TM-55-1670-251-20-and-P

TM-55-1670-251-20-and-P
TM 55-1670-251-20&P/TO 13D3-2-2
TECHNICAL MANUAL
ORGANIZATIONAL MAINTENANCE MANUAL
INCLUDING REPAIR PARTS AND SPECIAL TOOLS LIST
FOR
AERIAL RECOVERY KIT NSN 1670-00-264-8941
P/N 1670EG109A
HEADQUARTERS, DEPARTMENT OF THE ARMY,
6 JUNE 1975
TM 55-1670-251-20&P/TO 13D3-2-2
C6
CHANGE
HEADQUARTERS DEPARTMENTS OF
THE ARMY AND THE AIR FORCE
WASHINGTON, D.C., 9 July 2001
NO. 6
Organizational Maintenance Manual
Including Repair Parts and Special Tools List
For
AERIAL RECOVERY KIT, NSN 1670-00-264-8941
P/N 1670EG109A
DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.
TM 55-1670-251-20&P/T.O. 13D3-2-2, 6 June 1975, 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.
Remove pages
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A/B blank
----1-1 and 1-2
C-5 and C-6
C-7 and C-8
C-9 and C-10
Cover
A/B blank
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C-5 and C-6
C-7 and C-8
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2. Retain this sheet in front of manual for reference purposes.
TM 55-1670-251-20&P/TO 13D3-2-2
C6
By Order of the Secretary of the Army:
Official:
ERIC K. SHINSEKI
General, United States Army
Chief of Staff
JOEL B. HUDSON
Administrative Assistant to the
Secretary of the Army
0115502
DISTRIBUTION:
To be distributed in accordance with initial distribution number (IDN) 250005 requirements for
TM 55-1670-251-20&P.
TM 55-1670-251-20&P
T.O. 13D3-2-2
C5
CHANGE
HEADQUARTERS, DEPARTMENTS OF
THE ARMY AND THE AIR FORCE
WASHINGTON, D.C., 1 October 1996
NO 5
Organizational Maintenance Manual
Including Repair Parts and Special Tools List
For
AERIAL RECOVERY KIT, NSN 1670-00-264-8941
P/N 1670EG109A
DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.
TM 55-1670-251-20&P/T.O. 13D3-2-2, 6 June 1975, 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
1-1 through 1-4
----------------------------------A-1/(A-2 blank)
1-1 through 14
1-4.1/(1-4.2 blank)
2-9/(2-10 blank)
A-1/(A-2 blank)
Retain this sheet in front of manual for reference purposes.
TM 55-1670-251-20&P
T.O. 1313-2-2
C5
By Order of the Secretaries of the Army and Air Force:
DENNIS J. REIMER
General, United States Army
Chief of Staff
Official:
JOEL B. HUDSON
Administrative Assistant to the
Secretary of the Army
02452
RONALD R. FOGELMAN
General, USAF
Chief of Staff
HENRY VICCELLIO, JR.
General, USAF
Commander, Air Force Materiel Command
DISTRIBUTION:
To be distributed in accordance with DA Form 12-25-E, block no. 0005, requirements for TM 55-1670-251-20&P.
TM 55-1670-251-20&P/TO 13D3-2-2
C4
HEADQUARTERS
DEPARTMENT OF THE ARMY
WASHINGTON, D.C., 12 July 1989
CHANGE
No. 4
Organizational Maintenance Manual
Including Repair Parts and Special Tools List
for
AERIAL RECOVERY KIT, NSN 1670-00-264-8941
P/N 1670EG109A
TM 55-1670-251-20&P/TO 13D3-2-2-, 6 June 1975, 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
1-1 and 1-2
2-3 through 2-6
A-1/(A-2 blank)
1-1 and 1-2
2-3 through 2-6
A-1/(A-2 blank)
Retain this sheet in front of manual for reference purposes.
By Order of the Secretary of the Army:
CARL E. VUONO
Official:
GeneraI, United States Army
Chief of Staff
WILLIAM J. MEEHAN II
Brigadier General, United States Army
The Adjutant General
DISTRIBUTION:
To be distributed in accordance with DA Form 12-25A, Organizational Maintenance
requirements for Serial Recovery Kit (1670EG109A).
TM 55-1670-251-20&P/T.O. 13D3-2-2
C3
CHANGE
HEADQUARTERS
DEPARTMENT OF THE ARMY
WASHINGTON, D.C., 15 May 1987
No. 3
Organizational Maintenance Manual
Including Repair Parts and Special Tools List
For
AERIAL RECOVERY KIT, NSN 1670-00-264-8941
P/N 1670EG109A
TM 55-1670-251-20&P/T.O. 13D3-2-2, 6 June 1975, 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.
Remove pages
Insert pages
1-1 and 1-2
2-1 and 2-2
2-2.1/(2-2.2 blank)
A-1/(A-2 blank)
B-1 and B-2
C-7 thru C-10
1-1 and 1-2
2-1 and 2-2
2-2.1/(2-2.2 blank)
A-1/(A-2 blank)
B-1 and B-2
C-7 thru C-10
2. Retain this sheet in front of manual for reference purposes.
By Order of the Secretary of the Army:
JOHN A. WICKHAM, JR.
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, Organizational Maintenance requirements for
Aerial Recovery Kit (1670EG109A).
TM-55-1670-251-20&P/TO 13D3-2-2
LIST OF EFFECTIVE PAGES
Insert latest changed pages; dispose of superseded pages in accordance with regulations.
NOTE: On a changed page, the portion of the text affected by the latest change is indicated by a vertical line, or other
change symbol, in the outer margin of the page. Changes to illustrations are indicated by miniature pointing hands.
Changes to wiring diagrams are indicated by shaded areas.
Dates of issue for original and changed pages are:
Original
6 June 1975
Change 1
28 July 1980
Change 2
22 Sep 1982
Change 3
15 May 1987
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TM 55-1670-251-20&P/TO 13D3-2-2
TECHNICAL MANUAL
NO. 55-1670-251-20&P/
T.O. 13D3-2-2
HEADQUARTERS
DEPARTMENT OF THE ARMY
WASHINGTON, D.C., 6 JUNE 1975
ORGANIZATIONAL MAINTENANCE MANUAL
INCLUDING REPAIR PARTS AND SPECIAL TOOLS LIST
FOR
AERIAL RECOVERY KIT, NSN 1670-00-264-8941
P/N 1670EG109A
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 the
procedures, please let us know. Mail your letter or 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 Missile Command, ATTN: AMSAM-MMC-MA-NP, Redstone Arsenal,
AL 35898-5230.
You may also submit your recommended changes by E-mail directly to
[email protected] A reply will be furnished directly to you. Instruction 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 1.
INTRODUCTION
1-1
CHAPTER 2.
MAINTENANCE INSTRUCTIONS
2-1
APPENDIX A.
REFERENCES
A-1
APPENDIX B.
MAINTENANCE ALLOCATION CHARTS
B-1
APPENDIX C.
REPAIR PARTS AND SPECIAL TOOLS LIST
C-1
Change 6
i
TM
55-1670-251-20&P/TO
13D3-2-2
TABLE OF CONTENTS
CHAPTER
1.
INTRODUCTION
Section
I.
GENERAL
Scope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Maintenance Forms and Records . . . . . . . . . . . . . . . . . . . . . .
Reporting of Equipment Manual Improvements . . . . . . . . .
Destruction to Prevent Enemy Use . . . . . . . . . . . . . . . . . . .
II.
CHAPTER
2.
MAINTENANCE INSTRUCTIONS
Section
I.
PREPARATION FOR USE
Preparation of Kit at Start of Mission . . . . . . . . . . . . . . . . .
After-Use Inspection and Packaging . . . . . . . . . . . . . . . . . .
1-1
1-1
1-1
1-1
1-5
1-6
1-7
1-2
1-2
1-2
2-1
2-2
2-1
2-1
2-3
2-4
2-1
2-2
2-5
2-6
2-2
2-2
CLEANING AND LUBRICATION
Cleaning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Lubrication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
IV.
1-1
1-2
1-3
1-4
TOOLS AND EQUIPMENT
Common Tools and Equipment. . . . . . . . . . . . . . . . . . . . . . .
Special Tools and Equipment. . . . . . . . . . . . . . . . . . . . . . . .
III.
Page
DESCRIPTION AND DATA
Purpose and Use . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Technical Characteristics . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Description of Major Components . . . . . . . . . . . . . . . . . . . .
II.
Paragraph
PREVENTIVE MAINTENANCE CHECKS AND SERVICES
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Kit Container . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Nylon Rope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Load Stabilizers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Sling Assemblies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2-7
2-8
2-9
2-10
2-11
2-2
2-2
2-3
2-3
2-3
APPENDIX A.
REFERENCES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
A-1
B.
MAINTENANCE ALLOCATION CHARTS . . . . . . . . . . .
B-1
C.
REPAIR PARTS AND SPECIAL TOOLS LIST . . . . . . . .
C-1
ii.
TM 55-1670-251-20&P/TO 13D3-2-2
CHAPTER 1
INTRODUCTION
Section I. GENERAL
1-1.
Scope.
This manual contains a description of and maintenance instructions for the “Aerial Recovery Kit,” P/N
1670EG109A, NSN 1670-00-264-8941 which is used in recovery and evacuation of disabled aircraft.
1-2.
Maintenance Forms and Records.
The maintenance forms and records which are required by personnel who perform the maintenance functions prescribed in this manual are listed in DA PAM
738-751.
1-3. 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 the procedure,
please let us know. Mail your letter, DA Form 2028 (Recommended Changes to Publication and Blank Forms), or DA
Form 2028-2 located in the back of this manual directly to:
Commander, US Army Aviation and Missile Command,
ATTN: AMSAM-MMC-MA-NP, Redstone Arsenal, AL
35898-5230. A reply will be furnished to you. Reports by US
Air Force units should be submitted on AFTO Form 22,
Technical Order System Publication Deficiency Report, and
forwarded to the address prescribed above. An information
copy of the AFTO Form 22 shall be furnished to San Antonio
ALC/MMSTR, Kelly AFB TX 78241
1-4.
Destruction to Prevent Enemy Use.
For instructions applicable to the destruction of components of the Aerial Recovery Kit to prevent enemy use refer to TM 43-0002-1.
1-4.1 Preparation for Storage or Shipment.
For general technical information on preparation for
storage and shipment refer to TM 1-1500-204-23. For regulatory requirements pertaining to equipment placed in administrative storage refer to AR 750-1.
Change 6
1-1
TM 55-1670-251-20&P/TO 13D3-2-2
Section II. DESCRIPTION AND DATA
1-5
Purpose and Use.
The Aerial Recovery Kit contains the equipment
required for preparation, rigging and recovery of selected
aircraft, by any one of four prime movers, the UHID H, CH47, CH-54, and CH-53 helicopters.
1-6
Technical Characteristics.
a. The kit components are packaged in a bi-sectional
water tight aluminum container having the approximate
overall dimensions of 28.0 X 30.25 X 76.5 inches as shown
in figure 1-1. The kit assembly is air transportable as an
internal or external load. Six lift grips, three on each side of
the container assembly, are provided for use as tie-down or
suspension points for external transportation. Skid type
feet are provided to facilitate positioning of the container
either inside an aircraft or on the ground.
b. The container is constructed to have separable top
and bottom sections, each of which are Compartmented to
house the kit components in such a manner as to afford
easy accessibility and identification of the components.
Component part numbers are stenciled inside the container
compartments to enable easy recognition and hence
selection of components as required. Component locations
for each of these sections are shown in figure 1-2.
1-7
Description of Major Components.
The major components of the aerial recovery kit are
described below.
a. Anti-Chafe Pad PIN 1670EG044. The anti-chafe
pad is used to maintain the spacing of the belly band strap
assemblies and to afford padding to these assemblies in
the areas where they would normally contact the fuselage
of the slung aircraft thereby minimizing the risk of abrasion
to the belly bands and damage to the recovery aircraft.
b. Containers PIN 1670EG120 and P/N 5140-EG090-001. These containers provide storage of the kit
components to secure the contents and protect them from
adverse environmental conditions. The larger container,
PIN 1670EG] 20 is intended for long term storage and for
internal or external aircraft transport of the entire kit. The
smaller container P/N 5140-EG-090-001, supplements the
larger container for long term storage but is ideally suited
for normal handling of only those components of a kit
required for a given recovery operation.
c. Coupling Link Assembly PIN 1670EG079-1. The
coupling link assembly is used to connect with the belly
1-2 Change 5
band assembly to the spreader bar pendant assembly on
the rotor head shackle.
d. Drogue Chute Assembly P/N 1670EG029BI and
1670EG029B3. Drogue chutes are provided to maintain
the directional stability of slung aircraft. The smaller chute
(60.0 inch diameter) is used on most aircraft while the
larger chute (156 inch diameter) is required on the larger
and inherently unstable type of aircraft. Swivel attachments
prevent the chutes from winding up due to rotor downwash.
e. Gust Locks PIN 1670EG030A. The gust locks are
used to secure the control surface and to prevent motions
of ailerons, rudder, elevator, etc.
The load
f. Load-spreader PIN 1670EG035A1.
spreader is required for those aircraft where structural
frame members do not coincide with the required belly band
rigging stations. They reduce the risk of additional structure
damage to the recovered aircraft by distributing the belly
band loads over a large area.
g. Pendant Adapter PIN 1670EG093-1 and BOS-14KZ These pendant adapters have a rigid section between
the eyes at each end. A flexible pendant or sling set is
attached to one eye using a webbing ring assembly or a
steel apex fitting. The other end of the pendant adapter is
attached directly onto the helicopter cargo hook. The
pendant provides a light weight, non-conductive link which
also eases hook-up by allowing additional separation
between the hook-up crew and the lift helicopter. The PIN
1670EGO93-1 may be used on either the forward, aft, orcenter cargo hooks on the CH-47D. The new P/N BOS-14K7 has a smaller cross section at the rigid eye to allow
hook-up to the UH-60 cargo hook as well.
Pendant assemblies
h. Pendant Assemblies.
(flexible) are used primarily to lengthen the distance from
the cargo hook on the lift helicopter to the sling load. In
addition to the two nylon webbing pendants, PIN
1670EG028A and 1670EG028A3, the new polyester
roundlings, P/N PRS3C030, PRS7C065, and PRS7C070
provide excellent pendants, 30 foot, 65 foot and 70 foot
long respectively.
The
i. Positioning Strap PIN 1670EG036A-1.
positioning strap is used to prevent the slipping of the belly
bands, fore, aft, and laterally, from their required rigging
locations on an aircraft fuselage.
j. Probe Static Discharge PIN 1670EG068B-1. The
static discharge probe is used to bleed and ground the
static charge from the hovering recovery prime mover
helicopter, thereby allowing safe handling of the cargo hook
during hookup of the sling assembly.
TM 55-1670-251-20&P/TO 13D3-2-2
k. Sling Assembly, Belly Band PIN 1670EG057A-1 .
The belly band assemblies are used to cradle the downed
aircraft thereby eliminating the need of hardpoint
attachments for the sling system. Adjustable chain leg
assemblies (P/N 1670EGO68B 1) are provided for one belly
band assembly to provide a means of changing its length
relative to the other band assembly so as to achieve
appropriate attitude correction of the recovered aircraft.
The size 7 polyester roundslings, P/N PRSC7065 and
PRSC7070 may be used in lieu of the 1670EG056-1
webbing straps shown with this belly band. Lighter aircraft
may be rigged using two PRS2E017 roundslings choked to
form a 34 foot strap. The 1670EG068B1 adjustable chain
leg assemblies can be replaced with grab hook and chain
assembly from the standard 25,000 pound capacity
helicopter external cargo sling set.
I. Sling Rotor Head PIN 1670EG043-1. The rotor
head sling is used in conjunction with the pendant
assembly, to facilitate rotor head slinging of light helicopters
as an alternate method to belly band rigging. Rotor head
slinging is also accomplished by use of two, four or more
polyester roundslings choked around the barrel or arm of
the main rotor hub and jointed with an apex fitting assembly
from the standard 10,000 or 25,000 pound capacity
helicopter external cargo slings.
2 ing effect of the belly bands on the fuselage by
maintaining a fixed distance, which is equal approximately
to the width of the fuselage, between the two connecting
ends of the-belly band assembly. For the smaller aircraft,
particularly fixed wing, the spreader bar is aligned with the
center line of the fuselage. This orientation allows for
relocation of the vertex fitting on the spreader bar
arrangement to correct for attitude changes of the
recovered aircraft also the relative angle between the fore
and aft belly bands is reduced. Two polyester roundslings
P/N PRS3EOO8 can replace the P/N 1670EG034B 1 sling
legs for the spreader bar hoisting assembly.
o. Position Strap Anchors 1670EG075A1 and
1670EG075A3. The position strap anchors provide a
means for the webbing transition from two strap assemblies
of three bands each to three equivalent assemblies of two
bands each. The three strap legs are then covered by the
antichafe pad which prevents abrasion of the webbing and
also affords a more uniform loading between the belly band
and the airframe.
m. Spoiler Assembly P/N 167EGO32A. Spoilers are
required to destroy undesirable lifting tendencies of the
suspended fixed wing aircraft during forward flight. The
spoilers serve an important function in preventing the
recovered aircraft from "flying" into the recovery (prime
mover) helicopter ter.
n. Spreaded Bar Arrangement PIN 1670EG060B1.
The spreader bar is to be used with pendant assembly and
the sling assembly. Its function is two-fold depending upon
its orientation with respect to the recoverable aircraft. On
the larger type aircraft for example the CH-47, the spreader
bar arrangement will be positioned across the fuselage.
This reduces the crush TM 55-1670-251-20&P/TO 13D3-2-
Figure 1-1. Aerial Recovery Kit Container
(Part No. 1670EG120)
Figure 1-2. Stowage Diagram (sheet 1 of 2).
Change 5 1-3
TM 55-1670-251-20&P/TO 13D3-2-2
Figure 1-2. Stowage Diagram Concluded (sheet 2 of 2).
p. Polyester Roundslings. Roundslings consist of a
continuous loop load bearing core formed with polyester
yarn fully enclosed in a woven polyester protective cover.
Roundslings used with this kit are formed into eye and
eye slings with an additional wear pad sewn into each
eye. The seven foot and 17 foot roundslings have a
secondary protective sleeve which extends over the full
body of the sling. To reduce weight, the 30 foot, 65 foot,
and 70 foot roundslings have only a 24 inch sliding wear
pad to protect the sling where it is form into a basket or
otherwise contacts the load. The roundsling are very
flexible and conform to the load well whether in a straight
vertical pull, a choker or basket configuration. The
basket configuration allows smaller capacity slings to be
used as adjustable length links in larger capacity lines.
(1) PRS2E008. This eight foot long, size two
roundsling has a rated capacity of 4200 pounds in a
choker configuration. It is used for rotor head lift of the
OH-58, UH-1 and AH-1. Two are also used in the
supplemental lifting line for the UH-60. One forms a
basket around the tail cone and the other is formed into a
double basket to provide a two foot connecting strap
between the other eight foot and two 17 foot roundslings.
1-4 Change 5
(2) PRS2EO17.
This 17 foot size two
roundsling is used to make up the tail cone sling leg for
the UH-60 and AH-64 or as a lightweight belly band
strap.
(3) PRS3E008. This eight foot, size three
roundsling has a rated capacity of 6700 pounds in a
choker configuration. It is used as the main rotor head
slings on the UH-60 and AH-64 helicopters. It may be
used in lieu of the size two, PRS2E008, roundslings.
(4) PRS3E007.
This 17 foot, size three
roundsling has a rated capacity of 8400 pound in a single
line vertical configuration. It can be used in lieu of the
PRS3E017, size two roundsling. It can be used as a
pendant for OH-58, UH-i and AH-I.
(5) PRS5C030. This 30 foot long, size five
roundsling has a rated capacity of 13,200 pound as a
single line and 26,000 pound in a basket configuration. It
is used in a basket configuration to connect the main
rotor slings on the UH-60 and AH-64 to the apex fitting.
TM 55-1670-251-20&P/TO 13D3-2-2
(6) PRS7C065. This 65 foot, size seven
roundsling has a rated capacity of 21,200 pounds and is
used as a pendant for UH-60 and AH-64 helicopters. It
is also used as the aft rotor head lifting sling for dual
point recovery of the CH-47.
(7) PRS7C070. This 70 foot, size seven,
roundsling has a rated capacity of 21,200 pounds. It can
be used to increase the separation of the lift helicopter
and the recovered helicopter by connecting to the
PRS7C065 roundsling using an apex fitting from the
25,000 pound capacity helicopter external cargo sling. It
is also used as the forward lifting leg for dual hook
recovery of the CH-47.
The following readily
q. Standard Hardware.
available attaching hardware and fittings are used in
various rigging schemes. TM 55-1670-251-20&P/TO
13D3-2-2
(1) Apex fitting assemblies, P/N 3885000004045 and P/N 38850-00004-046. These are the apex
fitting from the standard 10,000 pound and 25,000 pound
capacity helicopter external cargo slings.
(2) Quick
disconnect
pins,
P/N
NAS1336C3C12 and NAS1336C3C17D. These 3/8 inch
PIP pins may be used in lieu of the NAS safety bolt and
nuts used with the 10,000 and 25,000 pound capacity
apex fitting assemblies.
(3) Adjustable chain assembly, P/N 3005000011-046 and 38850-00053-102. This chain and grab
hook assembly is used with the 25,000 capacity external
cargo sling. It can be used at the end of size 2 and size
3 roundslings or to replace the P/N 1670EG078BI chain
leg assembly.
Change 5 1-4.1/(1-4.2 blank)
TM 55-1670-251-20&P/TO 13D3-2-2
CHAPTER 2
MAINTENANCE INSTRUCTIONS
Section I. PREPARATION FOR USE
2-1. Preparation of the Kit
at Start of a Mission.
a. Generally, not all suspension components and equipment available in the aerial
recovery kit will be required to recover a
particular aircraft.
b. The kit components and equipment
which are not required for a given recovery mission can be removed from the kit and left behind
at the storage site. These components must however be replaced in the kit after completion of
the particular mission.
2-2. After-Use Inspection and Packaging.
All recovery equipment should be dried
and cleaned before repackaging into the container.
a. Repacking of Drogue Chutes. T h e
method of repacking the drogue chutes is shown
in figure 2-1. After a recovery in a wet terrain
it will be necessary to remove the mud before drying the webbing and fabric. Use standard parachute procedures for inspection.
b. Inspection of Tools. All tools used in
the previous recovery mission must be thoroughly
inspected, reconditioned and replaced if necessary.
c. Storage of the Equipment. All aerial
recovery kit equipment components and tools
which have been used, reconditioned, repaired or
replaced should be placed in their appropriate
compartment of the kit container as shown in
packaging diagram figure 1-2. The kit container
should then be locked and stored for a subsequent
recovery mission.
Section Il. TOOLS AND EQUIPMENT
2-3. Common Tools and Equipment.
Standard and commonly used tools and
equipment having general application are not part
of the kit equipment set. Such tools will normally
be included in the equipment of the maintenance
facility.
Figure 2-1. Drogue Chute Packaging.
2-1
TM 55-1670-251-20&P/TO 13D3-2-2
2-4. Special Tools and Equipment.
No special tools or equipment are required over
and above basic tools common to general mechanics tool
box of MOS 67.
Figure .2-2. Spreader Bar Assembly.
Section III. CLEANING AND LUBRICATION
2-5. Cleaning.
cleaned of foreign material to allow mating tubes to slide
freely. All shackle bearing surfaces should be clean.
a. The kit equipment should be cleaned before
repackaging into the container. All fabric components
are to be allowed to dry and then brushed clean to
prevent an accumulation of grit which will accelerate
abrasion. Drogue chutes should be allowed to dry,
shaken clean and repacked.
c. Remove grease or oil from webbing with dry
cleaning solvent (tetrachlorethylene) NSN
6850-00-264-9038. No repairs such as splicing or
restitching are authorized.
WARNING
Do not use pressurized air for cleaning the
nylon components as this will have a
tendency to force grit into weave.
b. Metal components should be wiped clean prior
to repackaging. Specifically the spreader bar assembly
(P/N 1670EG051A1), shown in figure 2-2, should be
2-6. Lubrication.
In general, no lubrication is required for any of the
kit components.
CAUTION
Do not lubricate metal components of the
sling assemblies as this will accumulate
grit and accelerate wear.
Section IV. PREVENTIVE MAINTENANCE CHECKS, SERVICE AND REPAIR
2-7. General.
a. This section contains general instructions for
inspection maintenance and repair of the Aerial
Recovery Kit components. In the following paragraphs,
and table 2-1 specific repair and inspection instructions
are presented to restore the major items to a serviceable
condition.
b. Preventive maintenance and repair of the kit
components is most easily accomplished as a post mission
operation since the items required cleaning and handling
for repackaging.
c. Two categories of inspection are applicable to
this kit:
2-2
Change 3
(1) A routine inspection of each component will
be made by the user before and after use.
(2) An inspection of the kit will be performed
every six months using the Preventative Maintenance
Checks and Services (PMCS), Table 2-1 by a qualified
Military Parachute Rigger, or a qualified Army Aircraft
Quality Control and Technical Inspector. To facilitate
recording of this inspection, each kit will be stamped in
1 inch lettering with the date the kit is placed in service
by the using unit. The stamped date will be used in
determining the date of the next inspection. The marking
will be with either Orange Yellow Parachute Marking
Ink, NSN 7510-00-634-6583 or Strata Blue Parachute
Marking Ink, NSN 7510-00-286-5362. If found
serviceable upon each six months inspection, the new
TM 55-1670-251-20&P/TO 13D3-2-2
date will be stamped on the container. At no time will the
kit be used beyond the six month period without being
inspected. Components judged unserviceable will be
disposed of. Prior to disposal, all serviceable components
will be cannibalized from the condemned item for future use.
2-8. Kit Container (Figure 1-1).
The container should be inspected for holes, dents
and damage to the seal and its receptacle. The seal and
its mating surface must be kept free of grit. Small
indentations can be repaired as deemed necessary.
Check sling suspension points.
Change 3
2-2.1/(2-2.2 blank)
TM 55-1670-251-20&P/TO 13D3-2-2
Table 2-1. Preventive Maintenance Checks and Services
Key: X-After Use
Y-Prior to Use
Z-Periodic (6 month) Inspection
Interval and
Sequence No.
X
1
Work time
(M/H)
Procedures
(inspect for)
Item Inspected
Y
Z
1
1
Kit packed for use
Determine that all components are present for use
0.8
2
2
Kit Container
Check for holes, dents, damage to seal and grit between
seal and mating surface. Check sling suspension points
for wear and damage, latches and strikes for freedom
of action. Check inspection record for last date of
inspection.
0.8
0.8
2
3
3
Drogue Chutes
Check for evidence of fraying and abrasion of canopy,
shroud lines and riser lines. Examine hook swivel for
freedom of action. Check for dampness, fungus acid,
grease, oil, dirt, foreign material, holes, cuts, tears,
and broken lines and webbing.
3
4
4
Fabric Material
Check for legibility of data markings, completeness,
dampness, fungus, dirt, acid, grease, oil, foreign
material, rips, burns, cuts, frays, tears, holes, thin
spots, loose weaving and loose or broken stitching, lines
or webbing.
0.8
4
5
6
Hardware Components
Check for corrosion, rough spots, burrs, breaks, cracks,
bends, and missing or worn tie chord, clevis pin or
safety pin.
0.9
for example, lifting grips for wear and damage.
Check latches and strikes for freedom of
operation.
2-9. Nylon Rope.
Inspect for cuts, frays, oil or grease stains and
rust at points of contact with metal. Remove
grease or oil by spot cleaning with dry cleaning
solvent (tetrachlorethylene), NSN 6850-00-2649039. Replace as required.
2-10. Load Stabilizers.
The load stabilizers of the aerial recovery kit are
shown in figure 2-3 items (1) through (4). These
are as follows:
a. Drogue Chutes. There are two types of
drogue chutes, 156 inches and 60 inches diameter
when inflated, item (1) and (2), respectively.
The drogue chutes if wet should be suspended and
allowed to dry after use. When dry shake and
brush to remove grit. Check for evidence of fraying and abrasion of canopy, shroud lines, and riser
lines. Examine hook swivel for freedom of operation. Repackage into bag as shown in Figure 2-1.
The maximum amount of wear which can be
tolerated before replacement of the chute assembly
is defined in TM 10-1670-201-23.
a.1. Drogue chutes manufactured before
June 1980. Inspect and repair as follows:
(1.) Swivel assemblies either be smoothed down and/or remove any casting flash by grinding or filing, or tape over the metal portion that
contacts the webbing with appropriate tape.
(2.) Overstitch the zig zag stitch pattern
with a three point WW Stitch Pattern using size FF
Nylon Thread.
b. Gust Lock Assembly. Inspect for pin
wear and general deformation. Straighten as
required. Check the shock bungee chord assemblies for cuts and abrasion. Replace as required.
c. Spoiler Assembly. Check the assemblies
for evidence of fraying and abrasion of nylon
straps and the integrity of their attachment to
the spoilers. A reduction of 50% in section area
of one strap or the loss of one rivet per attachment necessitates the repair or replacement of
the strap assembly. Check the rubber to aluminum
bond and rebond if required using adhesive liquid
FED-MM-A-139. Straighten spoiler angles.
Replace when beyond economical repair.
2-11. Sling Assemblies.
The sling assemblies of the aerial recovery kit are shown in figure 2-4. These are as
follows :
a. Anchor Positioning Straps. Inspect
Change 4 2-3
TM 55-1670-251-20&P/TO 13D3-2-2
Figure 2-3.
Figure 2-4.
2-4
TM 55-1670-251-20&P/TO 13D3-2-2
Figure 2-5. Sling Assembly Belly Band P/N 1670EG057A1.
for wear and any burrs which may abrade the
belly bands. Remove burrs, check for free running
of anchor on belly bands. If the positioning
anchor strap cannot be adjusted to obtain a free
sliding movement, it should be replaced.
b. Anti Chafe Pad. Inspect outer lines
of pad assembly for tears and abrasion. Check
“Velcro” bonded attachment. Before initiating
repair to liner, allow felt filler to dry thoroughly.
Rebond “Velcro” as required. Replace pad assembly when beyond economical repair.
c. Belly Band Assembly. Using disassembly procedures illustrated in figure 2-5,
remove quick disconnect pins, (1) and (2) and
separate link, from the belly bands, Remove the
spools from the belly bands. Inspect the belly
bands for fraying and abrasion, particularly in
the region of the spools. Any evidence of abrasion
of the nylon belly-bands shall warrant replacement
(individual straps may be replaced). Inspect the
spools and inside the link for smoothness of surface, remove any burrs that are evident. Any
deformation of the spools or pins shall warrant
replacement. Check fitting for evidence of cracks
in vicinity of welds and for peeling of protective
plating. Replace if cracks or peeling are evident.
Assembly is opposite of above procedure.
d. Chain Leg Assembly. Use disassembly
procedures illustrated in figure 2-6. Remove the
quick disconnect. pin and pull the large diameter
clevis pin from the fitting. Remove the cotter pin
and slide the small diameter pin from the fitting
thus releasing the chain. Remove the chain from
the grab link and inspect both components for
1.
2.
3.
4.
Pin
Chain
Cotter Pin
Disconnect Pin
5.
6.
7.
8.
Strap Webbing
Clevis Pin
Fitting
Pin
Figure 2-6. Chain Leg Assembly
P/N 1670EG078B1.
Change 4
2-5
TM 55-1670-251-20&P/TO 13D3-2-2
freedom of operation and alignment. Replace if
locking mechanism does not operate freely or if
the pin is bent. Inspect both clevis pins for alignment, cracks and wear. If pins are bent or worn
in excess of 0.02 inches-replace. Inspect the
clevis fitting for indications of wear, cracks or
bending particularly at the pin holes. If worn in
excess of 0.02 inches-replace. Inspect the chain
for evidence of wear and cracks. Any cracks or
wear in excess of 0.02 inches shall be cause for
replacement. Assembly is the opposite of that
stated for disassembly. Replace cotter pin with a
new pin.
e. Coupling Link Assembly. Use disassembly procedures illustrated in figure 2-7.
Depress the quick disconnect pin lock detent and
remove pin from the clevis pin. Remove clevis pin
and separate fitting links. Check quick disconnect
pin for freedom of operation and for alignment.
Inspect the clevis pin for wear and cracks if the
pin diameter is worn such that it can be detected
by feel, particularly in the area of the clevis
connection or is cracked it should be replaced.
Inspect the coupling links for wear, cracks or
peeling of the plating. If wear in the area of the
belly band assembly exceeds 0.02 inches or if peeling or cracks are evident-replace the links as
an assembly.
f. Load Spreader Assembly. D i s assemble as shown in figure 2-8 if required.
Inspect the fabric cover assembly and closure
strips for tears. Check the tube assemblies for
binding or deformation by touch. Check the bond
betveen the velcro tape and cover assembly and
the pad assembly. Re-bond as required. Repair
tears in the cover assembly by bonding on a patch
using adhesive Liquid FED-MM-A-139. If there
is evidence of tube deformation cut the closure
strip, remove tube and replace with a new unit.
Bond on a new closure strip.
Figure 2-8. Spreader Load Assembly
P/N 1670EG035A1.
g. Pendant Assembly. Suspend pendant
assembly from nylon ring and allow to dry
thoroughly. Remove grit from webbing by shaking and brushing. Do not use pressurized air as
this will force particles into webbing. Inspect
sling. leg and ring assembly for indications of
abrasion. If abrasion is apparent on any of the
load carrying components, they must be replaced.
L Pin
2. Wire
3. Clevis Pin
4. Fitting Links
Figure 2-7. Coupling Link Assembly
P/N 1670EG079-1.
2-6
h. Pendant Assembly UH-1 Type. S a m e
as above.
i. Pendant Adapter. Suspend pendant
adapter, allow to dry, inspect for indication of
abrasion, replace as required.
j. Positioning Strap Arrangement. Inspect
the assemblies of the arrangement for evidence of
TM 55-1670-251-20&P/TO 13D3-2-2
fraying and abrasion. Check buckle for burrs
which may cause abrasion and deburr as required.
Replace frayed or abraded straps.
k. Rotor Head Sling Arrangement. Check
each strap assembly (figure 2-9 ) for evidence of
fraying and abrasion. If this type of wear is
evident the assembly should be replaced. Inspect
the shackle assembly (1) and (2) for evidence of
wear. Burrs which may occur on the body of the
pin or on the shackle tube should be polished
smooth. If the protective plating is worn through
or peeling, or if there are any indications of
cracks the assembly should be replaced.
1. Spreader Bar Arrangement. Using
disassembly procedures illustrated in figure 2-10,
1. Rotor head shackle pin
2. Rotor head shackle
remove pin assemblies to release the strap assemblies from the spreader bar assembly and shackle.
Remove pin assembly from spreader bars (3) and
(5). Separate spreader bars and examine both
segments for dents, galling and weld cracks.
Localized dents are acceptable if they do not
impair the sliding engagement of the spreader
bars. Those areas exhibiting galling should be
smoothed by burnishing. Any evidence of cracks,
(these are most likely to appear in the vicinity
of the welds) shall warrant replacement. Check
all pin assemblies for burrs and wear. If burrs
are evident they should be smoothed by burnishing. If the protective plating of any pin is
worn through it should be replaced. Any lanyards
that are frayed or broken should be replaced.
3. Strap assembly
4. Antichafe pad
Figure 2-9. Rotor Head Sling Arrangement P/N 1670EG043-1.
2-7
TM 55-1670-251-20&P/TO 13D3-2-2
Figure 2-10. Spreader Bar Arrangement P/N
2-8
1670EG060B.
TM 55-1670-251-20&P/TO 13D3-2-2
CAUTION
Each load rigged with polyester slings is
to be checked to ensure the proper load
capacity is indicated on the identification
tag prior to use. The rigging is to be
inspected to insure that the roundsling is
protected from being cut by sharp
corners, sharp edges, protrusions or
abrasive surfaces. Roundslings are not
to be dragged on flours or other abrasive
surfaces. No repair of round-ins is
authorized.
m. Polyester Roundslinger. Polyester roundslings
are to be visually inspected for structural integrity of the
lifting eyes, the-protective covers and the wear (antichafe) pads prior to rigging. The polyester roundsling
shall be removed from service if any of the following is
visible.
(2) Melting, charring or weld spatter of any
part of the polyester roundsling.
(3) Holes, tears, cuts, embedded particles,
abrasive wear, or snags that expose the core fibers of
the polyester roundsling.
(4) Broken or worn stitching in the cover
which exposes the core fibers.
(5) Fittings when damaged, stretched or
distorted in any way.
(6) Polyester roundslings that are knotted.
(7) Acid or alkali burns of the polyester
roundsling.
(8) Any conditions which cause doubt as to
the strength of the polyester roundsling.
(1) If polyester roundsling identification tag is
missing or unreadable.
Change 5 2-9/(2-10 blank)
TM 55-1670-251-20&PjO 13D3-2-2
APPENDIX A
REFERENCES
AR 750-1
Army Material Maintenance Concepts and Policies
TM 10-1670-201-23
Maintenance of Parachutes and Other Airdrop Equipment, General
DA PAM 738-751
Functional Users Manual for The Army Maintenance Management
System-Aviation (TAMMS-A)
TM 43-0002-1
Procedures for the Destruction of Air Delivery Equipment to Prevent Enemy Use
TM 1-1500-204-23 (Series)
General Aircraft Maintenance Manual
*U.S. GOVERNMENT PRINTNG OFFICE: 1996. 755-825/40278
Change 5 A-1/(A-2 blank)
TM 55-1670-251-20&P/TO 13D3-2-2
APPENDIX B
MAINTENANCE ALLOCATION CHARTS
Section I. INTRODUCTION
B-1. Summary.
a. This appendix assigns maintenance functions and repair operations to be performed by the lowest
appropriate maintenance echelon. Section II defines the maintenance operations required; Section III lists the tool
and test equipment requirements and Section IV presents a list of operating supplies.
b. Columns in the maintenance allocation chart areas follows:
(1) Part or Component. This column shows only the nomenclature or standard item name, Additional
descriptive data are included only where clarification is necessary to identify the part. Components and parts
comprising a major end item are listed alphabetically. Assemblies and subassemblies are in alphabetical sequence
with their components listed alphabetically immediately below the assembly listing.
(2) Maintenance Function. This column indicates various maintenance functions allocated to the echelon
capable of performing the operation.
(a) Service. To clean, to preserve, and to replenish fuel and lubricants.
(b) Adjust. To regulate periodically to prevent malfunction.
(c) Inspect. To verify serviceability and to detect the first stage of electrical or mechanical failure
by scrutiny.
(d) Test. To verify serviceability and to detect the first stages of electrical or mechanical failure
by use of special equipment such as gages and meters.
(e) Replace. To substitute serviceable assemblies, subassemblies and parts for unserviceable
components.
(f) Repair. To restore to a serviceable condition by replacing unserviceable parts or by any other
action required utilizing tools, equipment, and skills available, to include welding, grinding, riveting, straightening,
adjusting, etc.
(g) Calibrate. To determine, check or rectify the graduation of an instrument, weapon, or weapons
system, or components of a weapons system.
(h) Rebuild. To restore to a condition comparable to new by disassembling the item to determine
the condition of its component parts and reassembling it using serviceable, rebuilt, or new assemblies, subassemblies,
and parts.
(3) 1st, 2nd, 3rd, 4th, 5th Echelon. The symbol X placed in columns 1 thru 5 indicated the echelon
responsible for performing that particular maintenance operation, but does not necessarily indicate that repair parts
will be stocked at that level. Normally there will be no deviation from the assigned level of maintenance. In cases
of operational necessity, maintenance functions assigned to a maintenance level may, on a one-time basis and at the
request of the lower maintenance level, be specifically authorized by the maintenance officer of the level of maintenance
to which the function is assigned. The special tools, equipment, etc. required by the lower level of maintenance to
perform this function will be furnished by the maintenance level to which the function is assigned. This transfer of
a maintenance function to a lower maintenance level does not relieve the higher maintenance level of the responsibility
for the function. The higher level of maintenance has the authority to determine:
1) If the lower level is capable of performing the work.
2) If the lower level will require assistance or technical supervision and on-site inspection.
3) If the authorization will be granted.
(4) Tools Required. This column indicates codes assigned to individual tool, test equipment, and
maintenance equipment referenced. The grouping of codes in this column of the maintenance allocation chart indicates
the tool, test and maintenance equipment required to perform the maintenance function.
c. Columns in the allocation of tools for maintenance functions are as follows:
(1) Tools Required for Maintenance Functions. This column lists tools, test, and maintenance
equipment required to perform the maintenance functions.
(2) lst, 2nd, 3rd, .4th, 5th Echelon. To be assigned at a later date.
Change
3
B-1
TM 55-1670-251-20&P/TO 13D3-2-2
(3) Tool Code. This column lists the tool code assigned.
B-2. Mounting Hardware.
The basic entries of this maintenance allocation chart do not include mounting hardware such
as screws, nuts, bolts, washers, brackets, and clamps.
B-2
TM
55-1670-251-20&P/TO
13D3-2-2
Section Il. MAINTENANCE ALLOCATION CHART
GROUP NO. (1)
8001
8002
8003
8004
B-3
TM
55-1670-251-20&P/TO
GROUP NO. (1)
8005
B-4
13D3-2-2
TM
55-1670-251-20&P/TO
13D3-2-2
APPENDIX C
REPAIR PARTS AND SPECIAL TOOLS LIST
(Current as of 17 December 1974)
Section I. INTRODUCTION
C-1. Scope.
This appendix lists the repair parts and bulk materials required for performance of organizational
maintenance of the Aerial Recovery Kit.
C-2. General.
This Repair Parts and Special Tools List is divided into the following sections:
a. Section II. Repair Parts List. A list of repair parts authorized for use in the performance of
maintenance. Parts are listed in figure and item number sequence. Bulk materials are listed in NSN
sequence.
b. Section III. Special Tools List. (Not applicable).
c. Section IV. National Stock Number and Reference Number Index. A list, in ascending numerical sequence, of all National stock numbers appearing in the listing, followed by a list, in alphameric
sequence, of all reference numbers appearing in the listing. National stock numbers and reference
numbers are cross-referenced to each illustration figure and item number appearance.
C-3. Explanation of Columns.
The following provides an explanation of columns found in the tabular listing:
a. Source, Maintenance, and Recoverability Codes (SMR).
(1) Source Code. Source codes are assigned to support items to indicate the manner of
acquiring support items for maintenance, repair, or overhaul of end items. Source codes are entered in
the first and second positions of the Uniform SMR Code format as follows:
Code
PA
PB
Definition
Item procured and stocked for anticipated or known usage.
Item procured and stocked for insurance purpose because essentiality dictates
that a minimum quantity be available in the supply systems.
NOTE: Cannibalization or salvage may be used as a source of supply for any items source coded above
except aircraft support items as restricted by AR 700-42.
(2) Maintenance Code. Maintenance codes are assigned to indicate the levels of maintenance
authorized to USE and REPAIR support items. The maintenance codes are entered in the third and
fourth positions of the Uniform SMR Code format as follows:
(a) The maintenance code entered in the third position will indicate the lowest maintenance level authorized to remove, replace, and use the support item. The maintenance code entered in
the third position will indicate the following level of maintenance.
Code
O
Application/Explanation
Support item is removed, replaced, used at the organizational level.
(b) The maintenance code entered in the fourth position indicates whether the item is
to be repaired and identifies the lowest maintenance level with the capability to perform complete repair
(i.e., all authorized maintenance functions). This position will contain the following maintenance code:
C-1
TM 55-1670-251-20&P/TO 13D3-2-2
Application/Explanation
Code
Nonreparable. No repair is authorized.
Z
(3) Recoverability Code. Recoverability codes are assigned to support items to indicate the
disposition action on unserviceable items. The recoverability code is entered in the fifth position of the
Uniform SMR Code format as follows:
Definition
Code
Nonreparable
item. When unserviceable, condemn and dispose at
Z
the level indicated in position 3.
b. National Stock Number. Indicates the National stock number assigned to the item and will be
used for requisitioning purposes.
c. Description. Indicates the Federal item name and, if required, a minimum description to
identify the item. The description column includes the following:
(1) Reference Number and Manufacturer Code. 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, specification standards and
inspection requirements, to identify an item or range of items. The primary number is followed by the
Federal supply code for manufacture (FSCM) in parentheses. The FSCM is a 5-digit numeric code
listed in SB 708-42 which is used to identify the manufacturer, distributor, or Government agency, etc.
NOTE: When a stock numbered item is requisitioned, the repair part received may have a different
reference number than the part being replaced.
(2) Usable on Code. (Not applicable).
d. Unit of Measure (U/M). Indicates the standard of the basic quantity of the listed item as
used in performing the actual maintenance function. This measure is expressed by a two-character alphabetical abbreviation (e.g,. EA, IN, PR, etc.). When the unit of measure differs from the unit of issue,
the lowest unit of issue that will satisfy the required units of measure will be requisitioned.
e. Quantity Incorporated in Unit. Indicates the quantity of the item in the breakout shown on
the illustration figure, which is prepared for an assembly. A “V” appearing in this column in lieu of a
quantity indicates that no specific quantity is applicable.
f. Illustration. This column is divided as follows:
(1) Figure Number. Indicates the figure number of the illustration in which the item is
shown.
(2) Item Number. The number used to identify each item called out in the illustration.
C-4. How To Locate Repair Parts.
a. When National Stock Number or Reference Number is Unknown:
(1) First. Identify the repair part on the exploded view illustration and note the item
number of the repair part.
(2) Second. Using the Repair Parts Listing, find the item number listed in the illustration
column.
b. When National Stock Number or Reference Number is Known:
(1) First. Using the Index of National Stock Numbers and Reference Numbers find the
pertinent National stock number or reference number. This index is in ascending NSN sequence followed
by a list of reference numbers in ascending alphameric sequence, cross-referenced to the illustration
figure and item number.
(2) Second. After finding the figure and item number, locate the figure and item in the
illustration column of the Repair Parts Listing.
C-5. Abbreviations.
(Not applicable).
C-2
Figure C-1.
TM 55-1670-251-20&P/TO 13D3-2-2
C-3
TM
C-4
55-1670-251-20&P/TO
13D3-2-2
Figure C-1.
TM 55-1670-251-20&P/TO
Change
C-5
Figure C-1.
13D3-2-2
2
TM 55-1670-251-20&P/TO 13D3-2-2
DESCRIPTION
SMR
CODE
NATIONAL
STOCK
NUMBER
1670-00-264-8941
ILLUSTRATION
USABLE
ON
CODE
REFERENCE NUMBER & MFR CODE
1670EG109A
(81996)
UNIT
OF
MEA
QTY
INC
IN
UNIT
KIT, AERIAL RECOVERY-AIRCRAFT . . . . . . . . . . . . . .
FIG
NO
ITEM
NO
C-1
SECTION II
REPAIR PARTS LIST
PBOZZ
1670-00-391-8585
1670EG120
(81996)
CONTAINER, AERIAL RECOVERY KIT . . . . . . . . . . . .
EA
1
C-1
1
PAOZZ
1670-00-111-2239
1670EG086-1
(81996)
. HANDLE, BAIL-BOTTOM . . . . . . . . . . . . . . . . . . . . . . . .
EA
6
C-1
2
PAOZZ
1670-00-111-2240
1670EG086-2
(81996)
. HANDLE, BAIL-TOP . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
EA
6
C-1
3
PAOZZ
1670-00-111-2241
1670EG086-9
(81996)
. HANDLE, BAIL-LIFT . . . . . . . . . . . . . . . . . . . . . . . . . . . .
EA
4
C-1
4
PBOZZ
1670-00-391-8588
1670EG120-1
(81996)
. SHELL, CONTAINER, BOTTOM . . . . . . . . . . . . . . . . . .
EA
1
C-1
5
PBOZZ
1670-00-391-8589
1670EG120-2
(81996)
. SHELL, CONTAINER, TOP . . . . . . . . . . . . . . . . . . . . . . .
EA
1
C-1
6
PBOZZ
1670-00-393-0472
1670EG035A1
(81996)
SPREADER ASSEMBLY, AERIAL RECOVERY . . . . . .
EA
4
C-1
7
PBOZZ
1670-00-393-0457
1670EG073-1
(81996)
. COVER, LOAD SPREADER . . . . . . . . . . . . . . . . . . . . . . .
EA
1
C-1
8
PBOZZ
1670-00-391-8501
1670EG035A5
(81996)
. PAD, SPREADER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
EA
2
C-1
9
PBOZZ
1670-00-574-8044
1670EG068B1
(81996)
PROBE, STATIC DISCHARGE . . . . . . . . . . . . . . . . . . . . .
EA
1
C-1
10
PAOZZ
1670-00-391-8499
1670EG029B3
(81996)
CHUTE, DROGUE, AIR RECOVERY-60 IN. DIA . . . . .
EA
1
C-1
11
PAOZZ
1670-00-391-8607
1670EG029B1
(81996)
CHUTE, DROGUE, AIR RECOVERY-156 IN. DIA . . . .
EA
1
C-1
11
PAOZZ
1670-00-391-8605
1670EG030A
(81996)
GUST LOCK ASSEMBLY, AERIAL RECOVERY . . . . .
EA
14
C-1
12
PBOZZ
1670-00-393-0454
1670EG032A
(81996)
SPOILER ASSEMBLY, AERIAL RECOVERY . . . . . . . .
EA
8
C-1
13
PAOZZ
1670-00-391-8583
1670EG075A1
(81996)
ANCHOR, POSITIONING STRAP-STRAIGHT . . . . . . .
EA
8
C-1
14
PAOZZ
1670-00-574-8046
1670EG075A3
(81996)
ANCHOR, POSITIONING STRAP-ANGLED . . . . . . . . .
EA
4
C-1
14
PAOZZ
1670-00-391-8511
1670EG044
(81996)
PAD ASSEMBLY, AITI-CHAFE . . . . . . . . . . . . . . . . . . . . .
EA
8
C-1
15
PBOZZ
1670-01-388-3917
PRS5E030
(81996)
CH-47 PENDANT ASSY . . . . . . . . . . . . . . . . . . . . . . . . . . .
EA
1
C-1
16
PAOZZ
1670-00-393-0460
1670EG070B1
(81996)
. RING ASSEMBLY, AERIAL RECOVERY . . . . . . . . . . .
EA
1
C-1
17
PBOZZ
1670-00-393-0455
1670EG069-1
(81996)
. SLING LEG, AERIAL RECOVERY . . . . . . . . . . . . . . . . .
EA
1
C-1
18
PAOZZ
1670-01-388-8479
PRS3E017
(81996)
UH-60 PENDANT ASSY . . . . . . . . . . . . . . . . . . . . . . . . . . .
EA
1
C-1
19
C-6
Change 6
TM 55-1670-251-20&P/TO 13D3-2-2
DESCRIPTION
SMR
CODE
NATIONAL
STOCK
NUMBER
REFERENCE NUMBER & MFR CODE
ILLUSTRATION
USABLE
ON
CODE
UNIT
OF
MEA
QTY
INC
IN
UNIT
FIG
NO
ITEM
NO
PAOZZ
1670-00-393-0507
1670EG067B1
(81996)
. ADAPTER RING, AERIAL RECOVERY . . . . . . . . . . . .
EA
1
C-1
20
PAOZZ
1670-00-393-0460
1670EG070B1
(81996)
. RING ASSEMBLY, AERIAL RECOVERY . . . . . . . . . . .
EA
1
C-1
21
PBOZZ
1670-00-393-0455
1670EG069-1
(81996)
. SLING LEG, AERIAL RECOVERY . . . . . . . . . . . . . . . . .
EA
1
C-1
22
PAOZZ
1670-00-393-0489
1670EG036A1
(81996)
POSITIONING STRAP, AERIAL RECOVERY . . . . . . . .
EA
12
C-1
23
PAOZZ
1670-00-574-8049
1670EG093-1
(81996)
PENDANT ADAPTER, AERIAL RECOVERY . . . . . . . .
EA
1
C-1
23A
PBOZZ
1670-01-388-3901
PR57E065
(81996)
BELLY BAND ASSY (ROUND SLING DOUBLED) . . .
EA
1
C-1
24
PAOZZ
1670-00-391-8523
1670EG048A1
(81996)
. LINK ASSEMBLY, AERIAL RECOVERY . . . . . . . . . . .
EA
2
C-1
25
PAOZZ
1670-00-391-8556
1670EG048A5
(81996)
. . SPOOL, LINK ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . .
EA
2
C-1
26
PAOZZ
1670-01-388-3845
PR52E017
(81996)
BELLY BAND STRAP, (DOUBLED) . . . . . . . . . . . . . . . . .
EA
2
C-1
27
PBOZZ
1670-00-391-8549
1670EG060B1
(81996)
HOISTING ASSEMBLY, AERIAL RECOVERY . . . . . . .
EA
2
C-1
28
PBOZZ
1670-00-391-8513
1670EG051A1
(81996)
. SPREADER BAR, AERIAL RECOVERY . . . . . . . . . . . .
EA
1
C-1
29
PBOZZ
1670-00-391-8509
1670EG050C1
(81996)
. . TUBE ASSEMBLY, SPREADER BAR, INNER . . . . .
EA
1
C-1
30
PBOZZ
1670-00-391-8521
1670EG049B1
(81996)
. . TUBE ASSEMBLY, SPREADER BAR, OUTER . . . . .
EA
1
C-1
31
PAOZZ
1670-00-391-8512
1670EG052A5
(81996)
. . PIN ASSEMBLY, SPREADER BAR . . . . . . . . . . . . . . .
EA
1
C-1
32
PAOZZ
1670-00-393-0506
1670EG054A3
(81996)
. PIN ASSEBMLY, AERIAL RECOVERY . . . . . . . . . . . . .
EA
2
C-1
33
PAOZZ
1670-00-391-8578
1670EG053B1
(81996)
. SHACKLE ASSEMBLY, AERIAL RECOVERY . . . . . .
EA
2
C-1
34
PBOZZ
1670-01-388-8480
PR53E008
(81996)
HOISTING ASSY STRAP . . . . . . . . . . . . . . . . . . . . . . . . . .
EA
4
C-1
35
PBOZZ
1670-00-391-0505
1670EG045B1
(81996)
. VERTEX FITTING ASSEMBLY AERIAL RECOVERY
EA
1
C-1
36
PAOZZ
1670-00-393-0508
1670EG042B1
(81996)
. . HOUSING, VERTEX FITTING . . . . . . . . . . . . . . . . . . .
EA
1
C-1
37
PAOZZ
1670-00-393-0500
1670EG040C1
(81996)
. . PIN ASSEMBLY, AERIAL RECOVERY . . . . . . . . . . . .
EA
1
C-1
38
PAOZZ
1670-00-393-0465
1670EG040C9
(81996)
. . PIN ASSEMBLY, AERIAL RECOVERY . . . . . . . . . . . .
EA
2
C-1
39
PAOZZ
4010-00-391-8608
1670EG078B1
(81996)
CHAIN ASSEMBLY, SINGLE LINK . . . . . . . . . . . . . . . . .
EA
2
C-1
40
PAOZZ
4010-00-391-8609
1670EG078B9
(81996)
. CHAIN, WELDED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
EA
1
C-1
41
PAOZZ
1670-00-391-8579
1670EG078B7
(81996)
. CLEVIS, DOUBLE LINK . . . . . . . . . . . . . . . . . . . . . . . . .
EA
1
C-1
42
Change 6
C-7
TM 55-1670-251-20&P/TO 13D3-2-2
DESCRIPTION
SMR
CODE
NATIONAL
STOCK
NUMBER
ILLUSTRATION
USABLE
ON
CODE
REFERENCE NUMBER & MFR CODE
UNIT
OF
MEA
QTY
INC
IN
UNIT
FIG
NO
ITEM
NO
PAOZZ
4010-00-391-8611
1670EG078B11
(81996)
. LINK, CHAIN, END . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
EA
1
C-1
43
PBOZZ
1670-00-574-8048
1670EG043-1
(81996)
SLING ASSEMBLY, ROTOR HEAD . . . . . . . . . . . . . . . . .
EA
1
C-1
44
PAOZZ
1670-00-574-8043
1670EG061C1
(81996)
. SHACKLE ASSEMBLY, ROTOR HEAD SLING . . . . .
EA
1
C-1
45
PAOZZ
1670-01-388-6789
PR52E008
(81996)
ROTOR HEAD SLING STRAP ASSY . . . . . . . . . . . . . . . .
EA
4
C-1
45A
PAOZZ
1670-00-398-9670
1670EG079-1
(81996)
COUPLING LINK ASSEMBLY, AERIAL
RECOVERY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
EA
2
C-1
46
FT
V
BULK
SH
V
BULK
GL
V
BULK
INK, MARKING, PARACHUTE-STRATA-BLUE, 1 PT
CAN, . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
MIL-I-6903, TYPE IV
PT
V
BULK
INK, MARKING, PARACHUTE-ORANGE-YELLOW, 1
PT BOTTLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
MIL-I-6903, TYPE IV
PT
V
BULK
YD
V
BULK
MARKER, TUBE TYPE-STRATA-BLUE INK, FELT
TIP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
FED GG-M-00114
EA
V
BULK
MARKER, TUBE TYPE-ORANGE-YELLOW
INK, FELT TIP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
FED GG-M-00114
EA
V
BULK
BALL POINT PEN-STRATA-BLUE INK, MEDIUM
POINT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
FED GG-B-0060
EA
V
BULK
GL
V
BULK
PT
V
BULK
FT
V
BULK
FT
V
BULK
BULK MATERIALS
PAOZZ
PAOZZ
PAOZZ
PAOZZ
PAOZZ
PAOZZ
PAOZZ
PAOZZ
PAOZZ
4020-00-753-2886
5350-00-221-0872
6850-00-264-9038
7510-00-286-5362
7510-00-634-6583
7510-00-663-0196
7520-00-230-2734
7520-00-469-7596
7520-00-491-2917
ROPE, NYLON–1-1/4 IN. CIR, 20 FT PER LB.
4,800 LB . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
BREAKING STRENGTH, 1,200 FT PER
REEL, MIL-R-17343
CLOTH, ABRASIVE-FERRIC OXIDE &
QUARTZ, JEAN CLOTH . . . . . . . . . . . . . . . . . . . . . . . .
BACKING, 9 IN. W, 11 IN. LG, 24 SHEETS PER
CARTON
DRY CLEANING SOLVENT-LIQUID, 5 GAL
PAIL, FED P-D-680 . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TAPE, PRESSURE SENSITIVE ADHESHIVE-2
IN. W., OLIVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
DRAB, FILM BACKING, OPAQUE, 60 YD
ROLL, FED PPP- T-60, TYPE III
PAOZZ
8010-00-297-2124
ENAMEL-OLIVE DRAB, SEMIGLOSS, 1 GAL CAN. .
FED TT-E-485, TYPE II
PAOZZ
8040-00-262-9062
ADHESIVE-LIQUID, 1 PT CAN, FED
MMM-A-139, CLASS 2 . . . . . . . . . . . . . . . . . . . . . . . . . .
PAOZZ
8305-00-267-3114
CORD, ELASTIC-3/8 IN. DIA, 300 LB BREAKING
STRENGTH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
MIL-C-5651, TYPE I
PAOZZ
C-8
8315-00-926-4930
Change 6
FASTENER TAPE, PILE-BLACK, NYLON, 2 IN. W,
MIL-F-21840, TYPE II, CLASS 1
.
TM 55-1670-251-20&P/TO 13D3-2-2
DESCRIPTION
SMR
CODE
NATIONAL
STOCK
NUMBER
ILLUSTRATION
USABLE
ON
CODE
REFERENCE NUMBER & MFR CODE
PAOZZ
8315-00-926-4931
FASTENER TAPE, HOOK-BLACK, NYLON, 2 IN. W .
MIL-F-21840, TYPE II, CLASS 1
PAOZZ
9310-00-160-7858
STENCILBOARD-OILED, 36 IN. LG, 24 IN. W, 1/64
IN. THK, . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
100 SHEETS PER WRAPPER, FED
UU-S-625, TYPE II, GRADE 1
UNIT
OF
MEA
QTY
INC
IN
UNIT
FIG
NO
FT
V
BULK
SH
V
BULK
ITEM
NO
PAOZZ
MIL-R-6130, TYPE 1, GRADE A, 1/4” THICK AND 1”
WIDE RUBBER STRIP . . . . . . . . . . . . . . . . . . . . . . . . . . . .
IN
V
BULK
PAOZZ
40 05 DURAMETER “COMMERCIAL” RUBBER
SOFT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
IN
V
BULK
SECTION III
SPECIAL TOOLS LIST
(NOT APPLICABLE)
Change 3
C-9
TM 55-1670-251-20&P/TO 13D3-2-2
SECTION IV
NATIONAL STOCK NUMBER AND REFERENCE NUMBER INDEX
C-10
STOCK
NUMBER
FIGURE
NUMBER
ITEM
NUMBER
STOCK
NUMBER
FIGURE
NUMBER
ITEM
NUMBER
1670-01-388-8479
1670-01-388-3917
1670-00-391-8499
1670-00-391-8501
1670-00-391-8509
1670-00-391-8511
1670-00-391-8512
1670-00-391-8513
1670-00-391-8521
1670-00-391-8523
1670-00-391-8549
1670-00-391-8556
1670-00-391-8578
1670-00-391-8579
1670-00-391-8583
1670-00-391-8585
1670-00-391-8588
1670-00-391-8589
1670-00-391-8605
1670-00-391-8607
1670-00-393-0454
1670-00-393-0455
1670-00-393-0455
1670-00-393-0457
1670-01-388-3845
1670-00-393-0460
1670-00-393-0460
1670-00-393-0465
1670-01-388-8480
1670-00-393-0472
1670-00-393-0489
1670-00-393-0500
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
19
16
11
9
30
15
32
29
31
25
28
26
34
42
14
1
5
6
12
11
13
18
22
8
27
17
21
39
35
7
23
38
1670-00-393-0505
1670-00-393-0506
1670-00-393-0507
1670-00-393-0508
1670-00-398-9670
1670-00-374-8043
1670-00-574-8044
1670-00-574-8046
1670-00-574-8048
1670-00-574-8049
1670-01-388-3901
1670-01-388-6789
4010-00-391-8608
4010-00-391-8609
4010-00-391-8611
4020-00-753-2886
5340-00-111-2239
5340-00-111-2240
5340-00-111-2241
5350-00-221-0872
6850-00-264-9038
7510-00-286-5362
7510-00-634-6583
7510-00-663-0196
7520-00-230-2734
7520-00-469-7596
7520-00-491-2917
8010-00-297-2124
8040-00-262-9062
8305-00-267-3114
8315-00-926-4930
8315-00-926-4931
9310-00-160-7858
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
BULK
C-1
C-1
C-1
BULK
BULK
BULK
BULK
BULK
BULK
BULK
BULK
BULK
BULK
BULK
BULK
BULK
BULK
36
33
20
37
46
45
10
14
44
23A
24
45A
40
41
43
2
3
4
REFERENCE
NUMBER
MFG
CODE
FIG
NUMBER
ITEM
NUMBER
REFERENCE
NUMBER
MFG
CODE
FIG
NUMBER
ITEM
NUMBER
PRS5E030
PRS3E017
1670EG029B1
1670EG029B3
1670EG030A
1670EG032A
PRS3E008
1670EG035A1
1670EG035A5
1670EG036A
160EG040C1
1670EG040C9
1670EG042B1
1670EG043-1
1670EG044
1670EG045B1
1670EG048A1
1670EG048A5
1670EG049B1
1670EG050C1
1670EG051A1
1670EG052A5
1670EG053B1
1670EG054A3
PRS2E017
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
16
19
11
11
12
13
35
7
9
23
38
39
37
44
15
36
25
26
31
30
29
32
34
33
27
PRS7E065
1670EG060B1
1670EG061C1
PRS2E008
1670EG067B1
1670EG068B1
1670EG069-1
1670EG069-1
1670EG070B1
1670EG070B1
1670EG073-1
1670EG075A1
1670EG075A3
1670EG078B1
1670EG078B11
1670EG078B7
1670EG078B9
1670EG079-1
1670EG086-1
1670EG086-2
1670EG086-9
1670EG093-1
1670EG120
1670EG120-1
1670EG120-2
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
81996
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
C-1
24
28
45
45A
20
10
18
22
17
21
8
14
14
40
43
42
41
46
2
3
4
23A
1
5
6
Change 6
TM 55-1670-251-20&P/TO 13D3-2-2
This publication is published for the use of all concerned. By order of the Secretaries of the Army,
and the Air Force.
Official:
VERNE L. BOWERS,
Major General, United States Army
The Adjutant General
Official:
JACK R. BENSON,
Colonel, USAF,
Director of Administration.
FRED C. WEYAND
General, United States Army
Chief of Staff
DAVID C. JONES
General, USAF
Chief of Staff
DISTRIBUTION:
To be distributed in accordance with DA Form 12-31, Organizational Maintenance requirements
for CH-47A, CH-47B/C, CH-54A, CH-54B, UH-1B, UH-1C/M, and UH-1D/H aircraft.
U.S. GOVERNMENT PRINTING OFFICE: 1990-0-262-925 (35055).
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:
Subject
“Whomever” [email protected]
[email protected]
DA Form 2028
1. From: Joe Smith
2. Unit: home
3. Address: 4300 Park
4. City: Hometown
5. St: MO
6. Zip: 77777
7. Date Sent: 19-OCT-93
8. Pub no: 55-2840-229-23
9. Pub Title: TM
10. Publication Date: 04-JUL-85
11. Change Number: 7
12. Submitter Rank: MSG
13. Submitter FName: Joe
14. Submitter MName: T
15. Submitter LName: 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.
RECOMMENDED CHANGES TO EQUIPMENT TECHNICAL PUBLICATIONS
SOMETHING WRONG
THEN . .JOT DOWN THE
DOPE ABOUT IT ON THIS
FORM, CAREFULLY TEAR
IT OUT, FOLD IT AND
DROP IT IN THE MAIL!
PUBLICATION NUMBER
TM 1--1520--270--13&P
WITH THIS PUBLICATION?
FROM: (PRINT YOUR UNIT’S COMPLETE ADDRESS)
DATE SENT
PUBLICATION DATE
30 December 1998
10 January 1999
PUBLICATION TITLE
Operator’s manual MH60L Helicopter
BE EXACT
PIN--POINT WHERE IT IS IN THIS SPACE, TELL WHAT IS WRONG
AND WHAT SHOULD BE DONE ABOUT IT:
PAGE PARA- FIGURE TABLE
NO
NO
GRAPH
NO
PRINTED NAME, GRADE OR TITLE, AND TELEPHONE NUMBER
DA
FORM
1 JUL 79
2028--2
PREVIOUS EDITIONS
ARE OBSOLETE.
DRSTS-M verprint2, 1 Nov 80
SIGN HERE
P.S.- - IF YOUR OUTFIT WANTS TO KNOW AB OUT Y OUR
RECOMMENDATION, MAKE A CARBON COPY OF THIS
AND GIVE TO YOUR HEADQUARTERS.
RECOMMENDED CHANGES TO EQUIPMENT TECHNICAL PUBLICATIONS
SOMETHING WRONG
THEN . .JOT DOWN THE
DOPE ABOUT IT ON THIS
FORM, CAREFULLY TEAR
IT OUT, FOLD IT AND
DROP IT IN THE MAIL!
PUBLICATION NUMBER
TM 1-1520-270-13&P
WITH THIS PUBLICATION?
FROM: (PRINT YOUR UNIT’S COMPLETE ADDRESS)
DATE SENT
PUBLICATION DATE
30 December 1998
PUBLICATION TITLE
Operator's Manual MH-60L Helicopter
BE EXACT
PIN--POINT WHERE IT IS IN THIS SPACE, TELL WHAT IS WRONG
AND WHAT SHOULD BE DONE ABOUT IT:
PAGE PARA- FIGURE TABLE
NO
NO
GRAPH
NO
PRINTED NAME, GRADE OR TITLE, AND TELEPHONE NUMBER
DA
FORM
1 JUL 79
2028--2
PREVIOUS EDITIONS
ARE OBSOLETE.
DRSTS-M verprint2, 1 Nov 80
SIGN HERE
P.S.- - IF YOUR OUTFIT WANTS TO KNOW AB OUT Y OUR
RECOMMENDATION, MAKE A CARBON COPY OF THIS
AND GIVE TO YOUR HEADQUARTERS.
REVERSE OF DA FORM 2028-2 Reverse of DRSTS-M Overprint 2,
1 Nov 80
FOLD BACK
DEPARTMENT OF THE ARMY
OFFICIAL BUSINESS
COMMANDER
U.S. ARMY AVIATION AND MISSILE COMMAND
ATTN: AMSAM-MMC-MA-NP
REDSTONE ARSENAL, AL 35898-5230
TEAR ALONG PERFORATED LINE
FILL IN YOUR
UNITS ADDRESS
PIN: 022273-006
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