NSN 9540-01-495-0829

Part Details | STRUCTURAL ANGLE

9540-01-495-0829 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: 1MA100C0310057, 1MA100C03-10057, NAS342146061T6511, NAS342-14-6061T6511, 9540-01-495-0829, 01-495-0829, 9540014950829, 014950829

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95MAR 06, 200201-495-082937017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

ANGLE,STRUCTURAL | 9540-01-495-0829, 014950829

RIGHT QUARTER RADIUS

ANGLE,STRUCTURAL | 9540-01-495-0829, 014950829

UPPER RADIUS

ANGLE,STRUCTURAL | 9540-01-495-0829, 014950829

RIGHT QUARTER RADIUS

ANGLE,STRUCTURAL | 9540-01-495-0829, 014950829

UPPER RADIUS

ANGLE,STRUCTURAL | 9540-01-495-0829, 014950829
Cross Reference | NSN 9540-01-495-0829
Part Number Cage Code Manufacturer
1MA100C03-1005776301BOEING COMPANY, THEDBA BOEING
NAS342-14-6061T651180205NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES
Technical Data | NSN 9540-01-495-0829
Characteristic Specifications
MATERIAL ALUMINUM ALLOY 6061
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-6511 SOLUTION HEAT TREATED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE6 ANGLE
OVERALL HEIGHT0.875 INCHES NOMINAL
OVERALL WIDTH1.375 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.125 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.156 INCHES NOMINAL
BASE FLANGE THICKNESS0.125 INCHES NOMINAL
LEFT FLANGE THICKNESS AT BASE0.125 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