9540-00-542-2699 ANGLE,STRUCTURAL Index 9540-00-542-2701 ANGLE,STRUCTURAL

National Stock Number:
9540-00-542-2700

Federal Supply Class:
9540

National Item Identification Number:
005422700

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-200/50U583SAE INTERNATIONAL
AMS-QQ-A-200/581343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AND10133-140399237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
AND10133-1403/QQ-A-200/5-H11114153DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER PHILADELPHIA
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQ-A-200/581348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.125 INCHES NOMINAL
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.188 INCHES NOMINAL
FIRST TIP RADIUS0.125 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTH-111 STRAIN HARDENED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.125 INCHES NOMINAL
LENGTH20.000 FEET MINIMUM AND 30.000 FEET MAXIMUM
OVERALL HEIGHT1.500 INCHES NOMINAL
OVERALL WIDTH1.500 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-QQ-A-200/5 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 5086
NONDEFINITIVE SPEC/STD DATA5086 ALLOY AND H111 TEMPER
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP RADIUS0.125 INCHES NOMINAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.440 POUNDS PER LINEAR FOOT


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