2995-00-251-2584 SLEEVE,INSULATION,A Index 9540-00-251-2587 ANGLE,STRUCTURAL

National Stock Number:
9540-00-251-2586

Federal Supply Class:
9540

National Item Identification Number:
002512586

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:
1671027610INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP
1M26676301THE BOEING COMPANY
2289201634ALUMINUM CO OF AMERICA
AMS-QQ-A-200/30U583SAE INTERNATIONAL
60-269329321TRANSTAR METALS CORP
453377783ALCOA/REYNOLDS METALS COMPANY
P4533A01484REYNOLDS METALS CO
PA407506012TRANSTAR METALS CORP
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
BAC1503-151482918THE BOEING COMPANY


Techincal Specification:
BASE FLANGE THICKNESS0.094 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.094 INCHES NOMINAL
FIRST TIP RADIUS0.047 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-3511 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.094 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-Q-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2024
NONDEFINITIVE SPEC/STD DATA2024 ALLOY AND T3511 TEMPER
OVERALL HEIGHT0.750 INCHES NOMINAL
OVERALL WIDTH1.000 INCHES NOMINAL
SECOND TIP RADIUS0.047 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.186 POUNDS PER LINEAR FOOT


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