14.06.2014 Views

TO 1-1-700 - Robins Air Force Base

TO 1-1-700 - Robins Air Force Base

TO 1-1-700 - Robins Air Force Base

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

<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

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!