9540-00-540-5937 ANGLE,STRUCTURAL Index 9540-00-540-5942 ANGLE,STRUCTURAL

National Stock Number:
9540-00-540-5941

Federal Supply Class:
9540

National Item Identification Number:
005405941

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:
10133-070129321TRANSTAR METALS CORP
1715727610INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP
577301484REYNOLDS METALS CO
5066908588NATIONAL DISTILLERS AND CHEMICAL CORP BRIDGEPORT BRASS CO DIV
2-132638597LOCKHEED MARTIN CORPORATION
4030499267BOHN ALUMINUM AND BRASS CO DIV OF GULF AND WESTERN MFG CO SUB OF GULF AND WESTERN INDUSTRIES
AMS-QQ-A-200/11 ALLOY 7075 TMPR0U583SAE INTERNATIONAL
AMS-STD-1840U583SAE INTERNATIONAL
AMS10133-07010U583SAE INTERNATIONAL
AMS10133-070181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-STD-18481343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/11 ALLOY 7075 TMPR81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/11 ALL0Y 7075 TMPR81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
J219P10807482GENERAL ELECTRIC COMPANY
AND10133-07010U583SAE INTERNATIONAL
HA35910383KAISER ALUMINUM AND CHEMICAL CORP TRENTWOOD WORKS-MARKETING DEPT
AND10133-0701/ASTM B221-014153DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER PHILADELPHIA
S10171379CESSNA AIRCRAFT COMPANY
S9771379CESSNA AIRCRAFT COMPANY
S977EK50TEXTRON AVIATION INC
S1017EK50TEXTRON AVIATION INC
AND10133-070181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQ-A-200/1181348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
QQ-A-27781348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
AND10133-070199237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD


Techincal Specification:
BASE FLANGE THICKNESS0.063 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
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 HEIGHT0.875 INCHES NOMINAL
OVERALL WIDTH0.875 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 7075
NONDEFINITIVE SPEC/STD DATA7075 ALLOY AND 0 TEMPER
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP RADIUS0.063 INCHES NOMINAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.130 POUNDS PER LINEAR FOOT


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