used when ordering items by stock number.
(2) FIG. column. This column lists the number of the figure where the item is
identified/located. The figures are in numerical order in Section II and Section III.
F-6
TM 5-4930-234-13&P
(3) ITEM column. The item number identifies the item associated with the figure listed in
the adjacent FIG. column. This item is also identified by the NSN listed on the same
line.
b. PART NUMBER INDEX. Part numbers in this index are listed by part number in ascending
alphanumeric sequence (i.e., vertical arrangement of letter and number combination which
places the first letter or digit of each group in order A through Z, followed by the numbers 0
through 9 and each following letter or digit in like order).
(1) FSCM column. The Federal Supply Code for Manufacturer (FSCM) is a 5-digit
numeric code used to identify the manufacturer, distributor, or Government agency,
etc., that supplies the item.
(2) PART NUMBER column. Indicates the primary number used by the manufacturer
(individual, firm, corporation, or Government activity), which controls the design and
characteristics of the item by means of its engineering drawings, specifications
standards, and inspection requirements to identify an item or range of items.
(3) STOCK NUMBER column. This column lists the NSN for the associated part number
and manufacturer identified in the PART NUMBER and FSCM columns to the left.
(4) FIG. column. This column lists the number of the figure where the item is
identified/located in Sections II and III.
(5) ITEM column. The item number is that number assigned to the item as it appears in
the figure referenced in adjacent figure number column.
c. FIGURE AND ITEM NUMBER INDEX.
(1) FIG. column. This column lists the number of the figure where the item is
identified/located in Section II and III.
(2) ITEM column. The item number is that number assigned to the item as it appears in
the figure referenced in the adjacent figure number column.
(3) STOCK NUMBER column. This column lists the NSN for the item.
(4) FSCM column. The Federal Supply Code for Manufacturer (FSCM) is a 5-digit
numeric code used to identify the manufacturer, distributor, or Government agency,
etc., that supplies the item.
(5) PART NUMBER column. Indicates the primary number used by the manufacturer
(individual, firm, corporation, or Government activity), which controls the design and
characteristics of the item by means of its engineering drawings, specifications
standards, and inspection requirements to identify an item or range of items.
F-7
TM 5-4930-234-13&P
5.
SPECIAL INFORMATION.
a. USABLE ON CODE. The usable on code appears in the lower left corner of the
Description column heading. Usable on codes are shown as "UOC:
" in the Description
Column (justified left) on the last line applicable item description/ nomenclature. Uncoded items are
applicable to all models. Identification of the usable on codes used in the RPSTL are:
Code
Used On
EAL
EBV
AE83206R
AE83501R
b. ASSOCIATED PUBLICATIONS. Not Applicable
6.
HOW TO LOCATE REPAIR PARTS.
a. When National Stock Number or Part Number is NOT Known.
(1) First. Using the table of contents, determine the assembly group for subassembly
group to which the item belongs. This is necessary since figures are prepared for
assembly groups and subassembly groups, and listings are divided into the same
groups.
(2) Second. Find the figure covering the assembly group or subassembly group to which
the item belongs.
(3) Third. Identify the item on the figure and note the item number.
(4) Fourth. Refer to the Repair Parts List for the figure to find the part number for the
item number noted on the figure.
(5) Fifth. Refer to the Part Number Index to find the NSN, if assigned.
b. When National Stock Number or Part Number is Known:
(1) First. Using the Index of National
Stock Numbers and Part Numbers, find the
pertinent National Stock Number or Part Number. The NSN index is in National
Item Identification Number (NIIN) sequence (see 4a(1)). The part numbers in the Part
Number
index are listed in ascending alphanumeric sequence (see paragraph
4b).Both indexes cross-reference you to the illustration figure and item number of
the item you are looking for.
(2) Second. After finding the figure and item number, verify that the item is the one you
are looking for, then locate
the item number in the repair parts list for the figure.
7.
ABBREVIATIONS. Abbreviations used in this manual are listed in MIL-STD-12.
F-8
TM 5-4930-234-13&P
Figure 1. CCR Nozzle Assembly (Sheet 1 of 2)
F-9
TM 5-4930-234-13&P
1178C
Figure 1. CCR Nozzle Assembly (Sheet 2 of 2)
Change 3 F-10
SECTION II
(1)
(2)
(3)
ITEM SMR
NO CODE CAGEC
TM 5-4930-234-13&P C06
(6)
(4)
(5)
PART
NUMBER DESCRIPTION AND USABLE ON CODES (UOC)
QTY
GROUP 01.NOZZLE ASSEMBLY
FIGURE 1. CCR NOZZLE ASSEMBLY
1
2
3
4
PAOZZ
AOOZZ
PAOZZ
MOOZZ
96906
00624
81349
19099
MS16995-35
AE24791-009
M83413/7-1
677P18
5
6
7
8
XDOZZ
AOOFF
PAOZZ
MOOZZ
96906
00624
81349
19099
MS35340-57
AE24791-006
M83413/4-1
677P19
9
10
XDOZZ 96906
AOOFF 00624
MS35340-19
AE83931R
11
MOOZZ 19099
677P20
12
PAOZZ 76691
168-3-VC
13
PAOZZ 96906
MS27029-11
14
XDOFF 00624
AE83932R
15
PAOZZ 96906
MS27030-6
16
XDFZZ 81718
H-1833
17
XDFZZ 00624
AE83574R
18
AOOFF 00624
AE83936R
19
MOOZZ 19099
677P21
19
PAOZZ 81349
M83420/3-001
20
PAOZZ 76691
168-3-VC
21
AOOFF 00624
AE82155R
22
XDOZZ 00624
AE85183R
23
PAOZZ 00624
AE18900-076
SCREW, CAP, SOCKET HE........................................
GROUND CLIP ASSY..................................................
.CLIP, ELECTRICAL ....................................................
.CABLE MAKE FROM BULK MATERIAL P/N .............
AE24789-001, (FSCM 00624), 87.00
IN.REQUIRED..............................................................
.WASHER, LOCK.........................................................
GROUND PLUG ASSY ................................................
.PLUG, TIP ...................................................................
.CABLE HAKE FORM BULK MAT, P/N
AE24789-001 (FSCM 00624), 44.00
IN.REQUIRED..............................................................
.EYE CABLE ................................................................
PLUG ASSEMBLY .......................................................
UOC:EAL
.ROPE, WIRE MAKE FORM BULK MATERIAL ..........
P/N MIL-W-83420 (FSCM 81349), 16.00
IN.REQUIRED..............................................................
UOC:EAL
.SWAGING SLEEVE, WIRE ........................................
UOC:EAL
.PLUG, QUICK DISCONNE .........................................
UOC:EAL
CAM LOCK ASSEMBLY ..............................................
UOC:EAL
.GASKET PART OF KIT P/N AE20074-053 ................
PART OF KIT P/N AE20074-052 .................................
UOC:EAL
.CAM ARM & PIN ASSY ..............................................
UOC:EAL
.BODY, CAM LOCK .....................................................
UOC: EAL
CAP ASSEMBLY..........................................................
UOC:EBV
.ROPE, WIRE MAKE FROM BULK MATERIAL, .........
P/N MIL-W-83420 (FSCM 81349), 12.00
IN.REQUIRED..............................................................
UOC:EBV
.ROPE, WIRE...............................................................
UOC:EBV
.SWAGING SLEEVE, WIRE ........................................
UOC:EBV
.DUST CAP ASSEMBLY..............................................
UOC:EBV
..DUST CAP SUBASSY ...............................................
UOC:EBV
..SEAL ..........................................................................
UOC:EBV
F-11
1
1
1
1
1
1
1
1
1
1
2
1
1
1
2
1
1
1
1
2
1
1
1
SECTION II
(1)
(2)
(3)
ITEM SMR
NO CODE CAGEC
TM 5-4930-234-13&P C06
(6)
(4)
(5)
PART
NUMBER DESCRIPTION AND USABLE ON CODES (UOC)
24
PAFFF 00624
AE70725R
25
PAOZZ 00624
AE18900-076
26
PAOZZ 00624
AE83144Z
27
XDFZZ 00624
AE83630Z
28
XDFZZ 00624
AE10488-457
29
XDFZZ 00624
900803-4-28C
30
XDFZZ 00624
AE83933R
31
PAFZZ 00624
22504-230
32
XDFZZ 00624
AE84592R
33
PAOZZ 96906
MS29513-134
34
35
36
37
38
PAOZZ 00624
AOOOO 00624
XDOZZ 00624
PAFZZ 76691
PAFZZ 18876
AE83576R
AE83570R
AE83930R
168-3-VC
9083097
39
40
PAOZZ 84256
XDFZZ 00624
19-4CD
23052-3
41
XDFZZ 00624
23052-4
42
43
44
PBFFF 00624
XDFZZ 00624
XDFZZ 00624
AE85107R
AE84745R
AE83545R
45
46
47
48
49
XDFZZ
PAFZZ
PAFZZ
XDFZZ
XDFZZ
00624
96906
96906
00624
00624
AE10488-445
MS16995-79
MS16995-77
AE83550R
AE83549R
50
PAFZZ 96906
MS29513-129
51
XDFZZ 00624
AE84014H
52
53
54
XDFZZ 00624
XDFZZ 00624
PAFZZ 96906
AE83541Z
AE10488-450
MS29513-214
ADAPTER, PRESSURE FU.........................................
UOC:EBV
.SEAL ...........................................................................
UOC:EBV
.RING ...........................................................................
UOC:EBV
.PIN ..............................................................................
UOC:EBV
.SPRING.......................................................................
UOC:EBV
.WIRE ...........................................................................
UOC:EBV
.ADAPTER ...................................................................
UOC:EBV
.PACKING, PERFORMED ...........................................
UOC:EBV
.ADAPTER SUB ASSY ................................................
UOC:EBV
PACKING, PREFORMED PART OF KIT P/N..............
AE20074-053 ...............................................................
STRAINER PART OF KIT P/N AE20074-053..............
CAP ASSEMBLY..........................................................
.CAP .............................................................................
.SWAGING SLEEVE, WIRE ........................................
.ROPE,WIRE MAKE FROM BULK MATERIAL, ..........
P/N MIL-W-83420 (FSCM 81349), 16.00
IN.REQUIRED..............................................................
RING ............................................................................
LABEL, I.D....................................................................
UOC:EAL
LABEL, I.D....................................................................
UOC:EBV
NOZZLE SUBASSY FUEL ...........................................
.PLUNGER ...................................................................
..SLEEVE, SAFETY PART OF KIT P/N .......................
AE20074-053 ...............................................................
.SPRING, SAFETY SLV...............................................
.SCREW, CAP, SOCKET HE.......................................
.SCREW, CAP, SOCKET HE.......................................
.CAP, END ...................................................................
.GUIDE, BONDED PART OF KIT P/N .........................
AE20074-053 ...............................................................
.PACKING, PREFORMED PART OF KIT P/N.............
AE20074-053 PART OF KIT P/N AE20074052 ...............................................................................
.VALVE, CHECK PART OF KIT P/N AE20074 ............
-053 PART OF KIT P/N AE20074-052.........................
.RACK ..........................................................................
.SPRING,PSTN RETURN ............................................
.PACKING, PREFORMED PART OF KIT P/N.............
AE20074-053 PART OF KIT P/N AE20074052 ...............................................................................
F-12
QTY
1
1
1
1
1
1
1
1
1
1
1
1
1
2
1
1
1
1
1
1
1
1
2
1
1
1
1
1
1
1
1
SECTION II
(1)
(2)
(3)
ITEM SMR
NO CODE FSCM
TM 5-4930-234-13&P C03
(6)
(4)
(5)
PART
NUMBERDESCRIPTION AND USABLE ON CODES (UOC)
55 XDFZZ 96906
56 XDFZZ 00624
57 XDFZZ 80756
MS171530
AE83551R
RSN50S
58
59
60
61
62
AE83543Z
SSR-0087-S17
AE18033-025
AE83572R
AE26329-001
XDFZZ
XDFZZ
XDFZZ
XDFZZ
PBFZZ
00624
51814
00624
00624
00624
63 XDFZZ 00624
64 XDFZZ 00624
65 XDFZZ 00624
AE15881-078
AE83553R
AE93643E
66
67
68
69
70
71
72
73
74
75
76
77
78
XDFZZ
PAFZZ
XDFZZ
XDFZZ
XDFZZ
XDFZZ
XDFZZ
XDFZZ
PBFZZ
XDFZZ
XDFZZ
XDFZZ
XDFZZ
00624
96906
00624
00624
00624
00624
00624
00624
96906
00624
00624
00624
00624
AE18067-036
MS16562-225
AE84340R
AE10488-453
AE10488-449
AE15881-076
AE10488-448
AE18034-006
MS16634-4015
AE18033-023
AE83573R
AE83569R
AE10488-447
79
80
81
82
83
84
85
86
XDFZZ
XDFZZ
XDFZZ
XDFZZ
PAFZZ
XDFZZ
XDFZZ
XDFZZ
00624
00624
00624
00624
96906
00624
00624
00624
AE10488-446
AE83571R
AE84494R
AE15881-079
MS19060-4812
AE10488-451
AE83577R
AE18900-088
87 PAFZZ 00624
AE18900-148
88 XDFZZ 96906
MS29513-228
89 XDFZZ 00624
AE18900-089
90 XDFZZ 00624
AE18900-087
91 XDFZZ 00624
92 XDFZZ 00624
AE83554R23052-5
.PIN, SPRING ...........................................................................
.PISTON....................................................................................
.RING, RETAINING PART OF KIT P/N ....................................
AE20074-053 ............................................................................
.PLUG ......................................................................................
.WASHER, COMPRESSION ....................................................
.BUSHING.................................................................................
.PINION.....................................................................................
.KEY, MACHINE PART OF KIT P/N AE20074 .........................
-053...........................................................................................
.PIN, FLOW CONTROL ............................................................
.HANDLE ..................................................................................
.WASHER, NON-METALIC PART OF KIT P/N ........................
AE20074-053 ............................................................................
.WASHER PART OF KIT P/N AE20074-053 ............................
.PIN, SPRING ...........................................................................
.LATCH, THUMB ......................................................................
.SPRING, LATCH .....................................................................
.SPRING, IND RETURN ...........................................................
.PIN, INDICATOR .....................................................................
.SPRING, SAFETY ...................................................................
.SHAFT, INDICATOR ...............................................................
.RING, RETAINING ..................................................................
.BUSHING, INDICATOR...........................................................
.SLEEVE, PULLBACK ..............................................................
.SLEEVE, PRESS RGLTR........................................................
.SPRING, PRESS RGLTR PART OF KIT P/N .........................
AE20074-053 ............................................................................
.SPRING, PULLBACK SLV.......................................................
.SLEEVE, NOSE.......................................................................
.LATCH .....................................................................................
.PIN, RELEASE.........................................................................
.BALL, BEARING ......................................................................
.SPRING, RELEASE PIN..........................................................
.ADAPTER ................................................................................
.SEAL, ADAPTER PART OF KIT P/N.......................................
AE20074-053 PART OF KIT P/N AE20074052 ............................................................................................
.SEAL, VACUUM RELEASE PART OF KIT P/N ......................
AE20074-053 PART OF KIT P/N AE20074
-052...........................................................................................
.PACKING, PREFORMED PART OF KIT P/N .........................
AE20074-053 PART OF KIT P/N AE20074052 ............................................................................................
.SEAL, PRESS RGLTR PART OF KIT P/N ..............................
AE20074-053 PART OF KIT P/N AE20074052 ............................................................................................
.SEAL, PRESS RGLTR PART OF KIT P/N ..............................
AE20074-053 PART OF KIT P/N AE20074052 ............................................................................................
.BODY.......................................................................................
.LABEL, ID LABEL IDENTIFIES NOZZLE ...............................
F-13
QTY
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
6
2
2
2
1
1
1
1
1
1
1
1
SECTION II
(1)
(2)
(3)
ITEM SMR
NO CODE FSCM
TM 5-4930-234-13&P C03
(6)
(4)
(5)
PART
NUMBERDESCRIPTION AND USABLE ON CODES (UOC)
93 XDFZZ 00624
XDFZZ 00624
AE13186-009
AE11695-003
XDFZZ 00624
AE13186-012
PAFZZ 00624
AE20074-053
PAFZZ 00624
AE20074-052
SUBASSEMBLY, PN AE85107R, ONLY ..................................
.DECAL .....................................................................................
.PAK, GREASE PART OF KIT P/N AE20074-..........................
053 PART OF KIT P/N AE20074-052.......................................
.LABEL, REWORK PART OF KIT P/N .....................................
AE20074-053 PART OF KIT P/N AE20074052 ............................................................................................
REPAIR KIT, NOZZLE A ..........................................................
GASKET
( 1)
1-15
GASKET
( 1)
1-15
GUIDE, BONDED
( 1)
1-49
KEY, MACHINE
( 1)
1-62
LABEL, REWORK
( 2)
1PACKING, PREFORMED
( 1)
1-33
PACKING, PREFORMED
( 1)
1-50
PACKING, PREFORMED
( 1)
1-54
PACKING, PREFORMED
( 1)
1-88
PAK, GREASE
( 1)
1RING, RETAINING
( 1)
1-57
SEAL, ADAPTER
( 1)
1-86
SEAL, PRESS RGLTR
( 1)
1-89
SEAL, PRESS RGLTR
( 1)
1-90
SEAL, VACUUM RELEASE
( 1)
1-87
SLEEVE, SAFETY
( 1)
1-44
SPRING, PRESS RGLTR
( 1)
1-78
STRAINER
( 1)
1-34
VALVE, CHECK
( 1)
1-51
WASHER
( 1)
1-66
WASHER, NON-METALIC
( 1)
1-65
REPAIR KIT, NOZZLE A ..........................................................
GASKET
( 1)
1-15
GASKET
( 1)
1-15
LABEL, REWORK
( 2)
1PACKING, PREFORMED
( 1)
1-50
PACKING, PREFORMED
( 1)
1-54
PACKING, PREFORMED
( 1)
1-88
PAK, GREASE
( 1)
1SEAL, ADAPTER
( 1)
1-86
SEAL, PRESS RGLTR
( 1)
1-89
SEAL, PRESS RGLTR
( 1)
1-90
SEAL, VACUUM RELEASE
( 1)
1-87
VALVE, CHECK
( 1)
1-51
END OF FIGURE
F-14
QTY
1
1
2
1
1
SECTION II
(1)
(2)
(3)
ITEM SMR
NO CODE FSCM
TM 5-4930-234-13&P C03
(6)
(4)
(5)
PART
NUMBERDESCRIPTION AND USABLE ON CODES (UOC)
QTY
GROUP 02.BULK ITEMS LIST
FIGURE BULK
1 PAOZZ 00624
2 PAOZZ 81349
AE24789-001
MILW83420
.CABLE 100 FT PER ROLL .....................................................
.ROPE, WIRE ...........................................................................
UOC:EAL
END OF FIGURE
F-15/(F-16 Blank)
1
1
TM 5-4930-234-13&P
11876A
Figure 2. Special Tools (Sheet 1 of 2)
Change 3 F-17
TM 5-4930-234-13&P
11877A
Figure 2. special Tools (Sheet 2 of 2)
Change 3 F-18
SECTION II
(1)
(2)
(3)
ITEM SMR
NO CODE FSCM
TM 5-4930-234-13&P C03
(6)
(4)
(5)
PART
NUMBERDESCRIPTION AND USABLE ON CODES (UOC)
GROUP 03.SPECIAL TOOLS LIST
FIGURE 2.SPECIAL TOOLS
1 PEFFF 00624
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFFF
XBFZZ
XBFZZ
XBFFF
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFFF
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFZZ
XBFFF
XBFZZ
XBFZZ
XBFZZ
XBOFF
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
96906
00624
00624
00624
00624
00624
00624
00624
00624
96906
99862
00624
00624
00624
00624
00624
00624
00624
00624
S1391K
S1391-1
S1391-2
S1391-3
S1391-4
S1391-5
SC4568
SC4574
S1391-6
SC4569
SC4576
S1391-7
SC4566
SC4567
MS9390-220
S1391-8
S1391-9
SC4561
SC4562
SC4563
SC4564
S1391-10
SC4565
MS35650-3392
CL-35-SSC-N
S1391-11
S1391-12
S1391-13
S1391-14
SC4570
SC4571
S1391-15
AE83932R
KIT, ASSEMBLY TOOL CONTAINS ITEMS .........................1
THROUGH 32...........................................................................
.ADAPTER, TEST, PROOF ......................................................
.ADAPTER, TEST, PROOF ......................................................
.TOOL, STAKE, CAMLOCK......................................................
.TOOL, STAKE, PIN .................................................................
.PLATE, STAKE, CAMLOCK ....................................................
..PLATE, STAKE.......................................................................
..PIN, DOWEL...........................................................................
.PLATE, STAKE, PIN................................................................
..WELDMENT, PL, STAKE .......................................................
..PIN, DOWEL...........................................................................
.TOOL, TORQUE, ADAPTER...................................................
..PLATE, TORQUE ...................................................................
..TOOL, DRIVE, ADAPTER ......................................................
..PIN, STRAIGHT, HDLS ..........................................................
.TOOL, MECH, PIN, RLSE .......................................................
.TOOL, POSN, RGLTR.............................................................
..NUT.........................................................................................
..NUT, LOCATING ....................................................................
..NUT, LOCATING ....................................................................
..ROD, THREADED ..................................................................
.TOOL, POSN, RACK ...............................................................
..ADAPTER, THREADED .........................................................
..NUT, PLAIN, HEXAGON ........................................................
..SCREW, SWIVEL ...................................................................
.TOOL, TORQUE, PLUNGER ..................................................
.TOOL, TORQUE, SPANNER ..................................................
.BLOCK, POSN, PIN.................................................................
.TOOL, EXPANSION ................................................................
..PUSHER .................................................................................
..CONE......................................................................................
.JAW, VISE ...............................................................................
.CAM LOCK ASSEMBLY..........................................................
UOC:EBV
END OF FIGURE
F-19/(F-20 Blank)
QTY
SECTION IV
STOCK NUMBER
5305-00-051-8605
5999-00-134-5844
4010-00-222-4482
5330-00-250-0232
5330-00-265-1097
5935-00-572-5174
5330-00-612-2414
5330-00-641-0119
3110-00-838-5033
5315-00-841-4443
4730-00-915-5127
5305-00-981-3512
5305-00-988-7607
5365-00-989-0083
4010-01-005-4775
4030-01-088-6263
1
1
5330-01-237-3655
1
4930-01-237-3656
4730-01-237-3662
5315-01-237-3696
5330-01-237-3700
4930-01-238-3800
5180-01-241-3333
4930-01-266-8795
1
5330-01-275-7908
4930-01-278-6939
4930-01-278-6940
4930-01-350-1721
TM 5-4930-234-13&P C06
CROSS- REFERENCE-INDEXES
NATIONAL STOCK NUMBER INDEX
FIG.
ITEM
STOCK NUMBER
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
BULK
1
1
BULK
1
1
1
1
2
1
1
1
1
1
47
3
38
54
50
7
15
33
83
67
13
46
1
74
19
2
12
20
37
23
25
1
34
62
31
42
1
26
39
87
24
F-21
FIG.
ITEM
SECTION IV
TM 5-4930-234-13&P C06
NATIONAL STOCK NUMBER AND PART NUMBER INDEX
PART NUMBER INDEX
CAGEC
PART NUMBER
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
AE10488-445
AE10488-446
AE10488-447
AE10488-448
AE10488-449
AE10488-450
AE10488-451
AE10488-453
AE10488-457
AE11695-003
AE13186-009
AE13186-012
AE15881-076
AE15881-078
AE15881-079
AE18033-023
AE18033-025
AE18034-006
AE18067-036
AE18900-076
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
1100624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
AE18900-087
AE18900-088
AE18900-089
AE18900-148
AE20074-052
AE20074-053
AE24789-001
AE24791-006
AE24791-009
AE26329-001
AE70725R
AE82155R
AE83144Z
AE83541Z
AE83543Z
AE83545R
AES3549R
AE83550R
AE83551R
AE83553R
AE83554R
AE83569R
AE83570R
AE83571R
AE83572R
AE83573R
AE83574R
AE83576R
AE83577R
AE83630Z
STOCK NUMBER
5330-01-237-3655
5330-01-275-7908
4930-01-278-6940
4930-01-278-6939
4930-01-237-3656
5315-01-237-3696
4930-01-350-1721
4930-01-266-8795
4730-01-237-3662
F-22
FIG.
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
BULK
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
ITEM
45
79
78
72
70
53
84
69
28
93
71
63
82
75
60
73
66
23
25
90
86
89
87
1
6
2
62
24
21
26
52
58
44
49
48
56
64
91
77
35
80
61
76
17
34
85
27
SECTION IV
TM 5-4930-234-13&P C06
NATIONAL STOCK NUMBER AND PART NUMBER INDEX
PART NUMBER INDEX
CAGEC
PART NUMBER
00624
00624
00624
AE83930R
AE83931R
AE83932R
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
99862
81718
96906
96906
96906
96906
96906
96906
96906
96906
96906
96906
96906
96906
96906
96906
96906
96906
96906
81349
81349
81349
AE83933R
AE83936R
AE84014H
AE84340R
AE84494R
AE84592R
AE84745R
AE85107R
AE85183R
AE93643E
CL-35-SSC-N
H-1833
MS16562-225
MS16634-4015
MS16995-35
MS16995-77
MS16995-79
MS171530
MS19060-4812
MS27029-11
MS27030-6
MS29513-129
MS29513-134
MS29513-214
MS29513-228
MS35340-19
MS35340-57
MS35650-3392
MS9390-220
M83413/4-1
M83413/7-1
M83420/3-001
80756
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
RSN50S
SC4561
SC4562
SC4563
SC4564
SC4565
SC4566
SC4567
SC4568
SC4569
SC4570
SC4571
SC4574
SC4576
STOCK NUMBER
4930-01-238-3800
5315-00-841-4443
5365-00-989-0083
5305-00-988-7607
5305-00-051-8605
5305-00-981-3512
3110-00-838-5033
4730-00-915-5127
5330-00-612-2414
5330-00-265-1097
5330-00-641-0119
5330-00-250-0232
5935-00-572-5174
5999-00-134-5844
4010-01-005-4775
F-23
FIG.
1
1
1
2
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
2
2
1
1
1
BULK
1
2
2
2
2
2
2
2
2
2
2
2
2
2
ITEM
36
10
14
33
30
8
51
68
81
32
43
42
22
65
25
16
67
74
1
7
46
55
83
13
15
50
33
54
88
9
5
24
15
7
3
19
2
57
18
19
20
21
23
13
14
7
10
30
31
8
11
SECTION IV
TM 5-4930-234-13&P
NATIONAL STOCK NUMBER AND PART NUMBER INDEX
PART NUMBER INDEX
FSCM
PART NUMBER
51814
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
76691
SSR-0087-S17
S1391-1
S1391-10
S1391-11
S1391-12
S1391-13
51391-14
S1391-15
S1391-2
S1391-3
S1391-4
S1391-5
51391-6
S1391-7
S1391-8
S1391-9
S1391K
168-3-VC
84256
00624
00624
00624
00624
19099
19099
19099
19099
19099
00624
19-4CD
22504-230
23052-3
23052-4
23052-5
677P18
677P19
677P20
677P21
677P22
900803-4-28C
STOCK NUMBER
5180-01-241-3333
4030-01-088-6263
4930-01-266-8795
5330-01-237-3700
F-24
FIG.
1
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
1
1
1
1
1
1
1
1
1
1
1
1
1
1
ITEM
59
2
22
26
27
28
29
32
3
4
5
6
9
12
16
17
1
12
20
37
39
31
40
41
92
4
8
11
19
38
29
SECTION IV
TM 5-4930-234-13&P C06
CROSS REFERENCE INDEXES
FIG.
BULK
BULK
1
1
1
1
1
1
1
1
1
1
1
1
1
I
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
ITEM
1
2
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
FIGURE AND ITEM NUMBER INDEX
STOCK NUMBER
4930-01-237-3656
4010-01-005-4775
4930-01-278-6939
4930-01-278-6940
5305-00-988-7607
5999-00-134-5844
5935-00-572-5174
4030-01-088-6263
4730-00-915-5127
5330-00-612-2414
4010-01-005-4775
4030-01-088-6283
5330-01-237-3655
4930-01-350-1721
5330-01-237-3655
4930-01-266-8795
5330-01-237-3700
5330-00-641-0119
4730-01-237-3662
4030-01-088-6263
4010-00-222-4482
4930-01-266-8795
4930-01-238-3800
F-25
CAGEC
00624
81349
00624
00624
00624
00624
96906
00624
81349
19099
96906
00624
81349
19099
96906
00624
19099
76691
96906
00624
96906
81718
00624
00624
19099
81349
76691
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
96906
00624
00624
00624
76691
18876
84256
00624
00624
00624
00624
00624
PART NUMBER
AE24789-001
MILW83420
AE11695-003
AE13186-012
AE20074-053
AE20074-052
MS16995-35
AE24791-009
M83413/7-1
677P18
MS35340-57
AE24791-006
M8341C3/4-1
677P19
MS35340-19
AE83931 R
677P20
168-3-VC
MS27029-11
AE83932R
MS27030-6
H-1833
AE83574R
AE83936R
677P21
M83420/3-001
168-3-VC
AE82155R
AE85183R
AE18900-076
AE70725R
AE18900-076
AE83144Z
AE83630Z
AE10488-457
900803-4-28C
AE83933R
22504-230
AE84592R
MS29513-134
AE83576R
AE8357OR
AE83930R
168-3-VC
9083097
19-4CD
23052-3
23052-4
AE85107R
AE84745R
AE83545R
SECTION IV
TM 5-4930-234-13&P C06
CROSS-REFERENCE INDEXES
FIGURE AND ITEM NUMBER INDEX
FIG.
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
2
2
ITEM
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
1
2
STOCK NUMBER
5305-00-981-3512
5305-00-051-8605
5330-00-265-1097
5330-00-250-0232
5315-01-237-3696
5315-00-841-4443
5365-00-989-0083
3110-00-838-5033
4930-01-275-7908
5330-00-291-7337
5180-01-?41-3333
F-26
FSCM
00624
96906
96906
00624
00624
96906
00624
00624
00624
96906
96906
00624
80756
00624
51814
00624
00624
00624
00624
00624
00624
00624
96906
00624
00624
00624
00624
00624
00624
96906
00624
00624
00624
00624
00624
00624
00624
00624
96906
00624
00624
00624
00624
96906
00624
00624
00624
00624
00624
00624
00624
PART NUMBER
AE10488-445
MS16995-79
MS16995-77
AE83550R
AE83549R
MS29513-129
AE84014H
AE83541Z
AE10488-450
MS29513-214
MS171530
AE83551R
RSN50S
AE83543Z
SSR-0087-S17
AE18033-025
AE83572R
AE26329-001
AE15881-078
AE83553R
AE93643E
AE18067-036
MS16562-225
AE84340R
AE10488-453
AE10488-449
AE15881-076
AE10488-448
AE18034-006
MS16634-4015
AE18033-023
AE83573R
AE83569R
AE10488-447
AE10488-446
AE83571R
AE84494R
AE15881-079
MS19060-4812
AE10488-451
AE83577R
AE18900-088
AE18900-148
MS29513-228
AE18900-089
AE18900-087
AE83554R
23052-5
AE13186-009
S1391K
S1391-1
SECTION IV
TM 5-4930-234-13&P C06
CROSS-REFERENCE INDEXES
FIGURE AND ITEM NUMBER INDEX
FIG.
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
2
ITEM
STOCK NUMBER
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
FSCM
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
00624
96906
00624
00624
00624
00624
00624
00624
00624
00624
96906
99862
00624
00624
00624
00624
00624
00624
00624
00624
F-27/(F-28 Blank)
PART NUMBER
S1391-2
S1391-3
S1391-4
S1391-5
SC4568
S04574
S1391-6
SC4569
SC4576
S1391-7
SC4566
SC4567
MS9390-220
51391-8
S1391-9
S C4561
SC4562
SC4563
SC4564
S1391-10
SC4565
MS35650-3392
CL-35-SSC-N
S1391-11
S1391-12
S1391-13
S1391-14
SC4570
SC4571
S1391-15
AE83932R
TM 5-4930-234-13&P
These are the instructions for sending an electronic 2028
The following format must be used if submitting an electronic 2028. The subject line must be exactly the same and all
fields must be included; however only the following fields are mandatory: 1, 3, 4, 5, 6, 7, 8, 9,10,13, 15,16,17, and 27.
From:
To:
"Whomever"’ <[email protected]>
mpmt%[email protected]
Subject: DA Form 2028
From: Joe Smith
1.
Unit: home
2.
Address: 4300 Park
3.
City: Hometown
4.
St: MO
5.
Zip: 77777
6.
Date Sent: 19-OCT-93
7.
Pub no: 55-2840-229-23
8.
Pub Title: TM
9.
10. Publication Date: 04-JUL-85
11. Change Number: 7
12. Submitter Rank: MSG
13. Submitter FName: Joe
14. Submitter MName: T
15. Submitter LNamne: Smith
16. Submitter Phone: 123-123-1234
17. Problem: 1
18. Page: 2
19. Paragraph: 3
20. Line: 4
21. NSN: 5
22. Reference: 6
23. Figure: 7
24. Table: 8
25. item: 9
26. Total. 123
27. Text:
This is the text for the problem below line 27.
*U.S. GOVERNMENT PRINTING OFFICE: 1996 -755-025/40168
TM 5-4930-234-13&P
INDEX
Page
A
Additional Authorization List
Administrative Storage
D-1
4-13
C
Cam-Lock Coupling Assembly (Organizational)
Installation
Removal
Cam-Lock Coupling Assembly (Direct Support)
Disassembly
Inspection
Installation
Reassembly
Removal
Replacement
Cam-lock Coupling Gasket
Inspection
Reassembly
Removal
Replacement
CCR Nozzle Sub-Assembly
Cleaning
Disassembly
Inspection
Reassembly
Replacement
Testing
Components of End Item/Basic Issue Items
Connection of Nozzle, Model AE83206R
Connection of Nozzle, Model AE83501R
4-10
4-10
4-10
5-5
5-5
5-5
5-7
5-6
5-5
5-5
3-2
3-2
3-2
3-2
3-2
5-10
5-16
5-10
5-17
5-19
5-18
5-28
C-1
2-3
2-6
D
Destruction of Army Materiel To Prevent Enemy Use
Differences Between Models 1-3
Direct Support Maintenance Instructions
Disconnection of Nozzle, Model AE83206R
Disconnection of Nozzle, Model AE83501R
Dust Cap Assembly
Disassembly
Inspection
Installation
1-1
5-1
2-6
2-9
4-4
4-5
4-5
4-5
Change 2 I-1
TM 5-4930-234-13&P
INDEX (Continued)
Page
Dust Cap Assembly (Continued)
Reassembly
Removal
Replacement
Dust Plug Assembly
Disassembly
Inspection
Installation
Reassembly
Removal
Replacement
4-5
4-4
4-5
4-5
4-5
4-5
4-7
4-6
4-5
4-6
E
Equipment Characteristics, Capabilities, and Features
Equipment Description and Data
Expendable/Durable Supplies and Materials List
Explanation of Columns in the MAC
1-1
1-2
E-1
B-2
G
General Information
Ground Clip Assembly
Disassembly
Inspection
Installation
Reassembly
Removal
Replacement
Ground Plug Assembly
Disassembly4-7
Inspection
Installation
Reassembly
Removal
Replacement
1-1
4-9
4-9
4-10
4-10
4-10
4-9
4-10
4-7
4-7
4-8
4-7
4-7
4-7
I
Inspection
4-1
I-2
TM 5-4930-234-13&P
INDEX (Continued)
Page
L
Lubrication Instructions
3-1
M
Maintenance Allocation Chart
Maintenance Forms, Records, and Reports
Maintenance Functions
Maintenance Procedures (Operator)
Maintenance Procedures (Organizational)
Maintenance Procedures (Direct Support)
Miscellaneous Publications
B-1
1-1
B-1
3-2
4-4
5-5
A-1
N
Nomenclature Cross Reference List
1-3
O
Operating Controls
Operating Instructions
Operation of Nozzle, Model AE83206R
Operation of Nozzle, Model AE83501R
Operation Under Usual Conditions
Operation Under Unusual Conditions
Operator Maintenance Instructions
Operator Preventive Maintenance Checks and Services
Organizational Maintenance Instructions
2-1
2-1
2-5
2-6
2-3
2-9
3-1
2-2
4-1
P
Packaging
Preparation For Storage or Shipment
4-14
1-1,
Preventive Maintenance Checks and Services (Operator)
Principles of Operation
I-3
2-2
1-3
TM 5-4930-234-13&P
INDEX (Continued)
Page
R
References
A-1
Reporting Equipment Improvement Recommendations (EIR’s)
Repair Parts and Special Tools List
Repair Parts, Special Tools; Test Equipment, Measurement and Diagnostic
Equipment (TMDE); and Support Equipment
1-1
F-1
4-1
S
Safety, Care, and Handling
Service Upon Receipt
Strainer and O-Ring
Inspection
Reassembly
Removal
Replacement
1-3
4-1
3-4
3-5
3-5
3-4
3-5
T
Technical Manuals
Troubleshooting Procedures (Operator)
Troubleshooting Procedures (Organizational)
Troubleshooting Procedures (Direct Support)
A-1
3-1
4-1
5-1
U
Unisex Coupling Assembly (Organizational)
Installation
Removal
Unisex Coupling Assembly (Direct Support)
Disassembly
Inspection
Installation
Reassembly
Removal
Replacement
Unisex Coupling Seals
Inspection
Reassembly
Removal
Replacement
4-13
4-13
4-13
5-8
5-9
5-9
5-10
5-10
5-8
5-10
3-3
3-3
3-4
3-3
3-3
I-4
TM 5-4930-234-13&P
INDEX (Continued)
Page
Unisex Dust Cap
Disassembly
Inspection
Installation
Reassembly
Removal
Replacement
Unpacking
4-11
4-12
4-12
4-13
4-13
4-11
4-13
4-1
W
Warranty Information
1-1
I-5/( I-6 Blank)
TM 5-4930-234-13&P
By Order of the Secretary of the Army:
Official:
JOHN A. WICKHAM, JR.
General, United States Army
Chief of Staff
R. L. DILWORTH
Brigadier General, United States Army
The Adjutant General
DISTRIBUTION:
To be distributed in accordance with DA For, Organizational Direct Support and General Support Maintenance
requirements for Nozzle Assembly, Closed Circuit Refueling (CCN-101/14) (TM 5-4930-226-12&P)
*U.S. GOVERNMENT PRINTING OFFICE 1996 - 406-421 (61133)
PIN: 016228-000
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