9540-01-363-7426 ANGLE,STRUCTURAL Index 9540-01-363-7428 ANGLE,STRUCTURAL

National Stock Number:
9540-01-363-7427

Federal Supply Class:
9540

National Item Identification Number:
013637427

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:
1MA100D06-1009776301THE BOEING COMPANY
AMS-QQ-A-200/150U583SAE INTERNATIONAL
AMS43170U583SAE INTERNATIONAL
AMS431781343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/1581343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AND10134-160399237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQ-A-200/1581348FEDERAL 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 FLANGE0.156 INCHES NOMINAL
FIRST TIP INNER RADIUS0.125 INCHES NOMINAL
FIRST TIP OUTER RADIUS0.010 INCHES NOMINAL
FIRST TIP STYLESQUARE W/ INNER AND OUTER CORNER RADII
HEAT TREATMENTT-76511 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.125 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT1.500 INCHES NOMINAL
OVERALL WIDTH1.750 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONALLOY 7075 ASSN STD SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 7075
NONDEFINITIVE SPEC/STD DATA7075 ALLOY AND T76511 TEMPER
SECOND TIP INNER RADIUS0.125 INCHES NOMINAL
SECOND TIP OUTER RADIUS0.010 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLESQUARE W/ INNER AND OUTER CORNER RADII
WEIGHT PER UNIT MEASURE0.231 POUNDS PER LINEAR FOOT


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