MIL-C-7460 Revision A:1971
Withdrawn
Withdrawn
Chromium Plating, Porous Channel Type, Aircraft Engine Cylinders, General Specification for (No S/S Document)
Available format(s)
PDF
Published date
02-04-1971
Publisher
Withdrawn date
03-19-1993
US$20.00
Excluding Tax where applicable
Covers requirements for chromium plating the cylinder bore of aircraft engine cylinders.
| DocumentType |
Standard
|
| Pages |
15
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL-STD-1516 Revision B:1990 | Unified Code for Coating and Finishes for DOD Materiel (No S/S Document) |
| MIL C 16173 : E | CORROSION PREVENTIVE COMPOUND, SOLVENT CUTBACK, COLD APPLICATION |
| TT-E-489 Revision J:1994 | Enamel, Alkyd, Gloss, Low VOC Content (See Notice 2 for Replacement Information) |
| TT-V-109 Revision C:1978 | VARNISH, INTERIOR, ALKYD-RESIN (S/S BY A-A-1788) |
| TT-N-97 Revision D:2007 | Naphtha; Aromatic |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
Summarise
US$20.00
Excluding Tax where applicable
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