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NSN 5340-00-377-5658, 5340003775658
BRACKET,ANGLE

Federal Supply Classification
FSC 5340 - Hardware, Commercial
National Item Identification Number
NIIN 003775658
Codification Country
United States
Item Name Code
INC 16900
Criticality
(F) This item is a Flight Safety Critical Aircraft Part (FSCAP).
Hazardous Material Indicator Code
(P) There is no information in the HMIRS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product.
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DLMS® Summary

National Stock Number 5340-00-377-5658

National Stock Number (NSN) 5340-00-377-5658, or NIIN 003775658, (bracket,angle) was assigned March 16, 1974 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There are 2 manufacturer part numbers associated with this NSN. 2 of those part number(s) are considered obsolete. The manufacturer part numbers were originally supplied by 3 suppliers. Today, 2 suppliers are listed as Active suppliers for this NSN. Of the active suppliers, 2 suppliers are deemed design controlled or valid supply parts. ISO Group has several sources of supply for this NSN.

This part number has not been procured by the US Government in over a year. There have been 29 contracts issued for this part number, with 29 awards given. The US Government has only awarded those contracts to one supplier. The last contract numbers awarded were: SPE4AX24F6648, SPE4AX24F6648, SPE4AX23F6146, SPE4AX23F6146, SPE4AX23F3681. The total value of the awarded contracts has been US$ 300,385.98.

This NSN is somewhat common among different platforms, belonging to 7 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 Feb 20, 2014, this NSN's acquisition method was noted as: Acquire directly from the actual manufacturer, whether or not the prime contractor is the actual manufacturer. This part requires engineering source approval by the design control activity in order to maintain the quality of the part. An alternate source must qualify in accordance with the design control activity's procedures, as approved by the cognizant Government engineering activity. Valid AMCs: 1, 2, 3, 4 and 5.

This NSN is assigned to Item Name Code (INC) 16900. [A RIDGE ITEM, USUALLY OF FLAT MATERIAL, FORMED INTO A DIHEDRAL ANGLE (GENERALLY A RIGHT ANGLE) WHICH MAY BE REINFORCED; IT IS DESIGNED TO POSITION, ALIGN, OR SUPPORT AN ITEM(S) IN RELATION TO ANOTHER. EXCLUDES:BRACE (AS MODIFIED); BRACKET (1), MOUNTING; AND BRACKET, SHELF.]. This item is a Flight Safety Critical Aircraft Part (FSCAP). There is no information in the HMIRS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product. NSN 5340003775658 contains an unknown precious metal.

This NSN is associated to Schedule B 8302500000: hat-racks, hat pegs, brackets and similar fixtures, and parts thereof, of base metal. The Schedule B End Use is listed as cell phones and other household goods, n.e.c.. NAICS classification category 337127: institutional furniture manufacturing.

This information was last updated on .


Technical Characteristics

FABRICATION METHOD (NON-CORE)
(AARN) MACHINED
END ITEM IDENTIFICATION
(AGAV) W/S: ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); AIRCRAFT, EAGLE F-15; SUPPORT EQUIPMENT, C-5 AIRCRAFT; AIRCRAFT, F-16; ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); ADVANCE AIR TRAFFIC CONTR. & LAND. SYS (ATCALS) 404L; AIRCRAFT, F-111; ENGINE, AIRCRAFT, F100-PW-220 (F-15C/D/E)
FIRST LEG ANGLE
(CSSQ) 90.0 DEGREES NOMINAL
FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH
(AHRA) 0.165 INCHES MINIMUM AND 0.175 INCHES MAXIMUM
FIRST LEG END RADIUS
(AJFP) 0.165 INCHES MINIMUM AND 0.175 INCHES MAXIMUM
FIRST LEG HOLE ARRANGEMENT STYLE
(AKAU) ONE HOLE
FIRST LEG HOLE DIAMETER
(AHLK) 0.160 INCHES MINIMUM AND 0.170 INCHES MAXIMUM
FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH
(AHRB) 0.165 INCHES MINIMUM AND 0.175 INCHES MAXIMUM
FIRST LEG STYLE
(AJZU) END RADIUS
FIRST LEG THICKNESS
(AHPW) 0.023 INCHES MINIMUM AND 0.027 INCHES MAXIMUM
FIRST LEG WIDTH
(AHQN) 0.330 INCHES MINIMUM AND 0.350 INCHES MAXIMUM
FIRST LEG LENGTH
(ADLK) 0.405 INCHES MINIMUM AND 0.435 INCHES MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATION
(MDCL) AMS 5540 ASSN STD SINGLE MATERIAL RESPONSE
MATERIAL
(MATT) STEEL
SECOND LEG END RADIUS
(AJFQ) 0.095 INCHES MINIMUM AND 0.105 INCHES MAXIMUM
SECOND LEG HOLE ARRANGEMENT STYLE
(AKCU) NO HOLE
SECOND LEG LENGTH
(ADLL) 0.630 INCHES MINIMUM AND 0.650 INCHES MAXIMUM
SECOND LEG WIDTH
(AHLF) 0.190 INCHES MINIMUM AND 0.210 INCHES MAXIMUM
SECOND LEG RELATIONSHIP TO FIRST LEG
(CSSP) NOT IDENTICAL
SECOND LEG STYLE
(AKBU) END RADIUS
SECOND LEG THICKNESS
(AHPX) 0.023 INCHES MINIMUM AND 0.027 INCHES MAXIMUM
STYLE DESIGNATOR
(STYL) ANGLE
III END ITEM IDENTIFICATION
(AGAV) W/S: ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); AIRCRAFT, EAGLE F-15; SUPPORT EQUIPMENT, C-5 AIRCRAFT; AIRCRAFT, F-16; ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); ADVANCE AIR TRAFFIC CONTR. & LAND. SYS (ATCALS) 404L; AIRCRAFT, F-111; ENGINE, AIRCRAFT, F100-PW-220 (F-15C/D/E)

Manufacturer Part Numbers


Related Inventory

4038404
5340003775658
Condition FN
LOCK-AUG CONVG
Readily Available
4038404
5340-00-377-5658
Condition NE
LOCK AUG CONVG
Readily Available


 
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