9540-01-443-7365, BEAM,STRUCTURAL

National Stock Number:
9540-01-443-7365

Federal Supply Class:
9540

National Item Identification Number:
014437365

Description:
BEAM,STRUCTURAL

Detail:
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.

Manufacturer Information:

200062001-01	98748	AIR FORCE UNITED STATES DEPARTMENT OF THE DBA TINKER AFB OC ALC DSP
L2102057/1RS	43999	THE BOEING COMPANY

Techincal Specification:

BASIC SHAPE STYLE	T SHAPE
FIRST TIP STYLE	SQUARE END
FSC APPLICATION DATA	STRUCTURAL SHAPES
LEFT SIDE TOP FLANGE THICKNESS	0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM
LENGTH	23.970 INCHES MINIMUM AND 24.030 INCHES MAXIMUM
PART NAME ASSIGNED BY CONTROLLING AGENCY	FLANGE,RS
MATERIAL	ALUMINUM ALLOY 7075
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES	0.760 INCHES MINIMUM AND 0.780 INCHES MAXIMUM
RIGHT SIDE TOP FLANGE THICKNESS	0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM
RIGHT TOP INSIDE ANGLE	95.2167 DEGREES MINIMUM AND 96.2167 DEGREES MAXIMUM
SECOND TIP RELATIONSHIP TO FIRST TIP	IDENTICAL
SPECIAL FEATURES	USED IN THE HS PROJECT. THE /1RS IS USED TO MAKE P/N -003/005/007/009/0013/015/017/019/023/025/027
THIRD TIP RELATIONSHIP TO PRECEDING TIPS	IDENTICAL W/FIRST TIP
TOP FLANGE WIDTH	1.670 INCHES MINIMUM AND 1.690 INCHES MAXIMUM

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