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TO 1-1-700 - Robins Air Force Base

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<strong>TO</strong> 1-1-<strong>700</strong><br />

7.7.1.2.1 Where only partial refinishing (touch-up) is<br />

required for a few small scratches, nicks, or spots where corrosion<br />

was removed on painted surfaces, the following procedure<br />

shall be used:<br />

a. Scuff sand and feather out painted edges and all corroded<br />

or scratched surfaces to be refinished per maintenance<br />

painting and touch-up procedures in Chapter 5 of<br />

<strong>TO</strong> 1-1-8.<br />

b. Clean the entire surface to be touched-up of all dust,<br />

dirt, oil, and grease by solvent wiping per procedures in<br />

Chapter 3 of <strong>TO</strong> 1-1-8 prior to priming. Apply the same<br />

primers noted in paragraph 7.7.1.2 using maintenance<br />

painting and touch-up procedures in Chapter 5 of <strong>TO</strong> 1-<br />

1-8. No topcoat is required.<br />

7.7.2 Aluminum. When complete refinishing is required due<br />

to extensive corrosion or loss of film adhesion, disassemble<br />

the equipment and/or structure as far as practical; and remove<br />

the defective paint system per procedures in Chapter 2 of <strong>TO</strong><br />

1-1-8.<br />

using procedures in <strong>TO</strong> 42C2-1-7. Structures that are<br />

too large to be anodized shall be treated according to the<br />

paragraph below.<br />

MIL-DTL-81706 (ALODINE), COATING, CHEMICAL<br />

CONVERSION 23<br />

b. For both DEPOT and FIELD LEVEL maintenance, surfaces<br />

of repaired/refurbished aluminum alloy parts shall<br />

be treated to repair damaged areas in the anodize coating<br />

due to nicks, scratches, and corrosion removal with<br />

MIL-DTL-81706/MIL-DTL-5541, Class 1A chromate<br />

conversion coating per procedures in Section II of<br />

Chapter 5 in <strong>TO</strong> 1-1-691. For small areas, use MIL-<br />

DTL-81706, Class 1A, Form VI, Method D Touch-N-<br />

Prep (TNP) pens per procedures in Section II of<br />

Chapter 5 in <strong>TO</strong> 1-1-691.<br />

MIL-DTL-81706 (ALODINE), COATING, CHEMICAL<br />

CONVERSION 23<br />

MIL-PRF-23377, TYPE I & II, PRIMER, EPOXY CHEMI-<br />

CAL AND SOLVENT RESISTANT 38<br />

NOTE<br />

The presence of a white powdery oxide formation on<br />

cadmium plated fasteners will not in itself constitute<br />

reason for disassembly or overhaul unless these deposits<br />

interfere with proper operation of equipment. It<br />

will be sufficient to brush off accessible deposits of<br />

oxide with a stiff bristle brush, nonabrasive, and treat<br />

affected surface with MIL-DTL-81706/MIL-DTL-<br />

5541, Class 1A solution while treating the surrounding<br />

aluminum alloy structure.<br />

7.7.2.1 If the surface, when reassembled in its normal operating<br />

condition will be exposed to direct view, the following<br />

procedure shall be used:<br />

a. For DEPOT LEVEL maintenance only new/replacement<br />

aluminum alloy parts shall be anodized per MIL-A-<br />

8625, Type II, Class I (dichromate or duplex sealed)<br />

MIL-PRF-85582, PRIMER, EPOXY, WATERBORNE 69<br />

MIL-P-53030, PRIMER, EPOXY, WATER REDUCIBLE,<br />

LEAD, CHROME FREE 35<br />

c. Properly prepare the surface by solvent wiping per procedures<br />

in Chapter 3 of <strong>TO</strong> 1-1-8. Apply one coat of<br />

MIL-PRF-23377, Type I, Class C (solvent type), MIL-<br />

PRF-85582, Type I, Class C2 (waterborne) epoxy<br />

primer, or MIL-P-53030 (waterborne) epoxy primer to a<br />

DFT of 0.6 and 0.9 mils (0.0006 to 0.0009 inch). Application<br />

shall be per procedures in Chapters 4, 5, and 6 of<br />

<strong>TO</strong> 1-1-8.<br />

Change 1 7-27

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