9540-00-251-1796 ANGLE,STRUCTURAL Index 5330-00-251-1799 PACKING ASSEMBLY

National Stock Number:
9540-00-251-1798

Federal Supply Class:
9540

National Item Identification Number:
002511798

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:
1676627610INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP
1M13876301THE BOEING COMPANY
AMS-QQ-A-200/30U583SAE INTERNATIONAL
60-64729321TRANSTAR METALS CORP
399677783ALCOA/REYNOLDS METALS COMPANY
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
DIE1046801634ALUMINUM CO OF AMERICA
PA323506012TRANSTAR METALS CORP
CVC196380378TRIUMPH AEROSTRUCTURES, LLC
BAC1503-582481205THE BOEING COMPANY
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQA-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASE FLANGE THICKNESS0.156 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.156 INCHES NOMINAL
FIRST TIP RADIUS0.078 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-4 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.156 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2024
NONDEFINITIVE SPEC/STD DATA2024 ALLOY AND T4 TEMPER
OVERALL HEIGHT1.500 INCHES NOMINAL
OVERALL WIDTH1.500 INCHES NOMINAL
SECOND TIP RADIUS0.078 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.540 POUNDS PER LINEAR FOOT


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