9540-01-233-0622 ANGLE,STRUCTURAL Index 9540-01-233-0624 ANGLE,STRUCTURAL

National Stock Number:
9540-01-233-0623

Federal Supply Class:
9540

National Item Identification Number:
012330623

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:
1MA100D01-1010476301THE BOEING COMPANY
60-174829321TRANSTAR METALS CORP
8315101634ALUMINUM CO OF AMERICA
AMS-QQ-A-200/110U583SAE INTERNATIONAL
NAS341-1680205NATIONAL AEROSPACE STANDARDS COMMITTEE AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA INC NOT FOR RFQ OR SOLICITATION USE
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
PA1733106012TRANSTAR METALS CORP
NAS341-16-7075-080205NATIONAL AEROSPACE STANDARDS COMMITTEE AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA INC NOT FOR RFQ OR SOLICITATION USE
QQ-A-200/1181348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.313 INCHES NOMINAL
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.250 INCHES NOMINAL
FIRST TIP RADIUS0.313 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTO-ANNEALED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.313 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT1.750 INCHES NOMINAL
OVERALL WIDTH1.750 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 RADIUS0.313 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
SPECIFICATION/STANDARD DATA76301-1MA100 MANUFACTURERS STANDARD
WEIGHT PER UNIT MEASURE1.163 POUNDS PER LINEAR FOOT


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