NSN 9540-01-235-6000

Part Details | STRUCTURAL ANGLE

9540-01-235-6000 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: 1MA100D0110040, 1MA100D01-10040, QQA20011, QQ-A-200/11, NAS34211, NAS342-11, AMSQQA20011, AMS-QQ-A-200/11, 602403, 60-2403, 9540-01-235-6000, 01-235-6000, 9540012356000, 012356000

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95JUL 03, 198601-235-600037017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

RIGHT QUARTER RADIUS

UPPER RADIUS

RIGHT QUARTER RADIUS

UPPER RADIUS

Cross Reference | NSN 9540-01-235-6000
Part Number Cage Code Manufacturer
1MA100D01-1004076301BOEING COMPANY, THEDBA BOEING
QQ-A-200/1181348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
NAS342-1180205NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
60-240329321TRANSTAR METALS CORP
Technical Data | NSN 9540-01-235-6000
Characteristic Specifications
FABRICATION METHOD EXTRUDED
HEAT TREATMENT O-ANNEALED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT0.875 INCHES NOMINAL
OVERALL WIDTH1.125 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.125 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.125 INCHES NOMINAL
BASE FLANGE THICKNESS0.125 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE RIGHT QUARTER RADIUS
FIRST TIP RADIUS0.125 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE UPPER RADIUS
SECOND TIP RADIUS0.125 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.652 POUNDS PER LINEAR FOOT
SPECIFICATION/STANDARD DATA76301-1A100 MANUFACTURERS STANDARD