9540-00-288-1136 ANGLE,STRUCTURAL Index 9540-00-288-1140 ANGLE,STRUCTURAL

National Stock Number:
9540-00-288-1137

Federal Supply Class:
9540

National Item Identification Number:
002881137

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:
124968518355THE BOEING COMPANY
124968588277THE BOEING COMPANY
AMS-QQ-A-200/30U583SAE INTERNATIONAL
AND10135-04020U583SAE INTERNATIONAL
AND10135-040281343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
CM261471379CESSNA AIRCRAFT COMPANY
CM26147EK50TEXTRON AVIATION INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
AND10135-040299237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD


Techincal Specification:
BASE FLANGE THICKNESS0.040 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.060 INCHES NOMINAL
FIRST TIP DIAMETER0.120 INCHES NOMINAL
FIRST TIP RADIUS0.060 INCHES NOMINAL
FIRST TIP STYLERIGHT BULBOUS
HEAT TREATMENTT-3511 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.040 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT0.500 INCHES NOMINAL
OVERALL WIDTH0.625 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 TIPNOT IDENTICAL
SECOND TIP RADIUS0.040 INCHES NOMINAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.062 POUNDS PER LINEAR FOOT


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