9540-00-261-5107 ANGLE,STRUCTURAL Index 9540-00-261-5117 BEAM,STRUCTURAL

National Stock Number:
9540-00-261-5112

Federal Supply Class:
9540

National Item Identification Number:
002615112

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:
119994618355THE BOEING COMPANY
119994688277THE BOEING COMPANY
139155718355THE BOEING COMPANY
2-13938597LOCKHEED MARTIN CORPORATION
408677783ALCOA/REYNOLDS METALS COMPANY
139155788277THE BOEING COMPANY
734P01634ALUMINUM CO OF AMERICA
AMS-QQ-A-200/110U583SAE INTERNATIONAL
AMS10134-20030U583SAE INTERNATIONAL
AMS10134-200381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
BAC1503-428382918THE BOEING COMPANY
LS3206-398897LOCKHEED MARTIN CORP
AND10134-200399237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
QQ-A-200/1181348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASE FLANGE THICKNESS0.125 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.188 INCHES NOMINAL
FIRST TIP RADIUS0.125 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-6 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.125 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 7075
NONDEFINITIVE SPEC/STD DATAT6 TEMPER
OVERALL HEIGHT1.250 INCHES NOMINAL
OVERALL WIDTH2.000 INCHES NOMINAL
SECOND TIP RADIUS0.125 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.470 POUNDS PER LINEAR FOOT


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