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1680-01-631-2213

Quadrant Control Assembly

1680016312213 016312213 M886V0039-01 10-6083

A cockpit mounted, manually operated item, designed to regulate aircraft functions, which may include throttle, afterburner, flaps, trim tabs, and the like. May consist of lever(s), grip(s), switch(es), and fulcrum(s). Excludes wire rope and push-pull assemblies, and all quadrants or levers that are engine mounted. View more Quadrant Control Assembly

1680-01-631-2213 CONTROL ASSEMBLY,QUADRANT 1680016312213 016312213

Managed by United States
NSN Created on 4 Sep 2014
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
1680-01-631-2213 CONTROL ASSEMBLY,QUADRANT 1680016312213 016312213 1/1
NSN 1680-01-631-2213 (Generic Image) 1/1

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1680-01-631-2213 Related Documents Related Documents 1680-01-631-2213 1+ Documents (More...)

M886V0039-01 10-6083 A cockpit mounted, manually operated item, designed to regulate aircraft functions
RQST NE Updated Every Day 1680-01-631-2213 RQST Updated Every Day 1680-01-631-2213 RQST NE Related Documents
1680-01-631-2213 DEMIL: A | DEMILI : 1 | CRITICALITY : X | HMIC : N | PMIC : A | EDC: A | ADPEC : 0 1680

1680-01-631-2213 Demil Restrictions 1680-01-631-2213

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

1680-01-631-2213 is a Quadrant Control Assembly 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.

1680-01-631-2213 HTS and ScheduleB Import and Export 1680-01-631-2213

1680-01-631-2213 End Users End Users 1680-01-631-2213

Australia (ZA01)
Effective Date:
1 Sep 2014

1680-01-631-2213 Manufacturers Approved Sources 1680-01-631-2213

1680-01-631-2213 Technical Data Datasheet 1680-01-631-2213

Characteristic
Specifications
FIIG
A529V0
End Item Identification [AGAV]
Ch47-F Caas Tfps
Aircraft Mission Design Series [CZEK]
Ch47-F
Material Thickness [ABPX]
4.125 Inches Maximum
Overall Length [ABHP]
6.340 Inches Nominal
Overall Width [ABMK]
5.750 Inches Nominal
Part Name Assigned By Controlling Agency [CXCY]
Engine Condition Panel

1680-01-631-2213 Related Items NATO Stock Numbers Related to 1680-01-631-2213

1680-01-631-2213 Freight Data Freight Information 1680-01-631-2213

1680-01-631-2213 has freight characteristics managed by Australia.. 1680-01-631-2213 has a variance between NMFC and UFC when transported by rail and the description should be consulted.