WASHER, FLAT,
NATIONAL AEROSPACE STANDARDS COMMITTEE AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA INC NOT FOR RFQ OR SOLICITATION USE | 80205 |
CROSS-SECTIONAL SHAPE STYLE | RECTANGULAR |
HOLE DIAMETER | 0.149 INCHES NOMINAL |
PERIPHERAL SHAPE STYLE | ROUND |
CENTER HOLE SHAPE STYLE | ROUND |
THICKNESS | 0.032 INCHES NOMINAL |
OVERALL DIAMETER | 0.375 INCHES NOMINAL |
III END ITEM IDENTIFICATION | AIRCRAFT,AIRLIFTER C-17A |
MATERIAL | ALUMINUM ALLOY 7075 OVERALL |
MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
SURFACE TREATMENT | ANODIZE OVERALL |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 TYPE II CLASS 2(YELLOW) MIL SPEC SINGLE TREATMENT RESPONSE OVERALL |
A washer having a centrally located hole with a solid or laminated cross-section and two flat parallel bearing surfaces. The hole must be 75 percent or less than the largest dimension and the bearing surface finish is greater than 32 microinch ( .8 micrometer). The thickness cannot exceed 25 percent of the largest outside dimension. When the largest outside dimension is less than 1/4 inch or 6mm, the thickness must be . 6 inches ( .15mm) or greater and for items 1/4 inch (6mm) or larger, the thickness must be . 16 inches ( .4mm) or greater. The maximum tolerance is applied to dimensions and used as a determining factor. Items with separable lamination use SHIM. For items fabricated from ceramic or electrically rated materials by specification or industry standards use INSULATOR (1), WASHER. Excludes DISK, VALVE, graphite impregnated and lubricated items. |