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National Stock Number:
5340-01-250-1311
Federal Supply Class:
5340
National Item Identification Number:
012501311
Description:
BRACKET,DOUBLE ANGLE
Detail:
A rigid item usually fabricated from flat material, forming two alternate or two adjacent interior angles, both which are less than 180 degrees (3.141 radians). It is designed to position, align, and/or support an item. It may be reinforced. See also BRACKET, ANGLE and BRACKET (1), MOUNTING.
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Manufacturer Information:
| 7-311B25171-9 | 02731 | MCDONNELL DOUGLAS HELICOPTER CO INC | | 7-311B25171-9 | 8V613 | THE BOEING COMPANY |
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Techincal Specification:
| CENTER SECTION HEIGHT | 2.900 INCHES NOMINAL | | CENTER SECTION THICKNESS | 0.100 INCHES NOMINAL | | CENTER SECTION WIDTH | 4.310 INCHES NOMINAL | | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.500 INCHES NOMINAL | | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.310 INCHES NOMINAL | | FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE | | FIRST LEG ANGLE | 90.0 DEGREES NOMINAL | | FIRST LEG CORNER RADIUS | 0.120 INCHES NOMINAL | | FIRST LEG STYLE | CORNER RADIUS | | FIRST LEG THICKNESS | 0.100 INCHES NOMINAL | | FIRST LEG HOLE DIAMETER | 0.201 INCHES NOMINAL | | FIRST LEG LENGTH | 1.560 INCHES NOMINAL | | FIRST LEG WIDTH | 2.150 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/11,T4 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 6061 | | SECOND LEG ANGLE | 90.0 DEGREES NOMINAL | | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL | | SECOND LEG THICKNESS | 0.100 INCHES NOMINAL | | SECOND LEG LENGTH | 1.800 INCHES NOMINAL | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625,TYPE 3 MIL SPEC SINGLE TREATMENT RESPONSE | | SURFACE TREATMENT | ANODIZE |
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