TM 1-1520-240-10
6-5-1
SECTION V. MISSION EQUIPMENT
6-5-1. Mission Equipment.
CH-47D mission equipment includes the M-24 armament
subsystem, the M-41 armament subsystem,either
the M-130 flare dispenser system, AN/ALE-47 Counter-
Measures Dispenser System (MDS), AN/ALQ-156 missile
detector system, the cargo handling systems, the
cargo hooks and the static line retriever. The cargo handling
systems, (except HICHS) the cargo hooks, and the
static line retriever are included in the basic weight of the
helicopter or are listed on the chart C for the particular
helicopter. Figure 6-5-1 lists the weight and the moment/
1,000 for the M-24 armament subsystem, the
M-130 flare dispenser systems and the AN/ALE-47
CMDS. If spare ammunition containers are carried on a
particular mission, compute the moment/1,000 for each
spare container from the cargo moments chart. Figure
6-6-5 provides the weight and moments charts for internal
cargo, figure 6-6-6 charts for external cargo. HICHS
system weight and balance data is provided in table
6-5-2.
6-5-2. EAPS System Weight and Balance.
Table 6-5-1 provides planning data for changes to the
weight and balance with EAPS module/intake screen
removal/installation.
Table 6-5-1 EAPS Module/Engine Screen Weight
and Balance
Item Weight Arm Moment
EAPS Module 266 458 121,828
Fine Mesh Engine
Screens
100 462 46,200
Standard Mesh Engine
Screens
88 462 40,656
Table 6-5-2. Internal Cargo Handling System Weight and Balance
SECTION WEIGHT (LB) ARM MOM/1000
Cabin Section 647 323 208.91
Ramp Section 141 335 75.435
Ramp Extension 51 554 28.254
Ramp Extension Supports
(Stowed)
26 527 13.702
Ramp Support (Stowed) 13 550 7.150
System Totals 878 333.5
System Center of Gravity [379.9]
Table 6-5-3. Engine Air Particle Separator System Weight and Balance
REMOVED WEIGHT ARM MOM/1000
EAPS Filters -266 458 121.828
INSTALLED WEIGHT ARM MOM
Fine Mesh Screens +100 462 46,200
Standards Screens +100 462 40,656
TM 1-1520-240-10
6-5-2
Figure 6-5-1. Mission Equipment Weights and Moments (Sheet 1 of 2)
TM 1-1520-240-10
6-5-3/(6-5-4 blank)
Figure 6-5-1. Mission Equipment Weights and Moments (Sheet 2 of 2)
TM 1-1520-240-10
6-6-1
SECTION VI. CARGO LOADING
6-6-1. General.
This section contains information and instructions for
loading and securing cargo in the helicopter. t lists and
describes the items of equipment incidental to these operations,
instructions for their use, and illustrations where
necessary or desirable. It is not the intent of this section
to teach principles of cargo loading. It is the purpose of
this section to provide detailed information on cargo loading
with regard to this helicopter.
6-6-2. Cargo Compartment.
The cargo compartment (fig. 6-6-1) is 366 inches long, 90
inches wide, and 78 inches high. These dimensions are
uniform through out the cargo compartment, unless the
aircraft is configured with HICHS (fig. 6-6-1). The lower
rescue door is opened for rescue operations, aerial loading,
and external cargo transport operations. A hydraulically
operated door and ramp provide a means for quick
and efficient straight-in loading and unloading.
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