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 />
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