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NSN 1610-00-858-8550, 1610008588550
PLUG,FLUID TRANSFER

Federal Supply Classification
FSC 1610 - Aircraft Propellers and Components
National Item Identification Number
NIIN 008588550
Codification Country
United States
Item Name Code
INC 77777
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.
Availability: Readily Available Qualified Suppliers: Currently qualifying suppliers

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DLMS® Summary

National Stock Number 1610-00-858-8550

National Stock Number (NSN) 1610-00-858-8550, or NIIN 008588550, (plug,fluid transfer) was assigned January 1, 1962 in the Federal Logistics Information System (FLIS). 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 not been procured by the US Government in over 5 years.

Based on a planned procurement review by the Primary Inventory Control Activity (PICA) on Jul 02, 2006, 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) 77777. 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 1610008588550 contains an unknown precious metal.

This NSN is associated to Schedule B 8803100060: propellers and rotors and parts thereof, for use in military aircraft. The Schedule B End Use is listed as parts for military-type goods. NAICS classification category 336413: other aircraft parts and auxiliary equipment manufacturing.

This information was last updated on .


Technical Characteristics

GENERAL CHARACTERISTICS ITEM DESCRIPTION
(TEXT) BSTEEL,AMS 5610 PER HS 178 HAMILTON STANDARD,ROCKWELL HARDNESS RATING CSCALE 30 TO 46,DIM.,0.770 IN. NOM LG,0.996 IN. MIN,0.998 IN. MAX OD,0.625IN. MIN,0.630 IN. MAX OD LG,1.090 IN. MIN,1.100 IN. MAX FLANGE OD,0.050 IN.MIN,0.060 IN. MAX FLANGE W,0.655 IN. MIN,0.657 IN. MAX ID,0.610 IN. NOM IDLG,ONE INTERNAL OIL GROOVE AT CLOSED END 0.070 IN. W BY 0.725 IN. DIA,TWOEXTERNAL GROOVES ON OD 0.093 IN. W BY 0.885 IN. DIA LOCATED AT 0.055 IN. AND0.490 IN. FROM OPEN END,ONE CENTRAL GROOVE 0.230 IN. W BY 0.800 IN. DIALOCATED 0.205 IN. FROM OPEN END,CLOSED END OD 0.875 IN. DIA BY 0.085 IN. WSIX LUBRICATION HOLES 0.025 IN. DIA,EQUALLY SPACED,DRILLED THRU CENTRAL ODGROOVE AT 22 DEG ANGLE TO MEET INTERNAL GROOVE
GENERAL CHARACTERISTICS ITEM DESCRIPTION
(TEXT) STEEL,AMS 5610 PER HS 178 HAMILTON STANDARD,ROCKWELL HARDNESS RATING CSCALE 30 TO 46,DIM.,0.770 IN. NOM LG,0.996 IN. MIN,0.998 IN. MAX OD,0.625IN. MIN,0.630 IN. MAX OD LG,1.090 IN. MIN,1.100 IN. MAX FLANGE OD,0.050 IN.MIN,0.060 IN. MAX FLANGE W,0.655 IN. MIN,0.657 IN. MAX ID,0.610 IN. NOM IDLG,ONE INTERNAL OIL GROOVE AT CLOSED END 0.070 IN. W BY 0.725 IN. DIA,TWOEXTERNAL GROOVES ON OD 0.093 IN. W BY 0.885 IN. DIA LOCATED AT 0.055 IN. AND0.490 IN. FROM OPEN END,ONE CENTRAL GROOVE 0.230 IN. W BY 0.800 IN. DIALOCATED 0.205 IN. FROM OPEN END,CLOSED END OD 0.875 IN. DIA BY 0.085 IN. WSIX LUBRICATION HOLES 0.025 IN. DIA,EQUALLY SPACED,DRILLED THRU CENTRAL ODGROOVE AT 22 DEG ANGLE TO MEET INTERNAL GROOVE

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