NSN 9540-01-495-0845

Part Details | STRUCTURAL ANGLE

9540-01-495-0845 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: 1MA100C0310090, 1MA100C03-10090, NAS342306061T6511, NAS342-30-6061T6511, 9540-01-495-0845, 01-495-0845, 9540014950845, 014950845

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95MAR 06, 200201-495-084537017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

ANGLE,STRUCTURAL | 9540-01-495-0845, 014950845

RIGHT QUARTER RADIUS

ANGLE,STRUCTURAL | 9540-01-495-0845, 014950845

UPPER RADIUS

ANGLE,STRUCTURAL | 9540-01-495-0845, 014950845

RIGHT QUARTER RADIUS

ANGLE,STRUCTURAL | 9540-01-495-0845, 014950845

UPPER RADIUS

ANGLE,STRUCTURAL | 9540-01-495-0845, 014950845
Cross Reference | NSN 9540-01-495-0845
Part Number Cage Code Manufacturer
1MA100C03-1009076301BOEING COMPANY, THEDBA BOEING
NAS342-30-6061T651180205NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES
Technical Data | NSN 9540-01-495-0845
Characteristic Specifications
MATERIAL ALUMINUM ALLOY 6061
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-6511 SOLUTION HEAT TREATED
LENGTH10.000 INCHES MINIMUM AND 12.000 INCHES MAXIMUM
BASIC SHAPE STYLE6 ANGLE
OVERALL HEIGHT1.000 INCHES NOMINAL
OVERALL WIDTH1.750 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.094 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.156 INCHES NOMINAL
BASE FLANGE THICKNESS0.094 INCHES NOMINAL
LEFT FLANGE THICKNESS AT BASE0.094 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE RIGHT QUARTER RADIUS
FIRST TIP RADIUS0.094 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE UPPER RADIUS
SECOND TIP RADIUS0.094 INCHES NOMINAL