5310-00-516-6157 NUT,SELF-LOCKING,CLINCH Index 5310-00-516-6159 WASHER,FLAT

National Stock Number:
9540-00-516-6158

Federal Supply Class:
9540

National Item Identification Number:
005166158

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:
1249581-240088277THE BOEING COMPANY
1404401634ALUMINUM CO OF AMERICA
2418301634ALUMINUM CO OF AMERICA
388777783ALCOA/REYNOLDS METALS COMPANY
60-16029321TRANSTAR METALS CORP
7276103462HOWMET CORPORATION
AMS-QQ-A-200/110U583SAE INTERNATIONAL
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
PA60-16006012TRANSTAR METALS CORP
QQ-A-200/1181348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
S124958118355THE BOEING COMPANY
S124958188277THE BOEING COMPANY


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.093 INCHES NOMINAL
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.125 INCHES NOMINAL
FIRST TIP RADIUS0.093 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-6 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.093 INCHES NOMINAL
LENGTH20.000 FEET NOMINAL
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 DATA7075 ALLOY AND T6 TEMPER
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP RADIUS0.093 INCHES NOMINAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.180 POUNDS PER LINEAR FOOT


Click here to Register for Free 30-day Trial