5130-00-145-5698 DRILL,MASONRY,ROTARY DRIVEN Index 9540-00-145-5701 ANGLE,STRUCTURAL

National Stock Number:
9540-00-145-5699

Federal Supply Class:
9540

National Item Identification Number:
001455699

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:
3003201634ALUMINUM CO OF AMERICA
AMS-QQ-A-200/110U583SAE INTERNATIONAL
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS10135-10020U583SAE INTERNATIONAL
AMS10135-100281343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AND10135-100299237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
QQ-A-200/1181348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASE FLANGE THICKNESS0.063 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.095 INCHES NOMINAL
FIRST TIP RADIUS0.063 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-6 SOLUTION HEAT TREATED OR T-6511 SOLUTION HEAT TREATED
LEFT SIDE FLANGE THICKNESS0.063 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT0.750 INCHES NOMINAL
OVERALL WIDTH1.000 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 7075
NONDEFINITIVE SPEC/STD DATA2024 ALLOY AND T6 TEMPER OR T6511 TEMPER
SECOND TIP DIAMETER0.190 INCHES NOMINAL
SECOND TIP RADIUS0.095 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER BULBOUS
WEIGHT PER UNIT MEASURE0.150 POUNDS PER LINEAR FOOT


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