9540-00-529-8796 ANGLE,STRUCTURAL Index 2995-00-529-8799 STUD ASSEMBLY

National Stock Number:
9540-00-529-8798

Federal Supply Class:
9540

National Item Identification Number:
005298798

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:
111920618355THE BOEING COMPANY
111920688277THE BOEING COMPANY
3002201634ALUMINUM CO OF AMERICA
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/3 ALL0Y 2024 TMPR -81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/3 ALLOY 2024 TMPR -0U583SAE INTERNATIONAL
AMS-QQ-A-200/3 ALLOY 2024 TMPR -81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
PA287706012TRANSTAR METALS CORP
QQA200-381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.062 INCHES NOMINAL
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.062 INCHES NOMINAL
FIRST TIP RADIUS0.031 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-4 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.062 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT0.750 INCHES NOMINAL
OVERALL WIDTH1.125 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2024
NONDEFINITIVE SPEC/STD DATA2024 ALLOY AND T4 TEMPER
REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICSAS DIFFERENTIATED BY EXTRA LONG REFERENCE NUMBER AMS-QQ-A-200/3 ALLOY 2024 TMPR T3511
SECOND TIP RADIUS0.031 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.140 POUNDS PER LINEAR FOOT


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