9540-00-145-7556 ANGLE,STRUCTURAL Index 9540-00-145-7574 ANGLE,STRUCTURAL

National Stock Number:
9540-00-145-7557

Federal Supply Class:
9540

National Item Identification Number:
001457557

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:
10163970898BEECHCRAFT CORPORATION
1016397EK50TEXTRON AVIATION INC
1099677783ALCOA/REYNOLDS METALS COMPANY
1162301634ALUMINUM CO OF AMERICA
60-1157229321TRANSTAR METALS CORP
AMS-QQ-A-200/30U583SAE INTERNATIONAL
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
BAC1503-45081205THE BOEING COMPANY
PA552006012TRANSTAR METALS CORP
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
S10971379CESSNA AIRCRAFT COMPANY
S1097EK50TEXTRON AVIATION INC


Techincal Specification:
BASE FLANGE THICKNESS0.050 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.050 INCHES NOMINAL
FIRST TIP STYLESQUARE END
HEAT TREATMENTT-3511 SOLUTION HEAT TREATED
LEFT SIDE FLANGE THICKNESS0.050 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT0.500 INCHES NOMINAL
OVERALL WIDTH0.500 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 RELATIONSHIP TO FIRST TIPIDENTICAL
WEIGHT PER UNIT MEASURE0.058 POUNDS PER LINEAR FOOT


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