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NSN 1615-00-848-4888, 1615008484888
FITTING ASSEMBLY,RETENTION STRAP

Federal Supply Classification
FSC 1615 - Helicopter Rotor Blades, Drive Mechanisms and Components
National Item Identification Number
NIIN 008484888
Codification Country
United States
Item Name Code
INC 77777
Criticality
(F) This item is a Flight Safety Critical Aircraft Part (FSCAP).
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 1615-00-848-4888

National Stock Number (NSN) 1615-00-848-4888, or NIIN 008484888, (fitting assembly,retention strap) was assigned September 22, 1967 in the Federal Logistics Information System (FLIS). This NSN does not replace any other NSNs.

There are 2 manufacturer part numbers 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. ISO Group has several sources of supply for this NSN.

This part number has not been procured by the US Government in over 5 years.

There has been very little 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 Jun 10, 2020, 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 is a Flight Safety Critical Aircraft Part (FSCAP). There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials. NSN 1615008484888 does not contain precious metals.

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) STEEL BPS 299-947-055 COMP 4340,CADMIUM-PLATED QQ-P-416 CLASS 2 TYPE 2,DIM.,3.465 IN. NOM O/A LG,3.985 IN. NOM FLANGE OD,0.625 IN. NOM FLANGE W,3.490 IN. MIN,3.495 IN. MAX BODY OD,1.886 IN. MIN,1.890 IN. MAX W BY 2.750IN. LG APERTURE,TWO IN-LINE HOLES 1.125 IN. MIN,1.126 IN. MAX DIA DRILLED THRU OD PERPENDICULAR TO APERTURE LG 0.963 IN. FROM INNER FLANGE FACE,ONE SEMI-ROUND TAB EXTENSION ON LOWER APERTURELG 0.625 IN. LG BY 1.240 IN. W,BOTTOM EDGE OF TAB CUT W/17 GEAR TEETH,14.5 DEG PRESSURE ANGLE,48 DIAMETRAL PITCH,0.06545 IN. CIRCULAR PITCH,2.875 IN. PITCH DIA,2.810 IN. MIN,2.830 IN. MAX MINOR DIA,2.910 IN. MIN,2.917 IN. MAX MAJOR DIA,FLANGED END APERTURE CLOSED W/NO. 204-012-111-1 CUP,ITEM USED ON MAIN ROTOR ASSEMBLY
GENERAL CHARACTERISTICS ITEM DESCRIPTION
(TEXT) QSTEEL BPS 299-947-055 COMP 4340,CADMIUM-PLATED QQ-P-416 CLASS 2 TYPE 2,DIM.,3.465 IN. NOM O/A LG,3.985 IN. NOM FLANGE OD,0.625 IN. NOM FLANGE W,3.490 IN. MIN,3.495 IN. MAX BODY OD,1.886 IN. MIN,1.890 IN. MAX W BY 2.750IN. LG APERTURE,TWO IN-LINE HOLES 1.125 IN. MIN,1.126 IN. MAX DIA DRILLED THRU OD PERPENDICULAR TO APERTURE LG 0.963 IN. FROM INNER FLANGE FACE,ONE SEMI-ROUND TAB EXTENSION ON LOWER APERTURELG 0.625 IN. LG BY 1.240 IN. W,BOTTOM EDGE OF TAB CUT W/17 GEAR TEETH,14.5 DEG PRESSURE ANGLE,48 DIAMETRAL PITCH,0.06545 IN. CIRCULAR PITCH,2.875 IN. PITCH DIA,2.810 IN. MIN,2.830 IN. MAX MINOR DIA,2.910 IN. MIN,2.917 IN. MAX MAJOR DIA,FLANGED END APERTURE CLOSED W/NO. 204-012-111-1 CUP,ITEM USED ON MAIN ROTOR ASSEMBLY

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