5340-01-212-4808 CLAMP,LOOP Index 9540-01-212-4810 CHANNEL,STRUCTURAL

National Stock Number:
9540-01-212-4809

Federal Supply Class:
9540

National Item Identification Number:
012124809

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:
1MA100D05-1015976301THE BOEING COMPANY
60-876829321TRANSTAR METALS CORP
AMS-QQ-A-200/110U583SAE INTERNATIONAL
NAS342-6280205NATIONAL AEROSPACE STANDARDS COMMITTEE AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA INC NOT FOR RFQ OR SOLICITATION USE
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
QQ-A-200/1181348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASE FLANGE THICKNESS0.313 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.250 INCHES NOMINAL
FIRST TIP STYLESQUARE END
HEAT TREATMENTT-73511 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.313 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 7075
NONDEFINITIVE SPEC/STD DATAT73511 TEMPER
OVERALL HEIGHT2.000 INCHES NOMINAL
OVERALL WIDTH2.500 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL
SPECIFICATION/STANDARD DATA80205-NAS342 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD
WEIGHT PER UNIT MEASURE1.538 POUNDS PER LINEAR FOOT


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