9540-00-145-5797 ANGLE,STRUCTURAL Index 9540-00-145-5803 ANGLE,STRUCTURAL

National Stock Number:
9540-00-145-5802

Federal Supply Class:
9540

National Item Identification Number:
001455802

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:
1366401634ALUMINUM CO OF AMERICA
60-1239229321TRANSTAR METALS CORP
828177783ALCOA/REYNOLDS METALS COMPANY
AMS-QQ-A-200/30U583SAE INTERNATIONAL
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
BAC1504-151181205THE BOEING COMPANY
PA533006012TRANSTAR METALS CORP
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
S9571379CESSNA AIRCRAFT COMPANY
S957EK50TEXTRON AVIATION INC


Techincal Specification:
BASE FLANGE THICKNESS0.050 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.062 INCHES NOMINAL
FIRST TIP STYLESQUARE END
HEAT TREATMENTT-3511 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.050 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT0.800 INCHES NOMINAL
OVERALL WIDTH0.800 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2024
NONDEFINITIVE SPEC/STD DATA2024 ALLOY AND T3511 TEMPER
SECOND TIP DIAMETER0.120 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP RADIUS0.062 INCHES NOMINAL
SECOND TIP STYLEUPPER BULBOUS
WEIGHT PER UNIT MEASURE0.102 POUNDS PER LINEAR FOOT


Click here to Register for Free 30-day Trial