5120-01-233-0619 WRENCH,SOCKET Index 9540-01-233-0621 ANGLE,STRUCTURAL

National Stock Number:
9540-01-233-0620

Federal Supply Class:
9540

National Item Identification Number:
012330620

Description:
ANGLE,STRUCTURAL

Detail:
A STRUCTURAL SHAPE FABRICATED FROM A FERROUS OR NONFERROUS MATERIAL AND RESEMBLING THE LETTER L IN CROSS-SECTIONAL FORM. THE EDGES MAY HAVE A BULB, BE ROUNDED, AND THE INSIDE CORNER MAY HAVE A FILLET.


Manufacturer Information:
10133-120429321TRANSTAR METALS CORP
1MA100D01-1005376301THE BOEING COMPANY
AMS-QQ-A-200/110U583SAE INTERNATIONAL
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AND10133-120499237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
AND10133-1204-7075-099237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.188 INCHES NOMINAL
FABRICATION METHODROLLED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.188 INCHES NOMINAL
FIRST TIP RADIUS0.188 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTO-ANNEALED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.188 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT1.250 INCHES NOMINAL
OVERALL WIDTH1.250 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 7075
NONDEFINITIVE SPEC/STD DATAO TEMPER
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP RADIUS0.188 INCHES NOMINAL
SECOND TIP STYLELEFT QUARTER RADIUS
SPECIFICATION/STANDARD DATA76301-1MA100 MANUFACTURERS STANDARD
WEIGHT PER UNIT MEASURE0.512 POUNDS PER LINEAR FOOT


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