TO 1-1-700 - Robins Air Force Base
TO 1-1-700 - Robins Air Force Base
TO 1-1-700 - Robins Air Force Base
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<strong>TO</strong> 1-1-<strong>700</strong><br />
CHAPTER 10<br />
CORROSION PRONE AREAS<br />
10.1 COMMON AREAS.<br />
There are certain corrosion prone areas common to shelters,<br />
vans, radomes, and C-E-M equipment. Corrosion prone areas<br />
should be cleaned, inspected, and treated more frequently than<br />
less corrosion prone areas. The following paragraphs describe<br />
the areas and contain illustrations to aid in inspections. However,<br />
the list is not complete and should be expanded by referring<br />
to the equipment system specific maintenance manuals<br />
and maintenance inspection cards for each specific piece of C-<br />
E-M equipment, shelter, or radome that show other possible<br />
trouble spots.<br />
10.2 DISSIMILAR METALS.<br />
When two dissimilar metals make electrical contact in the<br />
presence of an electrolyte, which metal will corrode and the<br />
rate at which corrosion occurs depends on the difference in<br />
their activities, that is, their positions in Figure 3-16 of Chapter<br />
3 of this manual. The higher a metal is in this table and the<br />
greater the difference in activity between the two metals, the<br />
faster corrosion occurs. For example, magnesium would corrode<br />
very quickly when coupled with gold in a humid atmosphere.<br />
But aluminum would corrode very slowly, if at all, in<br />
contact with cadmium. A flashlight battery (or dry cell) is an<br />
example of galvanic corrosion put to practical use. A zinc<br />
battery casing steadily corrodes supplying a steady flow of<br />
electrons, but only when the switch is closed. When the switch<br />
is open, there is no corrosion because electrons are not able to<br />
leave the zinc anode. Pay particular attention to dissimilar<br />
metal joints for signs of galvanic corrosion (see Figure 10-1).<br />
C-E-M equipment, shelters, and radomes usually contain dissimilar<br />
metals. The use of dissimilar metals in the selection of<br />
materials and hardware i.e., screws, washers, and nuts, should<br />
be eliminated wherever possible. Where contact between dissimilar<br />
metals cannot be avoided, the choice of contacting<br />
material and associated hardware material is important. Materials<br />
should be chosen such that the part most prone to corrode<br />
(anode) is the easiest and least expensive to replace. At bimetallic<br />
junctions, where finishes are removed to provide good<br />
electrical connection, a protective finish/sealant shall be reapplied<br />
to the completed connection after it is made to prevent<br />
corrosion. Attaching parts, such as nuts (standard, speed, and<br />
self-locking), bushings, spacers, washers, screws (standard<br />
and self-tapping), sleeves for shake-proof fastener studs,<br />
clamps, bolts, etc., do not need to be painted in detail except<br />
when dissimilar metal or wood contact is involved with the<br />
materials being joined or exposure to a corrosive interior environment<br />
or the exterior environment will occur in service.<br />
However, all parts shall be installed wet with sealant.<br />
10.3 FASTENERS.<br />
There are hundreds of fasteners on/in C-E-M equipment and<br />
shelter and radome surfaces, and areas around these fasteners<br />
are trouble spots. These areas are subject to operational loads<br />
and/or moisture intrusion which make the skin material highly<br />
susceptible to corrosion at fastener locations (see Figure 10-2).<br />
Equipment installation, shipping, or setup strains cause paint<br />
to crack around the fasteners which provides a path for corrosive<br />
materials to enter the joint between fastener heads and<br />
skin panels. Any paint that is not highly flexible will crack to<br />
some degree around fasteners. Fasteners should be installed<br />
using a corrosive preventative compound, bonding agent, or<br />
sealant to prevent corrosion between itself and the attaching<br />
structure (see Figure 10-3). See Chapter 4 of <strong>TO</strong> 35E4-1-162<br />
and Chapter 12 of this manual for sealant application.<br />
Figure 10-1. Galvanic Corrosion Adjacent To Steel Fasteners<br />
10-1