Bill of Materials for Blocking and Tiedown of the SEE, HME, and HMMH on the M345 Trailer (Fig 5-1)
Application of Materials for Blocking and Tiedown of the SEE, HME, and HMMH on the M345 Trailer
This manual provides transportability guidance for
logistical handling and movement of the small
emplacement excavator (SEE), high mobility entrencher (HME), and high mobility material handler (HMMH). It contains information considered
appropriate for safe transport of the SEE and its
variants. The information includes significant
technical and physical characteristics, as well as
safety considerations,
movement by the various transport modes. Where
considered necessary, metric equivalents appear in
parentheses following the dimensions or other
measurements. This manual is for transportation
officers and other personnel responsible for moving
the SEE, HME, and HMMH, or for providing
transport services.
required for worldwide
1-2. Reporting of Recommendations
and Comments
Users of this manual are encouraged to submit
comments and to recommend changes for its im-
provement.Comments and recommendations
should be prepared on DA Form 2028 (Recommended Changes to DA Publications and Blank
Forms) and forwarded to Commander, Military
Traffic Management Command Transportation Engineering Agency, ATTN: MTTE-TRS, PO Box
6276, Newport News, VA 23606–0276. Electrically
transmitted messages should be addressed
MTMCTEA FT EUSTIS VA//MTTE-TRS//.
1-3. Definitions of Warnings,
to CDR
Cau-
tions, and Notes
Throughout this manual, warnings, cautions, and
notes emphasize important or critical guidance.
They are used for the following conditions:
a. Warning. Instructions that, if not followed,
could result in injury to or death of personnel.
b. Caution. Instructions that, if not strictly observed, could result in damage to or destruction of
equipment.
c. Note. An operating procedure or condition
that must be emphasized.
1-1
CHAPTER 2
TRANSPORTABILITY DATA
Section I. GENERAL
TM 55-2420-224-14
2-1. Scope
This chapter provides transportability characteris-
tics of the SEE, HME, and HMMH.
2-2. Description
The SEE, HME, and HMMH are commercial items
of construction equipment. The tractor portion of
the equipment is a light truck chassis equipped
with a diesel engine, multispeed range transmission, and offroad flotation tires. The tractor has a
45-mile-per-hour (72-km/h) highway convoy speed
as well as a full drive rough-terrain capability.
a. The SEE tractor configuration consists of the
basic tractor with a 3/4-cubic-yard-capacity front
end loader and rear-mounted backhoe. The backhoe has a 7-cubic-foot-capacity bucket, as shown in
figure 2-1.
b. The HME variant consists of the same basic
tractor as the SEE, but with a dozer blade (85
inches wide and 32 inches high) on the front end
and an entrencher on the rear. No photograph is
available at this time.
c. The HMMH variant consists of the same
basic tractor as the SEE, but with a 4,000-pound
(1814-kg)-capacity forklift mounted to the front
and a 6,000 pound (2722-kg)-capacity crane at-
tached to the rear of the vehicle, as shown in
figure 2-2.
2-3. Transportability Drawings
Figures 2-3 through 2-5 are detailed side- and
rear-view transportability drawings of the SEE,
HME, and HMMH with dimensions, tiedown and
lifting provisions, and load-rating capacities.
2-1
2-2
TM 55-2420-224-14
Figure 2-1.
TM 55-2420-224-14
2-3
Figure 2-2.
2-4
TM 55-2420-224-14
Figure 2-3.
2-5
TM 55-2420-224-14
Figure 2-4.
2-6
TM 55-2420-224-14
Figure 2-5.
TM 55-2420-224-14
Section II. CHARACTERISTICS AND RELATED DATA
2-4. General Transportability Characteristics
Data contained here apply to the model numbers or national stock numbers (NSN) shown. Changes in
model numbers or NSN may affect the loadability of the item as related to the guidance in this manual.
Lower cost shipping can be obtained by reducing
each SEE, HME, and HMMH to its minimum
dimensions for terminal handling and ocean transport. Both side mirrors are to be folded in, and the
rear-mounted attachment is placed in the travel
position.
2-6. Unusual Characteristics
These vehicles have no unusual characteristics
that would require special attention be given to
temperature,
atmospheric pressure, or humidity
variations during their exposure to normal transportation environments.
2-7. Hazardous and Dangerous Characteristics
Under usual circumstances, the SEE, HME, and
HMMH will not present any hazardous or dangerous characteristics during exposure to normal
transportation environments.
NOTE
Those regulations and/or transportation
procedures normally associated with vehicles containing diesel fuel apply.
2-8
CHAPTER 3
SAFETY
TM 55-2420-224-14
3-1. General
General safety considerations and precautions for
movement are as follows:
a. Check each vehicle to ensure that all loose
items are properly secured.
b. When backing a vehicle, ensure that no
personnel or obstacles are in danger of being hurt
or damaged by the vehicle.
WARNING
Fire extinguishers must be readily available during all loading and unloading
operations.
WARNING
When vehicle engine is operating, provide
proper ventilation during loading and unloading operations.
of carbon monoxide fumes could be fatal.
Prolonged inhalation
3-2. Specific Safety Requirements
Appropriate chapters of this manual contain pertinent safety requirements by individual mode.
3-1
TM 55-2420-224-14
CHAPTER 4
AIR TRANSPORTABILITY GUIDANCE
4-1. Scope
This chapter provides air transportability guidance
for movement of the SEE, HME, and HMMH. It
covers significant technical and physical characteristics and safety considerations. Also, it prescribes
the materials required to prepare, load, and un-
load the SEE, HME, and HMMH when transported in the C–130, C–141, and C–5 US Air Force
aircraft and the Boeing 747 Civil Reserve Air
Fleet (CRAF) aircraft.
4-2. Maximum Use of Aircraft Capacity
Additional cargo, including personnel within allowable load limits and restrictions prescribed by
pertinent safety regulations, may be transported
with these vehicles on US Air Force aircraft.
4-3. Applicability
a. US Air Force Aircraft. When prepared for
loading as described in paragraph 4-5, the SEE,
HME, and HMMH are transportable in C-130,
C-141, and C-5 aircraft.
b. Tiedown Devices.
HMMH will be tied down according to section IV
of applicable procedures in TO 1C-XXX–9.
c. Loadmaster. The loadmaster will ensure that
the loaded equipment is secured according to
restraint criteria outlined in TO 1C–XXX–9.
Air Force aircraft loads in this manual
are illustrated to a minimum restraint of
3 g forward, 1.5 g aft, 1.5 g lateral and 2
g vertical. (Reference 1C-XXX-9 and
MIL-STD-1791.)
The SEE, HME, and
NOTE
4-4. Safety
In addition to safety precautions
chapter 3, the following precautions
SEE, HME, and HMMH:
a. Ensure that the fuel tanks are
one-fourth or more than three-fourths full.
b. Check each vehicle carefully to ensure that
all loose items are properly secured.
c. Check each vehicle to ensure there are no
fluid leaks.
d. Check all tiedown provisions and attached
structural members for any damage.
e. Check tire pressure to ensure tires are at
recommended highway pressure.
contained in
apply for the
not less than
f. Check batteries to ensure they are protected
against short circuits and secured so that leakage
of acid cannot occur (reference TM 38–250, para
8-47a). Also, check the fuel tanks and hydraulic
systems to ensure they comply with TM 38–250.
WARNING
Fire extinguishers must be readily available during all loading and unloading.
WARNING
Provide proper ventilation during loading.
Prolonged inhalation of exhaust fumes
could be fatal.
WARNING
Do not allow the vehicle to exceed 3 miles
per hour (walking speed) inside the aircraft or on the loading ramps.
4-5. Preparation of Equipment
a. Fold both mirrors and secure them with rope
to the roll over protection structure (ROPS).
b. Secure rear attachments with 1/2-inch wire
rope (safety cable) and two clips, when shipped in
the travel position.
tight) around the ROPS (or tiedown provision as
directed) and rear attachment to restrain the
attachment in case the mechanical lock is not
engaged or fails.
Install wire rope taut (not
4-6. Transport by US Aircraft
a. The SEE, when shipped in C–130 and C–141
aircraft, will have the backhoe attachment in the
operational configuration. The SEE should be
backed into the C-130 and C-141 aircraft using
two qualified operators. One driver operates the
tractor and the other operates the backhoe, adjust-
ing height during loading and unloading opera-
tions. Each SEE requires two stacks of parking
shoring (2 x 6 inches x 4 feet, two per stack)
between the front end loader and the aircraft floor.
Also, place two stacks of shoring (2 x 6 inches x 4
feet, two per stack) under lowered bucket and
aircraft floor.
b. The HME and HMMH, when shipped in
C–130 and C–141 aircraft, must be in the travel
configuration.
(1) HME. Install 1/2-inch wire rope (safety
cable) through ROPS and over entrenched attach-
ment, forming a loop. Secure the loop by pulling
and installing the wire rope taut (not tight) with
two 1/2-inch clips. Each HME requires two stacks
4-1
TM 55-2420-224-14
of parking shoring (2 x 6 inches x 4 feet, two per
stack) between the front dozer blade and the
aircraft floor.
(2) HMMH. Install 1/2-inch wire rope (safety
cable) around top crane arm and through left
center tiedown provision on chassis, forming a
loop. Secure the loop by pulling the wire rope taut
(not tight) and installing two 1/2-inch clips. Repeat
same procedure for right side, except loop wire
rope through right provision on chassis. Each
HMMH requires two stacks of parking shoring (2
x 6 inches x 5 feet, two per stack) between the
front forklift tines and the aircraft floor. Also the
rear outriggers are to be secured with 1/2-inch
wire rope (safety cable) looped around each outrigger and secured with two 1/2-inch clips.
c. The C–5 aircraft can transport the SEE,
HME, and HMMH in the travel configurations.
(1) SEE. Install 1/2-inch wire rope (safety
cable) taut (not tight) around the ROPS and the
backhoe attachment and secure with two 1/2-inch
clips. Also, install on right outrigger a 1/2-inch
wire rope (safety cable) taut (not tight) through the
bucket tiedown provisional and around outriggers.
Repeat procedures for left outrigger. Each SEE
requires two stacks of parking shoring (2 x 6
inches x 4 feet, two per stack) between the front
end loader and the aircraft floor.
(2) HME and HMMH. To transport the HME
and HMMH in the C–5 aircraft, follow the same
procedures in paragraph 4-6b.
d. The shoring is required to protect the aircraft
floor and any downward motion of the front or
rear implements on the aircraft floor.
e. All shoring material will be furnished by the
shipper and installed as directed by the aircraft
loadmaster.
f. The aircraft commander or his/her representa-
tive ensures that the vehicles are loaded/unloaded
and properly secured in the aircraft according to
the criteria in section IV of the appropriate technical order.
g. Typical tiedown diagrams (figs 4-1 through
4–3) are based on acceptable methods. They can be
used as a guide for loading and securing the SEE,
HME, and HMMH aboard aircraft and also for
preparing a vehicle for air transport. The tiedowns
are part of the aircraft equipment.
4-7. Transport by LVAD and LAPE
The SEE is certified for low altitude parachute
extraction (LAPE) from US Air Force C–130 aircraft and certified for low velocity airdrop (LVAD)
from US Air Force C-130 and C-141 aircraft.
Preparation and procedures for LAPE and LVAD
airdrops are described in FM 10–539 and TO
13C7-1-17.
4-8. Helicopter Transport
The SEE is within the external lift capability of
the CH–47D helicopter in either single-hook (fig
4–3) or dual-hook (fig 4–4) configuration at airspeeds of 100 knots. The load is also suitable for
external transport by the CH–54 helicopter (fig
4-5) at airspeeds of 95 knots.
(1) Ensure that the front end loader assembly
travel locks at the ends of both front end loader
boom cylinders are properly pinned in place.
(2) Secure steering wheel, doors, and all loose
equipment with cord and tape as necessary.
(3) Fold side mirrors inboard and tie or tape
as required.
(4) Tape windshield wipers to windshield.
(5) Securely tie and tape engine compartment
hood.
(6) Tie or tape the hydraulic lines and hoses
close to the forward lifting provisions to prevent
possible entanglement during hookup.
c. Rigging Procedures.
(1) Place apex fitting on top of the falling
object protection system (FOPS). Route the outer
sling legs (1 and 2) to the front of the SEE and the
inner sling legs (3 and 4) to the rear of the SEE.
NOTE
Sling legs 1 and 3 should be the same side
of the load.
(2) Loop the chain ends of sling legs 1 and 2
through the respective front lifting provisions, and
insert link 3 into the grabhook. Wrap a felt sheet
around the chain ends of the sling legs and secure
with tape or nylon cord (fig 4–7).
(3) Loop the chain end of sling leg 3 through
the right rear lifting provision (closest to the
backhoe bucket) and insert link 10 into the grabhook. Wrap a felt sheet (cushioning material)
around the chain end of
with tape or nylon cord.
links (fig 4-8).
the sling leg and secure
Tape or tie excess chain
4-2
4-3
TM 55-2420-224-14
Figure 4-1.
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