9540-01-233-0625 ANGLE,STRUCTURAL Index 9540-01-233-0627 ANGLE,STRUCTURAL

National Stock Number:
9540-01-233-0626

Federal Supply Class:
9540

National Item Identification Number:
012330626

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:
10133-050229321TRANSTAR METALS CORP
1MA100D01-1000476301THE BOEING COMPANY
AMS-QQ-A-200/110U583SAE INTERNATIONAL
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS10133-050281343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AND10133-050299237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
SAE AMS101330U583SAE INTERNATIONAL
SAE AMS10133-05020U583SAE INTERNATIONAL
SAE AMS10133-050281343SOCIETY OF AUTOMOTIVE ENGINEERS INC
SAE AMS1013381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
QQ-A-200/1181348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
AND10133-0502-7075-099237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.078 INCHES NOMINAL
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.094 INCHES NOMINAL
FIRST TIP RADIUS0.078 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTO-ANNEALED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.078 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT0.625 INCHES NOMINAL
OVERALL WIDTH0.625 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 RADIUS0.078 INCHES NOMINAL
SECOND TIP STYLEUPPER RADIUS
SPECIFICATION/STANDARD DATA81343-SAE AMS10133 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD
WEIGHT PER UNIT MEASURE0.108 POUNDS PER LINEAR FOOT


Click here to Register for Free 30-day Trial