NSN 9540-00-145-7542

Part Details | STRUCTURAL ANGLE


9540-00-145-7542 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: AND101342002, AND10134-2002, 1244707, 1244707, QQA20011, QQ-A-200/11, 21355, 2-1355, AMSQQA20011, AMS-QQ-A-200/11, 9540-00-145-7542, 00-145-7542, 9540001457542, 001457542

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95JAN 01, 196300-145-754237017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

RIGHT QUARTER RADIUS

UPPER RADIUS

RIGHT QUARTER RADIUS

UPPER RADIUS


Cross Reference | NSN 9540-00-145-7542
Part Number Cage Code Manufacturer
AND10134-200299237AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD
124470788277BOEING COMPANY, THEDBA BOEING
124470718355BOEING COMPANY, THEDBA BOEING
QQ-A-200/1181348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
2-135538597LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC

Technical Data | NSN 9540-00-145-7542
Characteristic Specifications
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-6 SOLUTION HEAT TREATED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT1.000 INCHES NOMINAL
OVERALL WIDTH2.000 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.156 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.156 INCHES NOMINAL
BASE FLANGE THICKNESS0.156 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE RIGHT QUARTER RADIUS
FIRST TIP RADIUS0.156 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE UPPER RADIUS
SECOND TIP RADIUS0.156 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.530 POUNDS PER LINEAR FOOT
NONDEFINITIVE SPEC/STD DATA7075 ALLOY AND T6 TEMPER