NSN 9540-00-251-2569

Part Details | STRUCTURAL ANGLE

9540-00-251-2569 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: DIE734GG, ASTM B221, 1M224, BAC15032814, BAC1503-2814, S76, QQA20011, QQ-A-200/11, E121119, E121119, 14730, 134413, 13441-3, LS3246, 3073, AMSQQA20011, AMS-QQ-A-200/11, E121119, CVC1935, 9540-00-251-2569, 00-251-2569, 9540002512569, 002512569

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95JAN 01, 196300-251-256937017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

RIGHT QUARTER RADIUS

UPPER RADIUS

RIGHT QUARTER RADIUS

UPPER RADIUS

Cross Reference | NSN 9540-00-251-2569
Part Number Cage Code Manufacturer
DIE734GG01634ALUMINUM CO OF AMERICA
ASTM B22181346AMERICAN SOCIETY FOR TESTING ANDMATERIALS
1M22476301BOEING COMPANY, THEDBA BOEING
BAC1503-281482918BOEING COMPANY, THEDBA BOEING
S7671379CESSNA AIRCRAFT COMPANYDBA TEXTRON AVIATION
QQ-A-200/1181348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
E1211190WLU1GENERAL DYNAMICS CORPCONVAIR DIV
E12111914170HUGHES MISSILE SYSTEMS COSAN DIEGO
1473027610INTERNATIONAL LIGHT METALS CORPSUB OF MARTIN MARIETTA CORP
13441-327610INTERNATIONAL LIGHT METALS CORPSUB OF MARTIN MARIETTA CORP
LS324698897LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS
307301484REYNOLDS METALS CO
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
E1211197B709TRACOR FLIGHT SYSTEMS INCSUB OF TRACOR INC
CVC193580378TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT
Technical Data | NSN 9540-00-251-2569
Characteristic Specifications
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-6 SOLUTION HEAT TREATED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT1.000 INCHES NOMINAL
OVERALL WIDTH1.500 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.156 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.156 INCHES NOMINAL
BASE FLANGE THICKNESS0.156 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE RIGHT QUARTER RADIUS
FIRST TIP RADIUS0.078 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE UPPER RADIUS
SECOND TIP RADIUS0.078 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.440 POUNDS PER LINEAR FOOT