9540-00-540-5936 ANGLE,STRUCTURAL Index 9540-00-540-5941 ANGLE,STRUCTURAL

National Stock Number:
9540-00-540-5937

Federal Supply Class:
9540

National Item Identification Number:
005405937

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:
118887388277THE BOEING COMPANY
119997318355THE BOEING COMPANY
1463027610INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP
2-130938597LOCKHEED MARTIN CORPORATION
5029808588NATIONAL DISTILLERS AND CHEMICAL CORP BRIDGEPORT BRASS CO DIV
953501484REYNOLDS METALS CO
AND10133-060199237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
FS10101-0808-289446HILLER AIRCRAFT CORPORATION
HA35610383KAISER ALUMINUM AND CHEMICAL CORP TRENTWOOD WORKS-MARKETING DEPT
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.063 INCHES NOMINAL
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.094 INCHES NOMINAL
FIRST TIP RADIUS0.063 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTO-ANNEALED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.063 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT0.750 INCHES NOMINAL
OVERALL WIDTH0.750 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2024
NONDEFINITIVE SPEC/STD DATA0 TEMPER
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP RADIUS0.063 INCHES NOMINAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.110 POUNDS PER LINEAR FOOT


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