9540-00-145-8446 ANGLE,STRUCTURAL Index 9540-00-145-8449 ANGLE,STRUCTURAL

National Stock Number:
9540-00-145-8447

Federal Supply Class:
9540

National Item Identification Number:
001458447

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:
1104A77783ALCOA/REYNOLDS METALS COMPANY
1503-881381205THE BOEING COMPANY
2-112238597LOCKHEED MARTIN CORPORATION
609999267BOHN ALUMINUM AND BRASS CO DIV OF GULF AND WESTERN MFG CO SUB OF GULF AND WESTERN INDUSTRIES
77V01634ALUMINUM CO OF AMERICA
AMS-QQ-A-200/20U583SAE INTERNATIONAL
AMS-QQ-A-200/281343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS41540U583SAE INTERNATIONAL
AND10133-200299237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQ-A-200/281348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASE FLANGE THICKNESS0.125 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.250 INCHES NOMINAL
FIRST TIP RADIUS0.125 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-6 SOLUTION HEAT TREATED OR T-6511 SOLUTION HEAT TREATED
LEFT SIDE FLANGE THICKNESS0.125 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT2.000 INCHES NOMINAL
OVERALL WIDTH2.000 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-QQ-A-200/2 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2014
NONDEFINITIVE SPEC/STD DATA7075 ALLOY AND T6 TEMPER OR T6511 TEMPER
SECOND TIP RADIUS0.125 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.580 POUNDS PER LINEAR FOOT


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