9540-00-145-5715 ANGLE,STRUCTURAL Index 6680-00-145-5718 METER,TIME TOTALIZING

National Stock Number:
9540-00-145-5716

Federal Supply Class:
9540

National Item Identification Number:
001455716

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:
AM000002-2580GCL4L3HARRIS TECHNOLOGIES INTEGRATED SYSTEMS L.P.
AMS-QQ-A-200/110U583SAE INTERNATIONAL
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS10134-16040U583SAE INTERNATIONAL
AMS10134-160481343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS41540U583SAE INTERNATIONAL
AND10134-160499237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQA200-1181348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
S-1250457T-720076301THE BOEING COMPANY


Techincal Specification:
BASE FLANGE THICKNESS0.156 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.156 INCHES NOMINAL
FIRST TIP RADIUS0.156 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-6 SOLUTION HEAT TREATED OR T-6511 SOLUTION HEAT TREATED
LEFT SIDE FLANGE THICKNESS0.156 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
OVERALL HEIGHT1.500 INCHES NOMINAL
OVERALL WIDTH1.750 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 7075
NONDEFINITIVE SPEC/STD DATA7075 ALLOY AND T6 TEMPER OR T6511 TEMPER
SECOND TIP RADIUS0.156 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.570 POUNDS PER LINEAR FOOT


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