NSN 9540-01-339-1570

Part Details | STRUCTURAL ANGLE

9540-01-339-1570 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: AND101331003, AND10133-1003, 1MA100C0110033, 1MA100C01-10033, QQA2008, QQ-A-200/8, AMSQQA2008, AMS-QQ-A-200/8, 101331003, 10133-1003, 9540-01-339-1570, 01-339-1570, 9540013391570, 013391570

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95MAY 17, 199101-339-157037017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

RIGHT QUARTER RADIUS

UPPER RADIUS

RIGHT QUARTER RADIUS

UPPER RADIUS

Cross Reference | NSN 9540-01-339-1570
Part Number Cage Code Manufacturer
AND10133-100399237AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD
1MA100C01-1003376301BOEING COMPANY, THEDBA BOEING
QQ-A-200/881348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
AMS-QQ-A-200/881343SOCIETY OF AUTOMOTIVE ENGINEERS INC
10133-100329321TRANSTAR METALS CORP
Technical Data | NSN 9540-01-339-1570
Characteristic Specifications
FABRICATION METHOD EXTRUDED
HEAT TREATMENT O-ANNEALED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT1.000 INCHES NOMINAL
OVERALL WIDTH1.000 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.125 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.188 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 MEASURE0.281 POUNDS PER LINEAR FOOT
NONDEFINITIVE SPEC/STD DATAO TEMPER
END ITEM IDENTIFICATIONF-15 AIRCRAFT