5340-00-251-2566 STRIKE,CATCH Index 9540-00-251-2569 ANGLE,STRUCTURAL

National Stock Number:
9540-00-251-2568

Federal Supply Class:
9540

National Item Identification Number:
002512568

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:
1M12776301THE BOEING COMPANY
238201484REYNOLDS METALS CO
AMS-QQ-A-200/30U583SAE INTERNATIONAL
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
BAC1503-416282918THE BOEING COMPANY
DIE78Y01634ALUMINUM CO OF AMERICA
CVC195080378TRIUMPH AEROSTRUCTURES, LLC
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
LS325798897LOCKHEED MARTIN CORP


Techincal Specification:
BASE FLANGE THICKNESS0.093 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.093 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 THICKNESS0.093 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 T3511 TEMPER
OVERALL HEIGHT1.250 INCHES NOMINAL
OVERALL WIDTH1.250 INCHES NOMINAL
SECOND TIP RADIUS0.047 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.270 POUNDS PER LINEAR FOOT


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