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1680-01-487-0570

Aircraft Seat Frame Section

1680014870570 014870570 7352582

A prefabricated item of various sizes and shapes designed to be joined with other sections of frame work. This will form the basic structure of a frame for a SEAT, AIRCRAFT. View more Aircraft Seat Frame Section

1680-01-487-0570 FRAME SECTION,SEAT,AIRCRAFT 1680014870570 014870570

Managed by United States
NSN Created on 23 Jul 2001
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
1680-01-487-0570 FRAME SECTION,SEAT,AIRCRAFT 1680014870570 014870570 1/1
NSN 1680-01-487-0570 (Generic Image) 1/1

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1680-01-487-0570 Related Documents Related Documents 1680-01-487-0570 5+ Documents (More...)

Documents 1680-01-681-9718 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-487-0570
Aircraft Seat Frame Section 1680014870570 https//www.nsnlookup.com /nato/nato-stock-numbers/inc
5950-00-735-2582 5950007352582 007352582 is a transformer consisting of one or more primary winding(s) and one or more secondary winding(s). it may be designed for direct connection to an alternating current source for purposes of changing the secondary volts and amperes or designed to eliminate metallic interconnection between circuits in an overall one to one voltage ratio, with or without additional output windings, or items designed to automatically maintain a constant output voltage within specified limits under varying input or load conditions. also includes items having a provision for mechanically changing the turns ratio or inductive coupling in progressive increments by means of voltage taps, ratio adjuster, or devices oe similar design. for transformers having winding(s) common to both input and output circuits, see transformer (1), power, autotransformer. excludes transformer (1), pulse.
1680-01-681-9718 Aircraft Seat Frame Section 1003204-037RNCC: 3 | RNVC: 2 | DAC: 3 16 Jul 2019 1680-01-487-0570

1680-01-487-0570 Demil Restrictions 1680-01-487-0570

DEMIL: B | DEMILI: 3 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

1680-01-487-0570 is a Aircraft Seat Frame Section that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.

1680-01-487-0570 HTS and ScheduleB Import and Export 1680-01-487-0570

1680-01-487-0570 End Users End Users 1680-01-487-0570

Turkey (ZW01)
Effective Date:
1 Jul 2001

1680-01-487-0570 Manufacturers Approved Sources 1680-01-487-0570

1680-01-487-0570 Technical Data Datasheet 1680-01-487-0570

Characteristic
Specifications
FIIG
A23900
Material [MATT]
Steel
Overall Length [ABHP]
27.750 Inches Nominal
Overall Width [ABMK]
18.000 Inches Nominal
General Characteristics Item Description [TEXT]
1.000 Inch Thick Bar
End Item Identification [AGAV]
Mj-1A

1680-01-487-0570 Related Items NATO Stock Numbers Related to 1680-01-487-0570

1680-01-487-0570 Freight Data Freight Information 1680-01-487-0570

1680-01-487-0570 has freight characteristics managed by Turkey.. 1680-01-487-0570 has a variance between NMFC and UFC when transported by rail and the description should be consulted.