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NSN 9540-01-478-9726, 9540014789726
BEAM,STRUCTURAL

Federal Supply Classification
FSC 9540 - Structural Shapes, Nonferrous Base Metal
National Item Identification Number
NIIN 014789726
Codification Country
United States
Item Name Code
INC 37018
Criticality
(X) This item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.
Hazardous Material Indicator Code
(N) There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials.
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DLMS® Summary

National Stock Number 9540-01-478-9726

National Stock Number (NSN) 9540-01-478-9726, or NIIN 014789726, (beam,structural) was assigned October 4, 2000 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There is only one manufacturer part number associated with this NSN. None of the associated part number(s) are considered obsolete. The manufacturer part numbers were originally supplied by one supplier. Today, one supplier is listed as an Active supplier for this NSN. Of the active suppliers, only one supplier is deemed design controlled or valid supply parts.

This part number has been procured by the US Government within the last year, but shows no recent (last 90 days) procurement activity. There have been 5 contracts issued for this part number, with 5 awards given. The US Government has only awarded those contracts to one supplier. The last contract numbers awarded were: SPE8E424PQ090, SPE8E423V1382, SPE8E423P0041, SPE8E520P0622, SPE8E519P0309. The total value of the awarded contracts has been US$ 10,606.80.

This NSN is somewhat common among different platforms, belonging to 2 different weapons systems.

There has been a small amount of demand for this national stock number. The demand for this NSN originated from less than 5 countries. Based on a planned procurement review by the Primary Inventory Control Activity (PICA) on Apr 21, 2016, this NSN's acquisition method was noted as: Suitable for Competitive Acquisition. (Potential sources shall include dealers/distributors.) The Government does not have adequate data, lacks rights to data, or both, needed to purchase this part from additional sources. Valid AMCs: 1, 2, 3, 4 and 5.

This NSN is assigned to Item Name Code (INC) 37018. [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.]. This item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials. NSN 9540014789726 does not contain precious metals.

This NSN is associated to Schedule B 7601209500: other unwrought aluminum alloys, nesoi. The Schedule B End Use is listed as aluminum and alumina.

This information was last updated on .


Technical Characteristics

MATERIAL
(MATL) ALUMINUM ALLOY, QQ-A-200/11
III END ITEM IDENTIFICATION
(AGAV) APACHE HELICOPTER
III PART NAME ASSIGNED BY CONTROLLING AGENCY
(CXCY) EXTRUSION, TEE, ALUMINUM ALLOY
UNABLE TO DECODE
(MATL) UNABLE TO DECODE
END ITEM IDENTIFICATION
(AGAV) APACHE HELICOPTER
BASIC SHAPE STYLE
(AGTA) T SHAPE
FABRICATION METHOD
(AARN) EXTRUDED
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG
(BPXJ) 0.125 INCHES NOMINAL
FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG
(BPXL) 0.125 INCHES NOMINAL
FIRST TIP STYLE
(CMZY) SQUARE END
HEAT TREATMENT
(HEAT) T-6 SOLUTION HEAT TREATED OR T-6511 SOLUTION HEAT TREATED
OVERALL HEIGHT
(ABKW) 3.250 INCHES NOMINAL
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES
(BPXD) 0.750 INCHES NOMINAL
LEFT SIDE TOP FLANGE THICKNESS
(ADXR) 0.060 INCHES NOMINAL
LEFT TOP INSIDE ANGLE
(CSMZ) 90.0 DEGREES NOMINAL
LEG THICKNESS
(AJJP) 0.060 INCHES NOMINAL
LENGTH
(ABRY) 2.000 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATION
(MDCL) QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE
MATERIAL
(MATT) ALUMINUM ALLOY 7075
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES
(BPXG) 0.750 INCHES NOMINAL
RIGHT SIDE TOP FLANGE THICKNESS
(ADXS) 0.060 INCHES NOMINAL
RIGHT TOP INSIDE ANGLE
(CRZC) 90.0 DEGREES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP
(CNQJ) IDENTICAL
PART NAME ASSIGNED BY CONTROLLING AGENCY
(CXCY) EXTRUSION, TEE, ALUMINUM ALLOY
THIRD TIP RELATIONSHIP TO PRECEDING TIPS
(CNQL) IDENTICAL W/FIRST TIP
TOP FLANGE WIDTH
(BQJG) 1.500 INCHES NOMINAL

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