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Page Title:
Section II. DESCRIPTION AND DATA |
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  TM 55-1730-229-12
TO 35C2-3-473-1
of this equipment. Marine Corps
TO PREVENT ENEMY USE. Army and
personnel shall refer to MCO P4450.7.
Marine Corp personnel shall refer to
TM 750-244-3 as a source for
procedures for the destruction of
STORAGE.
material to prevent enemy use.
a. (A) Army refer to TB 740-97-
1-7. (A,F,MC) ADMISISTRATIVE
2 and TM 1-1500-204-23 (Series).
STORAGE. Army personnel shall refer
b. (F) Air Force - Refer to TO
to TM 1-1500-204-23 (Series) General
35-1-4 for the end item Generator
Aircraft Maintenance Manual for
Sets and to TO 38-1-5 for installed
procedures for storage of this
engine.
equipment. Air Force personnel shall
refer to TO 35-1-4, Processing and
c. (N, MC) Navy and Marine
Inspection of Aerospace Ground
Corps refer to individual service
Equipment, for storage and shipment
directives for requirements.
Section II. DESCRIPTION AND DATA
Control and regulation of the AGPU
electrical and pneumatic systems is
a. General. The Aviation
semi-automatic. Electronic devices
Ground Power Unit (AGPU) P/N 83-360A
monitor and regulate electrical
and P/N 83-360D is a gas turbine
voltage, frequency, and current; as
engine-driven, wheel mounted, self-
well as pneumatic outputs. Control
propelled (up to 3 mpg on flat
of the hydraulic system is semi-
surface), enclosed unit. The AGPU
automatic, in that the operator must
can be towed (20 mph maximum), and is
set hydraulic pressure, and select
air transportable. The AGPU provides
operating modes.
ac/dc electrical, hydraulic, and
b. Exterior Features. A view
pneumatic power. The power is
of the AGPU from the right rear is
available individually, or in any
combination. The AGPU provides the
1-5 show interior views with the rear
ground power requirements for
and right side access doors open.
aircraft such as the following:
Fig. 1-6 shows a view of the left
AH-1, AH-64, C-12, CH-47, OH-6, OH-
front.
58, OV-1, U-21, UN-1, UH-60.
Change 8
1-2.1/(1-2.2 blank)
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