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1680-01-504-1712

Aircraft Control Stick

1680015041712 015041712 KC52703-001

A lever used for maintaining control of an aircraft about its pitch and roll axis. Excludes operation of trim tabs or the like. It is distinguished from a CONTROL COLUMN in that its side to side movement controls the aircraft about its roll axis. View more Aircraft Control Stick

1680-01-504-1712 CONTROL STICK,AIRCRAFT 1680015041712 015041712

Managed by United States
NSN Created on 21 Jan 2003
Data Last Changed
January 2023
NATO Update Count
4
NATO Data Quality
1680-01-504-1712 CONTROL STICK,AIRCRAFT 1680015041712 015041712 1/1
NSN 1680-01-504-1712 (Generic Image) 1/1

1680-01-504-1712 Stock and Availability Marketplace 1680-01-504-1712

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1680-01-504-1712 Related Documents Related Documents 1680-01-504-1712 1+ Documents (More...)

KC52703-001 A lever used for maintaining control of an aircraft about its pitch and roll axis.
United States (US) 4. 1680-01-504-1712 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1680-01-504-1712 RQST Updated Every Day 1680-01-504-1712 RQST NE Restrictions

1680-01-504-1712 Demil Restrictions 1680-01-504-1712

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

1680-01-504-1712 is a Aircraft Control Stick 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.

1680-01-504-1712 HTS and ScheduleB Import and Export 1680-01-504-1712

1680-01-504-1712 End Users End Users 1680-01-504-1712

New Zealand (ZE01)
Effective Date:
1 May 2014

1680-01-504-1712 Manufacturers Approved Sources 1680-01-504-1712

1680-01-504-1712 Technical Data Datasheet 1680-01-504-1712

Characteristic
Specifications
FIIG
A529V0
Aircraft Location [CZDJ]
Stick Assy, Pilot/Co-Pilot Collective Control
Aircraft Mission Design Series [CZEK]
Sh-2G
Overall Length [ABHP]
15.920 Inches Nominal

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1680-01-504-1712 Freight Data Freight Information 1680-01-504-1712

1680-01-504-1712 has freight characteristics managed by Australia.. 1680-01-504-1712 has a variance between NMFC and UFC when transported by rail and the description should be consulted.