NSN 9540-01-478-9731

Part Details | STRUCTURAL BEAM

9540-01-478-9731 A structural shape fabricated from a ferrous or nonferrous material and resembles the following cross-sectional forms: For the letter H, both flanges of the H section are equal or longer than the width measured along the axis of the web; for the letter I, a 16 2/3 percent slope on the inside face of the ferrous type flange, either one or both of the nonferrous type flanges are shorter than the length measured along the axis of the web; for the letters T and Z, on nonferrous type, the web is usually at right angles to the flanges. Letter H section may have a maximum of 5 percent slope on the inside face of the flanges.

Alternate Parts: HS1006DD152211, HS1006DD15-2211, 9540-01-478-9731, 01-478-9731, 9540014789731, 014789731

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95OCT 04, 200001-478-973137018 ( BEAM, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

T SHAPE

BEAM,STRUCTURAL | 9540-01-478-9731, 014789731

SQUARE END

BEAM,STRUCTURAL | 9540-01-478-9731, 014789731

SQUARE END

BEAM,STRUCTURAL | 9540-01-478-9731, 014789731

SQUARE END

BEAM,STRUCTURAL | 9540-01-478-9731, 014789731

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BEAM,STRUCTURAL | 9540-01-478-9731, 014789731
Cross Reference | NSN 9540-01-478-9731
Part Number Cage Code Manufacturer
HS1006DD15-22118V613BOEING COMPANY, THEDBA BOEING
Technical Data | NSN 9540-01-478-9731
Characteristic Specifications
MATERIAL ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-200 TO 3 FED SPEC 1ST MATERIAL RESPONSE
FABRICATION METHOD EXTRUDED
HEAT TREATMENTJ$DRG
LENGTH22.344 INCHES NOMINAL
BASIC SHAPE STYLE T SHAPE
OVERALL HEIGHT1.000 INCHES NOMINAL
LEFT SIDE TOP FLANGE THICKNESS0.125 INCHES NOMINAL
RIGHT SIDE TOP FLANGE THICKNESS0.125 INCHES NOMINAL
LEG THICKNESS0.125 INCHES NOMINAL
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1.000 INCHES NOMINAL
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1.000 INCHES NOMINAL
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG0.094 INCHES NOMINAL
FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG0.094 INCHES NOMINAL
TOP FLANGE WIDTH2.000 INCHES NOMINAL
LEFT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
RIGHT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE SQUARE END
SECOND TIP RELATIONSHIP TO FIRST TIP IDENTICAL
THIRD TIP RELATIONSHIP TO PRECEDING TIPS IDENTICAL W/FIRST TIP
END ITEM IDENTIFICATIONAPACHE HELICOPTER
PART NAME ASSIGNED BY CONTROLLING AGENCYEXTRUSION, TEE, ALUMINUM ALLOY