9540-00-145-7548 ANGLE,STRUCTURAL Index 9540-00-145-7551 ANGLE,STRUCTURAL

National Stock Number:
9540-00-145-7550

Federal Supply Class:
9540

National Item Identification Number:
001457550

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:
AMS-QQ-A-200/30U583SAE INTERNATIONAL
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200A0U583SAE INTERNATIONAL
AMS-QQ-A-200A81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AND10135-060199237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
ASTM B221-02 ALL0Y 2024 TMPR T481346AMERICAN SOCIETY FOR TESTING AND MATERIALS
ASTM B221-02 ALLOY 2024 TMPR T481346AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASE FLANGE THICKNESS0.050 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.075 INCHES NOMINAL
FIRST TIP RADIUS0.050 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-4 SOLUTION HEAT TREATED
LEFT SIDE FLANGE THICKNESS0.050 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT0.563 INCHES NOMINAL
OVERALL WIDTH0.750 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
SECOND TIP DIAMETER0.150 INCHES NOMINAL
SECOND TIP RADIUS0.075 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER BULBOUS
WEIGHT PER UNIT MEASURE0.090 POUNDS PER LINEAR FOOT


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