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2530-00-233-7862

Vehicular Components Boot

2530002337862 002337862 3003-27

A flexible, nonmetallic item designed to prevent entry of dust, moisture and other contaminants into critical areas around vehicular steering and brake components and the like. Sealing may be either static or dynamic. The item may include mounting hardware (support plates, clamps and the like). See also BOOT, POWER TRANSMISSION COMPONENTS. Excludes BOOT, DUST AND MOISTURE SEAL. View more Vehicular Components Boot

2530-00-233-7862 BOOT,VEHICULAR COMPONENTS 2530002337862 002337862

Managed by United States
NSN Created on 5 Mar 1971
Data Last Changed
November 2023
NATO Update Count
6
NATO Data Quality
2530-00-233-7862 BOOT,VEHICULAR COMPONENTS 2530002337862 002337862 1/1
NSN 2530-00-233-7862 (Generic Image) 1/1

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2530-00-233-7862 Related Documents Related Documents 2530-00-233-7862 5+ Documents (More...)

3 9 Dec 1970 3040-00-421-9544 Shouldered Shaft 3003-15RNCC: 3 | RNVC: 2 | DAC: 5 14 Dec 1970 2530-00-233-7862
5306-01-093-9685 5306010939685 010939685 is an externally threaded fastener whose threaded portion is of one nominal diameter, no. 10 (0.190 in.) (5 mm) or larger. it has a round unthreaded neck or shank all or part of which is of greater diameter than the threaded portion. the head is not designed to be held or driven with an inserted drivers. a locking feature may be incorporated in the design of the head or threads. for items with a thread diameter smaller than no. 10 (0.190 in.) (5 mm) and those items with an inserted drive head, use screw, shoulder. for items which are no. 10 (0.190 in.) (5 mm) or larger in size and are both shouldered and have an externally relieved body, use bolt, externally relieved body. excludes thumbscrew.
1560-01-514-9841 1560015149841 015149841 is a movable airfoil, whether hinged, pivoted or mounted on tracks, forming part of the leading or trailing edge of a wing of an aircraft. it is designed for the specific purpose of lowering the landing speed by varying the effective camber and may be used in accelerated takeoffs and improved climbs. excludes leading edge devices that prevent stalls by ducting air over the top of a wing through extended slats. excludes slat,aircraft.
Aug 1973 2530-00-238-5319 Vehicular Components Boot 32643RNCC: 3 | RNVC: 2 | DAC: 3 2 Nov 1970 2530-00-233-7862

2530-00-233-7862 Demil Restrictions 2530-00-233-7862

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: P | PMIC: U | EDC: | ADPEC:

2530-00-233-7862 is a Vehicular Components Boot that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. The precious metals content of this item is unknown.

2530-00-233-7862 Manufacturers Approved Sources 2530-00-233-7862

2530-00-233-7862 Management Data Management Data 2530-00-233-7862

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Aug 1999
Department of the Navy (DN)
EA
Subscribe
1
MOE
USC
Code
Statement
Order of Use
Jump To Code
Qty Per Assy
UOM
Technical Document
Quantative Expression
Department of the Navy (DN)
N
V
Discontinued Without Replacement

Navy Navy

Cognizance:
9C

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