9540-00-145-5731 ANGLE,STRUCTURAL Index 5330-00-145-5739 PACKING,PREFORMED

National Stock Number:
9540-00-145-5732

Federal Supply Class:
9540

National Item Identification Number:
001455732

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:
13287918355THE BOEING COMPANY
13287988277THE BOEING COMPANY
1M31276301THE BOEING COMPANY
2433701634ALUMINUM CO OF AMERICA
847801634ALUMINUM 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
LS327498897LOCKHEED MARTIN CORP
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
VS18314170HUGHES MISSILE SYSTEMS CO SAN DIEGO


Techincal Specification:
BASE FLANGE THICKNESS0.072 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.125 INCHES NOMINAL
FIRST TIP RADIUS0.062 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-3511 SOLUTION HEAT TREATED
LEFT SIDE FLANGE THICKNESS0.062 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT1.000 INCHES NOMINAL
OVERALL WIDTH1.125 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 DIAMETER0.218 INCHES NOMINAL
SECOND TIP RADIUS0.109 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER BULBOUS
WEIGHT PER UNIT MEASURE0.200 POUNDS PER LINEAR FOOT


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