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 11<br />
CORROSION REMOVAL<br />
11.1 GENERAL.<br />
This chapter covers procedures for corrosion removal and surface<br />
treatment. When corrosion is detected, a specific and<br />
immediate corrective action is required. Each type of corrosion<br />
has its own peculiarities and requires special treatment.<br />
Complete treatment involves a thorough inspection of all corroded<br />
areas and evaluation of the corrosion damage (refer to<br />
Chapter 9 of this manual), paint removal per <strong>TO</strong> 1-1-8, corrosion<br />
removal per this chapter and <strong>TO</strong> 1-1-691, application of<br />
chemical surface treatments per this chapter, sealing (refer to<br />
Chapter 12 of this manual), and application/touch-up of protective<br />
paint finishes per <strong>TO</strong> 1-1-8 and Chapter 7 of this manual.<br />
11.1.1 Training. Personnel assigned to perform corrosion<br />
removal corrective maintenance tasks shall be specially<br />
trained in the use of chemical paint removers specified in <strong>TO</strong><br />
1-1-8; abrasive materials, powered and hand tools, depth and<br />
area measurement of metal removed outlined in this chapter<br />
and in <strong>TO</strong> 1-1-691; and determination of damage limits from<br />
the applicable system specific maintenance manuals. Inadequate<br />
training will lead to further damage of equipment and<br />
poses a safety hazard to the individual.<br />
11.1.2 Corrosion Risk. Parts including housings, covers,<br />
supports, brackets, cabinets, and chassis are required for structural<br />
support and mounting bases for electrical and electronic<br />
components. Corrosion on these parts should be treated as<br />
soon as possible to eliminate long term deterioration. Severe<br />
corrosion usually results from coating failure caused by handling<br />
or environmental exposure and subsequent attack of<br />
exposed metal. The corrosion attack is caused by exposure to<br />
elements such as moisture, corrosive deposits, and/or microbial<br />
contamination.<br />
11.1.3 Maintenance Level. Major repairs should be performed<br />
at Depot Level maintenance. Preventive maintenance,<br />
corrosion control, and touchup procedures should be accomplished<br />
at the Intermediate Level maintenance and/or Organizational/Unit<br />
Level maintenance.<br />
11.2 CORRECTIVE ACTIONS.<br />
Corrective maintenance depends on: the type of surface<br />
involved (metallic or composite); the area of the damaged surface<br />
(small corrosion spot or large corroded area); and the<br />
degree of corrosion, as determined per Chapter 9 of this manual.<br />
11.2.1 Exposure. Composite materials, such as fiberglass or<br />
graphite/boron epoxy matrix structures, shall not be exposed<br />
to chemical paint removers, but shall only be scuff sanded to<br />
the primer coat.<br />
11.2.2 Mechanical Procedures. Since composite materials<br />
do not corrode, corrosion removal techniques are not applicable<br />
and shall not be used. Corrosion shall always be removed<br />
by the mildest effective technique. For mechanical procedures<br />
specific to the various metal alloys, refer to Table 11-1 and<br />
Table 11-2.<br />
11.3 CORROSION REMOVAL METHODS.<br />
Corrosion can be removed by either mechanical or chemical<br />
methods. Certain factors must be considered prior to starting<br />
any corrosion removal operation. The most important factor to<br />
consider is that corrosion products must be removed completely<br />
without causing additional damage to the structure during<br />
the process. This can be accomplished by first removing<br />
all corrosion visible through a 10X magnifying glass, then<br />
removing an additional two mils (0.0020 inch) to ensure that<br />
all deposits have been eliminated. Failure to remove all corrosion<br />
allows the corrosion to continue even after affected surfaces<br />
are refinished. Additional factors to consider are:<br />
a. Before attempting to remove corrosion products, strip<br />
the paint from the area to be worked and clean contaminants<br />
from the surface. Surface contaminants and paint<br />
interfere with corrosion removal procedures and make<br />
the operation more difficult.<br />
b. Protect adjacent components and parts from corrosion<br />
residue and possible damage that could be caused by the<br />
removal operation. Corrosion residue can cause additional<br />
corrosion and damage the surface finish of the<br />
surrounding area. An accidental slip of a corrosion<br />
removal tool can quickly result in additional damage.<br />
c. Prior to corrosion removal, determine the allowable limits<br />
from the system specific equipment manuals and/or<br />
technical orders. When removing corrosion from critical<br />
equipment structure, take the following steps:<br />
(1) If allowable metal removal or damage limits will not<br />
be exceeded, remove corrosion completely. Metal<br />
loss due to corrosion damage is cumulative. Metal<br />
loss from prior corrosion removal operations and<br />
corrosion removal from areas on the opposite side of<br />
a part must be considered when assessing the degree<br />
of corrosion damage.<br />
11-1