1315-00-145-7536 CARTRIDGE,105 MILLIMETER Index 9540-00-145-7541 ANGLE,STRUCTURAL

National Stock Number:
9540-00-145-7539

Federal Supply Class:
9540

National Item Identification Number:
001457539

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:
115237118355THE BOEING COMPANY
115237188277THE BOEING COMPANY
2-13338597LOCKHEED MARTIN CORPORATION
463077783ALCOA/REYNOLDS METALS COMPANY
60-8829321TRANSTAR METALS CORP
734LL01634ALUMINUM CO OF AMERICA
AMS-QQ-A-200/30U583SAE INTERNATIONAL
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
BAC1503-420582918THE BOEING COMPANY
LS337898897LOCKHEED MARTIN CORP
PA420006012TRANSTAR METALS CORP
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASE FLANGE THICKNESS0.188 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.188 INCHES NOMINAL
FIRST TIP RADIUS0.125 INCHES NOMINAL
FIRST TIP STYLESQUARE END
HEAT TREATMENTT-3511 SOLUTION HEAT TREATED
LEFT SIDE FLANGE THICKNESS0.188 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT1.250 INCHES NOMINAL
OVERALL WIDTH1.500 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 RADIUS0.125 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.580 POUNDS PER LINEAR FOOT


Click here to Register for Free 30-day Trial