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TM 55-3805-261-14
CHAPTER 4
AIR TRANSPORTABILITY GUIDANCE
points on the vehicle, the corresponding fittings to which
4-1. Scope
the devices are secured, the number and capacity of
This chapter provides air transportability guidance for
devices, and the wood shoring required for loading and
movement of the grader, road, motorized, DED, heavy,
securing the vehicle on C-130, C-141, and C-5 aircraft.
CCE. It covers technical and physical characteristics,
The minimum acceptable restraint factors (g loads) are
as well as safety considerations, and prescribes the
identified In the applicable TO 1C -xxx-9's.
manpower, materials, and time required to prepare,
c. Loadmaster Responsibilities. The load master
load, and tie down the vehicle on, or unload the vehicle
will ensure that the vehicle is loaded and secured in
from, US Air Force cargo aircraft.
accordance with in the applicable TO 1C-xxx-9.
4-2. Maximum Utilization of Aircraft
4-4. Safety
The loads described in this section are not maximum
In addition to the safety precautions contained in
loads.
Additional cargo and/or personnel within
chapter 3, the following procedures should be noted:
allowable load limits and restrictions prescribed by
a. The vehicle fuel tanks must not be more than
pertinent safety regulations can be transported.
one quarter full.
b. The vehicle must be tied down in accordance
4-3. Applicability
with this manual and the applicable TO 1C-xxx-9 for
a.  US Air Force Aircraft.  The CCE grader is
each particular aircraft.
transportable in the C-130, C-141, and C-6 aircraft.
c.  Each vehicle or component must be checked
Procedures in this manual and those prescribed in the
carefully to ensure that all loose items are properly
Air Force loading instructions, technical orders (TO) IC-
secured.
xxx-9 series, are applicable to each aircraft.
d. Ground guides must be used when the vehicle is
b.
Tiedown.
The graders are tied down in
loaded in or unloaded off the aircraft.
accordance with the applicable TO [C-xxx-9, section IV.
e.  Fire extinguishers must be readily available
Suggested tiedown patterns are shown in figures 4-1
during all loading or unloading operations.
through 4-3. Tables 4-1 through 4-4 show the tiedown
devices required, the location of the tiedown
Table 4-1. Tiedown data for the Model 1 30G Type I or II
Grader in US Air Force C-130Aircraft (Fig. 4-1)
4-1

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