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1680-01-615-7678

Aircraft Ejection Seat Guide Rails

1680016157678 016157678 5923-21

A structure which is the interface between the SEAT, AIRCRAFT EJECTION and the aircraft. It guides the seat on its movement by means of a set of rollers on the back edges of the sides or by means of slippers on the inside of the main beam assembly. View more Aircraft Ejection Seat Guide Rails

1680-01-615-7678 GUIDE RAILS,AIRCRAFT EJECTION SEAT 1680016157678 016157678

Managed by United States
NSN Created on 23 Jan 2013
Data Last Changed
November 2023
NATO Update Count
3
NATO Data Quality
1680-01-615-7678 GUIDE RAILS,AIRCRAFT EJECTION SEAT 1680016157678 016157678 1/1
NSN 1680-01-615-7678 (Generic Image) 1/1

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1680-01-615-7678 Demil Restrictions 1680-01-615-7678

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

1680-01-615-7678 is a Aircraft Ejection Seat Guide Rails 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 is not suspected to be hazardous. This item does not contain a precious metal.

1680-01-615-7678 End Users End Users 1680-01-615-7678

United Kingdom (ZK01)
Effective Date:
1 Jan 2013

1680-01-615-7678 Manufacturers Approved Sources 1680-01-615-7678

1680-01-615-7678 Technical Data Datasheet 1680-01-615-7678

Characteristic
Specifications
End Item Identification [AGAV]
45Ton Hydraulic Axle Jack Model 5923(Regent Jack) Nsn 1730-009655744
Part Name Assigned By Controlling Agency [CXCY]
Guide

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1680-01-615-7678 Freight Data Freight Information 1680-01-615-7678

1680-01-615-7678 has freight characteristics.. 1680-01-615-7678 has a variance between NMFC and UFC when transported by rail and the description should be consulted.