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1680-01-653-5521

Aircraft Electrical Power Control Assembly

1680016535521 016535521 258T7200-6

An assembly consisting of devices used to control electrical power, i.e. circuit breakers, mechanical or solid state relays. It may or may not involve circuitry for accepting remote energizing, deenergizing controlling signals and/or circuitry for providing remote indication of energized, deenergized status. View more Aircraft Electrical Power Control Assembly

1680-01-653-5521 POWER CONTROL ASSEMBLY,ELECTRICAL,AIRCRAFT 1680016535521 016535521

Managed by United States
NSN Created on 28 Mar 2016
Data Last Changed
November 2023
NATO Update Count
2
NATO Data Quality
1680-01-653-5521 POWER CONTROL ASSEMBLY,ELECTRICAL,AIRCRAFT 1680016535521 016535521 1/1
NSN 1680-01-653-5521 (Generic Image) 1/1

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1680-01-653-5521 Related Documents Related Documents 1680-01-653-5521 5+ Documents (More...)

Documents 1680-01-699-9951 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-653-5521
Aircraft Electrical Power Control Assembly 1680-01-653-5521 1680016535521 016535521 is an assembly
3293Positioning Guide5365144493293 144493293 7200-6 https//www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-653-5521
Aircraft Electrical Power Control Assembly 1680-01-653-5521 1680016535521 016535521 is an assembly
005800111 2990-00-580-0111 2990005800111 005800111 https//www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-653-5521
Aircraft Electrical Power Control Assembly 1680-01-653-5521 1680016535521 016535521 is an assembly
1680-01-687-5079 1680016875079 016875079 is an assembly consisting of devices used to control electrical power, i.e. circuit breakers, mechanical or solid state relays. it may or may not involve circuitry for accepting remote energizing, deenergizing controlling signals and/or circuitry for providing remote indication of energized, deenergized status.
Aircraft Electrical Power Control Assembly 16E3646-831RNCC: 3 | RNVC: 2 | DAC: 3 10 Mar 2022 1680-01-653-5521

1680-01-653-5521 Demil Restrictions 1680-01-653-5521

DEMIL: Q | DEMILI: 6 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

IUID Required

1680-01-653-5521 is a Aircraft Electrical Power Control Assembly 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 Non-Critical Munitions List Item or a Non-Sensitive Commerce Control List Item and cannnot be in the possession of any party outside of the USA who is a 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 confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.

1680-01-653-5521 HTS and ScheduleB Import and Export 1680-01-653-5521

1680-01-653-5521 End Users End Users 1680-01-653-5521

US Air Force (FBB4)
Effective Date:
1 Mar 2016

1680-01-653-5521 Manufacturers Approved Sources 1680-01-653-5521

1680-01-653-5521 Management Data Management Data 1680-01-653-5521

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Oct 2022
Department of the Air Force (DF)
EA
Subscribe
1
Mar 2016
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
TK
KC-46 TANKER
Price Validation Code:
E
The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
Expendability
Recoverability
Repairability:
T
Expendable. Reparable. Condemn at Depot. AF Recoverable Assembly Management System (AFRAMS).

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1680-01-653-5521 Freight Data Freight Information 1680-01-653-5521

1680-01-653-5521 has freight characteristics.. 1680-01-653-5521 has a variance between NMFC and UFC when transported by rail and the description should be consulted.