NSN 9540-01-354-5859

Part Details | STRUCTURAL ANGLE

9540-01-354-5859 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: 1E118, 1E-118, QQA2003, QQ-A-200/3, AMSQQA2003, AMS-QQ-A-200/3, 60105782024T81, 60-10578/2024-T81, 9540-01-354-5859, 01-354-5859, 9540013545859, 013545859

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95MAR 01, 199201-354-585937017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

RIGHT QUARTER RADIUS

UPPER RADIUS

RIGHT QUARTER RADIUS

UPPER RADIUS

Cross Reference | NSN 9540-01-354-5859
Part Number Cage Code Manufacturer
1E-11843999BOEING COMPANY, THEDBA BOEING
QQ-A-200/381348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
60-10578/2024-T8129321TRANSTAR METALS CORP
Technical Data | NSN 9540-01-354-5859
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 HEIGHT1.000 INCHES NOMINAL
OVERALL WIDTH1.000 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.093 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.093 INCHES NOMINAL
BASE FLANGE THICKNESS0.093 INCHES NOMINAL
LEFT INSIDE ANGLE75.0 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 RADIUS0.046 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.214 POUNDS PER LINEAR FOOT
NONDEFINITIVE SPEC/STD DATAT81 TEMPER