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TM 55-5811-900-14
CHAPTER 4
AIR TRANSPORTABILITY GUIDANCE
Section I. GENERAL
up to one-half full when shipped either attached to
4-1. Scope
or separated from the carrier.
This chapter provides air transportability guidance for
movement of the Trailblazer/Tacjam System. Examples
c. The required number of tiedowns plus their
of tiedown diagrams and tiedown data for loading this
capacity must be checked and the criteria for gravity
system into US Air Force C-5 and C-141 aircraft are
forces must be adhered to.
presented in this chapter, as well as tiedown diagrams
d. The carrier must be restrained for air transport
and tiedown data for loading this system externally on
in accordance with the applicable procedures in section
US helicopters.
IV of Air Force TO 1C-5A-9 and TO 1C141B-9.
Procedures outlined in these manuals are for general
4-2. Maximum Utilization of Aircraft
guidance.
Additional cargo, including nuclear weapons and/ or
personnel, within allowable load limits and restrictions as
WARNING
prescribed by pertinent safety regulations (app), can be
Fire extinguishers must be readily available
transported with the Trailblazer/Tacjam system in US Air
during all loading and unloading operations.
Force aircraft.
WARNING
4-3. Safety
Proper ventilation must be provided when
In addition to the safety precautions contained in
loading and unloading.
Prolonged
inhalation of carbon monoxide fumes may
a. The activity offering the vehicles or items for air
be fatal.
transport will notify the aircraft commander or his
representative when ammunition or explosives are to be
CAUTION
transported within a system.
Do not allow carriers to exceed 3 miles per
b. The vehicle fuel tanks must not be more
hour (walking speed) on the loading ramps
or inside the aircraft.
than three-fourths full; the trailer tanks may be
Section II. TRANSPORT BY US AIR FORCE AIRCRAFT
4-4. General
rows of shoring 24 inches wide and spaced to match the
carrier tracks. Loaded height of the carrier may be
a. The Trailblazer/Tacjam systems in the reduced
reduced slightly by use of or 1/2-inch plywood shoring
configuration (shelter removed from carrier) are
instead of 2 X 12-inch lumber. Shoring must be laid
transportable by the C-5, and C-141 aircraft.
from the ground end of the aircraft ramp extension into
b. The aircraft commander or his representative is
the cargo compartment so that, when the carrier is in the
responsible for insuring that the system described is
tiedown position, the tracks are on the shoring. Shoring
loaded or offloaded and properly secured in the aircraft
is provided by the transporting unit or activity.
in accordance with the criteria in section IV of TO 1C-
Trailblazer/Tacjam system components are loaded as
5A-9 and TO 1C-141B9, as applicable.
shown in figures 4-1 through 4-5 and tables 4-1 through
c. Metal parts of the carrier tracks must not make
contact with the aircraft loading ramp or cargo
d. Clearance of the shelters in a C-141 aircraft is
compartment floor. The use of shoring is always
shown in figure 4-6. A K-loader or similar device should
required when the carrier is loaded and offloaded. Two
be used for loading the shelters.
by twelve-inch lumber must be used to provide two
4-1
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