NSN 9540-01-353-4621

Part Details | STRUCTURAL ANGLE

9540-01-353-4621 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: 1E719, 1E-719, QQA2003, QQ-A-200/3, AMSQQA2003, AMS-QQ-A-200/3, 6030192024TT81, 60-3019/2024T-T81, 6030192024T81, 60-3019/2024-T81, 9540-01-353-4621, 01-353-4621, 9540013534621, 013534621

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95FEB 11, 199201-353-462137017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

SQUARE W/ INNER AND OUTER CORNER RADII

SQUARE W/ INNER AND OUTER CORNER RADII

Cross Reference | NSN 9540-01-353-4621
Part Number Cage Code Manufacturer
1E-71943999BOEING COMPANY, THEDBA BOEING
QQ-A-200/381348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
60-3019/2024T-T8129321TRANSTAR METALS CORP
60-3019/2024-T8129321TRANSTAR METALS CORP
Technical Data | NSN 9540-01-353-4621
Characteristic Specifications
MATERIAL ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-200 TO 3 FED SPEC 1ST MATERIAL RESPONSE
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-81 SOLUTION HEAT TREATED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT0.875 INCHES NOMINAL
OVERALL WIDTH1.500 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.080 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.062 INCHES NOMINAL
OUTER RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.031 INCHES NOMINAL
BASE FLANGE THICKNESS0.080 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE SQUARE W/ INNER AND OUTER CORNER RADII
FIRST TIP INNER RADIUS0.031 INCHES NOMINAL
FIRST TIP OUTER RADIUS0.031 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP IDENTICAL
WEIGHT PER UNIT MEASURE0.221 POUNDS PER LINEAR FOOT
NONDEFINITIVE SPEC/STD DATAT81 TEMPER