TM 1-1500-204-23-1
CHAPTER 10
ARCTIC, DESERT, AND TROPIC MAINTENANCE
10-1.
General.
Arctic,
desert,
and
tropic
maintenance, inspections, and operations are explained
In the following paragraphs.
10-2.
Arctic Maintenance. The following paragraphs
contain the basic principles and procedures which are
essential for efficient utilization of aircraft, equipment,
and personnel in arctic areas. The operation of aircraft
In arctic regions is seriously handicapped because of the
effect
of
the
elements
on
both
personnel
and
equipment. With a decrease in temperature, an
increase In time required to perform duties is inflicted
due to reduced flexibility of packings and rubber parts,
higher viscosity of lubricants, and binding of metal parts
due to contraction. General procedures for all aircraft
are discussed within these paragraphs. For specific
problems on a particular aircraft or piece of equipment,
refer to the applicable maintenance manual.
a.
Precautions. Maintenance personnel shall
observe the following precautions as a guide to
successful performance of duty In severe weather.
(1)
Exercise care when stepping or walking
on snow or frost-covered or very cold surfaces.
Wearing proper shoes will aid In walking on slippery
surfaces and reduce the possibility of injures from
slipping.
(2)
Exercise caution when touching very cold
metal with bare hands, moisture on hands will tend to
freeze skin to metal. When practical, wear gloves and
cover metal tool handles
(3)
Do not exert excessive torque or tension
on bolts, nuts, cables, or similar items when making
repairs on equipment that has been exposed to extreme
cold. These items tend to freeze or snap as metal
expands upon warming.
b.
Preheating. The following paragraphs explain
general procedures for preheating aircraft and engines.
CAUTION
Do not permit air from heaters with
temperature In excess of 251oF
(122oC) to blast against ignition
harness, flexible hose, self-sealing
tanks, or other rubberized or fabric
materials. Damage may otherwise
result.
(1)
Preheat requirements. Engine preheat is
normally required only on reciprocating engines. Jet
engines do not require preheat unless the available
auxiliary power unit is not sufficient to overcome
additional starter loads. Preheat requirements can be
considerably reduced by following proper oil dilution
procedures.
(2)
Preheat for starting . At low temperature,
apply heat to engine as a starting aid. Reduce starter
loads by preheating engine, thereby reducing oil
viscosity. Generally, preheat will not be required If
temperature is above 0°F (-180C) and engine oil has
been properly diluted
(3)
Preheat time. Preheat time required to
prepare an engine for starting depends on outside air
temperature, size of engine, heater output, and velocity
and direction of wind. Also, when oil dilution, method of
preheat application, or use of covers and nose shields
are inefficiently applied, the required preheat time will
be lengthened.
(4)
Preheat application. Apply heat to both
the power and accessory sections until cylinder heat,
temperature reaches 68°F (20°C). Do not rely entirely
upon temperature gauge as readings may be misleading
because of thermocouple being located in path of heater
blast. Where heater supply is limited, concentrate heat
on rear accessory section, particularly main oil drain, oil
lines, and oil sump, with second priority going to nose
gear, propeller hub, and power section.
10-1