5360-00-145-4540 SPRING Index 9540-00-145-4545 ANGLE,STRUCTURAL

National Stock Number:
9540-00-145-4543

Federal Supply Class:
9540

National Item Identification Number:
001454543

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:
1288301634ALUMINUM CO OF AMERICA
17936418355THE BOEING COMPANY
17936488277THE BOEING COMPANY
1M21476301THE BOEING COMPANY
2-151538597LOCKHEED MARTIN CORPORATION
5212227610INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP
E1210010WLU1GENERAL DYNAMICS CORP CONVAIR DIV LINDBERGH FIELD FACILITY
E12100114170HUGHES MISSILE SYSTEMS CO SAN DIEGO
E12100163910BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION I
E1210017B709TRACOR FLIGHT SYSTEMS INC SUB OF TRACOR INC
LS345898897LOCKHEED MARTIN CORP
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASE FLANGE THICKNESS0.051 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.063 INCHES NOMINAL
FIRST TIP RADIUS0.063 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-4 SOLUTION HEAT TREATED
LEFT SIDE FLANGE THICKNESS0.051 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT0.625 INCHES NOMINAL
OVERALL WIDTH0.750 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2024
NONDEFINITIVE SPEC/STD DATAT4 TEMPER
SECOND TIP RADIUS0.063 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.080 POUNDS PER LINEAR FOOT


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