9540-00-140-2399 ANGLE,STRUCTURAL Index 9540-00-140-2401 ANGLE,STRUCTURAL

National Stock Number:
9540-00-140-2400

Federal Supply Class:
9540

National Item Identification Number:
001402400

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-200/110U583SAE INTERNATIONAL
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AND10134-050199237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
AND10134-0501/QQ-A-200/11-014153DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER PHILADELPHIA
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
LS10134-0501-698897LOCKHEED MARTIN CORP
QQ-A-200/1181348FEDERAL 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 FLANGE0.063 INCHES NOMINAL
FIRST TIP RADIUS0.250 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTO-ANNEALED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.050 INCHES NOMINAL
LENGTH12.000 FEET NOMINAL
OVERALL HEIGHT0.500 INCHES NOMINAL
OVERALL WIDTH0.625 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 7075
NONDEFINITIVE SPEC/STD DATA7075 ALLOY AND ANNEALED CONDITION
SECOND TIP RADIUS0.250 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.060 POUNDS PER LINEAR FOOT


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