9540-01-367-1982 STRUCTURAL SECTION,SPECIAL SHAPE Index 9540-01-367-1984 ANGLE,STRUCTURAL

National Stock Number:
9540-01-367-1983

Federal Supply Class:
9540

National Item Identification Number:
013671983

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:
1MA100B04-1003076301THE BOEING COMPANY
AMS-QQ-A-200/30U583SAE INTERNATIONAL
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
AND10134-100699237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD


Techincal Specification:
BASE FLANGE THICKNESS0.094 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.125 INCHES NOMINAL
FIRST TIP RADIUS0.094 INCHES NOMINAL
FIRST TIP STYLESQUARE END W/ LOWER RADIUS
HEAT TREATMENTT-8511 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.094 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2024
NONDEFINITIVE SPEC/STD DATA2024 ALLOY AND T8511 TEMPER
OVERALL HEIGHT0.875 INCHES NOMINAL
OVERALL WIDTH1.000 INCHES NOMINAL
SECOND TIP RADIUS0.094 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLESQUARE END W/ UPPER RADIUS


Click here to Register for Free 30-day Trial

© 2025 NSN-Now. All rights reserved.    Privacy Policy  |  Contact Us