NSN 9540-01-233-0629

Part Details | STRUCTURAL ANGLE

9540-01-233-0629 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: 1MA100D0110169, 1MA100D01-10169, QQA20011, QQ-A-200/11, NAS34124, NAS341-24, NAS3412470750, NAS341-24-7075-0, AMSQQA20011, AMS-QQ-A-200/11, 9540-01-233-0629, 01-233-0629, 9540012330629, 012330629

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95MAY 24, 198601-233-062937017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

RIGHT QUARTER RADIUS

UPPER RADIUS

RIGHT QUARTER RADIUS

UPPER RADIUS

Cross Reference | NSN 9540-01-233-0629
Part Number Cage Code Manufacturer
1MA100D01-1016976301BOEING COMPANY, THEDBA BOEING
QQ-A-200/1181348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
NAS341-2480205NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES
NAS341-24-7075-080205NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 9540-01-233-0629
Characteristic Specifications
FABRICATION METHOD EXTRUDED
HEAT TREATMENT O-ANNEALED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT2.500 INCHES NOMINAL
OVERALL WIDTH2.500 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.438 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.250 INCHES NOMINAL
BASE FLANGE THICKNESS0.438 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE RIGHT QUARTER RADIUS
FIRST TIP RADIUS0.438 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE UPPER RADIUS
SECOND TIP RADIUS0.438 INCHES NOMINAL
SPECIFICATION/STANDARD DATA76301-1A100 MANUFACTURERS STANDARD
NONDEFINITIVE SPEC/STD DATAO TEMPER