NSN 9540-00-288-1137

Part Details | STRUCTURAL ANGLE

9540-00-288-1137 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.

Alternate Parts: AND101350402, AND10135-0402, ASTM B221, 1249685, 1249685, CM2614, QQA2003, QQ-A-200/3, AND101350402, AND10135-0402, AMSQQA2003, AMS-QQ-A-200/3, 9540-00-288-1137, 00-288-1137, 9540002881137, 002881137

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95JAN 01, 196300-288-113737017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

UPPER RADIUS

RIGHT BULBOUS

UPPER RADIUS

RIGHT BULBOUS

Cross Reference | NSN 9540-00-288-1137
Part Number Cage Code Manufacturer
AND10135-040299237AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD
ASTM B22181346AMERICAN SOCIETY FOR TESTING ANDMATERIALS
124968588277BOEING COMPANY, THEDBA BOEING
124968518355BOEING COMPANY, THEDBA BOEING
CM261471379CESSNA AIRCRAFT COMPANYDBA TEXTRON AVIATION
QQ-A-200/381348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
AND10135-040281343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 9540-00-288-1137
Characteristic Specifications
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-3511 SOLUTION HEAT TREATED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT0.500 INCHES NOMINAL
OVERALL WIDTH0.625 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.040 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.060 INCHES NOMINAL
BASE FLANGE THICKNESS0.040 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE RIGHT BULBOUS
FIRST TIP RADIUS0.060 INCHES NOMINAL
FIRST TIP DIAMETER0.120 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE UPPER RADIUS
SECOND TIP RADIUS0.040 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.062 POUNDS PER LINEAR FOOT